Arrangement of at least one sensor on the landing gear of an aircraft for measuring its weight and position of center of gravity
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United States of America Patent
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-
Apr 27, 1993
Grant Date -
N/A
app pub date -
Sep 23, 1991
filing date -
Oct 20, 1990
priority date (Note) -
Expired
status (Latency Note)
Importance
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).
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