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Low Differential Pressure GeneratorA method and apparatus for evaluating low differential pressure transducers includes a pressure generator in the form of a piston-cylinder assembly having a piston that may be manually positioned precisely within the cylinder to change the volume and thus the pressure at respective sides of the piston. At one side of the piston the cylinder communicates with a first chamber and at the other side of the piston the cylinder communicates with a second chamber, the first and second chambers being formed within a common tank by a partition wall. The chambers each communicate with the transducer to be evaluated and a standard pre-calibrated transducer the transducers being connected fluidly in parallel so that a pressure differential between air in the two chambers resulting from movement of the piston within the cylinder is communicated to both the transducer to be evaluated and the standard transducer, and the outputs of the transducers is observed and recorded.
Document ID
19980021806
Acquisition Source
Kennedy Space Center
Document Type
Other - Patent
Authors
Stout, Stephen J.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Deyoe, Richard T.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Date Acquired
August 17, 2013
Publication Date
December 2, 1997
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: NASA-Case-KSC-11804-1
Patent Application Number: US-Patent-Appl-SN-695071
Patent Number: US-Patent-5,693,871
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-KSC-11804-1|US-Patent-5,693,871
Patent Application
US-Patent-Appl-SN-695071
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