Aeronautics and astronautics – Aircraft structure – Details
Reexamination Certificate
2007-07-02
2011-12-06
Collins, Timothy D (Department: 3644)
Aeronautics and astronautics
Aircraft structure
Details
C244S11000H
Reexamination Certificate
active
08070101
ABSTRACT:
The present invention relates to a locking system (20) for a movable lateral cowl (8) of a turbine engine nacelle intended to be connected to a pylon (4) of an aircraft, comprising, on the one hand, a clevis (21) intended to be connected to the pylon, and, on the other hand, a rod (22) intended to be mounted on the movable cowl and capable of engaging with the clevis when the movable cowl is in the closed position, characterized in that the rod is mounted so that it can move translationally along a substantially longitudinal axis of the movable cowl so as to form a slider which can shift between a locked position, in which it is engaged with the clevis and provides a structural connection between the pylon and the movable cowl, and an unlocked position, in which it is disengaged from the clevis and allows the movable cowl to be opened.
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International Search Report PCT/FR2007/001113; Dec. 19, 2007.
Bouret Georges Alain
Vauchel Guy Bernard
Aircelle
Cantor & Colburn LLP
Collins Timothy D
Stehle Jamie S
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