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Helicopter Engine Technology for the 21 st Century Mike Epstein GE Military Propulsion Engineering October 7, 2010 9 th Symposium On Jet Engines and Gas Turbines Technion, Haifa

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Helicopter Engine Technology

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    Helicopter Engine Technology for the21st Century

    Mike Epstein

    GE Military PropulsionEngineering

    October 7, 2010

    9th Symposium On Jet Enginesand Gas Turbines

    Technion, Haifa

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    2

    GE Aviation

    GE Businesses a

    nd Portfolio

    EnergyInfrastructure

    TechnologyInfrastructure

    NBC UniversalConsumer &

    Industrial

    $37B $43B $10B$15B

    CommercialCommercial

    Services SystemsBusiness &

    General AviationMilitary engines

    & Services

    $4.1B $7.1B $4.2B $2.9B $0.4B

    Capital

    $51B

    F110 T700F136 GE38 T64F414

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    3

    GE Aviation

    GE Helicopter Engine ExperienceU.S. Military

    International Military

    Commercial/Civil CH-53K

    S-92

    T64

    GE38

    CT58/T58

    CT7/T700

    50 Years/80+ Million Hours Of Experience

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    4

    GE Aviation

    Military rotorcraft environment: hot, high

    and harsh.

    Search and rescueCargo lift Attack

    SupplySpecial Ops

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    5

    GE Aviation

    Helicopters and engines operating in desert are subjected to

    extreme sand environments

    CH-53E Landing in Desert

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    6

    GE Aviation

    T64 Compressor Following Service In

    Desert:

    Airfoil Erosion.Degraded power and stall margin.

    Engine removals after only 100

    hours.

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    7

    GE Aviation

    Voice of the CustomerTechnology Needs

    Sand tolerant compressors and

    turbines for desert operations

    Higher power and higher power to

    weight ratios to conduct missions

    in high / hot environment

    Reduced fuel burn Extend mission payload/ range.

    Minimize fuel logistics footprint.

    Reduce fuel costs.

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    8

    GE Aviation

    Compressors with robust

    geometry, materials and erosioncoatings

    Sand tolerant hot sections Environmentally tolerant coatings Clean cooling air circuits designed with

    CFD

    Improved inlet particleseparators

    Sand tolerant coatings and engine

    architecture Blisk with TiN Coating

    CFD Modeling of inlet particleseparator

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    9GE Aviation

    Erosion Coating Technology proven on T64 Engine

    Extended Time on Wing 2-3X

    coatednon-coated

    T64 Rainbow Compressor Sand Ingestion Test at Kirtland AFB

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    10GE Aviation

    Physical Ng limit

    Corrected speed limit

    Fuel flow limit

    Temperature limit

    Sea Level6000 feet

    12,000 feet

    OAT

    SHP

    Engine Lapse Rate and Limiters

    Engine SHP limiters limited by

    Corrected speed materials/ design

    Fuel flow efficiency/ system design

    Turbine Temperature materials / design

    Compressor Physical speed materials / design

    Typical engine power lapse rate

    Materials anddesign

    technologyadvances allowthese limits tobe raised.

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    11GE Aviation

    Technologies for increased power and

    improved fuel burnHigher efficiency thermodynamiccycles

    Improved compressor and turbine efficienciesfrom CFD

    Reduced cooling flows

    Higher Pressure ratios

    Higher Turbine Temperatures

    Improved Materials / Processes/Designs Ceramic Matrix Composite turbine components Advanced blade cooling designs

    Technology Reducing Operating Costs

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    12GE Aviation

    Innovations for tomorrow . . .Leaving no stone unturned

    Fuel burn technologies . . .Aero, loading, component efficiency, weight

    Advances in materials . . .Metallurgy, composites, ceramics

    Nanotechnology . . .Unique strength, weight, fatigue properties

    Alternative Fuels . . .Ensuring broad operational capability

    Novel titaniumalloys

    Ceramic-matrix

    composites

    Nano layers

    Highly loadedcomponents

    2015+

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    13GE Aviation

    Ceramic Matrix Composites (CMCs)Less weight and better performance with reduced cooling

    Introducing compositesbeyond fan modules.

    Benefits for highertemperature components:Turbine airfoils

    Combustors.

    1/3 density of metal forreduced weight

    better fuel burn

    CMC prototype turbine nozzle

    GE Ceramic Composite Products Site. State

    of Delaware, U.S.

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    14GE Aviation

    SFC and Power/Weight ImprovementTechnology continues to improve fuel efficiency andpower to weight ratio of turboshaft engines.

    T55-714A

    GE38-1B FATE Goal

    AE1107C

    PW150A

    State-of-the-artproducttechnology

    Developingtechnology

    T55-714A

    GE38-1B FATE Goal

    AE1107C

    PW150A

    State-of-the-artproducttechnology

    Developingtechnology

    SFC versus Power to Weight

    Power to Weight Ratio

    SFC

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    15GE Aviation

    Helicopter payload and range benefitImpact of Advanced technology

    Mission Radius

    Pa

    yload

    Mission Radius

    P

    ayload

    Helicopter with

    Legacy Engine

    Technology

    Helicopter

    retrofit with

    Advanced

    Technology

    Engine

    Improved SFCchanges slope

    Improved Power increases

    TOGW capability

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    16GE Aviation

    Continuous Technology Infusion has doubled thepower of the T700/ CT7 family

    CT7-8C3,000 SHP

    401701700

    CT7-2A~1500 SHP

    701D2,000 SHP

    2X Power

    CT7-82,600 SHP

    FADEC

    3D Aero Compressor

    Hot Section DurabilityImprovements

    Hot Section

    Hot Section 3-Stg PT

    401C701C

    1,900 SHP

    ITEP

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    17GE Aviation

    GE38-1B Applying the Technology

    7500 SHP Class - Builds on T700 architecture

    GE38 Versus T64 :

    18% Improved SFC

    57% More power

    63% Fewer Parts

    Engine mounted FADEC with

    Prognostics & HealthManagement (PHM)

    Sand tolerant andCorrosion ResistantMaterials

    Top mounted accessories

    Rugged Compressor witherosion coating

    Modern turbineaerodynamics,materials and cooling

    schemes

    Simple, robust, long-life configuration

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    18GE Aviation

    GE38 Video

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    19GE Aviation

    Advanced technology programs.

    AATEAdvanced Affordable Turbine Engine (US Army)

    Program goal 25% specificfuel consumption; maintain T700weight; 65% power; and 35%acquisition and operational &

    support.Detailed design reviewcompleted May 09 programsruns through Jan 12.

    Engine Upgrade for Black Hawkand Apaches & Future Aircraft

    Advanced cooling. Advanced Aero. IPS.

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    20GE Aviation

    Advanced technology programs.

    ADVENTAdaptive Versatile Engine Technology (USAF)

    Phase I: Detailed design of fan rig,

    core and engine technology

    demonstrators (9/09)

    Phase II: Procure, assemble andtest fan rig and core engine. Full

    engine demonstrator in planning.

    Contract runs through 9/2013.

    Position for Next Gen Air Vehicles.

    Advanced cycle. CMCs. Advanced cooling.

    Advanced Aero.

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    21GE Aviation

    Development programs

    F136Joint Strike Fighter

    Up to 5,000 aircraft potential.

    Demonstrated successful engineoperation and obtained criticalvalidation data.

    Test focus in 2010 6 engines,

    approximately 1,000 hours. Currenttesting aligned to support CTOLfirst flight in 2011.

    CMCs Advanced cooling. Advanced Aero. Controls

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    22GE Aviation

    Alternative FuelsEconomic, Strategic, Environmental

    Source: The Oil Drum. Sam Foucher blog.

    GOM oil spillmore regulation,slower growth, more costly oil.

    Oil spot market pricescalm fornow.

    - Last 18 months, flat and expensive.

    - Tied to economic outlook.

    Biofuelsmilitary and commercial

    approval moving towards completion.

    Biofuelsviable YESscalable?

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    23GE Aviation

    Summary

    GE driving technology tomeet customer needs

    GE is developing andleveraging technologiesto greatly improve

    rotorcraft missioncapability High Hot operation

    Harsh Environments

    GE Technology reducescost of ownership

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