SlideShare a Scribd company logo
Global Aircraft Engine Manufacturing Innovation & Development
Dr. Hooman Rezaei
IAEA President & CEO
China Aerospace Propulsion Technology Summit, May 28-29, Chengdu, China
@IAEA1, : International Aircraft Engine Association
www.aeroenginecloud.com
IAEA Hit 9000 Member Milestone
The only e-commerce cloud is launched integrating A-Z of the industry
Global individual and corporate membership directory/listing
Live aircraft engine listing for sale/lease/demand
Live aircraft engine part & component listing for sale/lease/demand
Market pricing set for engine & parts by asking price & auction
News, events, courses, job opportunities, resume, consulting resources
International Aircraft Engine Institute was just born in Newport Beach, CA
Non-profit academic arm of International Aircraft Engine Association
Launched by offering 5 day executive programs globally in:
Design, Manufacturing, Maintenance & Operation, Lease & Finance
Collaborating with several institutions to offer in several regions
2 www.aeroenginecloud.com
Commercial Engine Industry Overview
Ascend December 31, 2013
3
WORLD: ALL COMMERCIAL AIRCRAFT TYPE
Manufacturer Aircraft Engines Share
CFMI 8,646 17,656 39%
GE Aviation 4,562 9,929 22%
Rolls Royce 2,640 5,811 13%
IAE 2,355 4,710 11%
Pratt & Whitney 2,076 4,710 11%
Other 581 2,020 5%
Total 20,860 44,836
* Active commercial aircraft in operation with airlines
www.aeroenginecloud.com
CFMI is the world market leader
Commercial Engine Industry Overview
Ascend December 31, 2013
4
ASIA PACIFIC: ALL COMMERCIAL AIRCRAFT TYPES
Manufacturer Aircraft Engines Share
CFMI 2,646 5,374 46%
IAE 910 1,820 16%
GE Aviation 821 1,888 16%
Rolls Royce 649 1,482 13%
Pratt & Whitney 398 998 9%
Other 46 168 1%
Total 5,470 11,730
* Active commercial aircraft in operation with airlines
www.aeroenginecloud.com
CFMI is the market leader in Asia Pacific
Commercial Engine Industry Overview
Ascend December 31, 2012
5
Engine Manufacturer Ranking – Boeing/Airbus Types
2012 Deliveries Backlog
Manufacturer Engines Share Engine Share
CFMI 1,278 53% 8,742 47%
IAE 422 17% 1,568 8%
GE Aviation 388 16% 1,812 10%
Rolls Royce 238 10% 2,214 12%
Engine Alliance 56 2% 356 2%
Pratt & Whitney 34 1% 1,228 7%
Undecided - - 2,560 14%
Total 2,416 18,480
www.aeroenginecloud.com
CFMI is leading the new engine order
Engine Architecture
Gearbox on LEAP’s Architecture?Open Rotor?
6 www.aeroenginecloud.com
Reduction Gear Architecture
7
2 Shaft Engine with 25-45 Klbf
BPR 15:1
Gear Ration ~ 4:1
Carbon Fiber Variable Pitch Fan Blades
TSFC -15% vs. todays GTF
RR Announced Ultrafan with Geared Architecture
www.aeroenginecloud.com
Open Rotor Architecture
8
Challenges: Noise and Safety
GE36 engine, which was shown to cut fuel burn by around 30% compared with turbofans. The GE36
featured a turbojet core driving dual counter-rotating eight-blade propfans in a pusher configuration. The
engine was tested on a Boeing 727 (one engine) and a Boeing MD-90 (both engines).
www.aeroenginecloud.com
Open Rotor Architecture
9
Airbus, Snecma Tackle Open-Rotor Integration 2030+
Europe's Clean Sky program
Chapter 14 noise limits
Flight demonstrator on 340-300 end of this year
2030-timeframe narrow body
Snecma alternatives:
CR turbofan with -16% SFC & -20 dB than Leap-1
CROR with -26% SFC & -10 dB than Leap-1
Tested three generations of blade sets
HERA1, 3 and 5
Achieved -5.2 EPNdB (Effective Perceived Noise) reduction
1.1% efficiency increase between the HERA1 and 3 blade
sets, both for the original direct-drive CROR design.
Additional 2.7-EPNdB noise reduction and 0.5% efficiency
improvement with the HERA5 blade set, the first for the
geared CROR
www.aeroenginecloud.com
Light Aircraft (Air Taxi) – Eclipse vs. Honda
10
PW610F
Eclipse 550
HF120
Honda Jet
The 600-3000 lbf Market
www.aeroenginecloud.com
GE Passport: Fan Blisk & CMC Application
11
• Low vibration due to fan titanium blisk
with friction welded blade
• CMC material usage for harsh
environment parts such as the mixer
and center body assemblies. In total it
uses 15 CMC parts for a weight savings
of more than 40 pounds per engine
• Ox-Ox CMC material used on three
parts: exhaust mixer, center body and
core cowls.
• Normal HPC airfoils @ 20-micron finish,
appear smooth to the eye, Passport’s
HPC @ 4-5 micron range surface
roughness smaller than normal laminar
boundary layer, smooth to the air
Bombardier Global 7000 & 8000 Large-cabin Business Jets
www.aeroenginecloud.com
Significant Rise in Additive Manufacturing
12 www.aeroenginecloud.com
Lighter, Rapid, Cheaper Manufacturing & Prototyping
GE Passport: Integrated Propulsion System
13
• Low drag front end with single-piece air
inlet
• Fan cowl which is structurally integrated
to the engine
• Translating O-duct thrust reverser that
provides improved fan flowpath while
eliminating door links
• Lower bifurcation, latches and split lines
• New integrated mounting system for
reduced engine distortion and
enhanced on-wing performance.
• Nexcelle to introduce IPS on LEAP-X1C
& C919
www.aeroenginecloud.com
Marching Towards More Integrated Design & Manufacturing
THANK YOU!
QUESTIONS?
IAEA on @IAEA1, International Aircraft Engine Association
14 www.aeroenginecloud.com

More Related Content

What's hot

Linear Air Case Study Presentation
Linear Air Case Study PresentationLinear Air Case Study Presentation
Linear Air Case Study Presentation
Cherry Malhotra
 
Audi TFSI 2.0
Audi TFSI 2.0Audi TFSI 2.0
Audi TFSI 2.0
Spectralus
 
Hyundai Motor Holds World Premiere of All-new Elantra in Korea
Hyundai Motor Holds World Premiere of All-new Elantra in KoreaHyundai Motor Holds World Premiere of All-new Elantra in Korea
Hyundai Motor Holds World Premiere of All-new Elantra in Korea
steeringnews
 
Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...
Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...
Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...
Leonardo ENERGY
 
Hi tech-air-power-pvt-ltd
Hi tech-air-power-pvt-ltdHi tech-air-power-pvt-ltd
Hi tech-air-power-pvt-ltd
Hi- Tech Air Power Pvt. Ltd.
 
Design and Fabrication of Blended Wing Body
Design and Fabrication of Blended Wing BodyDesign and Fabrication of Blended Wing Body
Design and Fabrication of Blended Wing Body
vivatechijri
 

What's hot (6)

Linear Air Case Study Presentation
Linear Air Case Study PresentationLinear Air Case Study Presentation
Linear Air Case Study Presentation
 
Audi TFSI 2.0
Audi TFSI 2.0Audi TFSI 2.0
Audi TFSI 2.0
 
Hyundai Motor Holds World Premiere of All-new Elantra in Korea
Hyundai Motor Holds World Premiere of All-new Elantra in KoreaHyundai Motor Holds World Premiere of All-new Elantra in Korea
Hyundai Motor Holds World Premiere of All-new Elantra in Korea
 
Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...
Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...
Efficient motor systems for a Net Zero world, by Conrad U. Brunner - Impact E...
 
Hi tech-air-power-pvt-ltd
Hi tech-air-power-pvt-ltdHi tech-air-power-pvt-ltd
Hi tech-air-power-pvt-ltd
 
Design and Fabrication of Blended Wing Body
Design and Fabrication of Blended Wing BodyDesign and Fabrication of Blended Wing Body
Design and Fabrication of Blended Wing Body
 

Viewers also liked

10G Ethernet Overview & Use Cases
10G Ethernet Overview & Use Cases10G Ethernet Overview & Use Cases
10G Ethernet Overview & Use Cases
IBM System Networking
 
Research in Composites for Aero Engine Applications
Research in Composites for Aero Engine ApplicationsResearch in Composites for Aero Engine Applications
Research in Composites for Aero Engine Applicationssicchiuricciu
 
A brief history of jet (gas turbine) engines
A brief history of jet (gas turbine) engines A brief history of jet (gas turbine) engines
A brief history of jet (gas turbine) engines
Zafar Jami
 
GE SPS ID Fan Erection Sequence
GE SPS ID Fan Erection SequenceGE SPS ID Fan Erection Sequence
GE SPS ID Fan Erection SequenceSuvendu Samal
 
Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1
Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1
Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1Ali Sohi
 
GE Inspection: Industrial Process Control with Computed Tomography (CT)
GE Inspection: Industrial Process Control with Computed Tomography (CT)GE Inspection: Industrial Process Control with Computed Tomography (CT)
GE Inspection: Industrial Process Control with Computed Tomography (CT)
GE Sensing & Inspection Technologies GmbH
 
History of aircraft_materials_r2010
History of aircraft_materials_r2010History of aircraft_materials_r2010
History of aircraft_materials_r2010Gifton Koil Raj
 

Viewers also liked (10)

10G Ethernet Overview & Use Cases
10G Ethernet Overview & Use Cases10G Ethernet Overview & Use Cases
10G Ethernet Overview & Use Cases
 
Research in Composites for Aero Engine Applications
Research in Composites for Aero Engine ApplicationsResearch in Composites for Aero Engine Applications
Research in Composites for Aero Engine Applications
 
A brief history of jet (gas turbine) engines
A brief history of jet (gas turbine) engines A brief history of jet (gas turbine) engines
A brief history of jet (gas turbine) engines
 
GE SPS ID Fan Erection Sequence
GE SPS ID Fan Erection SequenceGE SPS ID Fan Erection Sequence
GE SPS ID Fan Erection Sequence
 
Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1
Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1
Ali Hashemi Sohi -AVIMA10-Mater thesis-New aero engine concepts1
 
GE Inspection: Industrial Process Control with Computed Tomography (CT)
GE Inspection: Industrial Process Control with Computed Tomography (CT)GE Inspection: Industrial Process Control with Computed Tomography (CT)
GE Inspection: Industrial Process Control with Computed Tomography (CT)
 
History of aircraft_materials_r2010
History of aircraft_materials_r2010History of aircraft_materials_r2010
History of aircraft_materials_r2010
 
V2500 lbm issue 01
V2500 lbm issue 01 V2500 lbm issue 01
V2500 lbm issue 01
 
Trent 1000 presentation
Trent 1000 presentationTrent 1000 presentation
Trent 1000 presentation
 
Trent
TrentTrent
Trent
 

Similar to IAEA China Aerospace Propulsion Technology Summit 05272014

IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...
IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...
IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...rezaeiho
 
IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...
IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...
IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...
IRJET Journal
 
Embraer Investors Conference - June 18, 2013
Embraer Investors Conference - June 18, 2013Embraer Investors Conference - June 18, 2013
Embraer Investors Conference - June 18, 2013Embraer RI
 
IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013
IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013
IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013rezaeiho
 
Yoke arm engine
Yoke arm engineYoke arm engine
Yoke arm engine
aoopee
 
Rotor hub octnov 2015
Rotor hub octnov 2015Rotor hub octnov 2015
Rotor hub octnov 2015
Ian Corrigible
 
Ijmet 06 10_019
Ijmet 06 10_019Ijmet 06 10_019
Ijmet 06 10_019
IAEME Publication
 
IRJET- Design and Fluid Flow Analysis of F1 Race Car
IRJET- Design and Fluid Flow Analysis of F1 Race CarIRJET- Design and Fluid Flow Analysis of F1 Race Car
IRJET- Design and Fluid Flow Analysis of F1 Race Car
IRJET Journal
 
IAEA China Aerospace Propulsion Technology Summit 06122012
IAEA  China Aerospace Propulsion Technology Summit 06122012IAEA  China Aerospace Propulsion Technology Summit 06122012
IAEA China Aerospace Propulsion Technology Summit 06122012rezaeiho
 
Design and Analysis of Air Intake Manifold for Formula Student Cars
Design and Analysis of Air Intake Manifold for Formula Student CarsDesign and Analysis of Air Intake Manifold for Formula Student Cars
Design and Analysis of Air Intake Manifold for Formula Student Cars
IRJET Journal
 
DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS
  DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS  DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS
DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS
IAEME Publication
 
Future trends in automobiles
Future trends in automobilesFuture trends in automobiles
Future trends in automobiles
Dheeraj Kumar
 
GE Additive, 21st century Paradigm Shifter - Use cases in GE
GE Additive, 21st century Paradigm Shifter - Use cases in GEGE Additive, 21st century Paradigm Shifter - Use cases in GE
GE Additive, 21st century Paradigm Shifter - Use cases in GE
GE코리아
 
The Race For The Future Of Aircraft Seating
The Race For The Future Of Aircraft SeatingThe Race For The Future Of Aircraft Seating
The Race For The Future Of Aircraft Seating
Torben Haagh
 
IRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex Generator
IRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex GeneratorIRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex Generator
IRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex Generator
IRJET Journal
 
Spacerolls.pdf
Spacerolls.pdfSpacerolls.pdf
Spacerolls.pdf
Syler3
 
IRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment
IRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel ExperimentIRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment
IRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment
IRJET Journal
 
Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...
Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...
Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...
Owens Corning Composites Solution Business
 
Opening Address: SpeedNews AMB Conference
Opening Address: SpeedNews AMB ConferenceOpening Address: SpeedNews AMB Conference
Opening Address: SpeedNews AMB Conference
ICF
 

Similar to IAEA China Aerospace Propulsion Technology Summit 05272014 (20)

IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...
IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...
IAEA UBM Airline Engineering & Maintenance Conference Americas San Francisco ...
 
IMA2G_RnD
IMA2G_RnDIMA2G_RnD
IMA2G_RnD
 
IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...
IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...
IRJET- Performance of Homogeneous Charge Compression Ignition Engine with Euc...
 
Embraer Investors Conference - June 18, 2013
Embraer Investors Conference - June 18, 2013Embraer Investors Conference - June 18, 2013
Embraer Investors Conference - June 18, 2013
 
IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013
IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013
IAEA Embry Riddle Aircraft Engine & Fleet Planning February 28 2013
 
Yoke arm engine
Yoke arm engineYoke arm engine
Yoke arm engine
 
Rotor hub octnov 2015
Rotor hub octnov 2015Rotor hub octnov 2015
Rotor hub octnov 2015
 
Ijmet 06 10_019
Ijmet 06 10_019Ijmet 06 10_019
Ijmet 06 10_019
 
IRJET- Design and Fluid Flow Analysis of F1 Race Car
IRJET- Design and Fluid Flow Analysis of F1 Race CarIRJET- Design and Fluid Flow Analysis of F1 Race Car
IRJET- Design and Fluid Flow Analysis of F1 Race Car
 
IAEA China Aerospace Propulsion Technology Summit 06122012
IAEA  China Aerospace Propulsion Technology Summit 06122012IAEA  China Aerospace Propulsion Technology Summit 06122012
IAEA China Aerospace Propulsion Technology Summit 06122012
 
Design and Analysis of Air Intake Manifold for Formula Student Cars
Design and Analysis of Air Intake Manifold for Formula Student CarsDesign and Analysis of Air Intake Manifold for Formula Student Cars
Design and Analysis of Air Intake Manifold for Formula Student Cars
 
DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS
  DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS  DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS
DEVELOPMENT OF MULTI CYLINDER CRD-I ENGINE TO MEET EURO VI EMISSION NORMS
 
Future trends in automobiles
Future trends in automobilesFuture trends in automobiles
Future trends in automobiles
 
GE Additive, 21st century Paradigm Shifter - Use cases in GE
GE Additive, 21st century Paradigm Shifter - Use cases in GEGE Additive, 21st century Paradigm Shifter - Use cases in GE
GE Additive, 21st century Paradigm Shifter - Use cases in GE
 
The Race For The Future Of Aircraft Seating
The Race For The Future Of Aircraft SeatingThe Race For The Future Of Aircraft Seating
The Race For The Future Of Aircraft Seating
 
IRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex Generator
IRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex GeneratorIRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex Generator
IRJET- Aerodynamic Analysis on a Car to Reduce Drag Force using Vertex Generator
 
Spacerolls.pdf
Spacerolls.pdfSpacerolls.pdf
Spacerolls.pdf
 
IRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment
IRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel ExperimentIRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment
IRJET- Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment
 
Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...
Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...
Enabling Economical Vehicle Light Weighting Through New Glass Reinforcement S...
 
Opening Address: SpeedNews AMB Conference
Opening Address: SpeedNews AMB ConferenceOpening Address: SpeedNews AMB Conference
Opening Address: SpeedNews AMB Conference
 

More from rezaeiho

HR Profile
HR ProfileHR Profile
HR Profilerezaeiho
 
Speaker Interviews Hooman
Speaker Interviews HoomanSpeaker Interviews Hooman
Speaker Interviews Hoomanrezaeiho
 
International Aircraft Engine Association Overview 02092012
International Aircraft Engine Association Overview 02092012International Aircraft Engine Association Overview 02092012
International Aircraft Engine Association Overview 02092012rezaeiho
 
IAEA Press Release 1-27 Final
IAEA Press Release 1-27 FinalIAEA Press Release 1-27 Final
IAEA Press Release 1-27 Finalrezaeiho
 
IAEA Aviation Leasing 09222014
IAEA Aviation Leasing 09222014IAEA Aviation Leasing 09222014
IAEA Aviation Leasing 09222014rezaeiho
 
IAEA - ENGINE MRO PLANNING 04032012
IAEA - ENGINE MRO PLANNING 04032012IAEA - ENGINE MRO PLANNING 04032012
IAEA - ENGINE MRO PLANNING 04032012rezaeiho
 
Embry Riddle Executive Program
Embry Riddle Executive ProgramEmbry Riddle Executive Program
Embry Riddle Executive Programrezaeiho
 
ISABE-2003-1110
ISABE-2003-1110ISABE-2003-1110
ISABE-2003-1110rezaeiho
 
Hooman_Rezaei_asme_paper2
Hooman_Rezaei_asme_paper2Hooman_Rezaei_asme_paper2
Hooman_Rezaei_asme_paper2rezaeiho
 
Hooman_Rezaei_asme_paper1
Hooman_Rezaei_asme_paper1Hooman_Rezaei_asme_paper1
Hooman_Rezaei_asme_paper1rezaeiho
 
Iaea Press Release Feb 6 2012
Iaea Press Release Feb 6 2012Iaea Press Release Feb 6 2012
Iaea Press Release Feb 6 2012rezaeiho
 
International Aircraft Engine Association Charter Feb 6 2012
International Aircraft Engine Association Charter Feb 6 2012International Aircraft Engine Association Charter Feb 6 2012
International Aircraft Engine Association Charter Feb 6 2012rezaeiho
 

More from rezaeiho (12)

HR Profile
HR ProfileHR Profile
HR Profile
 
Speaker Interviews Hooman
Speaker Interviews HoomanSpeaker Interviews Hooman
Speaker Interviews Hooman
 
International Aircraft Engine Association Overview 02092012
International Aircraft Engine Association Overview 02092012International Aircraft Engine Association Overview 02092012
International Aircraft Engine Association Overview 02092012
 
IAEA Press Release 1-27 Final
IAEA Press Release 1-27 FinalIAEA Press Release 1-27 Final
IAEA Press Release 1-27 Final
 
IAEA Aviation Leasing 09222014
IAEA Aviation Leasing 09222014IAEA Aviation Leasing 09222014
IAEA Aviation Leasing 09222014
 
IAEA - ENGINE MRO PLANNING 04032012
IAEA - ENGINE MRO PLANNING 04032012IAEA - ENGINE MRO PLANNING 04032012
IAEA - ENGINE MRO PLANNING 04032012
 
Embry Riddle Executive Program
Embry Riddle Executive ProgramEmbry Riddle Executive Program
Embry Riddle Executive Program
 
ISABE-2003-1110
ISABE-2003-1110ISABE-2003-1110
ISABE-2003-1110
 
Hooman_Rezaei_asme_paper2
Hooman_Rezaei_asme_paper2Hooman_Rezaei_asme_paper2
Hooman_Rezaei_asme_paper2
 
Hooman_Rezaei_asme_paper1
Hooman_Rezaei_asme_paper1Hooman_Rezaei_asme_paper1
Hooman_Rezaei_asme_paper1
 
Iaea Press Release Feb 6 2012
Iaea Press Release Feb 6 2012Iaea Press Release Feb 6 2012
Iaea Press Release Feb 6 2012
 
International Aircraft Engine Association Charter Feb 6 2012
International Aircraft Engine Association Charter Feb 6 2012International Aircraft Engine Association Charter Feb 6 2012
International Aircraft Engine Association Charter Feb 6 2012
 

IAEA China Aerospace Propulsion Technology Summit 05272014

  • 1. Global Aircraft Engine Manufacturing Innovation & Development Dr. Hooman Rezaei IAEA President & CEO China Aerospace Propulsion Technology Summit, May 28-29, Chengdu, China @IAEA1, : International Aircraft Engine Association www.aeroenginecloud.com
  • 2. IAEA Hit 9000 Member Milestone The only e-commerce cloud is launched integrating A-Z of the industry Global individual and corporate membership directory/listing Live aircraft engine listing for sale/lease/demand Live aircraft engine part & component listing for sale/lease/demand Market pricing set for engine & parts by asking price & auction News, events, courses, job opportunities, resume, consulting resources International Aircraft Engine Institute was just born in Newport Beach, CA Non-profit academic arm of International Aircraft Engine Association Launched by offering 5 day executive programs globally in: Design, Manufacturing, Maintenance & Operation, Lease & Finance Collaborating with several institutions to offer in several regions 2 www.aeroenginecloud.com
  • 3. Commercial Engine Industry Overview Ascend December 31, 2013 3 WORLD: ALL COMMERCIAL AIRCRAFT TYPE Manufacturer Aircraft Engines Share CFMI 8,646 17,656 39% GE Aviation 4,562 9,929 22% Rolls Royce 2,640 5,811 13% IAE 2,355 4,710 11% Pratt & Whitney 2,076 4,710 11% Other 581 2,020 5% Total 20,860 44,836 * Active commercial aircraft in operation with airlines www.aeroenginecloud.com CFMI is the world market leader
  • 4. Commercial Engine Industry Overview Ascend December 31, 2013 4 ASIA PACIFIC: ALL COMMERCIAL AIRCRAFT TYPES Manufacturer Aircraft Engines Share CFMI 2,646 5,374 46% IAE 910 1,820 16% GE Aviation 821 1,888 16% Rolls Royce 649 1,482 13% Pratt & Whitney 398 998 9% Other 46 168 1% Total 5,470 11,730 * Active commercial aircraft in operation with airlines www.aeroenginecloud.com CFMI is the market leader in Asia Pacific
  • 5. Commercial Engine Industry Overview Ascend December 31, 2012 5 Engine Manufacturer Ranking – Boeing/Airbus Types 2012 Deliveries Backlog Manufacturer Engines Share Engine Share CFMI 1,278 53% 8,742 47% IAE 422 17% 1,568 8% GE Aviation 388 16% 1,812 10% Rolls Royce 238 10% 2,214 12% Engine Alliance 56 2% 356 2% Pratt & Whitney 34 1% 1,228 7% Undecided - - 2,560 14% Total 2,416 18,480 www.aeroenginecloud.com CFMI is leading the new engine order
  • 6. Engine Architecture Gearbox on LEAP’s Architecture?Open Rotor? 6 www.aeroenginecloud.com
  • 7. Reduction Gear Architecture 7 2 Shaft Engine with 25-45 Klbf BPR 15:1 Gear Ration ~ 4:1 Carbon Fiber Variable Pitch Fan Blades TSFC -15% vs. todays GTF RR Announced Ultrafan with Geared Architecture www.aeroenginecloud.com
  • 8. Open Rotor Architecture 8 Challenges: Noise and Safety GE36 engine, which was shown to cut fuel burn by around 30% compared with turbofans. The GE36 featured a turbojet core driving dual counter-rotating eight-blade propfans in a pusher configuration. The engine was tested on a Boeing 727 (one engine) and a Boeing MD-90 (both engines). www.aeroenginecloud.com
  • 9. Open Rotor Architecture 9 Airbus, Snecma Tackle Open-Rotor Integration 2030+ Europe's Clean Sky program Chapter 14 noise limits Flight demonstrator on 340-300 end of this year 2030-timeframe narrow body Snecma alternatives: CR turbofan with -16% SFC & -20 dB than Leap-1 CROR with -26% SFC & -10 dB than Leap-1 Tested three generations of blade sets HERA1, 3 and 5 Achieved -5.2 EPNdB (Effective Perceived Noise) reduction 1.1% efficiency increase between the HERA1 and 3 blade sets, both for the original direct-drive CROR design. Additional 2.7-EPNdB noise reduction and 0.5% efficiency improvement with the HERA5 blade set, the first for the geared CROR www.aeroenginecloud.com
  • 10. Light Aircraft (Air Taxi) – Eclipse vs. Honda 10 PW610F Eclipse 550 HF120 Honda Jet The 600-3000 lbf Market www.aeroenginecloud.com
  • 11. GE Passport: Fan Blisk & CMC Application 11 • Low vibration due to fan titanium blisk with friction welded blade • CMC material usage for harsh environment parts such as the mixer and center body assemblies. In total it uses 15 CMC parts for a weight savings of more than 40 pounds per engine • Ox-Ox CMC material used on three parts: exhaust mixer, center body and core cowls. • Normal HPC airfoils @ 20-micron finish, appear smooth to the eye, Passport’s HPC @ 4-5 micron range surface roughness smaller than normal laminar boundary layer, smooth to the air Bombardier Global 7000 & 8000 Large-cabin Business Jets www.aeroenginecloud.com
  • 12. Significant Rise in Additive Manufacturing 12 www.aeroenginecloud.com Lighter, Rapid, Cheaper Manufacturing & Prototyping
  • 13. GE Passport: Integrated Propulsion System 13 • Low drag front end with single-piece air inlet • Fan cowl which is structurally integrated to the engine • Translating O-duct thrust reverser that provides improved fan flowpath while eliminating door links • Lower bifurcation, latches and split lines • New integrated mounting system for reduced engine distortion and enhanced on-wing performance. • Nexcelle to introduce IPS on LEAP-X1C & C919 www.aeroenginecloud.com Marching Towards More Integrated Design & Manufacturing
  • 14. THANK YOU! QUESTIONS? IAEA on @IAEA1, International Aircraft Engine Association 14 www.aeroenginecloud.com