Arrangement of at least one sensor on the landing gear of an air

Aeronautics and astronautics – Landing gear – Wheel

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73 6501, B64C 2500

Patent

active

052055140

ABSTRACT:
An arrangement in which at least one sensor is provided on the landing gear of an aircraft for measuring its weight and the position of its center of gravity, and in which a sensor for a measurement of shear is arranged at a measurement point formed by a pair of lugs on an axle or bogie beam. The axle (9) or bogie beam is of constant cross section above the measurement point and symmetrical to a vertical axis which lies centrally between the two lugs of a pair (10, 13 and 14, 15 respectively).

REFERENCES:
patent: 4782706 (1988-11-01), Kister et al.

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