Measuring and testing – With fluid pressure – Leakage
Patent
1984-06-19
1986-03-04
Cangialosi, Salvatore
Measuring and testing
With fluid pressure
Leakage
C05B 100
Patent
active
H00000345
ABSTRACT:
An aircraft cabin pressure control system tester includes a first tester component having a vacuum pressure-sensing gage which indicates the static atmosphere in inches of Hg and a second tester component having a differential pressure-sensing gage which indicates the pressure/vacuum in inches of H.sub.2 O. When the components of the tester are connected respectively in communication with lines connecting the controller of the system to static atmosphere ports and a pressure regulator valve, the tester can be used to determine which one, if any, of the pressure controller, air compressor and regulator valve of the pressure control system is faulty.
REFERENCES:
patent: 2679753 (1954-06-01), Flamm
patent: 3156113 (1964-11-01), Dollar
patent: 3418843 (1968-12-01), Bosshart
patent: 3580050 (1971-05-01), Waldron
patent: 3747404 (1973-07-01), Novak
patent: 4092865 (1978-06-01), Strybel
patent: 4109536 (1978-08-01), Strybel
patent: 4375162 (1983-03-01), Eppley
patent: 4380166 (1983-04-01), Crombie
Cangialosi Salvatore
Lobo Ian J.
Scearce Bobby D.
Singer Donald J.
The United States of America as represented by the Secretary of
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