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Ramjet bypass duct and preburner configurationA combined turbofan and ramjet aircraft engine includes a forward bypass duct which allows the engine to operate more efficiently during the turbofan mode of operation. By mounting a ramjet preburner in the forward duct and isolating this duct from the turbofan bypass air, a transition from turbofan operation to ramjet operation can take place at lower flight Mach numbers without incurring pressure losses or blockage in the turbofan bypass air.
Document ID
20080003990
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Orlando, Robert J.
Date Acquired
August 24, 2013
Publication Date
May 17, 1994
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-058182
Patent Number: US-PATENT-5,311,735
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,311,735
Patent Application
US-PATENT-APPL-SN-058182
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