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Hybrid Exhaust ComponentAn exhaust includes a wall that has a first composite material having a first coefficient of thermal expansion and a second composite material having a second coefficient of the thermal expansion that is less than the first coefficient of thermal expansion.
Document ID
20150007179
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Pelletier, Gerard D.
Logan, Charles P.
McEnerney, Bryan William
Haynes, Jeffrey D.
Date Acquired
May 1, 2015
Publication Date
April 7, 2015
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-8,997,496
Patent Application Number: US-Patent-Appl-SN-13/172,411
Funding Number(s)
CONTRACT_GRANT: NNM06AB13C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,997,496
Patent Application
US-Patent-Appl-SN-13/172,411

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