Engine with a thrust reverser lockout mechanism

Patent metadata

Field	Value
Publication number	US-10344710-B2
Application number	US-201314888811-A
Country	US
Kind code	B2
Filing date	Jun 7, 2013
Priority date	Jun 7, 2013
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

A turbofan engine having a thrust reverser having at least one movable control surface, movable to and from a reversing position where at least a portion of the bypass air flow is at least partially reversed, a thrust reverser actuation system having multiple actuators and a lockout mechanism movable between an inhibit condition, wherein movement of the multiple actuators is prevented, and a permit condition, wherein movement of the multiple actuators is permitted.

First claim

What is claimed is:

1. A turbofan engine, comprising:
a turbine engine;
a nacelle surrounding the turbine engine and defining an annular bypass duct between the nacelle and the turbine engine and extending through the turbofan engine to define a generally forward-to-aft bypass air flow path;
a thrust reverser having at least one movable control surface, movable to and from a reversing position where at least a portion of the bypass air flow is at least partially reversed;
a thrust reverser actuation system having multiple actuators and a synchronization mechanism to synchronize the multiple actuators, with at least one of the multiple actuators, comprising,
a housing;
a rotatable lead screw having one end defining a first axial end surface of the rotatable lead screw located within the housing; and
a piston operably coupled to the rotatable lead screw and driven thereby between an extended position and a retracted position and where the piston is operably coupled to the at least one movable control surface to move the at least one movable control surface into and out of the reversing position; and
a lockout mechanism having a lockout piston, axially adjacent to the rotatable lead screw, having a second axial end surface selectively coupled to the first axial end surface of one end of the rotatable lead screw within the housing and axially movable between an inhibit condition, wherein rotation of the rotatable lead screw is prevented by engagement of the first and second axial end surfaces and movement of the multiple actuators is prevented, and a permit condition, wherein rotation of the rotatable lead screw is permitted by disengagement of the first and second axial end surfaces and movement of the multiple actuators is permitted, the lockout mechanism also including a handle operably coupled to axially move the lockout piston through a rotatable link and configured to move between a first position where the lockout mechanism is in the permit condition and a second position where the lockout mechanism is in the inhibit condition.

2. The turbofan engine of claim 1 wherein the lockout mechanism further comprises a biasing element to resist movement of the handle to the second position.

3. The turbofan engine of claim 1 wherein the synchronization mechanism includes a worm gear shaft operably coupled to the lead screw via a worm wheel.

4. The turbofan engine of claim 1 , further comprising a door located adjacent the handle and moveable between a closed position and an opened position wherein access to the handle is provided.

5. The turbofan engine of claim 4 wherein when the door is moved to the closed position it contacts the handle to move the lockout mechanism to the permit condition.

6. The turbofan engine of claim 1 wherein the lockout mechanism locks out each of the multiple actuators operably coupled to the synchronization mechanism.

7. The turbofan engine of claim 1 wherein the rotatable link is rotatable to an over-center position when the handle is moved to the second position.

8. The turbofan engine of claim 7 wherein the lockout mechanism further comprises a biasing element to bias the lockout piston to the over-center position.

9. The turbofan engine of claim 1 , further comprising a door located adjacent the handle and moveable between a closed position and an opened position wherein access to the handle is provided and wherein when the door is moved to the closed position it contacts the handle to move the handle to the first position and the lockout mechanism to the permit condition.

10. A turbofan engine comprising:
a turbine engine;
a nacelle surrounding the turbine engine and defining an annular bypass duct between the nacelle and the turbine engine and extending through the turbofan engine to define a generally forward-to-aft bypass air flow path;
a thrust reverser having at least one movable control surface, movable to and from a reversing position where at least a portion of the bypass air flow is at least partially reversed;
a thrust reverser actuation system having multiple actuators with each actuator having an extendable and retractable portion operably coupled to the at least one movable control surface to move the at least one movable control surface into and out of the reversing position and a synchronization mechanism to synchronize the multiple actuators;
a lockout mechanism selectively coupled to the extendable and retractable portion of one of the multiple actuators and movable between an inhibit condition, wherein movement of the multiple actuators is prevented, and a permit condition, wherein movement of the multiple actuators is permitted, the lockout mechanism comprising:
an axially moveable lockout piston having a first axial end surface;
a rotatable lead screw, axially adjacent to the lockout piston, with having one end defining a second axial end surface of the rotatable lead screw, the rotatable lead screw being selectively coupled to and decoupled from the lockout piston by engagement and disengagement of the first and second axial end surfaces caused by axial movement of the lockout piston; and
a handle for moving the lockout piston of the lockout mechanism axially between the inhibit condition and the permit condition by for moving the lockout piston into engagement with the second axial end surface of one end of the rotatable lead screw when the lockout mechanism is in the inhibit condition; and
a door located adjacent the handle and moveable between a closed position and an opened position, wherein upon moving the door to the closed position, the door contacts the handle to axially move the lockout piston of the lockout mechanism to the permit condition and axially move the lockout piston out of engagement with the second axial end surface of one end of the rotatable lead screw.

11. The turbofan engine of claim 10 wherein the handle is operably coupled to the lockout piston through a rotatable link that is rotatable to an over-center position when the handle is moved to the second position.

12. The turbofan engine of claim 11 wherein the lockout mechanism further comprises a biasing element to bias the lockout piston to the over-center position.

13. The turbofan engine of claim 10 wherein the handle is moveable between a first position where the lockout mechanism is in the permit condition and a second position where the lockout mechanism is in the inhibit condition.

Assignees

• Ge Aviation Systems Llc

Inventors

• Willett Kenneth R
• Ozanich Brent Michael
• Conway George Arnold
• Spiry Jonathan L
• Beck Daniel Peter
• Larkin Jeffrey Michael

Classifications

• F02K1/72

  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow · CPC title

• F02K1/766 Primary

  with blocking systems or locking devices; Arrangement of locking devices for thrust reversers · CPC title

• F05D2260/02

  Transport and handling during maintenance and repair · CPC title