DETECTION & RECTIFICATION OF TURBINE … 2013 Presentations/Day-2 at PMI...DETECTION & RECTIFICATION...

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DETECTION & RECTIFICATION OF TURBINE BALANCE DRUM LABYRINTH SEAL FAILURE OF TDBFP: A CASE STUDY Presented by Ujjwal Sarkar,Supdt(O&M/TMD) Sanatan Pal, Supdt(O&M/TMD) Bablu Das, Dy. Supdt(O&M/TMD) Mrinmoy Poddar,Sr. Supdt(O&M/TMD)

Transcript of DETECTION & RECTIFICATION OF TURBINE … 2013 Presentations/Day-2 at PMI...DETECTION & RECTIFICATION...

Page 1: DETECTION & RECTIFICATION OF TURBINE … 2013 Presentations/Day-2 at PMI...DETECTION & RECTIFICATION OF TURBINE BALANCE DRUM LABYRINTH ... turbine Moisture content of lube oil found

DETECTION & RECTIFICATION OF TURBINE BALANCE DRUM LABYRINTH SEAL FAILURE

OF TDBFP: A CASE STUDY

P r e s e n t e d b y

U j j w a l S a r k a r , S u p d t ( O & M / T M D ) S a n a t a n P a l , S u p d t ( O & M / T M D )

B a b l u D a s , D y . S u p d t ( O & M / T M D ) M r i n m o y P o d d a r , S r . S u p d t ( O & M / T M D )

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INTRODUCTION

TURBINE BFP BOOSTER

PUMP

GEAR BOX

STEAM INLET

EXHAUST STEAM

FW OUTLET

FW INTLET

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BALANCE DRUM FUNCTION

Thrust

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METHODOLOGY FOR FIND OUT ROOT CAUSE

• Thrust bearing temperature increases with increase in

load & decreases with decrease in load

• Seal steam consumption less i.e. seal steam controller

open less

• Chances of gland seal steam leakage

• Moisture content of lube oil found higher value

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CASE STUDY OF UNIT # 5 TDBFP

TDBFP # 5B was maintaining higher (92°C - 95°C)

than the normal operating value (55° to 60°C) from

January, 2012

TDBFP # 5A was maintaining higher thrust bearing

temperature (90°C - 94°C) from Febabury, 2012

Thrust bearing temperature used to increase with

the increase of load

The unit load was kept below 450 MW, due to high

thrust bearing temperature

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OBSERVATIONS

The thrust bearing temperature increased gradually for

both the turbine

For a particular operating point of pump, Steam

consumption & turbine speed was required to maintain

high

Gland steam leakage observed form both end of the

turbine

Moisture content of lube oil found higher value

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OBSERVATIONS

By throttling gland seal inlet valve manually, there is

no significant change in gland steam leakage

Re-circulation valve of both the TDBFP were found

passing

Internal Noise level of Booster Pump found higher

than the normal

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CORRELATION OF DATA

• High thrust bearing

temperature might be a

reason for failure of

thrust bearing and/ or

high thrust load acting on

the thrust bearing

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CORRELATION OF DATA

• high moisture

content in lube oil

and leakages from

the glands of the

turbine indicates the

failure of gland seals

and/ or balance drum

labyrinth seal failure

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CORRELATION OF DATA

• High steam consumption in both the TDBFP turbines was

mainly to compensate the passing of the re-circulation

valves of both the pumps

• scoring marks on the Thrust pad of Bearing on Booster

Pump Side due to high axial thrust on the bearing on

failure of balance drum

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CORRELATION OF DATA

• High internal noise due to short circuiting of feed water in Booster

Pump

• Thrust bearing temperature directly depends on thrust load on the

bearing. In this case it was observed that the thrust bearing

temperature of the turbine increases with increase in turbine load,

which clearly indicates that the balance drum was not functioning

properly.

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FINDINGS & ANALYSIS DURING OVERHAULING OF TURBINE

i. Rotor axial position found to be shifted towards main pump by 0.7

mm from the center position.

ii. Labyrinth fins of the turbine balance drum were found totally

damaged

iii. Deformation of Balance Drum Labyrinth Seal Segment (Elliptical

Shape with difference in diameter, on left-right to top-bottom, by

2.53 mm) of TDBFP #5B

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FINDINGS & ANALYSIS DURING OVERHAULING OF TURBINE

• Labyrinth fins of both the glands of turbine were found partially

damaged

• Inter-stage labyrinth clearance was within the limit

• Heavy scoring marks on Thrust Bearing Pad (on Booster Pump Side)

found and thrust float increased from design clearance (0.175 –

0.275 mm) to 0.520 mm.

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FINDINGS & ANALYSIS DURING OVERHAULING OF TURBINE

• Booster Pump was dismantled and found that Clearance between

Casing Wear ring & Impeller Wear ring increased beyond acceptable

limit

• Recirculation Valve Seat & Plug were found severely damaged

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REMEDIAL ACTION

All the fins of both side Gland Labyrinth Seal were replaced with

new fins

Thrust Bearing Pads were replaced with new pads and thrust float

was set to the designed value.

All the damaged Fins were removed from the Segments for balance

drum

Re-fining with new fins was carried out with special tools by

engaging specialized manpower

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REMEDIAL ACTION

Both half of the Seal Segment was fixed together

and the deformation was removed with Special

Mechanical Fixture

Machining of the fins was carried out at

Departmental Workshop with special Tools by

engaging Specialized Machinist

After placement of the Seal Segment in the

Casing, uniform clearance with Balance Drum

was ensured

Turbine was boxed up by ensuring all the

required dimensions to the design value

Balance Drum Seal & Gland Seal after replacement of Fins

Balance Drum with Seal During box up

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OBSERVATION AFTER OVERHAULING

No abnormality were observed for both pumps

All the bearing temperatures were within limit

Turbine speed found nearer to the design value

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CONCLUSIONS

i. Online continuous monitoring & analysis of turbo-visory

parameters as well as all operating parameters such as bearing

temperatures, vibration, axial shift, gland steam pressure, gland

steam control valve position, steam consumption etc are the vital

parameters for detecting balance drum failure

ii. Periodic overhauling of Drive Turbine should be followed as per

manufacturer’s recommendation

iii. It is suggested to replace the entire fins of these components

during each periodic overhauling

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THANK YOU