Aircraft cabin pressurization control system tester

Measuring and testing – With fluid pressure – Leakage

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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

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