US 6,604,355 B1Granted

Thrust reverser hook latch system

AssigneeThe Boeing Company

InventorJoe E. Sternberger

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Abstract

A hook latch antideployment system for a thrust reverser having at least one thrust reverser sleeve that translates between a deployed and stowed positions and a thrust reverser actuation system that translates the thrust reverser sleeve. The thrust reverser has a stationary element that remains stationary with respect to the thrust reverser sleeve when the thrust reverser sleeve translates. The hook latch anti-deployment system has a hook latch a hook member and a latch member. One of the hook and latch members is coupled to the thrust reverser sleeve for translation therewith and the other of the hook and latch members is affixed to the stationary element of the thrust reverser. The hook member engages the latch member when the thrust reverser sleeve is in its stowed position to prevent deployment of the thrust reverser sleeve. The hook latch system further includes a release mechanism coupled to the thrust reverser actuation system that releases the hook member from the latch member when the thrust reverser actuation system is actuated to deploy the thrust reverser sleeve to its deployed position.

Claims8

Dependent claims

In a thrust reverser having at least one thrust reverser sleeve that translates between a deployed and stowed positions and a thrust reverser actuation system that translates the thrust reverser sleeve, the thrust reverser further including a stationary element that remains stationary with respect to the thrust reverser sleeve when the thrust reverser sleeve translates, a hook-latch anti-deployment system comprising:

(a) a hook member coupled to the thrust reverser sleeve for translation therewith;
(b) a latch member coupled to the stationary element of the thrust reverser, the latch member engaging the hook member when the thrust reverser sleeve is in its stowed position to prevent the thrust reverser sleeve from moving from its stowed position;
(c) an actuator coupled to the thrust reverser actuation system and to the latch member, the actuator releasing the hook member from the latch member when the thrust reverser actuation system is actuated to deploy the thrust reverser sleeve to the deployed position, wherein the actuator has a shaft having a roller at an aft end, the hook member having an arcuate hook cam in which the roller at the aft end of the shaft is received when the thrust reverser sleeve is in the stowed position and the hook latch anti-deployment system is in a locked position;
and
upon actuation of the actuator when the thrust reverser actuation system is actuated to extend the thrust reverser sleeve to the deployed position, the actuator retracts the shaft, the roller at the aft end of the shaft of the actuator acting upon the arcuate hook cam of the hook member cams the hook member to a release position.

2 more elements

A hook-latch antideployment mechanism for a thrust reverser sleeve, comprising:

(a) a hook member coupled to the thrust reverser sleeve for translation therewith;
(b) the hook member having a hook cam extending from a forward facing side and a latch cam on a bottom side;
(c) the latch cam having a concave aft facing portion and a forward facing ramped portion;
(d) an actuator affixed to a stationary element of the thrust reverser, the actuator having a shaft that retracts when the actuator is actuated, the actuator having a return spring that returns the actuator shaft when the actuator is deactuated;
(e) the shaft of the actuator having a roller at an aft end of the shaft that is hooked by the hook cam when the thrust reverser sleeve is in a stowed position and the hook-latch system is in a locked position;
(f) a clevis latch having a clevis latch roller at an aft end that is received in the concave aft facing portion of the latch cam when the thrust reverser sleeve is in the stowed position hook-latch system is in a locked position;
and
(g) the actuator coupled to the thrust reverser actuation system wherein the actuator is actuated upon actuation of the thrust reverser actuation system to translate the thrust reverser sleeve aftly to a deployed positon, the retraction of the actuator shaft upon actuation of the actuator camming against the hook cam to cam the hook member to a release position where the latch cam can roll over the clevis latch roller.

5 more elements

Dependencies are inferred from the claim text.