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Design and development of a large diameter high pressure fast acting propulsion valve and valve actuatorThe design and development of a large diameter high pressure quick acting propulsion valve and valve actuator is described. The valve is the heart of a major test facility dedicated to conducting full scale performance tests of aircraft landing systems. The valve opens in less than 300 milliseconds releasing a 46-centimeter- (18-in.-) diameter water jet and closes in 300 milliseconds. The four main components of the valve, i.e., valve body, safety shutter, high speed shutter, and pneumatic-hydraulic actuator, are discussed. This valve is unique and may have other aerospace and industrial applications.
Document ID
19870006907
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srinivasan, K. V.
(S and Q Corp. Morgan Hill, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA. Lewis Research Center The 20th Aerospace Mechanics Symposium
Subject Category
Mechanical Engineering
Accession Number
87N16340
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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