Thrust reverser sleeve lock

• US 6,625,972 B1
• Filed: 08/30/2001
• Issued: 09/30/2003
• Est. Priority Date: 08/30/2001
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Sternberger, Joe E.
• Primary Examiner(s): KIM, TAE JUN
• Application Number:
  US09/943,715
• Time in Patent Office: 761 Days
• Field of Search: 602/262, 244/110.B, 239/265.19, 239/265.23, 239/265.27, 239/265.29, 239/265.31
• US Class Current: 60/226.2
• CPC Class Codes: F02K 1/76 Control or regulation of thrust reversers
• CPC Class Codes: F02K 1/766 with blocking systems or locking devices; Arrangement of locking devices for thrust reversers

Abstract

A thrust reverser system for a jet engine has a thrust reverser sleeve lock, preferably for each thrust reverser sleeve, that provides at least one of the redundant anti-deployment mechanisms of the thrust reverser. The thrust reverser sleeve lock has a lock pin that engages a thrust reverser sleeve when the thrust reverser sleeve is in a stowed position and the thrust reverser sleeve lock is in a lock position to prevent the thrust reverser sleeve from deploying. In an embodiment of the invention, the thrust reverser sleeve lock includes an single-action hydraulically actuated actutor to which the lock pin is affixed, the actuator extending the lock pin through a lock hole in the thrust reverser sleeve when the thrust reverser sleeve is in its stowed position and the thrust reverser sleeve lock is in a lock position.

Claims

1. In a thrust reverser for a jet engine having a plurality of anti-deployment mechanisms, at least one of the anti-deployment mechanisms comprising:

a thrust reverser sleeve lock, the thrust reverser sleeve lock including a lock pin coupled to an actuator for extending and retracting the lock pin between a locked and an unlocked position;

the actuator comprising a single-action actuator having a hydraulic port and a pneumatic port and being actuatable by at least one of pressurized hydraulic fluid and pressurized air; and

wherein the lock pin engages a thrust reverser sleeve of the thrust reverser when the lock pin is in the locked position and prevents the thrust reverser sleeve from moving away from a stowed position.

2. The apparatus of claim 1, wherein the thrust reverser includes a plurality of thrust reverser sleeves and at least one thrust reverser sleeve lock for each thrust reverser sleeve.

3. The apparatus of claim 2, wherein each thrust reverser sleeve includes a lock pin hole through which the lock pin of the thrust reverser sleeve lock for that thrust reverser sleeve extends when that thrust reverser sleeve lock is in a locked position.

4. The apparatus of claim 3, wherein each thrust reverser sleeve includes a guide fitting having a ramp which urges the lock pin of the associated thrust reverser sleeve lock towards its unlocked position as the thrust reverser sleeve moves toward a stowed position, the guide fitting further including a hole coaxially aligned with the lock pin hole in its thrust reverser sleeve, the lock pin extending through the lock pin hole in the associated thrust reverser sleeve and the hole in that thrust reverser sleeve'"'"'s guide fitting when the lock pin is in its lock position.

5. The apparatus of claim 1, wherein the lock pin is formed as part of the actuator.

6. The apparatus of claim 1, further comprising a manually operable mechanical release mechanism coupled to the actuator.

7. The apparatus of claim 6 wherein the manually operable mechanical release mechanism includes a lever having one end coupled to the actuator.

8. A thrust reverser sleeve lock for a thrust reverser sleeve of a thrust reverser, comprising:

the thrust reverser sleeve having a lock pin hole;

a single-action actuator having a lock pin that extends through the lock pin hole in the thrust reverser sleeve when the thrust reverser sleeve is in a stowed position and the actuator is in a lock position; and

a guide pin fitting affixed to an inner surface of the thrust reverser sleeve, the guide pin fitting having a ramp that moves across the lock pin in contact therewith as the thrust reverser sleeve moves to its stowed position to depress the lock pin away from the thrust reverser sleeve.

9. The thrust reverser sleeve lock of claim 8, wherein the actuator has a body having a shaft extending therethrough, the shaft having a first end coupled to a fixed element of the thrust reverser, the body of the actuator having the lock pin at a first end, the actuator having a spring that urges the body of the actuator toward the lock pin hole in the thrust reverser sleeve to extend the lock pin through the lock pin hole, the actuator body being moved away from the thrust reverser sleeve to retract the lock pin from the lock pin hole in the thrust reverser sleeve upon activation of the actuator.

10. The thrust reverser sleeve lock of claim 8, wherein the actuator comprises a hydraulic actuator.

11. The thrust reverser sleeve lock of claim 10, wherein the actuator further includes a pneumatic port, the actuator being actuable by at least one of pressurized hydraulic fluid and pressurized air.

12. The thrust reverser sleeve lock of claim 8, and further including a lever actuated manual operable mechanical release mechanism coupled to the actuator for manual actuation of the actuator.

13. A thrust reverser sleeve lock for a thrust reverser sleeve of a thrust reverser, comprising:

an actuator having a lock pin that, when the actuator is in a locked position, extends through a lock pin hole in the thrust reverser sleeve to lock the thrust reverser sleeve against movement away from a stowed position, and when the actuator is in an unlocked position is retracted from the lock pin hole;

the actuator having a hydraulic port and a pneumatic port and actuated by at least one of a hydraulic pressure and a pneumatic pressure.