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Flow diverter value and flow diversion methodA flow diverter valve applicable to any fluid flow system requiring rapid bleed or bypass is disclosed. Examples of application of the flow diverter valve to a liquid rocket and a turbojet aircraft engine are given. Features of the valve include: (1) an independent fluid source is used to activate the flow diverter valve toward its closed position during its initial stage of travel; (2) the flow diverter port area and size is unlimited and the valve travel is unlimited; and (3) the valve housing is fabricated such that the valve can be a one step valve, a two step valve, or include as many steps as are found desirable.
Document ID
19790025297
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Arline, S. B.
(United Aircraft Corp. East Hartford, Conn., United States)
Carlson, R. L.
(United Aircraft Corp. East Hartford, Conn., United States)
Date Acquired
September 3, 2013
Publication Date
May 26, 1964
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: NASA-CASE-HQN-00573-1
Patent Number: US-PATENT-3,134,389
Patent Application Number: US-PATENT-APPL-SN-129379
Accession Number
79N33468
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-HQN-00573-1|US-PATENT-3,134,389
Patent Application
US-PATENT-APPL-SN-129379
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