Aircraft weighing systems

Details Aircraft weighing systems Aircraft weighing systems

1981-07-15

1983-05-31

Ruehl, Charles A.

Measuring and testing

Dynamometers

Responsive to multiple loads or load components

7386254, 7386265, 177146, G01L 122, G01L 516

Patent

active

043855270

ABSTRACT:
An aircraft weighing system which includes substantially rectangular operator members (10) associated with jacks to support an aircraft (100). The operator member (10) includes a pair of central bearing beam members (51, 52) secured to opposite ends of a rigid load receiving member (53). The central bearing beam members (51, 52) are supported by side bearing beam members (31, 32, 41, 42) through rigid end members (63, 64) to maintain an angular relationship between ends of the beam members (31, 32, 41, 42, 51, 52) when loading is changed such that deflection of the beam members indicates the weight of the aircraft.

REFERENCES:
patent: 2488347 (1949-11-01), Thurston
patent: 2754107 (1956-07-01), Ernst et al.
patent: 2806686 (1957-09-01), Miller, Jr.
patent: 2859613 (1958-11-01), Green
patent: 3023627 (1962-03-01), Geyling
patent: 3439761 (1969-04-01), Laimins
patent: 3837222 (1974-09-01), Raskin
patent: 4071838 (1978-01-01), Block

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