Indicator of failure to close, namely for aircraft engine...

B - Operations – Transporting – 64 – D

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B64D 45/00 (2006.01) B64D 29/08 (2006.01) E05B 41/00 (2006.01) E05C 19/14 (2006.01)

Patent

CA 2325870

Indicator of failure to close, namely for aircraft engine nacelle cowlings. To prevent an operator from forgetting to activate the locking mechanism interposed between two components such as the nacelle cowlings (12.14) of an aircraft engine, when these elements are in the closed position, an indicator of failure to close is provided. This indicator includes retractable abutment elements (42.44), which automatically visibly maintain the two elements separated from one another, when these elements are moved from their open position to their closed position.

Indicateur de défaut de fermeture, notamment pour des capots de nacelle d'un moteur d'avion. Afin d'éviter qu'un opérateur oublie d'actionner des mécanismes de verrouillage interposés entre deux éléments tels que des capots (12,14) de nacelle d'un moteur d'avion, lorsque ces éléments sont en position fermée, on prévoit un indicateur de défaut de fermeture. Cet indicateur comprend des organes de butée escamotables (42,44) qui maintiennent automatiquement les deux éléments écartés l'un de l'autre, de manière visible, lorsque ces éléments sont déplacés de leur position ouverte dans leur position fermée.

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