Thrust reverser for an aircraft jet engine

Patent metadata

Field	Value
Publication number	US-9458793-B2
Application number	US-201314048206-A
Country	US
Kind code	B2
Filing date	Oct 8, 2013
Priority date	Apr 14, 2011
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

An assembly includes a suspension pylon and a thrust reverser which has vanes for deflecting flow and a cowl able to move between an open position and a closed position by an actuator. The thrust reverser further includes rails able to slide in slideways. In particular, the actuator is disposed in line with a corresponding rail. The actuator may be an actuator having a rotating nut connected to an endless screw or an actuator suitable for pulling on the corresponding rail or on the corresponding slideway.

First claim

What is claimed is:

1. An assembly comprising a suspension pylon and a thrust reverser comprising vanes for deflecting an air flow and a cowl able to move between an open position releasing said vanes and a closed position covering said vanes and furthermore comprising rails able to slide in slideways, the rails being mounted on said cowl or on either side of the suspension pylon, and the slideways being mounted on either side of the suspension pylon or on said cowl,
wherein the thrust reverser comprises at least one actuator able to slide the cowl between the open and closed positions, the at least one actuator being disposed along a sliding axis and in line with a corresponding rail such that forces exerted by the at least one actuator are exerted directly along the sliding axis of the corresponding rail, said at least one actuator being:
either an actuator having a rotating nut connected to an endless screw, for sliding the corresponding rail or a corresponding slideway,
or an actuator suitable for pulling on the corresponding rail or on the corresponding slideway.

2. The assembly according to claim 1 , wherein the slideways or the rails, are formed on a profile fixed to the suspension pylon forming a base of the suspension pylon, or on the suspension pylon.

3. The assembly according to claim 2 , wherein the actuator having the rotating nut is connected to an upstream end of the corresponding rail of the cowl or the corresponding slideway.

4. The assembly according to claim 3 , wherein each rotating nut is driven by a dedicated driving motor.

5. The assembly according to claim 1 , the rotating nut engaged with said endless screw is able to rotate around a longitudinal axis of the thrust reverser under an action of a driving motor, the endless screw being capable of translating along said longitudinal axis, the endless screw's movement being provided by the rotation of said rotating nut.

6. The assembly according to claim 5 , wherein an assembly formed by the driving motor and the rotating nut is mounted in a profile fixed to the suspension pylon or the assembly is mounted in the suspension pylon.

7. The assembly according to claim 5 , wherein an assembly formed by the endless screw and the driving motor is mounted on the cowl.

8. The assembly according to claim 5 , wherein a single driving motor is capable of driving the nuts of several actuators.

9. The assembly according to claim 1 , wherein each actuator capable of pulling on the corresponding rail or on the corresponding slideway to slide the cowl between the open and closed positions comprises at least one upstream pulley and one downstream pulley respectively mounted on either side of the corresponding rail or the corresponding slideway, each pulley being capable of rotating along an axis that is perpendicular to a longitudinal axis of a nacelle under an action of at least one driving motor, and a movement transmission element suitable for transmitting rotational movement from the pulleys to said rail or to said slideway.

10. The assembly according to claim 9 , wherein the at least one upstream pulley and the at least one downstream pulley and the at least one driving motor are mounted in a profile fixed to the suspension pylon or directly to the suspension pylon.

11. The assembly according to claim 9 , wherein the at least one pulley and the at least one driving motor are mounted in the cowl.

12. The assembly according to claim 9 , wherein a single driving motor is capable of driving the at least one upstream pulley and/or the at least one downstream pulley of several actuators.

13. The assembly according to claim 9 , wherein the at least one driving motor indifferently drives the at least one upstream pulley or the at least one downstream pulley of one and/or several actuators.

14. The assembly according to claim 1 , wherein the cowl is a single piece.

15. An assembly comprising a suspension pylon and a thrust reverser, the thrust reverser comprising:
vanes for deflecting an air flow;
a cowl able to move between an open position releasing said vanes and a closed position covering said vanes by at least one actuator; and
rails able to slide in slideways, the rails being mounted on said cowl or on either side of the suspension pylon, and the slideways being mounted on either side of the suspension pylon or on said cowl,
wherein the at least one actuator is disposed along a sliding axis and in line with a corresponding rail such that forces exerted by the at least one actuator are exerted directly along the sliding axis of the corresponding rail, and the slideways or the rails are formed on either side of lateral ends of a part mounted on the suspension pylon.

Assignees

• Aircelle Sa

Inventors

• Dezeustre Nicolas
• Kerbler Olivier
• Hurlin Herve
• Moradell-Casellas Pierre

Classifications

• F02K1/64

  Reversing fan flow · CPC title

• F05D2250/34

  translated · CPC title

• F02K1/625

  the aft end of the engine cowling being movable to uncover openings for the reversed flow · CPC title

• F02K1/72

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

• Y02T50/672

  Cross-Sectional Technologies · mapped topic