System for actuating a panel of a turbojet engine nacelle

Patent metadata

Field	Value
Publication number	US-10774786-B2
Application number	US-201916257765-A
Country	US
Kind code	B2
Filing date	Jan 25, 2019
Priority date	Jul 25, 2016
Publication date	Sep 15, 2020
Grant date	Sep 15, 2020

Abstract

A pod for a turbojet engine includes an outer cowl having a structure with at least one opening and a panel pivotably mounted about an axis between a closed position and an open position, and a system for actuating the panel designed to lock the panel in closed position and to move same between the closed position and the open position thereof. The actuation system includes a lateral connecting rod connected to the panel and to the structure, pivoting relative to the structure about a first pivoting axis and about a second pivoting axis, and a linear actuator attached to the lateral connecting rod. The actuator system is designed to move the lateral connecting rod during the extension of the actuator, and the lateral connecting rod exerts a force on the panel during the movement thereof, pivoting the panel about the axis thereof.

First claim

What is claimed is:

1. A nacelle for an aircraft turbojet engine, the nacelle comprising:
an outer cowling comprising:
a structure comprising at least one aperture; and
at least one panel pivotally mounted about an axis between a closed position that obstructs said at least one aperture and an open position in which part of a secondary air flow, flowing through an annular channel defined between said outer cowling and an inner fixed structure of the nacelle defining a fairing of the turbojet engine passes through the at least one aperture; and
an actuation system that locks the at least one panel in said closed position and displaces said at least one panel between said closed position and said open position, the actuation system comprising:
at least one lateral tie rod connected on one side to the at least one panel and connected to the structure of the outer cowling on another side, said at least one lateral tie rod being pivotally mounted relative to the structure of the outer cowling at a first location about a first pivot axis substantially parallel to a longitudinal axis of the nacelle and about a second pivot axis substantially perpendicular to the first pivot axis at a second location different than the first location; and
a linear actuator attached to said at least one lateral tie rod, the linear actuator extendable between a retracted position and an extended position, wherein the actuation system displaces the at least one lateral tie rod during extension of said linear actuator, causing the at least one lateral tie rod to pivot about said first and said second pivot axes, and so that the at least one lateral tie rod, bearing on the structure, exerts, during its displacement, a force on the at least one panel, causing a pivoting of said at least one panel about its axis.

2. The nacelle according to claim 1 , wherein the linear actuator is attached to the at least one lateral tie rod by a movement transmission device comprising: a yoke attached to the at least one panel and pivotally mounted about a vertical axis, a movable rod of the linear actuator being attached to said yoke; and a spider mounted to a second end of the at least one lateral tie rod via a ball joint connection.

3. The nacelle according to claim 2 , wherein the linear actuator and the movement transmission device are located in an inner space of the at least one panel.

4. The nacelle according to claim 1 , wherein the at least one panel is further mounted free in translation along an axis parallel to the longitudinal axis of the nacelle, wherein the actuation system drives the at least one panel from a downstream position to an upstream position of the nacelle when the at least one panel passes from the closed position to the open position.

5. The nacelle according to claim 4 , wherein at least one side wall of the at least one panel includes an oblong hole having a roller secured to the structure of the outer cowling such that the at least one panel is movable in translation along the axis parallel to the longitudinal axis of the nacelle, wherein the actuation system comprises a longitudinal tie rod having a first end connected to said structure of the outer cowling and a second end connected to a yoke of a movement transmission device.

6. The nacelle according to claim 4 , wherein at least one side wall of the at least one panel includes a rail receiving a ball joint or a slider secured to the structure of the outer cowling such that the at least one panel is movable in translation along the axis substantially parallel to the longitudinal axis of the nacelle, wherein the actuation system comprises a longitudinal tie rod having a first end connected to said structure of the outer cowling and a second end connected to a yoke of a movement transmission device.

7. The nacelle according to claim 1 , wherein a first end of the at least one lateral tie rod is connected to the structure of the outer cowling via a yoke pivotally mounted about the first pivot axis.

8. The nacelle according to claim 7 , wherein the at least one lateral tie rod is further pivotally mounted relative to the yoke about the second pivot axis.

9. The nacelle according to claim 1 , wherein the at least one panel includes an opening profiled on at least one side wall of the at least one panel, and the at least one lateral tie rod passes through said opening.

10. The nacelle according to claim 1 , wherein the linear actuator is attached to an upstream wall of the at least one panel.

11. The nacelle according to claim 1 , wherein the actuation system is one of two actuation systems that are symmetrical relative to an axis of symmetry of the at least one panel, each of the two actuation systems comprising a hydraulic, electrical, or aeraulic actuation motor.

12. The nacelle according to claim 1 , wherein the at least one panel is further translated in a direction parallel to the longitudinal axis of the nacelle, and the actuation system alternately drives the at least one panel between a downstream position to an upstream position of the nacelle when the at least one panel passes from the closed position to the open position.

13. The nacelle according to claim 1 , wherein the at least one panel is a panel of a secondary air flow ejection nozzle.

14. The nacelle according to claim 1 , wherein the outer cowling forms a sliding cowl of a thrust reverser device.

Assignees

• Safran Nacelles

Inventors

• Gonidec Patrick
• Chapelain Loïc
• Bouabdallah Faycel

Classifications

• F02K1/1207 Primary

  of one series of flaps hinged at their upstream ends on a fixed structure (F02K1/1215 - F02K1/1292 take precedence) · CPC title

• F05D2250/42

  with two degrees of freedom · CPC title

• F02K1/763 Primary

  with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title

• F05D2260/57

  using servos, independent actuators, etc. · CPC title

• F02K1/06

  Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K1/30) · CPC title