BALK DEVICE FOR DOOR LOCK

An assembly is provided for an aircraft. This aircraft assembly includes a latch (50), a balk element (62) and a fitting (36). The latch (50) is movable between an unlocked position and a locked position. The balk element (62) is rotatable between a balked position and an un-balked position. The bal...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	GHANDOUR, Imad D, HUYNH, Ken V
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ACCESSORIES THEREFOR AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FIXED CONSTRUCTIONS FLYING SUITS HANDCUFFS HELICOPTERS KEYS LOCKS PARACHUTES PERFORMING OPERATIONS SAFES TRANSPORTING WINDOW OR DOOR FITTINGS
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Beschreibung
Zusammenfassung:	An assembly is provided for an aircraft. This aircraft assembly includes a latch (50), a balk element (62) and a fitting (36). The latch (50) is movable between an unlocked position and a locked position. The balk element (62) is rotatable between a balked position and an un-balked position. The balk element (62) is configured to block the latch (50) from moving to the locked position when the balk element (62) is in the balked position. The fitting (36) includes a keeper (46). The fitting (36) is movable between an open position and a closed position. The fitting (36) is configured to push the balk element (62) into the un-balked position as the fitting (36) moves into the closed position. The latch (50) is configured to move to the locked position and engage the keeper (46) when the fitting (36) is in the closed position.