Pin assembly

Details Pin assembly Pin assembly

E - Fixed Constructions

05

B

E05B 15/02 (2006.01) B64D 11/00 (2006.01) E05B 9/02 (2006.01) E05B 9/04 (2006.01) E05C 1/08 (2006.01)

Patent

CA 2635322

The invention provides a pin assembly (10) useful for situations of high vibration, such as hatches or lockers on aircraft. Pin assembly (10) has a locking pin (12) adapted for insertion in a latching mechanism. Locking pin (12) has a maximum cross-section. Assembly (10) also includes a base (32) for locking pin (12) and at least one slip plate (20) which has an aperture (21) which is larger than the maximum cross-section of the locking pin (12).

L'invention concerne un ensemble goupille (10) servant dans des situations à vibrations intenses, telles que dans les trappes ou porte-bagages à bord des avions. L'ensemble goupille (10) a une goupille de verrouillage (12) conçue à des fins d'insertion dans un mécanisme de verrouillage. La goupille de verrouillage (12) a un maître couple. L'ensemble (10) comprend également une base (32) pour la goupille de verrouillage (12) et au moins une plaque de contact (20) qui a une ouverture (21) qui est supérieure au maître couple de la goupille de verrouillage (12).

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