ES2098 Accpet Test Req Rev Ab

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Data Control Level

1

Release Stamp

SPECIFICATION

ACCEPTANCE TEST REQUIREMENTS TAURUS 60-7901 / -7801 / -7801e / -7301 / -7001 / -6501 / -6201

ONE-SHAFT ENGINES CONVENTIONAL COMBUSTION

SPECIFICATION NO. ES 2098 ISSUED: 6/23/93; ERL 10986-1 (Date and ERL No.)

REVISION: (Letter, Date and ERL,PRD,CR No.)

A; 6/17/94; ERL11424-1 B; 7/10/94; ERL11465-1 C; 8/24/94; ERL11667-1 D; 9/20/94; ERL11562-2 E; 3/31/95; PRD11951-1 F; 5/10/95; PRD12053-1 G; 5/16/95; PRD11875-2 H; 7/11/95; PRD12098-1 J; 9/6/95; PRD12192-1 K; 7/23/96; PRD12687-1 L; 10/10/96; PRD12811-1

M; 11/12/96; PRD12850-1 N; 9/11/97; PRD13236-1 P; 11/9/98; PRD13707-1 R; 11/22/99; PRD13905-1 S; 10/30/00; PRD14457-1 T; 06/07/02; PRD14708-1 U; 06/04/02; PRD14785-1 V: 03/01/05; CR11015 W; 04/21/05; CR11220 Y; 05/26/05; CR11423 AA; 12/07/07; CR18578

Rev. Ltr/ CR # Signature & Title Date Prepared By:

D. Bessler

AB 29615 Approved By: Mario Eade

02-25-11

ATTENTION

This copyrighted work and the information herein is proprietary to Caterpillar Inc., Solar Turbines Incorporated, and/or subsidiaries of either. Without express, written proprietor permission, any copying, disclosure, or use except that for which it is loaned, is prohibited.

Engineering Specification No. ES 2098AB

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CONTENTS Paragraph Page 1.0 SCOPE 1

1.1 Conflicting Limits 1 1.2 Definition of Subject Equipment 1 1.3 Superseded Document 1

2.0 APPLICABLE DOCUMENTS 1

2.1 Specifications and ISO Practices 1 2.2 Drawings 2 2.3 CS and PT Tables 2

3.0 EQUIPMENT REQUIREMENTS 2

3.1 Test Articles 2 3.2 Facility Equipment 2 3.3 Facility Hardware 2 3.4 Test Instrumentation 3 3.5 Fuel 3 3.6 Lubricating Oil 3 3.7 Control 3

4.0 ACCEPTANCE REQUIREMENTS 3

4.1 Sequence of Tests 3

4.1.1 Start Sequence and Safeties Verification 3 4.1.2 Verify Pre-lube 3 4.1.3 Seal and Rotor Break-in 3 4.1.4 Engine/reduction Gearbox Break-in 3 4.1.5 Hot Restarts - Not Applicable 3

4.2 Mechanical Acceptance Requirements 3

4.2.1 Starts 3 4.2.2 Lightoff and Acceleration 4 4.2.3 Not Applicable 4 4.2.4 Oil Leakage 4 4.2.5 External Air Leakage 4 4.2.6 Lube Oil System Limits 4 4.2.7 Not applicable 4 4.2.8 Oil Tank Sump Pressure 4 4.2.9 Engine Vibration Limits 4 4.2.10 Variable Vanes 4 4.2.11 Bleed Valve 4 4.2.12 Compressor Diffuser Exit Temperature 4 4.2.13 Third Stage Turbine Inlet Temperature 4 4.2.14 Exhaust Gas Temperature 4


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CONTENTS (Continued) Paragraph Page

4.3 Performance Acceptance Requirements 4

4.3.1 Performance Analysis 4 4.3.2 Performance Evaluation 4 4.3.2.1 Corrected Performance 5 4.3.2.2 Mechanical Full Load Performance 6 4.3.3 Emissions Measurement 6 4.3.4 Water Injection 6

5.0 PREPARATION FOR DELIVERY 7

5.1 Engine Data Plates 7

5.1.1 Engine Nameplate 7

5.2 Borescope Inspection and Bolt Torque 7

5.2.1 Compressor 7 5.2.2 Gas Producer Turbine 7 5.2.3 Re-torque 7

5.3 Preservation 8

6.0 QUALITY ASSURANCE PROVISIONS 8

6.1 Responsibility 8 6.2 Calibration of Equipment 8 6.3 Documentation 8

6.3.1 Engine Records 8 6.3.2 Acceptance Records 8

6.4 WITNESS TEST 8

7.0 EXCEPTIONS TO ASME PTC 8


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TABLES

Table Page

1 (PT30348A) Performance Acceptance Requirements, 7901 Gas 10

1 (PT30349A) Performance Acceptance Requirements, 7901 Liquid 11

1 (PT30352) Performance Acceptance Requirements, 7801 Gas 12

1 (PT30353) Performance Acceptance Requirements, 7801 Liquid 13

2 Instrumentation Requirements 14

4 Seal and Rotor Break-in 19

5 Reduction Gearbox Break-in and Hot Re-Start Test Sequence 20

6 Performance and Emissions Test Sequence, Dry 21

6A Performance and Emissions Test Sequence, Wet 23

7 Engine Vibration Limits 25

8 Lube Oil System Limits 28

9 Compensator Selection Chart for Engine Retrofits to Packages that do not use PLC Software Compensation 29

PT30350A Reference Full Load Performance (7901) Gas Dry 39 PT30351A Reference Full Load Performance (7901) Liquid Dry 40 PT30137 Reference Full Load Performance (7801) Gas, Dry 41 PT30138 Reference Full Load Performance (7801) Liquid, Dry 42


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FIGURES

Figure Page 1a Total Oil Flow No. 1 Bearing Inlet and Reduction Gearbox

(196800-10X, 191100-104 and Above, 222150-10X) 30

1b Total Oil Flow No. 1 Bearing Inlet and Reduction Gearbox 31 (196800-20X and 302750-20X) 1c Total Oil Flow No. 1 Bearing Inlet and Reduction Gearbox 32 (All Other Reduction Drive Assemblies)

2 Total Oil Flow No. 2 and No. 3 Bearing Inlet 33

4 Oil Flow to Starter Gears (Air/Gas Start Only) (Reference Only) 34 5 Oil Tank Sump Pressure Limits 35

6 Velocity Spectrum Limit Curve: Reduction Gearbox Housing Horizontal 36

6a Acceleration Vibration Limit Curve: Reduction Gearbox Housing Vertical 37

7 Velocity Spectrum Limit Curve: Diffuser Forward Flange Horizontal 38

ADDENDUMS

No Page Addendum 1 Taurus 60-6201 Acceptance Test Requirements 43 Addendum 2 Taurus 60-6501 Acceptance Test Requirements 56 Addendum 3 Taurus 60-7001 Acceptance Test Requirements 69 Addendum 4 Taurus 60-7301 Acceptance Test Requirements 82 Addendum 5 Taurus 60-7801e Acceptance Test Requirements 91


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1.0 SCOPE - This specification contains the Engineering acceptance requirements for the Taurus 60-7901 and –7801 one-shaft engines. The following rating configurations are included as addendums:

AddendumNumber

Engine Requirements

1 Taurus 60-6201

2 Taurus 60-6501

3 Taurus 60-7001

4 Taurus 60-7301

5 Taurus 60-7801e

1.1 CONFLICTING LIMITS - In the event of a conflict between the test limits of this specification and any specific project definition, the limits contained in this specification shall prevail. Only a Change Request (CR) can amend the requirements of this specification or an Engineering Instruction (EI) issued by the Turbomachinery Engineering Product Support Group. 1.2 DEFINITION OF SUBJECT EQUIPMENT - This specification applies to new production engines and to units overhauled or remanufactured to "major overhaul" or "standard overhaul" criteria. This specification does not apply to units returned to serviceable condition by rework or repair of a specific defect. The activity performing the rework or repair may selectively use the appropriate sections of this specification for acceptance testing following the rework. 1.3 SUPERSEDED DOCUMENT - This specification supersedes the engine acceptance criteria contained in all previous releases of this document. 2.0 APPLICABLE DOCUMENTS - The following documents form a part of this specification to the extent specified herein. Documents shall be of the latest revision in effect on the day of the test. 2.1 SPECIFICATIONS AND ISO PRACTICES

Solar ES 9-97 Gas Turbine Emissions, Test Specifications ES 9-98 Fuel, Air, and Water (or Steam) for Solar Gas Turbine Engines ES 9-224 Lubricating Oil For Use In Solar Gas Turbines ES 9-248 Corrosion-Preventive Oil for Factory Test and Long Term

Preservation ES 9-249 Preservation, Turbomachinery, Air Side and Fuel Systems ES 2011 Gas Turbine Performance Users Guide ES 2058 Gas Turbine Performance Programmers Guide ES 2067 Control System Functional Requirements Taurus 60 1-Shaft Engine ES 2200 Nameplate Data for Gas Turbine Engines ES 2298 Trim Balance of Gas Turbine Products TMO Quality Departmental Instruction from Product Quality Practice 304.0 Entitled: "Quality Records" PSOP P13.02 Processing of Non-Conforming Material and W/N’s



P.TB03 Production Test Functional Practice Entitled “Certified Test Data Report”

ASME PTC-22, latest revision ASME Gas Turbine Power Plants Power Test Code

2.2 DRAWINGS

SOLAR MPDC List No. TTF-1 Taurus 60-7901, One-Shaft Engine MPDC List No. TTE-1 Taurus 60-7801, One-Shaft Engine 197003 Data Chart and Build Instructions 219005 Mechanical Installation 7901 219001 Mechanical Installation 7801 302750 1800 rpm Reduction Drive Gearbox 222150 1500 rpm Reduction Drive Gearbox

3.0 EQUIPMENT REQUIREMENTS 3.1 TEST ARTICLES - The standard top engine drawing part numbers of the production units to be tested to these requirements are shown in the MPDC list referenced in Section 2. Sales order unique engine configurations may reference all or part of this specification. 3.2 FACILITY EQUIPMENT - The engine may be tested on a customer's skid or on a facility device designed for acceptance testing (green run skid). The requirements, instrumentation and analytical procedures are the same for both. Loading shall be by means of a generator or dynamometer. 3.3 FACILITY HARDWARE - Facility hardware is defined as components normally considered a part of the engine assembly, which may be substituted by a facility component or omitted during test at the discretion of Test Engineering. Only the components below are candidates for this action:

• Generator and coupling • Fuel/water systems outboard of the fuel manifold assemblies and torch assemblies shown

on the engine MPDC listing • Air inlet duct and attachments • Exhaust collector and attachments • External Insulation blankets on the combustor assembly, and the exhaust duct • Bleed valve duct • Bleed valve (remanufactured units only) • Reduction gearbox and gearbox mounted speed pickups (remanufactured units only)

The components listed below are specifically excluded from being substituted with facility hardware unless documented on a Withholding Notice (W/N) or an approved Product Release Document (PRD):

• Fuel injectors • Torch assembly • Bleed valve and actuator (new production units) • Guide vane actuator • T5 thermocouple harness



3.4 TEST INSTRUMENTATION - Table 2 defines test instrumentation and includes an engine station schematic. 3.5 FUEL - Fuel used during test must meet the requirements of ES 9-98. 3.6 LUBRICATING OIL -Lubricating oil used during tests is to be grade 32 and shall conform to ES 9-224. 3.7 CONTROL -The operation of the engine must be controlled in accordance with the requirements ES 2067 unless specifically waived by this specification for test purposes. 4.0 ACCEPTANCE REQUIREMENTS 4.1 SEQUENCE OF TESTS - Operator safety, equipment protection, and good turbine practice should be used to determine the order of test. Care is especially important when retest or trouble- shooting procedures are in effect. The test sequences defined below are required for safety or valid test data considerations. The balance of the test sequences and detail procedures required to implement the intent of this specification are not contained herein and Test Engineering shall define them. Any retesting required as a result of engine disassembly or replacement of parts during test shall be documented as part of the disposition of the Withholding Notice (WN). Cool down procedures as part of the shut down sequence, will be utilized when appropriate (Ref. ES 2067). 4.1.1 START SEQUENCE AND SAFETIES VERIFICATION - If the engine is to be tested with a new contract skid and control console, proper functioning of the start sequence and safety devices must be confirmed by simulation prior to cranking the engine. A green run facility test skid and control console must comply with the engine control system requirements and should be periodically tested (Reference Paragraph 3.7). 4.1.2 VERIFY PRE-LUBE - Verify prelube operation and proper bearing oil pressure at each bearing oil supply port (see Table 8). 4.1.3 SEAL AND ROTOR BREAK-IN - Seal and rotor break-in must be accomplished before first light off for every build of the engine. If test is terminated anytime during break-in, any of the steps already completed do not have to be repeated. However, if the engine is disassembled and any seals are replaced, the entire break-in must be repeated. Additional rotor break-in may be required at any point during the acceptance test. If during a purge crank vibration levels exceed 0.5 mil, repeat entire break-in procedure (see Table 4). 4.1.4 ENGINE/REDUCTION GEARBOX BREAK-IN - Each engine and reduction gearbox must receive a progressive break-in per Table 5. This must be accomplished prior to full load operation. Break-in must be repeated any time a major rotating component, and/or rotor/gear support or bearing is replaced. 4.1.5 HOT RESTARTS – Not Applicable 4.2 MECHANICAL ACCEPTANCE REQUIREMENTS - Mechanical limit compliance must be verified for engine acceptance. 4.2.1 STARTS - The engine will demonstrate a minimum of one successful start on each fuel utilized.



4.2.2 LIGHTOFF AND ACCELERATION - There shall be consistent light off and surge-free acceleration. 4.2.3 NOT APPLICABLE 4.2.4 OIL LEAKAGE - There shall be no external oil leakage, including but not limited to oil leakage from case drains, or the proximity probe leads. There shall be no oil smoke in the exhaust. 4.2.5 EXTERNAL AIR LEAKAGE - There shall be no external air leakage that can be felt by hand 5 inches or more from the leak source at any flange area, except for the number 1 bearing vent. 4.2.6 LUBE OIL SYSTEM LIMITS - Bearing oil flows, and thrust bearing temperature shall be within the limits shown in Table 8. 4.2.7 NOT APPLICABLE 4.2.8 OIL TANK SUMP PRESSURE - Oil tank sump pressure (measured upstream of 2.0 inch orifice in vent pipe) versus compressor discharge pressure (PCD) shall not exceed the limits defined in Figure 5. 4.2.9 ENGINE VIBRATION LIMITS - Engine vibration acceptance levels shown in Table 7 apply only during steady state operation, at any load condition, when the engine is thermally stabilized, and only when performing runs in Table 6. Table 7 limits do not apply during transient conditions. Proximity probe vibration levels exceeding 5.0 mils on bearings 1 or 2 and/or 4.0 mils on bearing 3, during any operating condition, is cause for immediate shutdown and rejection. 4.2.10 VARIABLE VANES - The variable vanes shall operate following the schedule defined in ES 2067. 4.2.11 BLEED VALVE - The bleed valve shall operate following the schedule in ES 2067. 4.2.12 COMPRESSOR DIFFUSER EXIT TEMPERATURE - The difference in readings between the high and low compressor diffuser exit temperature (T2) probes shall not exceed 10ΕF during any steady state operation. 4.2.13 THIRD STAGE TURBINE INLET TEMPERATURE - Third stage turbine inlet temperature (T5) individual readings will be within ±150°F of the average during any steady state operation. 4.2.14 EXHAUST GAS TEMPERATURE - Exhaust gas temperature (T7)(not T7.PKG) individual readings will be within ±20°F of the average during any steady state operation with the bleed valve closed. 4.3 PERFORMANCE ACCEPTANCE REQUIREMENTS 4.3.1 PERFORMANCE ANALYSIS - Performance analysis shall be in accordance with Solar Specifications ES 2011 and ES 2058. 4.3.2 PERFORMANCE EVALUATION - Engine performance will be evaluated in accordance with ASME PTC-22procedures except as noted in paragraph 7.0. The performance and emissions test sequence for acceptance testing is defined in Table 6. Use the appropriate T6 table as specified below:



Table Fuel System Type

Table 6 Dry Engine (without water-injection)

Table 6A Wet Engines (with water-injection)

All engines are tested using a generator load during acceptance test, use assumed generator and gearbox efficiencies as specified below in calculating performance.

ηGenerator = 96.4%

ηGearbox = 98.0%

Performance will be tested at unity power factor electrical load. Performance on dual fuel units will be verified on both fuels. All engines are tested to corrected performance and full load. Corrected performance is an acceptance criteria as specified below. Full load is an emissions acceptance criteria; performance is for reference only. 4.3.2.1 CORRECTED PERFORMANCE (plot point) requirements are detailed in Table 1, 1A or 1B. Engine operation is established at rated NGP while varying load to achieve the corrected TRIT, performance, and all of the accept criteria specified in the appropriate Table 1. Corrected performance runs must be conducted such that the corrected TRIT is achievable without exceeding the actual TRIT limit:

Engine Corrected TRIT Actual TRIT

-7901, -7801, -7801e 1950°F 2050°F

-7301 1885°F 1985°F

-7001, -6501, -6201 1850°F 1950°F

Use the appropriate Table 1, as specified below, for corrected performance runs based on the current ambient temperature, T1. Actual TRIT is not to exceed the values in the table listed above.

Table Ambient Temperature

Table 1 T1 ≤ 70°F

Table 1A 70°F < T1 ≤ 90°F

Table 1B 90°F < T1



4.3.2.2 MECHANICAL FULL LOAD PERFORMANCE at the prevailing ambient temperature is according to acceptance criteria shown in the appropriate PT or CS performance table specified below.

Mechanical Full Load Performance Tables

(Reference Only)

PT30350A 7901 Gas Dry

PT30351A 7901 Liquid Dry

PT30137 7801 Gas Dry

PT30138 7801 Liquid Dry

Engine operation must be established within the limits indicated below at the prevailing ambient temperature.

Parameter Acceptable Limits

Engine Speed (NGP) 100% ± 0.1%

Power Turbine Inlet Temperature (T5 Average) T5 Topping ± 5°F

IGV Setting (degrees) As set in Corrected Performance Run

Mechanical full load performance data shall be taken for reference engineering evaluation only. It is not intended as pass-fail criterion. However, if mechanical full load performance is not met, notify the cognizant Performance Engineer. 4.3.3 EMISSIONS MEASUREMENT - Emissions shall always be recorded for full load data. For any other data points, emissions shall only be recorded when required by contract or by Engineering Instruction (E.I.) specific to the unit. If required, refer to ES 9-97 (Gas Turbine Emissions Test Specification) for instrumentation, operating procedures and data reduction. Note that emissions data should only be recorded at the mechanical full load (actual), not corrected conditions. The power equivalent to the term “100% of load” is the power developed by the engine when operating at the rated T5 temperature, or at rated gas producer speed, whichever is lower. The accept/reject requirements are the emissions values shown in the engine Application Check Sheet (ACS). Acceptance criteria is “oxygen based” NOx, corrected to ISO conditions (15% O2, 59F, 14.7 psia, 60% RH). If the engine is not meeting contract emissions levels, contact the cognizant combustion engineer. 4.3.4 WATER INJECTION – Performance acceptance shall be done dry; that is with water injection turned off, during the corrected performance run. The IGV setting and the T5 Base (compensator selection) for water injected units will be determined from the full load performance data point using either the water to fuel ratio based on contract requirements or the “wet” CS/PT tables. Adjust the water to fuel ratio to meet emissions requirements shown in the ACS. Injected water must meet the requirements of ES 9-98.



5.0 PREPARATION FOR DELIVERY 5.1 ENGINE DATA PLATES

5.1.1 ENGINE NAMEPLATE - Following engine performance testing, the following parameters will be placed in the appropriate data field on the engine Nameplate as specified in ES 2200. This is to be done by filling out the remaining information on the Temporary ID sheet which should be attached to the engine. This sheet is to be returned to Engine build with the engine, for Nameplate branding and attachment to the engine.

• T5 BASE (required for all engines) – The T60 specifically uses a T5 control method, therefore the reported T5 Base must be adjusted to match temperature 59°F. This T5 Base is obtained from the GTPERF Part B output from the corrected buy-off gas and/or liquid point (Table 6, Run 4). The exact parameter name is “T5 BASE (DEG. F) CONT. DUTY(59)”. As appropriate, value(s) should be reported in the format: Gas/Liquid. Engines equipped with a water manifold will have their values calculated from wet data.

• IGV SETTING (required for all engines) – The reported IGV setting is the angle (in

degrees) found necessary to obtain the corrected performance given at 59°F in Table 1. (Testing should always be initiated with the IGV’s set at the nominal value shown in Table 1, and adjusted as needed.) The IGV angle from Table 6, Run 4(dry or Run 4/5 wet), is used and reported.

• T5 COMPENSATOR (only for legacy controls systems where software does not

compensate between T5 Base and desired T5 Setpoint as used on original model –6201 and –6501; see ES2200) – This is the compensating resistor hardware PN, from Table 9, shipped with the engine. Table 9 utilizes the T5/TRIT ratio as specified in ES 2067. (Abbreviate: T5 COMP).

5.2 BORESCOPE INSPECTION AND BOLT TORQUE - After the engine completes test (and package test if applicable) and before it ships, visually and borescope inspect the specified blades for any foreign object damage. Any observed foreign object damage is grounds for rejection.

5.2.1 COMPRESSOR

• Visually inspect the bottom of the inlet muff, inside the screen and Inlet Guide Vane and leading edge of the first stage compressor rotor blades through the inlet muff.

• Borescope inspect the 11th stage stator and OGV through the compressor diffuser T2

port or fuel injector port. 5.2.2 GAS PRODUCER TURBINE

• Borescope inspect the trailing edge of the first stage gas producer turbine rotor blades and leading edge of the second stage gas producer turbine nozzle.

• Borescope inspect the trailing edge of the second stage gas producer turbine rotor

blades and leading edge of the third stage gas producer turbine blades through a T5 thermocouple port.

5.2.3 RE-TORQUE - Re-torque all T5 probe bolts, fuel injector bolts, bleed valve flange bolts, borescope plug bolts, and combustor pin bolts.



5.3 PRESERVATION - After all specified tests have been completed, the engine shall be preserved in accordance with Solar Specification ES 9-249 and ES 9-248. If engine runs are planned for package test, preserve following that test. Consult the product definition (PD) for applicable preservation requirements. 6.0 QUALITY ASSURANCE PROVISIONS 6.1 RESPONSIBILITY - Quality Assurance shall assure that the specified tests have been accomplished. Any discrepancy found between these test requirements and actual testing shall require review of test data by the Material Review Board. 6.2 CALIBRATION OF EQUIPMENT - Equipment required for test verification shall be calibrated in accordance with Solar procedures. 6.3 DOCUMENTATION - Copies of the tests performed and their results shall be compiled by Quality Assurance and be readily available for review. 6.3.1 ENGINE RECORDS - All completed records will be sent to Quality Control Records Center at Kearny Mesa for retention per QC79-3, A4.204. 6.3.2 ACCEPTANCE RECORDS - All data required to validate the compliance of the acceptance requirements of this specification and the sales contract shall be permanently recorded and summarized in the form of a Certified Test Report. Customer copies of the report are to be distributed by Project Management. All discrepancies found during acceptance testing shall be documented on the appropriate discrepancy report form (Withholding Notice) per Power Systems Operations Practice # P13.02 Processing of Non-Conforming Material and W/N’s. Any unresolved discrepancies remaining at the completion of testing, or deviations from this test specification, will be clearly identified and explained in the Certified Test Report. Copies of all certified test reports will be sent to Quality Control Records Center at Kearny Mesa for retention per TMO Quality Practice 304.0. 6.4 WITNESS TEST - A customer witnessed test shall consist of demonstrating engine operation at the settings at which acceptance performance and emission data are taken (reference Table 6). Additional demonstrations must be requested and approved through Project Management prior to the test. 7.0 EXCEPTIONS TO ASME PTC-22 - Testing per this specification meets the requirements of ASME PTC-22procedures except as follows:

• Solar's standard policy is not to calibrate instrumentation immediately before and after each engine test. Solar has a standard proven instrumentation calibration policy. This procedure is part of our Quality assurance instructions and can be provided to the customer on request.

• Instrumentation specifications listed in Table 2 take precedence over those in PTC-22. • Solar instrumentation does not meet all of the quantity and accuracy requirements of

PTC-22. The table listing Solar instrumentation quantity and accuracy is enclosed as Table 2. Also, because of the multi-product testing in each cell, Solar does not compensate inlet and exhaust temperature measurements for velocity and temperature gradients.



• Solar's standard practice is to measure static pressure not stagnation pressure in the turbine outlet duct.

• PTC-22requires gaseous fuel density to be measured with a Densitometer. Solar's

standard practice is to compute gaseous fuel density from measured pressures and temperatures.

• Solar takes exception to the PTC-22 Section 6 requirement for the minimum essential

information that should be provided in the test report. See Production Test Functional Practice (P.TB03) for Solar's Certified Test Data Report.



7901 CORRECTED PERFORMANCE

Parameters corrected to 59F, 80F or 100F, 60% relative humidity, sea level with no inlet or exhaust duct losses.

Parameter

ACCEPT/REJECT CRITERIA

Engine Speed(% of 14951 rpm for 60Hz Gbx % of 14944 rpm for 50Hz Gbx)

Turbine Rotor Inlet Temperature TRIT

Minimum Power (KWe)

Minimum Thermal Efficiency (%)

Maximum Heat Rate (Btu/KW-hr)

REFERENCE PERFORMANCE(2)

IGV Setting (degrees)

Turbine T5/TRIT Ratio

Maximum Compressor Mass Flow (lb/s)

Minimum Compressor Pressure Ratio

Minimum Turbine Exhaust Temperature (oF)

Minimum Heat Balance

(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is greater than 70 F. Table 1B should be used in lieu of Table 1A for corrected performance runs when T1 is greater than 90 F. Actual TRIT is not to exceed 2050 F for any test conditions.(2). Reference performance parameters are not an acceptance criteria. Contact Performance Engineering for disposition if indicated limits are exceeded.

11.9

962oF

0.70 - 0.78

49.6 47.1 44.8

1947 - 1953oF

5500

935oF 948oF

2 to 8 deg.

29.653

5023 4578

Corrected to 59oF Corrected to 100oFCorrected to 80oF

11,50711,167

30.556

99.9 - 100.1%

0.9800.980 0.980

11,956

10.8

Table 1.(1) -7901 Natural Gas Performance Acceptance Requirements (PT # 30348A)

San Diego Natural Gas

Table 1 Table 1A Table 1B

Gearbox and Generator Efficiencies are per Section 4.3.2

11.3

28.539





Parameter




Minimum Power (KWe)











0.70 - 0.78


Table 1

Table 1.(1) -7901 Liquid Performance Acceptance Requirements (PT # 30349A)

Liquid Fuel (Diesel #2)

Table 1B(Corrected to 59oF) (Corrected to 100oF)

Table 1A(Corrected to 80oF)

99.9 - 100.1%

1947 - 1953oF

5348 4885 4450

30.199 29.301 28.186

11,299 11,645 12,106

2 to 8 deg.

49.6 47.1 44.8

11.9 11.3 10.8

935oF 948oF 962oF

0.980 0.980 0.980





Parameter




Minimum Power (KWe)











11.3

27.911

Table 1.(1) -7801 Natural Gas Performance Acceptance Requirements (PT # 30352)

San Diego Natural Gas

Table 1 Table 1A Table 1B


12,225

10.8

0.980

99.9 - 100.1%

0.9800.980

11,82411,574

29.481

Corrected to 59oF Corrected to 100oFCorrected to 80oF

28.858

4940 4488

1947 - 1953oF

5335

935oF 948oF

2 to 8 deg.

0.70 - 0.78

49.6 47.1 44.8

11.9

962oF





Parameter




Minimum Power (KWe)











0.980 0.980 0.980

935oF 948oF 962oF

11.9 11.3 10.8

49.6 47.1 44.8

2 to 8 deg.

11,686 11,951 12,360

29.199 28.551 27.606

1947 - 1953oF

5206 4816 4375

99.9 - 100.1%

Table 1B(Corrected to 59oF) (Corrected to 100oF)

Table 1A(Corrected to 80oF)

Table 1

Table 1.(1) -7801 Liquid Performance Acceptance Requirements (PT # 30353)

Liquid Fuel (Diesel #2)


0.70 - 0.78



Table 2. Instrumentation Requirements

Parameter

Symbol

No. Req

.

Minimum Range

Accuracy(1)

(± or as noted)

Applicable Notes

ROTATIONAL SPEEDS Gas Producer

%NTURB (%NGP)

1

0 to 11,000 Hz

0.1%

1800 rpm GB Ref: 9967 Hz = 100% 100% = 14,951 rpm 1500 rpm GB Ref: 8717 Hz = 100% 100% = 14,944 rpm

PRESSURES Barometric Air Inlet Venturi (Total) Air Inlet Venturi (Static) Engine Inlet (Total) Engine Inlet Muff (Static) Inlet Housing (Static) Compressor Discharge Exhaust Collector (Static) Exhaust Duct Oil Supply Manifold Oil Supply, #1 Brg & RGB. Oil Supply, #2 and #3 Brg Oil Tank Static Oil Tank Vent Fuel Supply (natural gas) Fuel Supply (liquid fuel boost) Combustor Delta Pressure

P.BARO PV.PLNM DPVS. AVG PO. AVG (P1.0.AVG) PO.PKG (PS1.0.AV) P1AV.PKG (P1.PKG) PCD P7.PKG P7.AVG (P7.1.AVG) P.OIL PGB.OIL P.COMP.L P.SUMP P.VENT P.NG P.BOOST DP.COMB

1

1

4

4

1

3

1

3

4

1

1

1

1

1

2

1

1

27 to 32 in. HG 0 to 10 in. H2O 0 to -60 in. H2O 0 to -20 in. H2O 0 to -20 in. H2O 0 to -120 in. H2O 0 to 200 psig ±10 in. H2O ±10 in. H2O 0 to 75 psig 0 to 75 psig 0 to 75 psig 0 to 10 in. H2O 0 to 10 in. H2O 0 to 300 psig 0 to 75 psig 0 to 10 psid

0.04 in. HG 0.2 in. H2O 0.5 in. H2O 0.2 in. H2O 0.2 in. H2O 0.5 in. H2O 1.0% 0.2 in. H2O 0.2 in. H2O 2.0% 2.0% 2.0% 0.2 in. H2O 0.2 in. H2O 0.5% 1.0 psig 0.25%

7 7 3 2, 3, and 7 (Used to plot air flow versus ΔP/P) 3 3 and 7 2 and 7 2 ref only 8 8 2 6 and 7 2 and 6 ref only 11



Table 2. Instrumentation Requirements (Continued)

Parameter

Symbol

No. Req.

Minimum Range

Accuracy(

1) (± or as noted)

Applicable Notes

TEMPERATURES Ambient Barometer Temperature Air Inlet Venturi Engine Inlet Compressor Discharge 3rd Stage Turbine Inlet Engine Exhaust Collector Exhaust Stack Oil Supply Header Fuel Supply (natural gas) Fuel Supply (liquid fuel) Gas Producer Thrust Brg

T.AMB T. BARO TV T0.AVG (T1.0.AVG) T2.AVG (T2.0.AVG) T5.AVG (T5.1.AVG) T7.PKG T7.AVG (T7.1.AVG) TPKG.OIL T.NG T.LIQ TGP.TBRG

1 1 1 4 3 6 4

10 1 2 1 2

-40 to 120°F -40 to 120°F -40 to 120°F -40 to 120°F 0 to 800°F 0 to 1850°F 0 to 1100°F 0 to 1100°F 0 to 200°F 0 to 200°F 0 to 200°F 0 to 400°F

1.0°F 1.0°F 1.0°F 1.0°F 3.0°F 10.0°F 8.0°F 8.0°F 2.0°F 1.0°F 0.5% 1.8°F

10 7 3 and 7 3 and 7 2, 3 and 7 ref only 7 and 9 2 ref only 6 and 7 6 3, 6, 7 and 12

FLOWS Fuel-gas Fuel - liquid Water

WF.NG WF.LIQ F.WATER

2 1 1

0 to 3800 pph 0 to 4000 pph 0 to 4000 pph

1.0% 1.0% 2.0%

6, 7 and 13 6 and 13 6




Parameter

Symbol

No.

Req.

Minimum Range

Accuracy(1)

(± or as noted)

Applicable Notes

Oil Supply Reduction Gearbox (#1 Brg & GB) Compressor (#2 & #3 Brg)

FGB.OIL F.COMP.L

1

1

0 to 65 gpm 0 to 40 gpm

3.0% 3.0%

VIBRATIONS #1 bearing (proximity) #2 bearing (proximity) #3 bearing (proximity) GP Thrust Bearing, Axial Position Compressor Diffuser Flange Horizontal Turbine-Combustor, Aft Flange, Vert. Gearbox: (Accel - Vert) (Vel - Horiz)

VBRG.1 VBRG.2 VBRG.3 GP.AX V.COMP.H V.TURB.V VGB.VERA VGB.HOR

2 2 2

2

1

1

1 1

0 to 10 mils 0 to 10 mils 0 to 10 mils 0 to 20 mils 0 to 1.5 ips 0 to 1.5 ips 0 to 50G 0 to 1.5 ips

10.0% 10.0% 10.0% 10.0% 10% 10% 15% 10%

6. Check both pickups for acceptable performance. 4 4 4 4

MISCELLANEOUS Guide Vane Voltage Fuel Actuator Voltage

IGV.ACT FUEL.ACT

1

1

4 to 20 mA 4 to 20 mA

2.0% 2.0%

2, 14 2, 14

OUTPUT POWER

GEN.KW

1

6500 kW

32.5 kW

5




Notes: (1) Accuracy is systems maximum rms error, including transducer, readout, and calibration

unless otherwise stated. Also, all percent accuracies quoted are percent of actual reading, except vibration valves which are percent at 0.24 ips or 1.0 mil.

(2) This instrumentation is for reference only and not to be used to determine performance. (3) These sense points are available on the engine as it is packaged. (4) Reference Table 7 for specific pickup locations. (5) Power shall not be read directly but range and accuracy requirements pertain to

calculated power. (6) Not applicable to all units. (7) Read each channel individually unless otherwise directed. (8) Measure oil pressure at engine inlet downstream of any installed special/standby filters. (9) Ten thermocouples must be operational. (10) Barometer temperature recorded only when mercury barometer used. (11) Combustor delta pressure is measured directly as the difference between Pcd and the

torch drain. On dual fuel units use gas supply to torch not torch drain. (12) Use two RTD’s on loaded side only. (13) Maximum meter to meter Δ = 1.5%. (14) May be recorded as a 0-20 Volt or 0-50 mA signal, selected at the test engineer’s

discretion.




Engine Station Schematic



Table 4. Seal and Rotor Break-In During the following steps the engine rotor must not be allowed to come to a stop before the next crank, whether it is to repeat the last crank, or when going on to the next incremental step. Contact the cognizant design engineer if the vibration amplitudes are not below 0.5 mils after five cranks at any single step listed below. (1) Rotate (crank) engine, using the starter, to 10%±5% NGP. (2) Disengage starter. Listen for and document unusual noises on rundown. During rundown all

engine bearing proximity probe vibration readings must be below 0.5 mils; if not repeat steps 1 and 2 before the engine comes to a complete stop, otherwise continue with step 3 before the engine comes to a complete stop.

(3) Rotate (crank) engine, using the starter, to 20% ± 5% NGP. (4) Disengage starter. Listen for and document unusual noises on rundown. During rundown all


(5) Rotate (crank) engine for approximately 2 minutes, using the starter, to terminal crank speed

(approximately 20 to 35% NGP depending on the type of starter). (6) Disengage starter. Listen for and document unusual noises on rundown. During rundown all


(7) Initiate a normal start before the engine comes to a complete stop.



Table 5. Reduction Gearbox Break-In Test Sequence(1)

Run Number

kW

Minimum Duration

Reference Notes

1

0

Run for 15 minutes

1, 2

2

1600 ±5%

Run for 15 minutes

1, 3

3

3200 ± 5%

Run for 15 minutes

1, 3

TABLE 5 NOTES: (1) Runs 1, 2 and 3 are gearbox break-in runs. Gearbox break-in may be done on either fuel for dual

fuel engines. Run 1 must be done for all engines. Runs 2 and 3 are required only on engines equipped with a new reduction gearbox or a gearbox being run for the first time after a major rotating component, gear support or bearing has been replaced. Runs 2 and 3 are not required for engines being performance tested against a used facility gearbox.

(2) Record all operating parameters measured by instrumentation listed in Table 2. Do not record

emissions data. (3) Record performance data and all operating parameters measured by instrumentation listed in Table

2. Do not record emissions data.



Table 6. Performance and Emissions Test Sequence(1)

DRY ENGINES

Run # Purpose of Run

Load Reference Notes

4 Corrected Performance, T5 Base

At Max Corr TRIT

2, 3, 4, 5, 6

5 Mechanical Full Load, Emissions (Performance Reference Only)

100% 2, 3, 8

6 Emissions (Only when required by Engineering Instruction)

80% 2, 9

NOTES: (1) After successful completion of the gearbox break-in test sequence (Table 5), the engine shall

demonstrate performance in accordance with Section 4.3.2 for each fuel used. Emissions shall be collected for every official (buy-off) full load mechanical (uncorrected) data point during acceptance testing as specified in Section 4.3.3; do not record part load emissions data.

(2) Thermally stabilize the engine for specific performance run prior to taking data. For a thermally

stabilized engine: - If the engine is cool or cold (engine has not run in the last 3 hours), run for a minimum of one continuous hour with the last 45 minutes at the conditions per section 4.3.2. If the engine is warm (has run for 1 hour within the past 3 hours clock time), run for a minimum of 20 minutes. Oil supply temperature must be at 110°F to 155°F for a minimum of 20 minutes prior to taking data.

(3) The guide vanes shall be fully open and the bleed valve closed for performance tests, Runs 4 and 5.

See Build Instructions and Data Chart drawing (ref. paragraph 2.2) for the variable vane alignment rigging and open/closed settings. (Ref: Alignment rigging is with IGV at 5°. Initial full open position is as rigged. The closed position is with the 1st stage ring at the closed position.) The full open angular settings may vary as shown in Table 1.

The IGV’s shall be set to optimize the corrected performance . This will establish the final IGV setting for dry engines; IGV angle reporting shall be in accordance with Section 5.1.1 (to be stamped onto engine nameplate).

(4) T5 Base is to be determined and recorded for each fuel used and in accordance with Section 5.1.1(to be stamped on the engine nameplate).

FOR LEGACY CONTROLS SYSTEMS: Record T5 compensator part number(s) in accordance with section 5.1.1 if required (to be stamped onto engine nameplate).

(5) Record performance data and all operating parameters measured by instrumentation listed in Table

2. Do not record emissions data.



Table 6. Performance and Emissions Test Sequence (continued)

DRY ENGINE NOTES continued: (6) If T1 is hot such that corrected TRIT cannot be attained without exceeding actual TRIT, then conduct

Run 4 per Table 1A. (7) Not Used.

(8) Record performance data (based on the corrected inlet temperature (T1)), emissions data, and all

operating parameters measured by instrumentation listed in Table 2. Record vibration signatures for all channels being monitored (For dual fuel units, vibration signatures only need to be recorded on one fuel).

(9) Partial loads are determined as a fraction of the full load from the T1 performance CS or PT Tables

at the current ambient temperature in test.

With the engine thermally stabilized, record mechanical performance and, if required, emissions data. Data is required on both fuels for dual fuel units.



Table 6A. Performance and Emissions Test Sequence(1)

WET ENGINES (WITH WATER-INJECTION)

Run # Purpose of Run

Load Reference Notes

4 Corrected Performance, T5 Base (DRY)

At Max Corr TRIT

2, 3, 4, 5, 6

5 Mechanical Full Load, Emissions (Performance Reference Only)

100% 2, 3, 8, 9, 11

6 Emissions (When required by Engineering Instruction)

80% 2, 9, 10, 11, 12

NOTES: (1) After successful completion of the gearbox break-in test sequence (Table 5), The engine shall

demonstrate performance in accordance with Section 4.3.2 for each fuel used. Emissions shall be collected for every official (buy-off) full load mechanical (uncorrected) data point during acceptance testing as specified in Section 4.3.3.

(2) Thermally stabilize the engine for specific performance run prior to taking data. For a thermally

stabilized engine: - If the engine is cool or cold (engine has not run in the last 3 hours), run for a minimum of one continuous hour with the last 45 minutes at the required TRIT for the data point. If the engine is warm (has run for 1 hour within the past 3 hours clock time), run for a minimum of 20 minutes at the TRIT required for the data point. Oil supply temperature must be at 110 to 155 degrees for a minimum of 20 minutes.

(3) The guide vanes shall be fully open and the bleed valve closed for performance tests, Runs 4 and 5.

See Build Instructions and Data Chart drawing (ref. paragraph 2.2) for the variable vane alignment rigging and open/closed settings. (Ref: Alignment rigging is with IGV at 5°. Initial full open position is as rigged. The closed position is with the 1st stage ring at the closed position.) The full open angular settings may vary as shown in Table 1. The IGV’s shall initially be set to optimize the corrected performance of all engines (Run 4). However, the IGV’s may have to be reset to optimize performance while operating wet during the full load performance run (Run 5). This will establish the final IGV setting for wet engines. IGV angle reporting shall be in accordance with Section 5.1.1 (to be stamped onto engine nameplate).

(4) Run 4 is the corrected performance acceptance point for all engines. Water injected engines should

record this point with water injection turned off. T5 Base is to be determined and recorded (DRY) for each fuel used and in accordance with Section 5.1.1 (nameplate).

FOR LEGACY CONTROLS SYSTEMS: Record T5 compensator part numbers(s), per Table 9, in

accordance with Section 5.1.1 if required (nameplate). (5) Record performance data and all operating parameters measured by instrumentation listed in Table

2. Do not record emissions data. (6) If T1 is hot such that corrected TRIT cannot be attained without exceeding actual TRIT, oscillation or

pilot limits, then conduct Run 4 per Table 1A or 1B as specified in section 4.3.2.1.



Table 6A. Performance and Emissions Test Sequence (continued) WET ENGINE

NOTES continued: (7) Not Used.

(8) Record performance data (based on the corrected inlet temperature (T1)), emissions data, and all operating parameters measured by instrumentation listed in Table 2. Record vibration signatures for all channels being monitored (For dual fuel units, vibration signatures only need to be recorded on one fuel).

(9) Refer to the appropriate CS/PT table for the initial water to fuel ratio (W/F). Adjust water flow accordingly to satisfy the emissions requirements.

(10) Partial loads are determined as a fraction of the full load from the T1 performance CS or PT Tables

at the current ambient temperature in test.

Record mechanical performance and emissions data. Data is required on both fuels for dual fuel units. Water injected engines need only meet emissions requirements while running wet.

(11) Scale water flow as a percentage of full range of the water flow transmitter as 0 – 100. (For example: 2.5 GPM using a 0 – 10 GPM transmitter would be scaled as 25.) Record this scaled water flow (0 – 100) and the corrected T5 average as PLC control constants GASNOXTMP (LIQNOXTMP) and GASNOXACT (LIQNOXACT) respectively in the Certified Test Report. Record fuel flow for water to fuel ratio checks. If W/F ratio exceeds 1.0 contact the cognizant Product Support - Performance Engineer.

Note: If the water flow transmitter used during test is anything other than the transmitter to be used on the customer package, include the 0 – 100% range of the flow transmitter in the Certified Test Report for proper field calibration of the water flow schedule with the customer flow transmitter.

(12) Record the corrected T5 average at 80% load. This value shall be used as PLC control constant

H2O_ON_LMT. H2O_OFFLMT = H2O_ON_LMT – 50.



Table 7. Engine Vibration Limits

Casing Mounted Velocity Vibration

Pickups(1)

Filter Bandpass

(Hz)

Maximum Velocity

(rms)

Reduction gearbox housing - horizontal 15-1000 0.28 in/s(3) Compressor diffuser fwd flange - horizontal 15-2000 0.28 in/s(3) Combustor aft flange - vertical

15-2000 0.40 in/s(2)

Accelerometer

Reduction gearbox housing - vertical

15-12,000 16G rms (3)

Rotor Proximity Probes

Maximum Displacement (P-P)

Nos. 1, 2, and 3 bearings

15-1000 (4)(5)

Axial position indicator

n/a (5)(6)

Notes: (1) External pickups shall be installed and recorded during all acceptance tests to provide

baseline data for field support. A customer option for internal pickups does not negate this requirement.

(2) Reference criteria only. Limits shown are not intended for Accept/Reject. If Combustor

Aft Flange - Vertical vibration exceeds the maximum value shown, contact the cognizant Design Engineer for disposition.

(3) Broadband (overall) vibration readings shall not exceed these limits. Discrete

frequencies, as determined by spectral analysis, shall not exceed the limits shown in Figures 6, 6a, and 7.



Table 7. Engine Vibration Limits (continued) NOTES (continued) (4) The broadband overall vibration limit is 3.5 mils P-P, in addition, engine 1E limit is 2.3

mils P-P. Only on the #1 bearing, the following Gearbox frequencies are acceptable: 30, 60, and 98.7 Hz (60 cycle) or 25, 50, and 82.2 Hz (50 cycle) limit is 2 mils P-P and 1.5 mils P-P for harmonics. Other frequencies are limited to 0.5 mils P-P. Care shall be taken to separate the gearbox frequencies from true non-synchronous frequencies that may be present in the spectrum. Use of frequency analyzer in the 100 Hz or 200 Hz full-scale mode is recommended to achieve the needed accuracy.

(5) Customer option. Every engine is equipped with radial proximity probes which shall be

connected, functioning, and monitored during the engine acceptance test, by way of either a) customer purchased package equipment if ordered, or b) facility equipment if customer has not purchased the package option. Axial proximity probes are a customer option. Depending on the customer order, axial proximity probes may or may not be installed. If installed, axial probes must be connected, functioning, and monitored during the acceptance test, by way of either a) customer purchased package equipment if ordered, or b) facility equipment if customer has not purchased the package option.

(6) If axial position indicators are installed as a contract requirement, zero the monitoring

system with the engine at full load (or above 75% load). Set the alarm and shutdown limits in the thrust direction. The unloaded side monitor values are not used, therefore, set the maximum (at least above 20 mils).



Table 7. Engine Vibration Limits (continued)

1. Gearbox housing horizontal

bracket

3. Diffuser Forward Flange horizontal

bracket 2. Gearbox housing vertical accel.

4. Combustor aft flange vertical bracket

Vibration Pickups and Positions



Table 8. Lube Oil System Limits

Flow Requirements: Refer to Figures 1, 2, and 4 Oil Flow Versus Pressure Acceptance Limits (Applies to C32 oil only). Oil flow to the starter gears (Figure 4) is reference data only. Use the flow indicating sight glass to verify flow for acceptance test. Flows and pressures in the referenced figures are measured at each bearing inlet port and are applicable at the following conditions:

• 90 to 100% NGP • 110 to 155ΕF oil supply temperature. • 45 to 65 psig oil supply pressure.

Thrust Bearing Temperature Limit The maximum thrust bearing metal temperature (RTD measurement) is 230°F. Pre/Post Lube Oil Limits

Pressure Range • Maximum - 25 psig • Minimum - 6 psig



Compensator Selection List for a Continuous Duty Single Shaft EngineChart is Based on a T5 Setpoint of 1250oF and TRIT of 1950oF

T5/TRIT Ratio Compensator Ref Temperature Change

0.7822 to 0.7780 NA -1700.7779 to 0.7739 NA -1600.7738 to 0.7697 NA -1500.7696 to 0.7656 NA -1400.7655 to 0.7614 NA -1300.7613 to 0.7573 NA -1200.7572 to 0.7531 NA -1100.7530 to 0.7490 NA -1000.7489 to 0.7448 NA -900.7447 to 0.7407 NA -800.7406 to 0.7365 120902-1 -700.7364 to 0.7324 120902-2 -600.7323 to 0.7282 120902-3 -500.7281 to 0.7241 120902-4 -400.7240 to 0.7199 120902-5 -300.7198 to 0.7158 120902-6 -200.7157 to 0.7116 120902-7 -100.7115 to 0.7075 120902-8 00.7074 to 0.7033 120902-9 +100.7032 to 0.6992 120902-10 +200.6991 to 0.6950 120902-11 +300.6949 to 0.6909 120902-12 +400.6908 to 0.6867 120902-13 +500.6866 to 0.6826 120902-14 +600.6825 to 0.6784 120902-15 +70

Notes:

(1) Select the T5 compensator based on the T5/TRIT ratio determined during the dry engine'scorrected performance test.

Select the T5 compensator based on the T5/TRIT ratio determined during the wet engine'sreference full load performance test while operating wet.

(2) Identify the compensator P/N(s) on the engine Nameplate.If dual fuel units indicate different sequential dash numbers for each fuel, select the dashnumbers corresponding to the lowest ratio (the higher dash number). If the indicatedT5 compensator dash numbers are a three number spread in a dual fuel unit, selectthe compensator between the two indicated. (i.e., if fuel A indicates (-9), and fuel Bindicates (-11), select (-10).

(3) Record the T5 compensator part number and T5/T3 ratio in the Certified Test Report forpermanent tracking.

Table 9. T5 Compensator Selection Chart for Engine Retrofits to Packages that do not use PLC Software Compensation



Reference: Plot points used to develop maximum/minimum lines.

Pressure

(psig)

Flow (gpm)

Maximum Flow Line

45 65

57.7 66.0

Minimum Flow Line

45 65

41.2 47.3

Figure 1a. Total Oil Flow No. 1 Bearing Inlet and Reduction Gearbox Design

For 196800-10X, 191100-104 and above, 222150-10X

Oil Flow No.1 Bearing and Reduction Gearbox

66

47.3

57.7

41.2

0

10

20

30

40

50

60

70

45 65

Oil Pressure (psig)

Oil

Flow

(gpm

)

GPM MaxGPM Min



Reference: Plot points used to develop the minimum/maximum lines.

Pressure (psig)

Flow (gpm)

Maximum Flow Line

45 65

61 66

Minimum flow Line

45 65

41.2 47.3

Figure 1b. Total Oil Flow No. 1 Bearing Inlet and Reduction Gearbox For 196800-20X, 302750-20X

Oil Flow No.1 Bearing and Reduction Gearbox

47.3

66

41.2

61

0

10

20

30

40

50

60

70

45 65

Oil Pressure (psig)

Oil

Flow

(gpm

)

GPM MinGPM Max



Reference: Plot points used to develop the minimum/maximum lines.

Pressure (psig)

Flow (gpm)

Maximum Flow Line

45 65

54.2 62.8

Minimum flow Line

45 65

37.6 44

Figure 1c. Total Oil Flow No. 1 Bearing Inlet and Reduction Gearbox For All Other Reduction Drive Assemblies

Oil Flow No. 1 Bearing and Reduction Gearbox

62.8

44

54.2

37.6

0

10

20

30

40

50

60

70

45 65

Oil Pressure (psig)

Oil

Flow

(gpm

)

GPM MaxGPM Min




Pressure

(psig)

Flow (gpm)

Maximum Flow Line

45 65

39.4 46.6

Minimum Flow Line

45 65

28.0 33.3

Figure 2. Total Oil Flow No. 2 and No. 3 Bearing Inlet

Oil Flow Bearings No. 2, 3, and Thrust

24

26

28

30

32

34

36

38

40

42

44

46

48

40 45 50 55 60 65 70

OIL PRESSURE (PSIG)

OIL

FLO

W (G

PM)




Oil Pressure

(psig)

Starter Flow

(gpm) Maximum Flow Line

45 70

0.25 0.30

Minimum Flow Line

45 70

0.14 0.17

Figure 4. Oil Flow to Starter Gears (Air/Gas Start Only) (Reference Only)



Reference: Plot points to develop oil tank sump pressure limit.

PCD (psig)

SUMP

(in. of H2O) Maximum Pressure Line m = 1/20 b = -0.8

70

150

2.7 6.7

Figure 5. Oil Tank Sump Pressure Limits



Reference: Plot points used to develop maximum line.

Intercept

Velocity

Frequency

A

0.07

15

B

0.18

40

Figure 6. Velocity Spectrum Limit Curve: Reduction Gearbox Housing Horizontal



Figure 6a. Acceleration Vibration Limit Curve: Reduction Gearbox Housing Vertical



Reference: Plot points used to develop maximum lines.

Intercept

Velocity

Frequency

A

0.13

15

B

0.13

190

C

0.17

250

Figure 7. Velocity Spectrum Limit Curve: Diffuser Forward Flange Horizontal



TAURUS 60-7901 CONTINOUS DUTY, NATURAL GAS FUEL, DRYPERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO

ZERO INLET & EXHAUST LOSS WITH 60% RH & P1.0=14.696

T1 POWER HEAT RATE T5 TOPPING T1 POWER HEAT RATE T5 TOPPING(F) (KW) (BTU/KW-HR) LIMIT(F) (F) (KW) (BTU/KW-HR) LIMIT(F)

T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.010 6373 10813 T5BASE+ -10.0 61 5458 11190 T5BASE+ 0.411 6356 10817 T5BASE+ -9.9 62 5437 11201 T5BASE+ 0.612 6338 10823 T5BASE+ -9.7 63 5416 11213 T5BASE+ 0.813 6320 10828 T5BASE+ -9.5 64 5395 11226 T5BASE+ 1.014 6302 10833 T5BASE+ -9.4 65 5373 11239 T5BASE+ 1.315 6285 10839 T5BASE+ -9.2 66 5351 11254 T5BASE+ 1.516 6267 10844 T5BASE+ -9.0 67 5328 11269 T5BASE+ 1.817 6249 10850 T5BASE+ -8.8 68 5305 11285 T5BASE+ 2.018 6231 10855 T5BASE+ -8.6 69 5282 11302 T5BASE+ 2.319 6213 10861 T5BASE+ -8.5 70 5259 11318 T5BASE+ 2.520 6195 10867 T5BASE+ -8.3 71 5235 11335 T5BASE+ 2.821 6178 10874 T5BASE+ -8.1 72 5212 11352 T5BASE+ 3.122 6160 10881 T5BASE+ -7.9 73 5188 11370 T5BASE+ 3.423 6142 10888 T5BASE+ -7.7 74 5165 11389 T5BASE+ 3.624 6123 10895 T5BASE+ -7.5 75 5141 11407 T5BASE+ 3.925 6105 10902 T5BASE+ -7.3 76 5117 11427 T5BASE+ 4.226 6087 10909 T5BASE+ -7.1 77 5093 11447 T5BASE+ 4.527 6069 10916 T5BASE+ -6.8 78 5069 11467 T5BASE+ 4.828 6051 10923 T5BASE+ -6.6 79 5045 11488 T5BASE+ 5.129 6033 10930 T5BASE+ -6.4 80 5023 11507 T5BASE+ 5.430 6016 10938 T5BASE+ -6.2 81 5002 11526 T5BASE+ 5.731 5998 10945 T5BASE+ -6.0 82 4980 11546 T5BASE+ 5.932 5980 10952 T5BASE+ -5.7 83 4958 11566 T5BASE+ 6.233 5962 10960 T5BASE+ -5.5 84 4936 11587 T5BASE+ 6.534 5944 10967 T5BASE+ -5.3 85 4914 11608 T5BASE+ 6.835 5926 10975 T5BASE+ -5.0 86 4893 11628 T5BASE+ 7.036 5909 10982 T5BASE+ -4.8 87 4871 11649 T5BASE+ 7.337 5891 10990 T5BASE+ -4.5 88 4850 11670 T5BASE+ 7.638 5873 10997 T5BASE+ -4.3 89 4828 11691 T5BASE+ 7.939 5856 11005 T5BASE+ -4.0 90 4806 11713 T5BASE+ 8.240 5838 11012 T5BASE+ -3.8 91 4784 11736 T5BASE+ 8.441 5821 11019 T5BASE+ -3.5 92 4761 11759 T5BASE+ 8.842 5803 11027 T5BASE+ -3.2 93 4739 11782 T5BASE+ 9.043 5786 11034 T5BASE+ -3.0 94 4717 11806 T5BASE+ 9.344 5768 11042 T5BASE+ -2.8 95 4694 11829 T5BASE+ 9.645 5750 11049 T5BASE+ -2.6 96 4671 11854 T5BASE+ 10.046 5733 11057 T5BASE+ -2.4 97 4648 11879 T5BASE+ 10.347 5715 11065 T5BASE+ -2.3 98 4625 11905 T5BASE+ 10.648 5697 11073 T5BASE+ -2.1 99 4601 11931 T5BASE+ 10.949 5679 11081 T5BASE+ -1.9 100 4578 11956 T5BASE+ 11.350 5661 11089 T5BASE+ -1.7 101 4555 11981 T5BASE+ 11.651 5644 11098 T5BASE+ -1.5 102 4532 12007 T5BASE+ 12.052 5626 11106 T5BASE+ -1.3 103 4509 12033 T5BASE+ 12.353 5608 11114 T5BASE+ -1.1 104 4486 12060 T5BASE+ 12.754 5590 11123 T5BASE+ -0.9 105 4462 12087 T5BASE+ 13.155 5572 11131 T5BASE+ -0.8 106 4439 12114 T5BASE+ 13.556 5554 11140 T5BASE+ -0.6 107 4416 12142 T5BASE+ 13.857 5536 11150 T5BASE+ -0.4 108 4392 12170 T5BASE+ 14.358 5518 11158 T5BASE+ -0.2 109 4369 12198 T5BASE+ 14.659 5500 11167 T5BASE+ 0.0 110 4345 12227 T5BASE+ 15.160 5479 11178 T5BASE+ 0.2

PT30350A Reference Full Load Performance, Prevailing T1



TAURUS 60-7901 CONTINOUS DUTY, DIESEL FUEL, DRYPERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO



T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.010 6198 10935 T5BASE+ -10.1 61 5308 11322 T5BASE+ 0.411 6181 10940 T5BASE+ -10.0 62 5287 11334 T5BASE+ 0.612 6164 10945 T5BASE+ -9.8 63 5267 11346 T5BASE+ 0.813 6147 10950 T5BASE+ -9.7 64 5246 11359 T5BASE+ 1.114 6130 10955 T5BASE+ -9.5 65 5225 11372 T5BASE+ 1.315 6113 10961 T5BASE+ -9.3 66 5203 11386 T5BASE+ 1.516 6095 10966 T5BASE+ -9.1 67 5181 11402 T5BASE+ 1.817 6078 10972 T5BASE+ -9.0 68 5159 11418 T5BASE+ 2.018 6061 10977 T5BASE+ -8.8 69 5136 11435 T5BASE+ 2.319 6043 10983 T5BASE+ -8.6 70 5114 11452 T5BASE+ 2.520 6026 10990 T5BASE+ -8.4 71 5091 11469 T5BASE+ 2.821 6009 10997 T5BASE+ -8.2 72 5068 11487 T5BASE+ 3.122 5991 11004 T5BASE+ -8.0 73 5045 11505 T5BASE+ 3.423 5974 11011 T5BASE+ -7.8 74 5022 11524 T5BASE+ 3.624 5956 11018 T5BASE+ -7.6 75 4999 11543 T5BASE+ 3.925 5939 11025 T5BASE+ -7.4 76 4976 11562 T5BASE+ 4.226 5921 11032 T5BASE+ -7.2 77 4953 11583 T5BASE+ 4.527 5903 11040 T5BASE+ -7.0 78 4929 11604 T5BASE+ 4.828 5886 11047 T5BASE+ -6.8 79 4906 11625 T5BASE+ 5.129 5868 11054 T5BASE+ -6.5 80 4885 11645 T5BASE+ 5.430 5851 11062 T5BASE+ -6.3 81 4863 11665 T5BASE+ 5.731 5833 11069 T5BASE+ -6.1 82 4842 11685 T5BASE+ 6.032 5816 11077 T5BASE+ -5.9 83 4821 11706 T5BASE+ 6.233 5799 11084 T5BASE+ -5.6 84 4800 11727 T5BASE+ 6.534 5781 11092 T5BASE+ -5.4 85 4778 11748 T5BASE+ 6.835 5764 11100 T5BASE+ -5.2 86 4757 11770 T5BASE+ 7.136 5747 11107 T5BASE+ -4.9 87 4736 11791 T5BASE+ 7.337 5730 11115 T5BASE+ -4.7 88 4715 11813 T5BASE+ 7.638 5712 11123 T5BASE+ -4.4 89 4693 11835 T5BASE+ 7.939 5695 11130 T5BASE+ -4.2 90 4672 11857 T5BASE+ 8.240 5678 11138 T5BASE+ -3.9 91 4650 11880 T5BASE+ 8.541 5661 11145 T5BASE+ -3.7 92 4629 11904 T5BASE+ 8.842 5644 11153 T5BASE+ -3.4 93 4607 11928 T5BASE+ 9.143 5627 11160 T5BASE+ -3.1 94 4585 11952 T5BASE+ 9.444 5610 11168 T5BASE+ -2.9 95 4563 11977 T5BASE+ 9.745 5593 11176 T5BASE+ -2.7 96 4541 12002 T5BASE+ 10.046 5576 11183 T5BASE+ -2.5 97 4518 12028 T5BASE+ 10.347 5559 11192 T5BASE+ -2.3 98 4495 12054 T5BASE+ 10.748 5541 11200 T5BASE+ -2.1 99 4472 12080 T5BASE+ 11.049 5524 11208 T5BASE+ -1.9 100 4450 12106 T5BASE+ 11.350 5506 11217 T5BASE+ -1.7 101 4428 12132 T5BASE+ 11.751 5489 11226 T5BASE+ -1.5 102 4405 12159 T5BASE+ 12.152 5471 11234 T5BASE+ -1.4 103 4383 12185 T5BASE+ 12.453 5454 11243 T5BASE+ -1.2 104 4360 12213 T5BASE+ 12.854 5436 11252 T5BASE+ -1.0 105 4337 12240 T5BASE+ 13.255 5419 11261 T5BASE+ -0.8 106 4314 12269 T5BASE+ 13.656 5401 11271 T5BASE+ -0.6 107 4292 12297 T5BASE+ 14.057 5383 11280 T5BASE+ -0.4 108 4269 12326 T5BASE+ 14.358 5366 11289 T5BASE+ -0.2 109 4246 12355 T5BASE+ 14.759 5348 11299 T5BASE+ 0.0 110 4223 12384 T5BASE+ 15.160 5328 11310 T5BASE+ 0.2

PT30351A Reference Full Load Performance, Prevailing T1



TAURUS 60-7801 CONTINOUS DUTY, NATURAL GAS FUEL, DRYPERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO



T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.010 6134 11245 T5BASE+ 0 61 5299 11593 T5BASE+ 011 6117 11251 T5BASE+ 0 62 5281 11603 T5BASE+ 012 6100 11257 T5BASE+ 0 63 5263 11613 T5BASE+ 013 6083 11263 T5BASE+ 0 64 5245 11623 T5BASE+ 014 6066 11270 T5BASE+ 0 65 5228 11633 T5BASE+ 015 6049 11276 T5BASE+ 0 66 5210 11643 T5BASE+ 016 6032 11282 T5BASE+ 0 67 5193 11653 T5BASE+ 017 6015 11289 T5BASE+ 0 68 5176 11663 T5BASE+ 018 5999 11295 T5BASE+ 0 69 5158 11675 T5BASE+ 019 5982 11301 T5BASE+ 0 70 5138 11688 T5BASE+ 020 5966 11307 T5BASE+ 0 71 5118 11701 T5BASE+ 021 5950 11313 T5BASE+ 0 72 5099 11714 T5BASE+ 022 5933 11319 T5BASE+ 0 73 5079 11727 T5BASE+ 023 5917 11324 T5BASE+ 0 74 5060 11740 T5BASE+ 024 5901 11330 T5BASE+ 0 75 5041 11752 T5BASE+ 025 5885 11335 T5BASE+ 0 76 5021 11766 T5BASE+ 026 5869 11341 T5BASE+ 0 77 5002 11778 T5BASE+ 027 5853 11347 T5BASE+ 0 78 4984 11791 T5BASE+ 028 5837 11352 T5BASE+ 0 79 4964 11805 T5BASE+ 029 5822 11358 T5BASE+ 0 80 4940 11824 T5BASE+ 030 5806 11363 T5BASE+ 0 81 4916 11843 T5BASE+ 031 5790 11369 T5BASE+ 0 82 4892 11863 T5BASE+ 032 5776 11374 T5BASE+ 0 83 4868 11882 T5BASE+ 033 5760 11379 T5BASE+ 0 84 4844 11902 T5BASE+ 034 5745 11385 T5BASE+ 0 85 4821 11921 T5BASE+ 035 5730 11390 T5BASE+ 0 86 4798 11941 T5BASE+ 036 5715 11396 T5BASE+ 0 87 4775 11960 T5BASE+ 037 5700 11401 T5BASE+ 0 88 4752 11980 T5BASE+ 038 5685 11406 T5BASE+ 0 89 4729 12000 T5BASE+ 039 5670 11411 T5BASE+ 0 90 4707 12019 T5BASE+ 040 5654 11417 T5BASE+ 0 91 4685 12038 T5BASE+ 041 5638 11425 T5BASE+ 0 92 4663 12058 T5BASE+ 042 5621 11432 T5BASE+ 0 93 4641 12077 T5BASE+ 043 5605 11440 T5BASE+ 0 94 4620 12097 T5BASE+ 044 5588 11447 T5BASE+ 0 95 4599 12117 T5BASE+ 045 5571 11454 T5BASE+ 0 96 4578 12136 T5BASE+ 046 5555 11462 T5BASE+ 0 97 4557 12156 T5BASE+ 047 5539 11469 T5BASE+ 0 98 4536 12176 T5BASE+ 048 5523 11476 T5BASE+ 0 99 4513 12199 T5BASE+ 049 5507 11483 T5BASE+ 0 100 4488 12225 T5BASE+ 050 5489 11492 T5BASE+ 0 101 4463 12251 T5BASE+ 051 5472 11501 T5BASE+ 0 102 4438 12278 T5BASE+ 052 5454 11510 T5BASE+ 0 103 4413 12304 T5BASE+ 053 5437 11519 T5BASE+ 0 104 4389 12330 T5BASE+ 054 5419 11529 T5BASE+ 0 105 4365 12356 T5BASE+ 055 5402 11538 T5BASE+ 0 106 4341 12383 T5BASE+ 056 5385 11547 T5BASE+ 0 107 4318 12410 T5BASE+ 057 5368 11556 T5BASE+ 0 108 4295 12437 T5BASE+ 058 5352 11565 T5BASE+ 0 109 4272 12464 T5BASE+ 059 5335 11574 T5BASE+ 0 110 4249 12491 T5BASE+ 060 5317 11583 T5BASE+ 0

PT30137 Reference Full Load Performance, Prevailing T1



TAURUS 60 - 7801 CONTINUOUS DUTY, LIQUID FUEL, DRYPERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO





Engineering Specification No. ES 2098AB Addendum 1


ADDENDUM 1 Taurus 60-6201 ACCEPTANCE TEST REQUIREMENTS CONTENTS Paragraph Page 1.0 Scope 41 2.2 Drawings 41 4.3.2 Performance Evaluation 41 TABLES Table Page 1 Performance Requirements (for 6201), 59°F 42 1A Performance Requirements (for 6201), 80°F 43 9 T5 Compensator Selection Chart 44 CS 27822 Reference Full Load Performance (6201) Continuous, Dry, Gas 45 CS 27823 Reference Full Load Performance (6201) Continuous, Dry, Liquid 46 PT 30039 Reference Full Load Performance (6201) Continuous, Wet, Gas 47 PT 30079 Reference Full Load Performance (6201) Continuous, Wet, Liquid 48 CS 27824 Reference Full Load Performance (6201) Emergency, Dry, Gas 49 CS 27825 Reference Full Load Performance (6201) Emergency, Dry, Liquid 50 PT 30080 Reference Full Load Performance (6201) Emergency, Wet, Gas 51 PT 30081 Reference Full Load Performance (6201) Emergency, Wet, Liquid 52



1.0 SCOPE - This Addendum contains the Acceptance Test Requirements for the Taurus 60-6201 One-Shaft Engine. The provisions of the basic ES 2098 Specification apply to the Taurus 60-6201 engine except as specifically amended in the Addendum. 2.2 DRAWINGS

Solar

MPDC List No. TTA-1 Taurus 60-6201 One-Shaft Engine 180076 Data Chart and Build Instructions (6201) 180077 Mechanical Installation 196800 1800 rpm Reduction Drive Gearbox 191100 1500 rpm Reduction Drive Gearbox

4.3.2.2 PERFORMANCE EVALUATION

Reference Mechanical Full Load Performance Tables

CS 27822 6201 Continuous Dry Gas

CS 27823 6201 Continuous Dry Liquid

PT 30039 6201 Continuous Wet Gas

PT 30079 6201 Continuous Wet Liquid

CS 27824 6201 Emergency Dry Gas

CS 27825 6201 Emergency Dry Liquid

PT 30080 6201 Emergency Wet Gas

PT 30081 6201 Emergency Wet Liquid



CORRECTED PERFORMANCE

Parameters corrected to 59F, 60% relative humidity, sea level with no inlet or exhaust duct losses.Gearbox efficiency = 98.0% Generator efficiency = 96.4%

Parameter


Engine Speed 99.9 to 100.1%(% of 14951 rpm for 60Hz Gbx % of 14944 rpm for 50Hz Gbx)

Turbine Rotor Inlet Temperature TRIT 1830 to 1850oF

Turbine T5/TRIT Ratio 0.7294 to 0.8377

Minimum Power (KWe) (natural gas fuel) 4237 KW(Liquid Fuel) 4130 KW

Maximum Heat Rate (Btu/KW-hr) (natural gas fuel) 12,692 Btu/KW-hr(Liquid Fuel) 12,815 Btu/KW-hr

IGV Setting (degrees) 2 to 8 deg.


Compressor Pressure Ratio (min) 10.7

Compressor Mass Flow (pps) (max) 46.1 pps

Turbine Exhaust Temperature (oF) (min) 899oF

(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is hot thereby preventing 59F corrected performance without exceeding 1950F actual TRIT.(2). Table 1A should be used in lieu of Table 1 for GSE (Emergency Duty) package types.(3). Reference performance parameters are not an acceptance criteria. Contact the Performance Engineer for disposition if indicated limits are exceeded.

Table 1.(1) Performance Acceptance Requirements (-6201)

Continuous Duty

EmergencyDuty(2)



Table 1A.(1) Performance Acceptance Requirements (-6201)



Parameter





Minimum Power (KWe) (natural gas fuel)(Liquid Fuel)

Maximum Heat Rate (Btu/KW-hr) (natural gas fuel)(Liquid Fuel)



Compressor Pressure Ratio (min)

Compressor Mass Flow (pps) (max)

Turbine Exhaust Temperature (oF) (min)

(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is hot thereby preventing 59F corrected performance without exceeding 1950F actual TRIT. Applies to all GSE ratings.(2). Reference performance parameters are not an acceptance criteria. Contact the Performance Engineer for disposition if indicated limits are exceeded.

990oF905oF

43.7 pps 43.5 pps

2 to 8 deg.

10.1 10.4

2 to 8 deg.

12,700 Btu/KW-hr13,032 Btu/KW-hr 12,827 Btu/KW-hr12,898 Btu/KW-hr

4304 KW3779 KW 4197 KW3879 KW

0.7294 to 0.8377 0.7324 to 0.8361

1830 to 1850 1930 to 1950

99.9 to 100.1% 99.9 to 100.1%

Continuous Duty

EmergencyDuty



Table 9. T5 Compensator Selection Chart (-6201) for Engine Retrofits to PackagesWhich do not use PLC Software

Compensator selection list for Continuous/Emergency Duty single shaft engine.Chart is based on a T5 setpoint of 1400°F/1480oF and TRIT of 1850°F/1950oF.

GSC T5/TRIT Ratio GSE T5/TRIT Ratio Compensator Ref Temperature Change

0.8377 to 0.8333 0.8361 to 0.8320 120902-1 -70°0.8332 to 0.8290 0.8319 to 0.8278 120902-2 -60°0.8289 to 0.8247 0.8277 to 0.8237 120902-3 -50°0.8246 to 0.8203 0.8236 to 0.8195 120902-4 -40°0.8202 to 0.8160 0.8194 to 0.8154 120902-5 -30°0.8159 to 0.8117 0.8153 to 0.8112 120902-6 -20°0.8116 to 0.8074 0.8111 to 0.8071 120902-7 -10°0.8073 to 0.8030 0.8070 to 0.8029 120902-8 0°0.8029 to 0.7987 0.8028 to 0.7988 120902-9 +10°0.7986 to 0.7944 0.7987 to 0.7946 120902-10 +20°0.7943 to 0.7900 0.7945 to 0.7905 120902-11 +30°0.7899 to 0.7857 0.7904 to 0.7863 120902-12 +40°0.7856 to 0.7814 0.7862 to 0.7822 120902-13 +50°0.7813 to 0.7771 0.7821 to 0.7780 120902-14 +60°0.7770 to 0.7727 0.7779 to 0.7739 120902-15 +70°0.7726 to 0.7684 0.7738 to 0.7697 120902-16 +80°0.7683 to 0.7641 0.7696 to 0.7656 120902-17 +90°0.7640 to 0.7597 0.7655 to 0.7614 120902-18 +100°0.7596 to 0.7554 0.7613 to 0.7573 120902-19 +110°0.7553 to 0.7511 0.7572 to 0.7531 120902-20 +120°0.7510 to 0.7468 0.7530 to 0.7490 120902-21 +130°0.7467 to 0.7424 0.7489 to 0.7448 120902-22 +140°0.7423 to 0.7381 0.7447 to 0.7407 120902-23 +150°0.7380 to 0.7338 0.7406 to 0.7365 120902-24 +160°0.7337 to 0.7294 0.7364 to 0.7324 120902-25 +170°

Notes:







TAURUS 60-6201 CONTINUOUS DUTY, NATURAL GAS FUEL, DRY

REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO ZERO INLET & EXHAUST LOSS WITH 60% RH & P1.0=14.696

T1 POWER HEAT RATE T5 TOPPING T1 POWER HEAT RATE T5 TOPPING (F) (KW) (BTU/KW-HR) LIMIT(F) (F) (KW) (BTU/KW-HR) LIMIT(F)

T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.0 10 4866 12300 T5BASE+ 0 61 4202 12711 T5BASE+ 0 11 4852 12310 T5BASE+ 0 62 4184 12720 T5BASE+ 0 12 4839 12319 T5BASE+ 0 63 4166 12729 T5BASE+ 0 13 4825 12328 T5BASE+ 0 64 4149 12738 T5BASE+ 0 14 4812 12337 T5BASE+ 0 65 4131 12747 T5BASE+ 0 15 4798 12345 T5BASE+ 0 66 4114 12757 T5BASE+ 0 16 4786 12353 T5BASE+ 0 67 4097 12767 T5BASE+ 0 17 4772 12362 T5BASE+ 0 68 4080 12776 T5BASE+ 0 18 4760 12370 T5BASE+ 0 69 4062 12786 T5BASE+ 0 19 4746 12378 T5BASE+ 0 70 4045 12795 T5BASE+ 0 20 4734 12385 T5BASE+ 0 71 4029 12805 T5BASE+ 0 21 4721 12392 T5BASE+ 0 72 4012 12815 T5BASE+ 0 22 4708 12399 T5BASE+ 0 73 3995 12825 T5BASE+ 0 23 4696 12405 T5BASE+ 0 74 3978 12835 T5BASE+ 0 24 4683 12412 T5BASE+ 0 75 3962 12845 T5BASE+ 0 25 4671 12418 T5BASE+ 0 76 3945 12856 T5BASE+ 0 26 4660 12425 T5BASE+ 0 77 3928 12866 T5BASE+ 0 27 4647 12431 T5BASE+ 0 78 3912 12877 T5BASE+ 0 28 4636 12438 T5BASE+ 0 79 3896 12887 T5BASE+ 0 29 4624 12444 T5BASE+ 0 80 3879 12898 T5BASE+ 0 30 4612 12450 T5BASE+ 0 81 3863 12909 T5BASE+ 0 31 4600 12457 T5BASE+ 0 82 3847 12919 T5BASE+ 0 32 4589 12463 T5BASE+ 0 83 3832 12930 T5BASE+ 0 33 4577 12469 T5BASE+ 0 84 3816 12941 T5BASE+ 0 34 4566 12476 T5BASE+ 0 85 3799 12956 T5BASE+ 0 35 4555 12482 T5BASE+ 0 86 3783 12971 T5BASE+ 0 36 4542 12490 T5BASE+ 0 87 3767 12987 T5BASE+ 0 37 4528 12501 T5BASE+ 0 88 3750 13003 T5BASE+ 0 38 4514 12511 T5BASE+ 0 89 3734 13019 T5BASE+ 0 39 4500 12521 T5BASE+ 0 90 3719 13034 T5BASE+ 0 40 4486 12531 T5BASE+ 0 91 3703 13051 T5BASE+ 0 41 4473 12540 T5BASE+ 0 92 3687 13070 T5BASE+ 0 42 4459 12550 T5BASE+ 0 93 3671 13088 T5BASE+ 0 43 4445 12559 T5BASE+ 0 94 3655 13107 T5BASE+ 0 44 4432 12568 T5BASE+ 0 95 3639 13125 T5BASE+ 0 45 4419 12577 T5BASE+ 0 96 3624 13143 T5BASE+ 0 46 4405 12586 T5BASE+ 0 97 3609 13161 T5BASE+ 0 47 4392 12595 T5BASE+ 0 98 3593 13179 T5BASE+ 0 48 4379 12604 T5BASE+ 0 99 3578 13197 T5BASE+ 0 49 4365 12613 T5BASE+ 0 100 3564 13214 T5BASE+ 0 50 4352 12621 T5BASE+ 0 101 3549 13232 T5BASE+ 0 51 4339 12629 T5BASE+ 0 102 3535 13249 T5BASE+ 0 52 4327 12637 T5BASE+ 0 103 3521 13266 T5BASE+ 0 53 4314 12645 T5BASE+ 0 104 3507 13284 T5BASE+ 0 54 4301 12653 T5BASE+ 0 105 3493 13300 T5BASE+ 0 55 4288 12661 T5BASE+ 0 106 3479 13317 T5BASE+ 0 56 4276 12669 T5BASE+ 0 107 3466 13334 T5BASE+ 0 57 4263 12676 T5BASE+ 0 108 3452 13350 T5BASE+ 0 58 4250 12684 T5BASE+ 0 109 3438 13367 T5BASE+ 0 59 4237 12692 T5BASE+ 0 110 3422 13386 T5BASE+ 0 60 4220 12701 T5BASE+ 0

CS27822 Reference Full Load Performance, Prevailing T1



TAURUS 60-6201 CONTINUOUS DUTY LIQUID FUEL DRYREFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO

ZERO INLET & EXHAUST LOSS WITH 60% RH & P1.0=14.696 T1 POWER HEAT RATE T5 TOPPING T1 POWER HEAT RATE T5 TOPPING (F) (KW) (BTU/KW-HR) LIMIT(F) (F) (KW) (BTU/KW-HR) LIMIT(F)





TAURUS 60-6201 CONTINUOUS DUTY, GAS FUEL, WET (W/F=0.83 +/-0.1)REFERENCE PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6201 CONTINUOUS DUTY, LIQUID FUEL, WET (W/F=0.6 +/-0.1)REFERENCE PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6201 EMERGENCY DUTY NATURAL GAS FUEL DRYREFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO

ZERO INLET & EXHAUST LOSS WITH 60% RH & P1.0=14.696 T1 POWER HEAT RATE T5 TOPPING T1 POWER HEAT RATE T5 TOPPING(F) (KW) (BTU/KW-HR) LIMIT(F) (F) (KW) (BTU/KW-HR) LIMIT(F)

T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.0 10 5344 12096 T5BASE+ 0 61 4632 12561 T5BASE+ 011 5330 12107 T5BASE+ 0 62 4614 12569 T5BASE+ 0 12 5315 12117 T5BASE+ 0 63 4596 12577 T5BASE+ 0 13 5300 12127 T5BASE+ 0 64 4578 12585 T5BASE+ 0 14 5286 12137 T5BASE+ 0 65 4560 12593 T5BASE+ 0 15 5271 12147 T5BASE+ 0 66 4542 12600 T5BASE+ 0 16 5257 12157 T5BASE+ 0 67 4525 12608 T5BASE+ 0 17 5243 12166 T5BASE+ 0 68 4507 12615 T5BASE+ 0 18 5229 12176 T5BASE+ 0 69 4490 12622 T5BASE+ 0 19 5215 12185 T5BASE+ 0 70 4472 12628 T5BASE+ 0 20 5201 12194 T5BASE+ 0 71 4455 12635 T5BASE+ 0 21 5187 12203 T5BASE+ 0 72 4438 12641 T5BASE+ 0 22 5174 12211 T5BASE+ 0 73 4422 12647 T5BASE+ 0 23 5160 12220 T5BASE+ 0 74 4405 12653 T5BASE+ 0 24 5147 12228 T5BASE+ 0 75 4389 12659 T5BASE+ 0 25 5133 12237 T5BASE+ 0 76 4373 12664 T5BASE+ 0 26 5120 12245 T5BASE+ 0 77 4355 12673 T5BASE+ 0 27 5107 12253 T5BASE+ 0 78 4338 12682 T5BASE+ 0 28 5094 12260 T5BASE+ 0 79 4321 12691 T5BASE+ 0 29 5081 12268 T5BASE+ 0 80 4304 12700 T5BASE+ 0 30 5068 12276 T5BASE+ 0 81 4287 12710 T5BASE+ 0 31 5056 12283 T5BASE+ 0 82 4271 12719 T5BASE+ 0 32 5043 12290 T5BASE+ 0 83 4254 12729 T5BASE+ 0 33 5030 12297 T5BASE+ 0 84 4238 12738 T5BASE+ 0 34 5018 12304 T5BASE+ 0 85 4220 12751 T5BASE+ 0 35 5006 12311 T5BASE+ 0 86 4202 12767 T5BASE+ 0 36 4992 12320 T5BASE+ 0 87 4184 12783 T5BASE+ 0 37 4977 12331 T5BASE+ 0 88 4166 12799 T5BASE+ 0 38 4962 12343 T5BASE+ 0 89 4148 12815 T5BASE+ 0 39 4947 12353 T5BASE+ 0 90 4131 12830 T5BASE+ 0 40 4932 12364 T5BASE+ 0 91 4114 12846 T5BASE+ 0 41 4917 12375 T5BASE+ 0 92 4097 12861 T5BASE+ 0 42 4903 12385 T5BASE+ 0 93 4080 12877 T5BASE+ 0 43 4888 12395 T5BASE+ 0 94 4063 12892 T5BASE+ 0 44 4874 12406 T5BASE+ 0 95 4047 12908 T5BASE+ 0 45 4860 12416 T5BASE+ 0 96 4030 12923 T5BASE+ 0 46 4846 12426 T5BASE+ 0 97 4014 12938 T5BASE+ 0 47 4832 12435 T5BASE+ 0 98 3998 12953 T5BASE+ 0 48 4818 12445 T5BASE+ 0 99 3982 12969 T5BASE+ 0 49 4804 12455 T5BASE+ 0 100 3967 12984 T5BASE+ 0 50 4790 12464 T5BASE+ 0 101 3951 12999 T5BASE+ 0 51 4777 12473 T5BASE+ 0 102 3936 13014 T5BASE+ 0 52 4763 12482 T5BASE+ 0 103 3921 13029 T5BASE+ 0 53 4749 12492 T5BASE+ 0 104 3906 13043 T5BASE+ 0 54 4736 12501 T5BASE+ 0 105 3891 13058 T5BASE+ 0 55 4723 12509 T5BASE+ 0 106 3876 13074 T5BASE+ 0 56 4709 12518 T5BASE+ 0 107 3862 13088 T5BASE+ 0 57 4696 12527 T5BASE+ 0 108 3847 13103 T5BASE+ 0 58 4683 12535 T5BASE+ 0 109 3832 13118 T5BASE+ 0 59 4670 12543 T5BASE+ 0 110 3816 13135 T5BASE+ 0 60 4651 12552 T5BASE+ 0




TAURUS 60-6201 EMERGENCY DUTY, NATURAL GAS FUEL, WET (W/F=0.86 +/-0.1)REFERENCE PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6201 EMERGENCY DUTY, LIQUID FUEL, DRY REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6201 EMERGENCY DUTY, LIQUID FUEL, WET (W/F=0.63 +/-0.1)REFERENCE PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO





Specification No. ES 2098AB Addendum 2


ADDENDUM 2 Taurus 60-6501 - ACCEPTANCE TEST REQUIREMENTS CONTENTS Paragraph Page 1.0 Scope 54 2.2 Drawings 54 4.3.2 Performance Evaluation 54 TABLES Table Page 1 Performance Requirements (for 6501), 59°F 55 1A Performance Requirements (for 6501), 80°F 56 9 T5 Compensator Selection Chart 57 CS 27814 Reference Full Load Performance (6501) Continuous, Dry, Gas 58 CS 27815 Reference Full Load Performance (6501) Continuous, Dry, Liquid 59 CS 27816 Reference Full Load Performance (6501) Emergency, Dry, Gas 60 CS 27817 Reference Full Load Performance (6501) Emergency, Dry, Liquid 61 CS 27818 Reference Full Load Performance (6501) Continuous, Wet, Gas 62 CS 27819 Reference Full Load Performance (6501) Continuous, Wet, Liquid 63 CS 27820 Reference Full Load Performance (6501) Emergency, Wet, Gas 64 CS 27821 Reference Full Load Performance (6501) Emergency, Wet, Liquid 65




SOLAR

MPDC List No. TTB-1 Taurus 60-6501, One-Shaft Engine 180094 Data Chart and Build Instructions (6501) 180209 Mechanical Installation 196800 1800 rpm Reduction Drive Gearbox 191100 1500 rpm Reduction Drive Gearbox







CS 27818 6501 Continuous Wet Gas

CS 27819 6501 Continuous Wet Liquid

CS 27820 6501 Emergency Wet Gas

CS 27821 6501 Emergency Wet Liquid





Parameter



Turbine Rotor Inlet Temperature TRIT 1830 to 1850oF











Continuous Duty

EmergencyDuty(2)






Parameter













974oF

43.5 pps 43.5 pps

909oF

2 to 8 deg.

10.1 10.3

2 to 8 deg.


4507 KW3956 KW 4387 KW4063 KW

0.6645 to 0.7727 0.6701 to 0.7739

1830 to 1850 1930 to 1950

Continuous Duty

EmergencyDuty

99.9 to 100.1% 99.9 to 100.1%




Compensator selection list for Continuous/Emergency Duty single shaft engine.Chart is based on a T5 setpoint of 1250°F/1330oF and TRIT of 1850°F/1950oF.



Notes:







TAURUS 60-6501 CONTINUOUS DUTY, NATURAL GAS FUEL, DRY REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6501 CONTINUOUS DUTY, LIQUID FUEL, DRY







TAURUS 60-6501 EMERGENCY DUTY, NATURAL GAS FUEL, DRY







TAURUS 60-6501 EMERGENCY DUTY, LIQUID FUEL, DRY







TAURUS 60-6501 CONTINUOUS DUTY, NATURAL GAS FUEL, W/F RATIO=0.83(+/-0.1) REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6501 CONTINUOUS DUTY, LIQUID FUEL, W/F RATIO=0.60(+/-0.1)







TAURUS 60-6501 EMERGENCY DUTY, NATURAL GAS FUEL, W/F RATIO=0.86(+/-0.1) REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-6501 EMERGENCY DUTY, LIQUID FUEL, W/F RATIO=0.63(+/-0.1)





Specification No. ES 2098AA Addendum 3


ADDENDUM 3 Taurus 60-7001 - ACCEPTANCE TEST REQUIREMENTS CONTENTS Paragraph Page 1.0 SCOPE 67 2.2 DRAWINGS 67 4.3.2 PERFORMANCE EVALUATION 67 TABLES Table Page 1 Performance Requirements (for 7001), 59°F 68 1A Performance Requirements (for 7001), 80°F 69 9 T5 Compensator Selection Chart 70 CS 27806 Reference Full Load Performance (7001) Continuous, Dry, Gas 71 CS 27807 Reference Full Load Performance (7001) Continuous, Dry, Liquid 72 CS 27808 Reference Full Load Performance (7001) Emergency, Dry, Gas 73 CS 27809 Reference Full Load Performance (7001) Emergency, Dry, Liquid 74 CS 27810 Reference Full Load Performance (7001) Continuous, Wet, Gas 75 CS 27811 Reference Full Load Performance (7001) Continuous, Wet, Liquid 76 CS 27812 Reference Full Load Performance (7001) Emergency, Wet, Gas 77 CS 27813 Reference Full Load Performance (7001) Emergency, Wet, Liquid 78




Solar

MPDC List No. TTC-1 Taurus 60-7001, One-Shaft Engine 197003 Data Chart and Build Instructions (7001) 197011 Mechanical Installation 196800 1800 rpm Reduction Drive Gearbox 191100 1500 rpm Reduction Drive Gearbox







CS 27810 7001 Continuous Wet Gas

CS 27811 7001 Continuous Wet Liquid

CS 27812 7001 Emergency Wet Gas

CS 27813 7001 Emergency Wet Liquid





Parameter














Continuous Duty

EmergencyDuty(2)

1850 +/- 10oF

0.6616 to 0.7694






Parameter













Continuous Duty

EmergencyDuty

99.9 to 100.1% 99.9 to 100.1%

1850 +/- 10oF 1930 to 1950

0.6616 to 0.7694 0.6701 to 0.7739

4862 KW4298 KW 4761 KW4391 KW


2 to 8 deg.

11.4 11.5

2 to 8 deg.

944oF

47.1 pps 47.1 pps

880oF




Compensator selection list for Continuous/Emergency Duty single shaft engine.Chart is based on a T5 setpoint of 1250°F/1330oF and TRIT of 1850°F (+/-10oF)/1950oF.(+0/-20oF)



Notes:







TAURUS 60-7001 CONTINUOUS DUTY, NATURAL GAS FUEL, DRY REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-7001 EMERGENCY DUTY, NATURAL GAS FUEL, DRY



T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.0

10 6245 10865 T5BASE+ 0 61 5255 11480 T5BASE+ 0 11 6224 10872 T5BASE+ 0 62 5234 11490 T5BASE+ 0 12 6204 10879 T5BASE+ 0 63 5212 11500 T5BASE+ 0 13 6183 10886 T5BASE+ 0 64 5190 11511 T5BASE+ 0 14 6163 10893 T5BASE+ 0 65 5169 11522 T5BASE+ 0 15 6142 10902 T5BASE+ 0 66 5147 11533 T5BASE+ 0 16 6122 10911 T5BASE+ 0 67 5126 11545 T5BASE+ 0 17 6102 10920 T5BASE+ 0 68 5105 11557 T5BASE+ 0 18 6081 10930 T5BASE+ 0 69 5083 11569 T5BASE+ 0 19 6061 10940 T5BASE+ 0 70 5063 11581 T5BASE+ 0 20 6042 10950 T5BASE+ 0 71 5041 11596 T5BASE+ 0 21 6022 10960 T5BASE+ 0 72 5021 11611 T5BASE+ 0 22 6002 10971 T5BASE+ 0 73 5000 11626 T5BASE+ 0 23 5983 10981 T5BASE+ 0 74 4980 11641 T5BASE+ 0 24 5964 10992 T5BASE+ 0 75 4959 11655 T5BASE+ 0 25 5945 11003 T5BASE+ 0 76 4940 11670 T5BASE+ 0 26 5926 11020 T5BASE+ 0 77 4920 11684 T5BASE+ 0 27 5906 11042 T5BASE+ 0 78 4900 11698 T5BASE+ 0 28 5889 11062 T5BASE+ 0 79 4881 11712 T5BASE+ 0 29 5872 11081 T5BASE+ 0 80 4862 11727 T5BASE+ 0 30 5856 11099 T5BASE+ 0 81 4843 11740 T5BASE+ 0 31 5840 11117 T5BASE+ 0 82 4824 11754 T5BASE+ 0 32 5824 11133 T5BASE+ 0 83 4806 11767 T5BASE+ 0 33 5808 11149 T5BASE+ 0 84 4787 11782 T5BASE+ 0 34 5792 11164 T5BASE+ 0 85 4764 11802 T5BASE+ 0 35 5775 11178 T5BASE+ 0 86 4740 11825 T5BASE+ 0 36 5756 11186 T5BASE+ 0 87 4717 11847 T5BASE+ 0 37 5737 11195 T5BASE+ 0 88 4694 11869 T5BASE+ 0 38 5717 11205 T5BASE+ 0 89 4671 11892 T5BASE+ 0 39 5698 11216 T5BASE+ 0 90 4648 11915 T5BASE+ 0 40 5679 11228 T5BASE+ 0 91 4625 11937 T5BASE+ 0 41 5659 11241 T5BASE+ 0 92 4603 11959 T5BASE+ 0 42 5641 11255 T5BASE+ 0 93 4580 11982 T5BASE+ 0 43 5620 11268 T5BASE+ 0 94 4558 12004 T5BASE+ 0 44 5599 11281 T5BASE+ 0 95 4535 12026 T5BASE+ 0 45 5578 11294 T5BASE+ 0 96 4513 12049 T5BASE+ 0 46 5557 11307 T5BASE+ 0 97 4491 12071 T5BASE+ 0 47 5537 11319 T5BASE+ 0 98 4469 12094 T5BASE+ 0 48 5516 11332 T5BASE+ 0 99 4446 12116 T5BASE+ 0 49 5496 11344 T5BASE+ 0 100 4424 12141 T5BASE+ 0 50 5476 11357 T5BASE+ 0 101 4402 12166 T5BASE+ 0 51 5456 11369 T5BASE+ 0 102 4379 12192 T5BASE+ 0 52 5436 11382 T5BASE+ 0 103 4357 12216 T5BASE+ 0 53 5416 11394 T5BASE+ 0 104 4335 12242 T5BASE+ 0 54 5397 11406 T5BASE+ 0 105 4313 12267 T5BASE+ 0 55 5377 11418 T5BASE+ 0 106 4291 12292 T5BASE+ 0 56 5358 11430 T5BASE+ 0 107 4269 12317 T5BASE+ 0 57 5338 11441 T5BASE+ 0 108 4247 12342 T5BASE+ 0 58 5319 11450 T5BASE+ 0 109 4221 12374 T5BASE+ 0 59 5300 11460 T5BASE+ 0 110 4195 12406 T5BASE+ 0 60 5277 11470 T5BASE+ 0




TAURUS 60-7001 EMERGENCY DUTY, LIQUID FUEL, DRY







TAURUS 60-7001 CONTINUOUS DUTY, NATURAL GAS FUEL, W/F RATIO=0.83(+/-0.1) REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60-7001 EMERGENCY DUTY, NATURAL GAS FUEL, W/F RATIO=0.86(+/-0.1) REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO








TAURUS 60-7001 EMERGENCY DUTY, LIQUID FUEL, W/F RATIO=0.63(+/-0.1) REFERENCE FULL LOAD PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO








ADDENDUM 4 Taurus 60-7301 - ACCEPTANCE TEST REQUIREMENTS CONTENTS Paragraph Page 1.0 SCOPE 80 2.2 DRAWINGS 80 4.3.2 PERFORMANCE EVALUATION 80 TABLES Table Page 1 Performance Requirements (for 7301), 59°F 81 1A Performance Requirements (for 7301), 80°F 82 9 T5 Compensator Selection Chart 83 PT30006 Reference Full Load Performance (7301) Continuous, Dry, Gas 84

PT30007 Reference Full Load Performance (7301) Continuous, Dry, Liquid 85

PT30008 Reference Full Load Performance (7301) Continuous, Wet, Gas 86

PT30009 Reference Full Load Performance (7301) Continuous, Wet, Liquid 87




Solar

MPDC List No. TTD-1 Taurus 60-7301, One-Shaft Engine 197003 Data Chart and Build Instructions 197011 Mechanical Installation 196800 1800 rpm Reduction Drive Gearbox 191100 1500 rpm Reduction Drive Gearbox



PT30006 7301 Continuous Dry Gas

PT30007 7301 Continuous Dry Liquid

PT30008 7301 Continuous Wet Gas

PT30009 7301 Continuous Wet Liquid





Parameter



Turbine Rotor Inlet Temperature TRIT 1885 +/- 10oF









(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is hot thereby preventing 59F corrected performance without exceeding 1985F actual TRIT.(2). Reference performance parameters are not an acceptance criteria. Contact the Performance Engineer for disposition if indicated limits are exceeded.


Continuous Duty






Parameter












(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is hot thereby preventing 59F corrected performance without exceeding 1985F actual TRIT.(2). Reference performance parameters are not an acceptance criteria. Contact the Performance Engineer for disposition if indicated limits are exceeded.

Continuous Duty

99.9 to 100.1%

1885 +/- 10oF

0.6518 to 0.7580

4615 KW4520 KW

11,934 Btu/KW-hr12,060 Btu/KW-hr

2 to 8 deg.

11.5

47.1 pps

904oF



Compensator Selection List for a Continuous Duty Single Shaft EngineChart is Based on a T5 Setpoint of 1250oF and TRIT of 1885oF +/- 10oF

T5/TRIT Ratio Compensator Ref Temperature Change

0.7580 to 0.7537 120902-1 -700.7536 to 0.7495 120902-2 -600.7494 to 0.7452 120902-3 -500.7451 to 0.7410 120902-4 -400.7409 to 0.7367 120902-5 -300.7366 to 0.7325 120902-6 -200.7324 to 0.7282 120902-7 -100.7281 to 0.7240 120902-8 00.7239 to 0.7197 120902-9 +100.7196 to 0.7155 120902-10 +200.7154 to 0.7113 120902-11 +300.7112 to 0.7070 120902-12 +400.7069 to 0.7028 120902-13 +500.7027 to 0.6985 120902-14 +600.6984 to 0.6943 120902-15 +700.6942 to 0.6900 120902-16 +800.6899 to 0.6858 120902-17 +900.6857 to 0.6815 120902-18 +1000.6814 to 0.6773 120902-19 +1100.6772 to 0.6730 120902-20 +1200.6729 to 0.6688 120902-21 +1300.6687 to 0.6645 120902-22 +1400.6644 to 0.6603 120902-23 +1500.6602 to 0.6561 120902-24 +1600.6560 to 0.6518 120902-25 +170

Notes:





Table 9. T5 Compensator Selection Chart for Engine Retrofits to Packages that do not usePLC Software Compensation



TAURUS 60-7301 CONTINUOUS DUTY, NATURAL GAS FUEL, DRY

REFERENCE PERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO ZERO INLET & EXHAUST LOSS WITH 60% RH & P1.0=14.696






TAURUS 60-7301 CONTINUOUS DUTY, NATURAL GAS FUEL, W/F RATIO=0.70(+/-0.1)










T1.0 Minimum Maximum T5.0 T1.0 Minimum Maximum T5.0 10 6072 11536 T5BASE+ 0 61 5081 12173 T5BASE+ 011 6053 11545 T5BASE+ 0 62 5058 12189 T5BASE+ 012 6035 11553 T5BASE+ 0 63 5036 12204 T5BASE+ 013 6017 11562 T5BASE+ 0 64 5014 12220 T5BASE+ 014 6000 11572 T5BASE+ 0 65 4993 12235 T5BASE+ 015 5982 11581 T5BASE+ 0 66 4971 12250 T5BASE+ 016 5966 11591 T5BASE+ 0 67 4950 12265 T5BASE+ 017 5949 11601 T5BASE+ 0 68 4929 12280 T5BASE+ 018 5931 11611 T5BASE+ 0 69 4909 12295 T5BASE+ 019 5913 11622 T5BASE+ 0 70 4888 12310 T5BASE+ 020 5895 11633 T5BASE+ 0 71 4868 12325 T5BASE+ 021 5877 11644 T5BASE+ 0 72 4847 12340 T5BASE+ 022 5859 11655 T5BASE+ 0 73 4828 12355 T5BASE+ 023 5841 11668 T5BASE+ 0 74 4808 12369 T5BASE+ 024 5824 11680 T5BASE+ 0 75 4789 12386 T5BASE+ 025 5806 11693 T5BASE+ 0 76 4769 12403 T5BASE+ 026 5788 11707 T5BASE+ 0 77 4750 12420 T5BASE+ 027 5768 11723 T5BASE+ 0 78 4731 12437 T5BASE+ 028 5749 11739 T5BASE+ 0 79 4711 12454 T5BASE+ 029 5729 11756 T5BASE+ 0 80 4693 12471 T5BASE+ 030 5709 11774 T5BASE+ 0 81 4674 12488 T5BASE+ 031 5689 11793 T5BASE+ 0 82 4655 12505 T5BASE+ 032 5671 11808 T5BASE+ 0 83 4636 12521 T5BASE+ 033 5653 11822 T5BASE+ 0 84 4616 12540 T5BASE+ 034 5635 11836 T5BASE+ 0 85 4593 12563 T5BASE+ 035 5617 11849 T5BASE+ 0 86 4570 12587 T5BASE+ 036 5597 11864 T5BASE+ 0 87 4547 12611 T5BASE+ 037 5577 11878 T5BASE+ 0 88 4523 12635 T5BASE+ 038 5557 11892 T5BASE+ 0 89 4501 12660 T5BASE+ 039 5536 11906 T5BASE+ 0 90 4477 12686 T5BASE+ 040 5515 11920 T5BASE+ 0 91 4454 12713 T5BASE+ 041 5494 11933 T5BASE+ 0 92 4431 12740 T5BASE+ 042 5473 11947 T5BASE+ 0 93 4408 12767 T5BASE+ 043 5451 11960 T5BASE+ 0 94 4384 12794 T5BASE+ 044 5429 11972 T5BASE+ 0 95 4361 12821 T5BASE+ 045 5407 11985 T5BASE+ 0 96 4339 12848 T5BASE+ 046 5385 11999 T5BASE+ 0 97 4316 12875 T5BASE+ 047 5363 12013 T5BASE+ 0 98 4293 12902 T5BASE+ 048 5342 12026 T5BASE+ 0 99 4271 12929 T5BASE+ 049 5321 12039 T5BASE+ 0 100 4248 12956 T5BASE+ 050 5300 12052 T5BASE+ 0 101 4226 12983 T5BASE+ 051 5280 12064 T5BASE+ 0 102 4204 13010 T5BASE+ 052 5260 12076 T5BASE+ 0 103 4181 13037 T5BASE+ 053 5240 12087 T5BASE+ 0 104 4159 13064 T5BASE+ 054 5220 12097 T5BASE+ 0 105 4137 13093 T5BASE+ 055 5201 12108 T5BASE+ 0 106 4116 13122 T5BASE+ 056 5182 12118 T5BASE+ 0 107 4095 13151 T5BASE+ 057 5163 12128 T5BASE+ 0 108 4074 13180 T5BASE+ 058 5144 12137 T5BASE+ 0 109 4052 13213 T5BASE+ 059 5126 12145 T5BASE+ 0 110 4030 13248 T5BASE+ 060 5103 12158 T5BASE+ 0




ADDENDUM 5 TAURUS 60-7801e ACCEPTANCE TEST REQUIREMENTS CONTENTS Paragraph Page 1.0 SCOPE 57 2.2 DRAWINGS 57 4.3.2 PERFORMANCE EVALUATION 57 TABLES Table Page 1 Performance Requirements (7801e), 59°F 58 1A Performance Requirements (7801e), 80°F 60 PT30327 Reference Full Load Performance (7801e) 62 PT30328 Reference Full Load Performance (7801e) 63



1.0 SCOPE This Addendum contains the Acceptance Test Requirements for the Taurus 60-7801e One-Shaft Engine. The provisions of the basic ES 2098 Specification apply to the Taurus 60-7801e engine except as specifically amended in the Addendum. 2.2 DRAWINGS

Solar

MPDC List No. TTF-1 Taurus 60-7801e, One-Shaft Engine 219005 Mechanical Installation 136600 Reduction Drive Gearbox 196800 Reduction Drive Gearbox



PT30327 7801e Continuous Dry Gas

PT30328 7801e Continuous Dry Liquid



Table 1.(1) Performance Acceptance Requirements (-7801Se)



Parameter












(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is hot thereby preventing 59F corrected performance without exceeding 2050F actual TRIT.(2). Reference performance parameters are not an acceptance criteria. Contact Performance Engineering for disposition if indicated limits are exceeded.

Continuous Duty

99.9 to 100.1%

1930 - 1950oF

0.6784 to 0.7822

5335 KW5206 KW


-2 to 8 deg.

11.6

49.6 pps

935oF



Table 1A.(1) Performance Acceptance Requirements (-7801Se)



Parameter












(1). Table 1A should be used in lieu of Table 1 for corrected performance runs when T1 is hot thereby preventing 59F corrected performance without exceeding 2050F actual TRIT.(2). Reference performance parameters are not an acceptance criteria. Contact Performance Engineering for disposition if indicated limits are exceeded.

Continuous Duty

1930 - 1950oF


11.3

47.1 pps

948oF

-2 to 8 deg.

0.6784 to 0.7822

4940 KW4816 KW

99.9 to 100.1%



TAURUS 60-7801e CONTINOUS DUTY, NATURAL GAS FUEL, DRYPERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO







TAURUS 60 - 7801e CONTINUOUS DUTY, LIQUID FUEL, DRYPERFORMANCE AT TEST T1.0 & FUEL, CORRECTED TO





ES2098 Accpet Test Req Rev Ab

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