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Static pressure orifice system testing method and apparatusA method and apparatus are presented for pressure testing the static pressure orifices and associated connections used in wind tunnels. A cylindrical module, having in one end an open hemispherical calibration pressure chamber separated from and surrounded by an annular vacuum chamber is placed over the orifice of the system to be tested. O-rings ensure seating and a vacuum seal between the chambered end of the module and the surface around the orifice: one O-ring separates the outer chamber from the outside environment. Ports lead from each of the chambers out the other end of the module to tubes connected to a control box consisting of calibration pressure and vacuum supply lines, bleeder valves, and gauges.
Document ID
19800010088
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Culotta, R. F.
(NASA Langley Research Center Hampton, VA, United States)
Posey, D. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 8, 1980
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: US-PATENT-4,182,158
Patent Application Number: US-PATENT-APPL-SN-934576
Patent Number: NASA-CASE-LAR-12269-1
Accession Number
80N18358
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,182,158|NASA-CASE-LAR-12269-1
Patent Application
US-PATENT-APPL-SN-934576
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