US 5,609,020 A · Thrust reverser synchronization shaft lock

Abstract

A thrust reverser synchronization shaft lock system that includes a sync lock control valve (50) and two hydraulically controlled sync locks (60) attached to the synchronization shafts (5) of a jet engine thrust reverser system, is disclosed. The thrust reverser system further comprises an isolation valve (45), a directional control valve (47), a plurality of actuators (19), and synchronization shafts (5). The sync locks (60) are capable via the synchronization shafts (5) of preventing the actuators (19) from deploying the thrust reversers of the jet engines. The sync locks (60) remain in a locked state until an independent control signal sent from the flight deck positively instructs the sync lock control valve (50) to unlock the sync locks (60), ensuring that the unlocking of the sync locks (60) corresponds to a valid thrust reverser deploy signal. The sync locks (60) each comprise a housing (65), a connection means to one of the synchronization shafts (5), a rotating jaw (75) for connection to one of the synchronization shafts (5), a sliding jaw (81), an unlock latch (106), a lock spring (87), and a manual release mechanism (99). Normally the lock spring (87) causes teeth on the sliding jaw (81) to engage teeth on the rotating jaw (75). Hydraulic pressure forces the sliding jaw (81) to move away from the rotating jaw (75) to unlock the sync locks 60.

Claims15

Dependent claims

A thrust reverser synchronization shaft lock system for a jet engine hydraulic thrust reverser synchronization shaft, the synchronization shaft lock system comprising:

(a) a signal-controllable sync lock control valve having an input port a return port and a output port, the input port being suitable for connection to a supply line and the return port being connected to a return line;
and
(b) a sync lock connected to the output port of the sync lock control valve and connected to a synchronization shaft of a jet engine thrust reverser for prohibiting the synchronization shaft from rotating, the sync lock including:
(i) a rotating jaw including a cylindrical rotor having teeth on one of its circular faces and a shaft extending outwardly from the other cylindrical face, the shaft being coupled to the synchronization shaft;
(ii) a sliding jaw including a stator having teeth on one end for engaging the teeth on the rotating jaw, the sliding jaw also including a sliding drive rod and a piston, the sliding drive rod attached at one end to the stator and at the other end to the piston;
(iii) a lock spring for applying a force to the piston to urge the teeth of the sliding jaw into engagement with the teeth of the rotating jaw;
and
(iv) a conduit for coupling the output port of the sync lock control valve to the piston such that hydraulic pressure in the conduit creates a force that urges the teeth of the sliding jaw out of engagement with the teeth of the rotating jaw.

5 more elements

A sync lock for a jet engine hydraulic thrust reverser synchronization shaft lock, the sync lock comprising:

(a) a generally cylindrical housing including a first drive passage, a jaw chamber, a second drive passage, and a piston chamber;
(b) a connector for connecting the housing to the synchronization shaft of a jet engine hydraulic thrust reverser;
(c) a rotating jaw including a cylindrical rotor and a shaft, the rotor having rotor teeth on one of its circular faces, the shaft being affixed to the rotor and extending normal to the rotor opposite the circular face having rotor teeth, and the rotating jaw being positioned within the housing such that the shaft is in the first drive chamber and extends partly into the jaw chamber and the rotor is in the jaw chamber;
(d) a sliding jaw including a cylindrical stator, a sliding drive rod, and a piston, the stator having stator teeth on one of its circular faces suitable for engaging with the rotor teeth, one end of the sliding drive rod affixed to the stator and extending normal to the stator opposite the cylindrical face having stator teeth, the other end of the sliding drive rod affixed to one end of the piston, and the sliding jaw being positioned within the housing such that the stator is in the jaw chamber, the sliding drive rod extends from the jaw chamber through the second drive passage and into the piston chamber, and the piston is in the piston chamber;
(e) a compressed lock spring mounted in the piston chamber on one side of the piston for creating a force pressing the sliding jaw in the direction of the rotating jaw;
(f) an unlock pressure port extending through the housing to the portion of the piston chamber on the side of the piston opposite the lock spring, the unlock pressure port being suitable for allowing hydraulic fluid pressure to enter the piston chamber and force the sliding jaw to compress the lock spring further causing an uncoupling of the rotor teeth and the stator teeth;
and
(g) an unlock latch for maintaining the sync lock in an unlocked position when hydraulic fluid pressure from the unlock pressure port enters the piston chamber and the lock spring is further depressed.

5 more elements

Dependencies are inferred from the claim text.

Thrust reverser synchronization shaft lock

Life of this patent

Thrust reverser synchronization shaft lock

Life of this patent

Abstract

Claims15