System for weighing fixed wing and rotary wing aircraft by the measurement of cross-axis forces
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United States of America Patent
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-
Jul 2, 2002
Grant Date -
N/A
app pub date -
Jul 23, 1999
filing date -
Jul 23, 1999
priority date (Note) -
Expired
status (Latency Note)
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Abstract
Method and system for determining aircraft weight-related data. Strain sensors are affixed to aircraft support struts to generate signals related to strut strain. Tensioning apparatus applies known tension to the struts and computing apparatus calculates a calibration matrix relating loads to the strain sensor signals. The computer calculates the weight-related data from the calibration matrix and strain sensor signals.
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