On-board aircraft weighting and center of gravity determing appa

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177141, 73 6506, 244104FP, G01G 1910, G01L 716

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active

055218270

ABSTRACT:
An apparatus for determining the weight and/or center of gravity of an aircraft is disclosed and includes a plurality of fittings attached to each oleo strut on the aircraft for accessing the working fluid in the oleo strut, a computer, a first, electronically-responsive valve coupled to each fitting for controlling the fluid flow through the fitting in response to control signals from the computer, a pressure transducer coupled downstream of the first valve for measuring the pressure of the working fluid therein and coupled to the computer to provide a pressure measurement signals to the computer for each strut, and an inclinometer attached to the aircraft and electronically coupled to the computer for providing incline information to the computer. A method is disclosed that includes accessing the working fluid of each oleo strut cylinder, attaching a pump to each oleo strut cylinder, cycling each oleo strut cylinder between a near fully extended position and a near fully retracted position while recording pressure measurements in the cylinder at a plurality of points between the two positions while keeping the aircraft level, and mathematically manipulating the recorded pressure measurements to arrive at an approximation of the weight on each strut. The total weight can be then found by adding the weight on each strut plus any dead weight for each strut. The center of gravity may then be determined by summing the moments for each load on each strut and dividing the total or sum of the moments by the total weight to arrive at the center of gravity.

REFERENCES:
patent: Re23945 (1955-02-01), Kollisch
patent: 2302458 (1942-11-01), Miner
patent: 2443098 (1948-06-01), Dean
patent: 2520428 (1950-08-01), Nilakantan
patent: 2541429 (1951-02-01), Mathes et al.
patent: 2686426 (1954-08-01), Kolisch
patent: 2725193 (1955-11-01), Kolisch
patent: 2751921 (1956-06-01), Baldwin et al.
patent: 2817161 (1957-12-01), Stern et al.
patent: 2856127 (1958-10-01), Kolisch et al.
patent: 2901171 (1959-08-01), Kolisch
patent: 2987254 (1961-06-01), Kolisch
patent: 3063638 (1962-11-01), Kolisch
patent: 3191442 (1965-06-01), Hutchinson
patent: 3388242 (1968-06-01), Johnson
patent: 3443077 (1969-05-01), Lettvin
patent: 3473369 (1969-10-01), Garrison
patent: 3486017 (1969-12-01), Arseneau
patent: 3486371 (1969-12-01), Dybvad et al.
patent: 3494181 (1970-02-01), Boelkins et al.
patent: 3513300 (1970-05-01), Elfenbein et al.
patent: 3584503 (1971-06-01), Semour
patent: 3620074 (1971-11-01), Laimins et al.
patent: 3625053 (1971-12-01), Laimins
patent: 3626752 (1971-12-01), Levins
patent: 3638477 (1972-02-01), Brummer
patent: 3701279 (1972-10-01), Harris et al.
patent: 3727180 (1973-04-01), Lingel et al.
patent: 3746844 (1973-07-01), Azum et al.
patent: 3800895 (1974-04-01), Gale et al.
patent: 3808954 (1974-05-01), Persson et al.
patent: 3826321 (1974-07-01), Rigney et al.
patent: 4110605 (1978-08-01), Miller
patent: 4210902 (1980-07-01), Palekhin et al.
patent: 4225926 (1980-09-01), Wendt
patent: 4269070 (1981-05-01), Nelson et al.
patent: 4312042 (1982-01-01), Bateman
patent: 4328494 (1982-05-01), Goodall
patent: 4385527 (1983-05-01), Raskin
patent: 4463428 (1984-07-01), Gilliam
patent: 4490802 (1984-12-01), Miller
patent: 4494210 (1985-01-01), Miller
patent: 4502555 (1985-03-01), Gower
patent: 4507742 (1985-03-01), Bateman
patent: 4545019 (1985-10-01), Glover
patent: 4548079 (1985-10-01), Klatt
patent: 4639872 (1987-01-01), McHale et al.
patent: 4782706 (1988-11-01), Kister et al.
patent: 4935885 (1990-06-01), McHale et al.
patent: 4937754 (1990-06-01), Buisson et al.
patent: 4967384 (1990-10-01), Molinar et al.
patent: 4969112 (1990-11-01), Castle
patent: 4992775 (1991-02-01), Castle et al.
patent: 5034896 (1991-07-01), Orgun et al.
patent: 5131482 (1992-07-01), Davis et al.
patent: 5136513 (1992-08-01), Sol et al.
patent: 5167385 (1992-12-01), Hafner
patent: 5170366 (1992-12-01), Passarelli
patent: 5214586 (1993-05-01), Nance
patent: 5257756 (1993-11-01), Patzig et al.
patent: 5258582 (1993-11-01), Jungingen
patent: 5410109 (1995-04-01), Tarter et al.
A. C. Madougall and Dr. R. M. H. Cheng, "The Light-Weight System", SAWE Journal, 1980, pp. 41-46.
Brochure by Honeywell, Inc. "Weight and Balance System--Introducing the first realtime system for accurate weight and CG", 1989.

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