Aircraft landing gear automated inspection and life...

Communications: electrical – Aircraft alarm or indicating systems – Landing gear indicator

Reexamination Certificate

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Details

C244S10000R, C244S1020SS, C244S1040FP, C073S17800T, C267S064260

Reexamination Certificate

active

11092020

ABSTRACT:
A system for use in monitoring, measuring, computing and displaying the landing loads experienced while aircraft are executing either normal, overweight or hard landing events. Pressure sensors and motion sensors are mounted in relation to each of the landing gear struts to monitor, measure and record the impact loads and aircraft sink rates; experienced by landing gear struts, as the aircraft landing gear initially come into contact with the ground. The computer of this system measures the landing loads experienced by each landing gear strut and determines if a hard landing event has occurred. Additional features include automating the inspections required to aircraft components, after overweight or hard landing events.

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patent: 6237406 (2001-05-01), Nance
patent: 6237407 (2001-05-01), Nance
patent: 6293141 (2001-09-01), Nance
patent: 2006/0144997 (2006-07-01), Schmidt et al.

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