aviation propulsion technologies in the 21st century · 2019. 8. 27. · propulsion •wake...

26
Aviation Propulsion Technologies in the 21 st Century Mike Epstein GE Aviation 07 November, 2013 04 Kislev, 5774

Upload: others

Post on 29-Jan-2021

3 views

Category:

Documents


0 download

TRANSCRIPT

  • Aviation Propulsion Technologies in the 21st Century

    Mike Epstein GE Aviation 07 November, 2013 04 Kislev, 5774

  • 2 GE Aviation

    Our business units

    ~$147.4 Billion Revenue in 2012

    $16.1 B Operating Earnings

    Capital

    31% / $46.0 B

    Home & Business Solutions

    5% / $8.0 B

    Healthcare

    12% / $18.3 B

    Aviation

    14% / $20.0 B

    Transportation

    4% / $5.6 B

    Energy Management

    5% / $7.4 B

    Oil & Gas

    10% / $15.2 B

    Power & Water

    19% / $28.3 B

  • 3 GE Aviation

    “Longitude”… Author - Dava Sobel

    • Engineering crisis of the 18th century.

    • Longitude committee formed, prize defined by parliament.

    • John Harrison – by 1735 solves with an accurate ship-worthy clock.

    • Not really in widespread use until roughly 1780 or later.

    • Why?

  • 4

    GE Aviation

    Propulsion Challenge

    Challenges for Future Commercial Aircraft Propulsion GE Perspective 4

    Reduce commercial and military customer costs in an increasingly difficult environment

    Airline Operating Costs

    Regulatory Challenges

    CAEP/6 2008 / 2013

    CAEP/8 2014 / 2018

    EU Carbon Trading 2012

    ICAO CO2 Standard 2016-2020

    FAR Stage 5 2020

    Historical Fuel Prices

    Industry Revenue/Profits

    28%

    23% 18%

    14%

    7%

    6% 4% Fuel

    Labor

    Other Operating

    Trasnport-Related

    Professional Services

    Aircraft rents/ownership

    Non-aircraft rents/ownership

    Source: A4A Quarterly Cost Index, US Airlines

    (50.0)

    -

    50.0

    100.0

    150.0

    200.0

    250.0

    1975 1980 1985 1990 1995 2000 2005 2010

    $B

    Revenues

    Profits

    Sources: Air Transport Association/Bureau of Transportation Statistics

    Sources: Air Transport Association, International Air Transport Association

    US

    D/U

    SG

    -

    1.00

    2.00

    3.00

    4.00

    5.00

    1977 1981 1986 1990 1994 1999 2003 2008 2012

    >15% Growth Rate

  • 5

    GE Aviation

    Technologies and Architectures

  • 6

    GE Aviation

    0%

    10%

    20%

    30%

    40%

    50%

    60%

    70%

    80%

    90%

    100%

    1 2 3

    Booster

    Gooseneck

    HPC

    Cmb

    HPT

    Trans Duct

    LPT(th)

    LPT(tr)

    Fan

    Fan Duct

    Fan Nozzle

    Rear Frame

    Core Nozzle

    Fan Jet

    Core Jet

    Thermal

    Transfer

    Propulsive

    Loss

    Available

    Energy Availability For Every Unit of Fuel Chemical Energy…

    Unavailable (Losses)

    Available to

    Vehicle

    Thermal

    Transfer

    Propulsive

    Constant Pressure Combustor

    Fan Jet

    Compressor

    Booster

    HPT

    LPT

    Transition Duct

    Fan Fan Duct

    Core Jet

    Today’s Turbofan Is roughly 40%

    efficient

  • 7

    GE Aviation

    0%

    10%

    20%

    30%

    40%

    50%

    60%

    70%

    80%

    90%

    100%

    1 2 3

    Booster

    Gooseneck

    HPC

    Cmb

    HPT

    Trans Duct

    LPT(th)

    LPT(tr)

    Fan

    Fan Duct

    Fan Nozzle

    Rear Frame

    Core Nozzle

    Fan Jet

    Core Jet

    Thermal

    Transfer

    Propulsive

    Loss

    Available

    Energy Availability converted into transfer efficiencies…

    Unavailable (Losses)

    Available to

    Vehicle

    Thermal

    Transfer

    Propulsive

    Constant Pressure Combustor

    Fan Jet

    Compressor

    Booster

    HPT

    LPT

    Transition Duct

    Fan Fan Duct

    Core Jet

    60% loss can be categorized as: Thermal eff: Thermodynamic loss due to the Brayton Cycle

    Transfer efficiency: Loss converting energy from the core to the bypass Propulsive efficiency: Loss of converting fan and core exhaust into useable thrust

  • 8

    GE Aviation

    8

    GE Aviation

    𝑹𝒂𝒏𝒈𝒆 =𝑽𝟎

    𝑺𝑭𝑪∗

    𝑳

    𝑫∗ 𝐥𝐧

    𝑾𝒊𝒏𝒊𝒕𝒊𝒂𝒍𝑾𝒇𝒊𝒏𝒂𝒍

    = 𝑭𝑯𝑽 ∗ 𝞰𝒕𝒉𝒆𝒓𝒎𝒂𝒍 ∗ 𝞰𝒕𝒓𝒂𝒏𝒔𝒇𝒆𝒓 ∗ 𝞰𝒑𝒓𝒐𝒑𝒖𝒍𝒔𝒊𝒗𝒆 ∗𝑳

    𝑫∗ 𝐥𝐧 𝟏 +

    𝑾𝒇𝒖𝒆𝒍𝑾𝒑𝒂𝒚𝒍𝒐𝒂𝒅 + 𝑾𝒆𝒎𝒑𝒕𝒚

    • Highly Loaded Compressors

    • High OPR Low Emissions Combustors

    • Novel Alloys

    • Non-metallics

    • Low Loss Inlets

    • Variable Low Loss Exhausts

    • Very High BPR Turbofans

    • Constant Volume Combustion

    • Hybrid Electric Propulsion

    • Adaptive cycles • Distributed

    Power Transmission

    • Ultra High BPR Turbofans

    • Open Rotors

    • Distributed Propulsion

    • Wake Ingestion

    • Advanced Engine Architectures

    Opportunities for the future…

  • 9

    GE Aviation

    0.3

    0.35

    0.4

    0.45

    0.5

    0.55

    0.6

    0.65

    0.7

    0.75

    0.8

    0 10 20 30 40 50 60 70

    Overall Pressure Ratio (OPR)

    Th

    erm

    al

    Eff

    icie

    nc

    y

    T41=1500F

    T41=2000F

    T41=2500F

    T41=3000F

    T41=3500F

    Ericcson T41=1500F

    39k/0.8 (Mid-Cruise)

    Large Thermal Opportunity Beyond Conventional Brayton Cycle

    Topping, Bottoming Cycles

    Thermal Efficiency

  • 10

    GE Aviation

    • unsteady shock wave + combustion zone • pressure rise combustion • more efficient conversion of energy in fuel Shock

    Wave Combustion

    Zone

    Compression and Power Stroke

    Tube PDE

    1 Fuel fill

    2 Initiation

    3 Detonation

    4 Blowdown

    5 Purge Air

    Intake Stroke

    Exhaust Stroke

    IC Engine Analogy

    PDE Technology

  • 11

    GE Aviation

    Propulsive Efficiency

    Drive to lower SFC’s and more integrated engine /

    aircraft designs

    0.70

    0.75

    0.80

    0.85

    0.90

    0.95

    1.00

    1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0

    Fan Pressure Ratio

    Pro

    pu

    lsiv

    e E

    ffic

    ien

    cy

    LEAP56/LEAPX

    CFM56

    Open Rotor

    39k/0.8M Cruise

    Turbofan (Slimline)

    KDM3 /GE /

    July 21, 2009

    Distributed Propulsors

  • 12 GE Aviation

    Open rotor tests with NASA

    GE/NASA testing began in 2009

    Test builds on 1985 demonstration

    • Acoustics validation

    • Aero model validation

    • New blade concepts

    • Installation effects

    • Pitch change effects

    • Pylon, sidewall interaction

  • 13 GE Aviation

    Driving productivity through analytics

    IVHM Integrated Vehicle Health Management

    • Advanced prognostics & enterprise integration

    Over 25,000–b) engines monitored … and growing

    • Fuel efficiency

    • Asset utilization

    • Operations efficiency

    Digital workscope Fuel & carbon

    • Flight operations data analysis

    • Operations insights for fuel savings

    Improving productivity of assets

    Improving utilization of airplanes

    Improving service of our engines

    1% fuel burn reduction–a) = $10MM savings

    1 hour increase in aircraft utilization per day

    = $100MM+ annual benefit–c)

    5% annual productivity = $50MM cost savings

    per year

    • Optimize time on-wing

    (a- Assumes a typical 70 aircraft, $1B fuel bill, fuel cost is $3.25 per gallon

    (b- Includes CFM, GE & EA engines

    (c- Assumes fleet > 50 aircraft

  • 14 GE Aviation 10/31/2013

    Illustration of particulate matter concentration (Source: NASA)

    Global challenges Temperature, dust, pollution, gravel, sand, construction debris

    Levels of Dust World Wide

  • 15 GE Aviation

    Technology integration thru 2020 Keeping the pipeline filled

    Integrated engine and aircraft systems

    Adaptive cycles

    Advanced architectures

    2010 2020 Advanced turbofan

    Technology

    Architecture

    Composites Lean

    Combustion Adv. Cooling High-Temp Materials

    Flight Mgmt

    Integrated propulsion Integrated power generation

    Core efficiency New designs

    CMCs

  • 16

    GE Aviation

    UDF

    ADVENT

    HEETE

    AATE

    QCSEE

    E3

    80s

    00s

    70s

    90s

    TECH56

    FATE

    OPEN ROTOR

    10s

    Technology demonstrator programs

    Renewing our technology DNA for new products and upgrades of fielded

    products. Mostly USG funded, what comes next?

    AETD

  • 17

    GE Aviation

    Adaptive Engine Technology Development

    • AETD…new class of engines with up to 25% better fuel efficiency

    • Variable cycle technology

    • Technology demonstration that

    builds on ADVENT

    • Foundation for future generation

    of combat propulsion

  • 18

    GE Aviation

    New Products and Services

  • GEnx build-up, acceptance & flight test…

    September 2011

    19

  • 20 GE Aviation

    Test types

    • Performance

    • Ingestion – water, hail, ice, dust, birds

    • Acoustic

    • Fan blade-out

    • Emissions

    • Vibration

    • Endurance

    • Flight

    Make parts Run

    Development Tests

    Certify

    New Product Introduction (NPI) Taking our products from design to manufacturing

  • 21 GE Aviation

    Turbine Airfoils Rotating Parts

    Additive Manuf.

    Automation

    Composites Special Products

    Castings

    Structures

    Process development

    Demo production

    Full scale production

    Explore, develop and industrialize Advanced Manufacturing Technologies and transition to Supply Chain.

    Industrialization for cost, quality

    & delivery

    New Product Introduction (NPI) Lean labs

  • 22

    GE Aviation

    New military and commercial pipeline…

    • F414 Gripen

    • F414 INS6

    • CT7, T700 derivatives

    • LEAP

    • GE9X

    • GE38

  • 23

    GE Aviation

    Alternative Fuels

  • 24

    GE Aviation

    Aviation

    Alternative Fuels…

    • Drop in

    • Near Drop-in

    • Non Drop-in

  • 25 GE Aviation

    Imagination at workg

    C1 C3-C4 C6-C10 C12 C16 C20-40 C80 C100++

    Huge

    reserves

    Limited

    volumes

    Oil or equivalent based distillates – narrow

    price range

    Heavy ends. Freeze

    pt and emissions

    Conversion

    costs

    C1

    Wholesale price per Jet-A gallon equivalent $

  • 26

    GE Aviation

    26

    GE Aviation

    Summary Traditional fuel burn reduction strategies are beginning

    to yield diminishing returns – innovative technologies

    are required

    • Light weight, high propulsive efficiency

    • Advanced materials

    • Highly integrated

    • Big data, prognostics, IVHM

    • Non-Brayton cycles

    New products are the lifeblood of the business

    • Roadmaps near term to 2050+

    • Maintenance concept selection can have multi billion

    dollar impact to the bottom line.

    Aviation alternative fuels may play a significant role in

    our energy future

    787

    737 MAX*

    A320neo*

    C919*

    Honda Jet

    777X

    Global 7000

    *CFM engines 26 GE Aviation 10/31/2013