Aircraft fluid vessel testing

Details Aircraft fluid vessel testing Aircraft fluid vessel testing

1991-04-29

1992-10-13

Ng, Jin F.

Communications: electrical

Aircraft alarm or indicating systems

73 1H, 340515, 364509, G08B 2100

Patent

active

051554828

ABSTRACT:
An electrical test set especially suited for use in correlating the fill sensor's output indication for a pressure vessel with a known vessel fill condition. The vessel may be the hydrazine fuel container for an aircraft such as the U.S. Air Force F-16 fighter aircraft. The tester enables sensor system evaluation while the vessel is yet dismounted and in the refilling and refurbishing shop. In addition to verification of known vessel fill and satisfactory operation of the vessel level sensing apparatus, the tester eliminates the variables and inconvenience attending verification of sensor system operation on the aircraft by way of a cockpit instrument. The tester is provided with external and internal electrical energy sourcing and with operator friendly controls compatible with the instrumentation system in the host aircraft.

REFERENCES:
patent: 1304022 (1919-05-01), Cole
patent: 1414298 (1922-04-01), Montero
patent: 3176221 (1965-03-01), Stamler
patent: 3333469, Godfrey
patent: 3742342 (1973-06-01), Schick
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patent: 4178802 (1979-12-01), Yamamoto
patent: 4441157 (1984-04-01), Gerchman et al.
patent: 4821022 (1989-04-01), Jannotta
patent: 4918619 (1990-04-01), Orloff
General Radio Experimenter, vol. 30 No. 4, Sep. 1955, pp. 1-8, "A Calibrator for Aircraft Fuel Gages".

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