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NASA’s Efficient Quiet Integrated Propulsors (Equip) Technical ChallengeAdvances in aircraft propulsor technology - ducted and unducted - are key elements to developing a sustainable aviation future. Increasing propulsive efficiency comes with significant challenges. The long-term trend in aircraft engine design has been towards higher bypass ratios to increase efficiency and decrease noise. Current designs are pushing against limits on engine size; the engine must fit under the wing and overcome the nacelle weight, aerodynamic drag, and airframe integration penalties associated with an ultra-high bypass ratio. The next-generation ducted engines will have shorter inlets and smaller rotor-stator spacing to minimize nacelle area. This increases the potential for non-uniform flow at the fan face and less area for acoustic liners. Unducted engines eliminate the nacelle penalty while presenting challenges to noise and operability in distorted flow environments. The overall diameter in both cases raises questions about engine-airframe integration to maximize efficiency gains and minimize installation penalties. The National Aeronautics and Space Administration (NASA) Advanced Air Vehicles Program (AAVP) approved the Efficient Quiet Integrated Propulsor (EQuIP) Technical Challenge (TC) under the Advanced Air Transport Technology (AATT) Project to work on next-generation propulsor technologies in collaboration with NASA’s government and industry partners in the Sustainable Flight National Partnership. The EQuIP TC leverages NASA resources with Federal Aviation Administration (FAA) and industry investments under the FAA’s Continuous Lower Energy Emissions and Noise (CLEEN) program to address technical challenges on the propulsor subject to the flow field imposed by the engine-airframe-flight environment. The EQuIP TC complements NASA Aeronautics Research Mission Directorate’s (ARMD) existing investments in sustainable aviation for the next-generation of commercial aircraft and contributes to meeting the noise and efficiency goals set by the Sustainable Flight National Partnership and U.S. Aviation Climate Action Plan. This paper introduces the EQuIP TC, describes key parts of its development, and presents the background research used to scope its impact.
Document ID
20240007565
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Cliff Brown
(Glenn Research Center Cleveland, United States)
Jess Reinert
(Glenn Research Center Cleveland, United States)
David Stephens
(Glenn Research Center Cleveland, United States)
Ercan Dumlupinar
(Ames Research Center Mountain View, United States)
Date Acquired
June 12, 2024
Subject Category
Acoustics
Meeting Information
Meeting: 34th Congress of the International Council of the Aeronautical Sciences (ICAS)
Location: Florence
Country: IT
Start Date: September 9, 2024
End Date: September 13, 2024
Sponsors: Congress of the International Council of the Aeronautical Sciences
Funding Number(s)
WBS: 081876.02.03.19.01.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Propulsion
Integration
Public-Private Partnerships
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