Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES...

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Transcript of Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES...

Page 1: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas
Page 2: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

1.1. The roles of Vertical FlightThe roles of Vertical Flight2.2. Limitation of the helicopterLimitation of the helicopter3.3. The two solutionsThe two solutions

The advanced helicopterThe advanced helicopterThe TiltrotorThe Tiltrotor

4.4. The Industry GoalsThe Industry Goals5.5. The Advanced TechnologiesThe Advanced Technologies6.6. From technologies to productFrom technologies to product7.7. AGUSTA: the Future has beganAGUSTA: the Future has began

The AB139The AB139The BA609The BA609

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

1.1. The roles of Vertical FlightThe roles of Vertical Flight

Page 4: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

THE ROLES OF VERTICAL FLIGHT

•• HoveringHovering

•• TakeTake--Off and Landing in a restricted Off and Landing in a restricted area, not prepared terrains and with area, not prepared terrains and with obstaclesobstacles

UNIQUE ABILITIES OF THE UNIQUE ABILITIES OF THE HELICOPTERSHELICOPTERS

Page 5: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

THE ROLES OF VERTICAL FLIGHT

Increasing demand :Increasing demand :•• Transport of people and materialsTransport of people and materials

•• Point to point connection (VIP, corporate…)Point to point connection (VIP, corporate…)

•• OffshoreOffshore

•• Short range transportShort range transport

•• Search & RescueSearch & Rescue

•• Military air mobility (Peace keeping)Military air mobility (Peace keeping)

•• SecuritySecurity

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

2. Limitations of the helicopter2. Limitations of the helicopter

Page 7: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

LIMITATIONS OF THE HELICOPTER

•• Low productivityLow productivity

Low speedLow speed

high operating costshigh operating costs

•• Environmental impactEnvironmental impact

NoiseNoise

PollutionPollution

•• Public acceptancePublic acceptance

•• No rules in the ATMNo rules in the ATM

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

3. The two solutions3. The two solutionsThe advanced helicopterThe advanced helicopterThe TiltrotorThe Tiltrotor

Page 9: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

THE TWO SOLUTIONS

PERSPECTIVE OF FUTURE DEVELOPMENTOF VERTICAL FLIGHT

Helicopter Evolution

• Breakthrough Technologies• High productivity• High speed• High versatility

• All Weather• More performing• Quieter• Safer• More comfortable• Low pollution

TILTROTOR

HoveringSpeedRangeCruise

Page 10: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

INDUSTRY GOALS

Lower costsLower costs

Increased Increased performanceperformance PayloadPayload

RangeRange

EnduranceEndurance

Community Community AcceptanceAcceptance

Air Traffic Air Traffic ProceduresProcedures

All weatherAll weather

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

5. The Advanced Technologies5. The Advanced Technologies

Page 12: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

ADVANCED TECHNOLOGY SOLUTIONSADVANCED TECHNOLOGY SOLUTIONS

The technology solutions play an important role to The technology solutions play an important role to achieve the industry goal...achieve the industry goal...

Page 13: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

ADVANCED TECHNOLOGY SOLUTIONS: AERODYNAMICSADVANCED TECHNOLOGY SOLUTIONS: AERODYNAMICS

•• Higher Rotor efficiency (hover/forward flight)Higher Rotor efficiency (hover/forward flight)higher payloadhigher payloadhigher productivityhigher productivity

•• Full Full NavierNavier--Stokes codesStokes codesnoise reductionnoise reductionrotor/fuselage interactionrotor/fuselage interaction

•• Enhancement of the Enhancement of the Wind Tunnel testsWind Tunnel testsactive flow controlactive flow controlactive fiber compositeactive fiber compositestudy of new configurations (T/R)study of new configurations (T/R)

Page 14: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

ADVANCED TECHNOLOGY SOLUTIONS: DYNAMICSADVANCED TECHNOLOGY SOLUTIONS: DYNAMICS

•• Active Rotor Control (flaps, Active Rotor Control (flaps, twist, tip…)twist, tip…)

reduction of rotor/fuselage reduction of rotor/fuselage vibration vibration reduction of noisereduction of noise

•• Enhancement of the Enhancement of the experimental testsexperimental tests

systems systems characterisationcharacterisation•• Vibration Monitoring SystemsVibration Monitoring Systems

rotors, drive shaftsrotors, drive shafts……•• Stability enhancementStability enhancement

Study of new configurations Study of new configurations (T/R)(T/R)

Page 15: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

ADVANCED TECHNOLOGY SOLUTIONS: STRUCTURESADVANCED TECHNOLOGY SOLUTIONS: STRUCTURES

Traditional Metallic StructureTraditional Metallic Structure

Composite SolutionsComposite Solutions

…making compliance with the new stringent requirements:…making compliance with the new stringent requirements:CrashworthinessCrashworthinessBird StrikeBird StrikeEngine disk burst impactEngine disk burst impact

Introduction of the damage toleranceIntroduction of the damage tolerance

Page 16: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

ADVANCED TECHNOLOGY SOLUTIONS: SIMULATIONADVANCED TECHNOLOGY SOLUTIONS: SIMULATION

•• Evaluation and improvement of the Evaluation and improvement of the VTOL handling qualitiesVTOL handling qualities

•• Development of flight simulators with Development of flight simulators with Pilot and hardware in the loopPilot and hardware in the loop

Advanced control lawsAdvanced control laws

Automatic emergency Automatic emergency manoeuvresmanoeuvres

load reductionload reduction

•• Development and validation of the flight Development and validation of the flight mechanics codesmechanics codes

Page 17: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

ADVANCED TECHNOLOGY SOLUTIONS: AVIONICSADVANCED TECHNOLOGY SOLUTIONS: AVIONICS

Helmet Helmet Mounted Mounted DysplayDysplay Direct Voice Direct Voice

InputInputTactile Tactile Control Control

FeedbackFeedback

Side StickSide Stick

Differential Differential GPSGPS Terrain Terrain

Obstacle Obstacle DatabaseDatabase

3D flight path3D flight path

MANMAN--MACHINE INTERFACEMACHINE INTERFACE

ExtendExtendOperational EnvelopeOperational Envelope Reduce PilotReduce Pilot

WorkloadWorkload

Increase PilotIncrease PilotSituation AwarenessSituation Awareness

Page 18: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

6. From Technologies to product6. From Technologies to product

Page 19: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

FROM TECHNOLOGIES TO PRODUCTFROM TECHNOLOGIES TO PRODUCT

Aerodynamics

Dynamics

Strctures

Simulation

Avionics

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Available Available resources resources and and Collaboration Collaboration

NetworkNetwork

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

FROM TECHNOLOGIES TO PRODUCTFROM TECHNOLOGIES TO PRODUCT

MedicalService

VIP

BorderPatrol

Training

NavalOperationScout

LightUtility

LawEnforcement

Search &Rescue

OperatingCosts

SpeedRange

CabinSize

UsefulLoad

IFR

Comfort

Hot &High

The The competitive competitive

performance performance diamonddiamond

An example: An example:

the AGUSTA A109the AGUSTA A109

Page 21: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

FROM TECHNOLOGIES TO PRODUCTFROM TECHNOLOGIES TO PRODUCT

US101

NH90

InternationalResearchProjects

Training &simulation

BA609

AB139

Leading/primary role

TechnologyDrive

Industrialeffectiveness

PartenershipStrategic valuefor home nation

ClearVision &Mission

Marketpresence

EH101

AGUSTA AGUSTA Collaboration Collaboration

NetworkNetwork

Page 22: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

FROM TECHNOLOGIES TO PRODUCTFROM TECHNOLOGIES TO PRODUCT

The European The European Advanced TiltrotorAdvanced Tiltrotor

Page 23: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

7. AGUSTA: the Future has began7. AGUSTA: the Future has began

Page 24: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUNAGUSTA: THE FUTURE HAS BEGUN

Operator “directs” vehicle

Pilot behaviour integrated in the

machinePilot AidingCOCKPIT

INTEGRATION

60% Reduction-3 dB below req.FAA RequirementsEXTERNAL NOISE

No-Restriction to icing

FULL ICING (EH101)

Limited Icing CapabilityALL-WEATHER

350-400 Kts275 KtsTiltrotor = 250 Kts

200 Kts180 KtsHelicopter = 170 KtsCRUISE SPEED

1310L/D x Prop. Eff. = 7 at V cruise

0.870.8Hover = 0.78VEHICLE

EFFICIENCY

2022 TARGETAGUSTA TODAYCURRENT LEVELATTRIBUTE

SUGGESTED LONG RANGE VTOL TECHNOLOGY GOALSSUGGESTED LONG RANGE VTOL TECHNOLOGY GOALSG.Price, “G.Price, “Prospects for Prospects for the future of the the future of the Vertical Vertical Flight”, Flight”,

AIAA/ICAS “The AIAA/ICAS “The Next Next 100 100 YearsYears”, 14”, 14--17 17 July July 2003, 2003, DaytonDayton, Ohio, Ohio

Page 25: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUNAGUSTA: THE FUTURE HAS BEGUN

AB139AB139 BA609BA609

Page 26: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

The AB139The AB139

Page 27: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- AB139AB139

Commercial Helicopter derived from the Military A149Commercial Helicopter derived from the Military A149

ENGINES: P&WC PT6C-67CENGINES CONTROLED BY FADECWEIGHT 6 tonPAYLOAD 2.5 tonSPEED 167 ktsRANGE >400 nm

ENGINES: P&WC PT6C-67CENGINES CONTROLED BY FADECWEIGHT 6 tonPAYLOAD 2.5 tonSPEED 167 ktsRANGE >400 nm

Page 28: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

Primary structure of aluminum alloy and nomex/aluminum panels.

Fiber composite material are used for the secondary structure.

Better fuel tanks Better fuel tanks positionposition

• High space in the cabin• Better lift/drag ratio• Better crashworthiness

characteristic• light weight • Passenger cabin floor low

over the ground for easy loading and unloading

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- AB139AB139

Page 29: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- AB139AB139

Canted:Canted:Shorter mastShorter mast

higher performancehigher performance

Aerodynamically Aerodynamically and dynamically and dynamically

optimisedoptimised

Page 30: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- AB139AB139

Avionics System

Primus EpicTM Avionics System (Honeywell)

Electronic Display SystemElectronic Display SystemNavigation and Engine dataNavigation and Engine dataSystems parametersSystems parametersCaution, warning and advisory Caution, warning and advisory annunciationannunciationWindowsWindows--style Operating Systemstyle Operating SystemVoice Command SystemVoice Command SystemCentral Central MaitenanceMaitenance ComputerComputer

Page 31: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- AB139AB139

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- AB139AB139

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Present H/C

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

SUMMARY

The BA609The BA609

Page 34: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609

CapacitiesCrew 1-2Passengers seats 6-9Baggage comp. Volume 1.42 m3

PropulsionTwo P&W PT6C-67A (1940 Shp each)

Weights & dimensionsMax take off weight 7250 kgEmpty weight 4760 kgUseful load 2500 kgRotor Diameter 7.9 m

PerformanceMax Cruise Speed 275 ktsMax Range 750 nmCruise Altitude 7620 m

Page 35: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609

Offshore Resources Development

Aeroambulance

VIP / CorporateSearch and Rescue

Training

Page 36: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609

• 0 • 50 • 100 • 150 • 200 • 250 • 300 • 350• 0

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• 30,000

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•Al

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• BA609

VcruiseVcruise

275 275 KtsKts

High High cruise cruise

altitudealtitude

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2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609Airplane Position

PCA converts Nacelle position down to 0 degrees for airplane mode operations

Interconnect Drive Train

Helicopter Position

PCA converts Nacelle position up to 95 degrees for helicopter mode operations

Interconnect Drive Train

•• Satisfy severe safety requirementsSatisfy severe safety requirements

•• Double telescoping Double telescoping ballscrewsballscrews

•• Interconnecting shaftInterconnecting shaft

•• Angular displacement transducerAngular displacement transducer

Nacelle tilting mechanismNacelle tilting mechanism

Page 38: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609

Rotor SystemRotor System•• 3 blades3 blades

•• optimal twist for hover optimal twist for hover and cruiseand cruise

•• gimbal jointgimbal joint

•• different different elastomericelastomericcomponentscomponents

•• deicing systemdeicing system

Page 39: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609

Drive SystemDrive System

•• Interconnecting shaftInterconnecting shaft

•• Drive of both rotors in Drive of both rotors in case of engine failurecase of engine failure

•• No asymmetric flight or No asymmetric flight or controlscontrols

Page 40: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

AGUSTA: THE FUTURE HAS BEGUN AGUSTA: THE FUTURE HAS BEGUN -- BA609BA609

Flight Control SystemFlight Control System• Core of the BA609• Fly-by-wire

minimise pilot workloadsatisfy handling qualities req.

• Conversion from H/M to A/M and reverse• Conventional helicopter cockpit controls• Triplex flight control computers

• Control laws fully tested through Pilot-in-the-loop flight simulation techniques.

• Thousands of virtual maneuvers

• 3 dedicated simulators with pilots and harware in the loop

• optimised handling qualities of the aircraft • tested all possible failures and emergency

procedures.

Page 41: Presentazione di PowerPoint - ICAS Congress General Lectures...ENGINES: P&WC PT6C-67C ENGINES CONTROLED BY FADEC WEIGHT 6 ton PAYLOAD 2.5 ton SPEED 167 kts RANGE >400 nm 24 th Icas

2424thth IcasIcas CongressCongress, Yokohama, , Yokohama, JapanJapan.. AugustAugust 2929thth –– September September 33rdrd, 2004, 2004

CONCLUSIONSCONCLUSIONS

In the airspace future, the vertical flight will have a greater importance than today

The goals of the rotorcraft industry are to integrate the technology into business

AGUSTA, with the two last products, the AB139 and the BA609, has begun the future

Finmeccanica, the AGUSTA shareholder, has decided to strengthen the helicopter sector as one of its main core business

Finmeccanica announced the agreement with GKN for the acquisition of the latter's 50% shareholding in AgustaWestland.

Agusta will benefit of greater resources to reinforce its position to stay in the forefront of the vertical flight business of the two guiding avenues of both the conventional helicopter and the revolutionary Tilt-Rotor.