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NASA NTRS · 19790025297

Flow diverter value and flow diversion method

Abstract

A 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.

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BibTeXRIS

Arline, S. B., Carlson, R. L.. 1964-05-26. Flow diverter value and flow diversion method. https://ntrs.nasa.gov/citations/19790025297

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