Aircraft trim safety system and backup controls
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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N/A
Issued Date -
N/A
app pub date -
Jan 28, 2008
filing date -
Dec 19, 2005
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
Methods and apparatuses that control trim of an aircraft even in the presence of conflicting trim inputs, for example by disabling the trim input switches on the aircraft when conflicting switch inputs are received. When conflicting switch inputs are received and certain time conditions are met, the controller can disable the switch inputs and provide a backup and independent means to control the trim circuitry. The pilot can be allowed to re-enable the disabled inputs.
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Family
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Cited Art Landscape
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