SYSTEMS AND METHODS FOR DETECTING A JAM OF A FLAP OF A WING OF AN AIRCRAFT
A jam detection system for a flap (106) of a wing of an aircraft includes a linkage (116) coupled to the flap and a support (108) of the wing, and a sensor (118) configured to detect a position of at least a portion of the linkage. The sensor is further configured to compare the position of the leas...
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| creator | BOWERS, Bret A BLOCK, Samuel L TSAI, Kevin |
| description | A jam detection system for a flap (106) of a wing of an aircraft includes a linkage (116) coupled to the flap and a support (108) of the wing, and a sensor (118) configured to detect a position of at least a portion of the linkage. The sensor is further configured to compare the position of the least a portion of the linkage to a jam threshold to determine if a jam condition exists. The linkage can also be coupled to a carriage (114) moveably coupled to the support. |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | SYSTEMS AND METHODS FOR DETECTING A JAM OF A FLAP OF A WING OF AN AIRCRAFT |
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