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The Promise and Challenges of Ultra High Bypass Ratio Engine Technology and IntegrationIn this presentation, an overview of the research being conducted by the ERA Project in Ultra High Bypass aircraft propulsion and in partnership with Pratt & Whitney with their Geared TurboFan (GTF) is given. The ERA goals are shown followed by a discussion of what areas need to be addressed on the engine to achieve the goals and how the GTF is uniquely qualified to meet the goals through a discussion of what benefits the cycle provides. The first generation GTF architecture is then shown highlighting the areas of collaboration with NASA, and the fuel burn, noise and emissions reductions possible based on initial static ground test and flight test data of the first GTF engine. Finally, a 5 year technology roadmap is presented focusing on Ultra High Bypass propulsion technology research areas that are being pursued and being planned by ERA and P&W under their GTF program.
Document ID
20110011737
Acquisition Source
Headquarters
Document Type
Presentation
Authors
Hughes, Chris
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2011
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
HQ-STI-11-012
E-17843
Report Number: HQ-STI-11-012
Report Number: E-17843
Meeting Information
Meeting: 49th AIAA Aero Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 699959.02.09.03.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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