Turbofan comprising a system comprising a screen for closing off the bypass duct

Patent metadata

Field	Value
Publication number	US-11519362-B2
Application number	US-202117140707-A
Country	US
Kind code	B2
Filing date	Jan 4, 2021
Priority date	Jan 6, 2020
Publication date	Dec 6, 2022
Grant date	Dec 6, 2022

Abstract

A turbofan has a nacelle delimiting a duct for a bypass flow and comprises a fixed structure comprising a guide vane support with guide vanes, a mobile cowl able to move in translation between an advanced position and a retracted position, arms, each one being mobile in rotation between a stowed position and a deployed position and comprising a distal end and a proximal end, a flexible screen, of which an exterior edge is attached to the guide vane support rearward of the guide vanes, and wherein the distal end of each arm is fixed along the interior edge, actuators to cause the mobile cowl to move, and an operating system which moves each arm. Replacing the reversal doors and their drive mechanisms with the flexible screen and the set of rotationally-mobile arms allows a reduction in weight.

First claim

The invention claimed is:

1. A turbofan having a longitudinal direction and comprising a motor and a nacelle, surrounding the motor, which comprises a fan casing, in which a duct for a bypass flow is delimited between the nacelle and the motor and in which a flow of air flows in a flow direction, said nacelle comprising:
a fixed structure fixed to the fan casing and comprising a guide vane support bearing guide vanes,
a mobile cowl movable in translation, on the fixed structure, in a direction of translation between an advanced position in which the mobile cowl is positioned such that the mobile cowl is moved close to the fan casing and a retracted position in which the mobile cowl is positioned such that the mobile cowl is moved away from the fan casing so as to define, between the mobile cowl and the casing, an open window between the duct and the exterior of the nacelle, and facing the guide vanes,
a plurality of arms, each of the arms comprising a distal end and a proximal end which is mounted so as to be mobile in rotation on the mobile cowl about an axis of rotation parallel overall to the longitudinal direction, wherein each of the arms is mobile between a stowed position in which the arm is held against an exterior edge of the duct and a deployed position in which the arm extends across the duct,
a flexible screen formed as a portion of an annulus with an exterior edge having a large radius and an interior edge having a small radius, wherein the exterior edge is attached to the guide vane support rearward of the guide vanes, and wherein the distal end of each arm is fixed along the interior edge,
a set of actuators configured to cause the mobile cowl to move between the advanced position and the retracted position, and vice versa, and
an operating system configured to move each of the arms from the stowed position to the deployed position when the mobile cowl passes from the advanced position to the retracted position, and to move each of the arms from the deployed position to the stowed position when the mobile cowl passes from the retracted position to the advanced position.

2. The turbofan according to claim 1 , wherein the flexible screen is made up of a structure of flexible mesh to which a flexible skin is attached.

3. The turbofan according to claim 1 , wherein, between the proximal end and the distal end, each of the arms comprises a guide groove which extends between the distal and proximal ends and in which there slides at least one slider secured to the flexible screen.

4. The turbofan according to claim 1 , wherein the nacelle comprises a plate formed as a portion of an annulus, secured to the mobile cowl and on which the arms are rotatably mounted.

5. The turbofan according to claim 4 , wherein the nacelle comprises a guide secured to the mobile cowl, which is situated rearward of the guide vanes in the retracted position, and on which the flexible screen slides.

6. The turbofan according to claim 1 , wherein the operating system comprises:
a cam secured to one of the arms and having a tooth,
a groove on the fixed structure and in which the tooth is received, and
wherein, when the mobile cowl moves, the tooth follows the groove and rotates the arm secured to the tooth, and
for each of the arms, a transmission system which transmits the movement of the arm to a next arm.

7. The turbofan according to claim 6 , wherein the transmission system comprises, for two adjacent arms of the plurality of arms, a connecting rod mounted articulated between said two adjacent arms, and wherein a point of articulation of the connecting rod to each of the two adjacent arms is offset with respect to the axis of rotation of the two adjacent arms.

8. An aircraft comprising at least one turbofan according to claim 1 .

Assignees

• Airbus Operations Sas

Inventors

• Czapla Lionel
• Thubert Benjamin
• Le Fanic Julien

Classifications

• F05D2260/56

  using cams or eccentrics · CPC title

• F05D2300/601

  Fabrics · CPC title

• F05D2250/34

  translated · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• F02K1/72 Primary

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