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Clocked Thrust ReversersAn aircraft includes a fuselage including a propulsion system supported within an aft portion. A thrust reverser is mounted proximate to the propulsion system for directing thrust in a direction to slow the aircraft. The thrust reverser directs thrust at an angle relative to a vertical plane to reduce interference on control surfaces and reduce generation of underbody lift.
Document ID
20170004948
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Suciu, Gabriel L.
Chandler, Jesse M.
Date Acquired
June 2, 2017
Publication Date
May 30, 2017
Subject Category
Aerodynamics
Funding Number(s)
CONTRACT_GRANT: NNX11AB35A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,663,239
Patent Application
US-Patent-Appl-SN-14/440,718
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