Turbofan comprising a system comprising flexible screens for closing off the bypass duct

Patent metadata

Field	Value
Publication number	US-11242821-B2
Application number	US-202117140717-A
Country	US
Kind code	B2
Filing date	Jan 4, 2021
Priority date	Jan 6, 2020
Publication date	Feb 8, 2022
Grant date	Feb 8, 2022

Abstract

A turbofan having a nacelle delimiting a duct for a bypass flow and including a fixed structure including a guide vane support with guide vanes, a mobile cowl movable in translation between an advanced position and a retracted position, arms, each one being mobile in rotation on the guide vane support between a stowed position and a deployed position and comprising a distal end and a proximal end, for each pair of adjacent arms, a flexible screen extending angularly between the two arms, and of which an exterior edge is attached to the guide vane support, and wherein the distal end of each arm is fixed along the interior edge, a link rod mounted articulated between the distal ends, actuators to cause the mobile cowl to move, and an operating system which moves each arm. Such an arrangement 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 an extended 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 them, an open window between the duct and the exterior of the nacelle, and facing the guide vanes,
a plurality of arms, each one comprising a distal end and a proximal end which is mounted so as to be mobile in rotation on the guide vane support about an axis of rotation parallel overall to the longitudinal direction, wherein each arm is mobile between a stowed position in which the arm is outside the duct and a deployed position in which the arm is across the duct,
for each pair of adjacent arms, a flexible screen extending angularly between each pair of adjacent arms and 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 of the pair of adjacent arms is fixed along the interior edge of the flexible screen,
for each pair of adjacent arms, a link rod, of which a first end is mounted articulated to the distal end of one of the arms of the pair and a second end is mounted articulated to the distal end of the other arm of the same pair,
a set of actuators causing the mobile cowl to move between the advanced position and the extended position, and vice versa, and
an operating system configured to move each arm from the stowed position to the deployed position when the mobile cowl passes from the advanced position to the extended position, and to move each arm from the deployed position to the stowed position when the mobile cowl passes from the extended 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 arm comprises a guide groove which extends between the proximal and distal 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 guide vane support and on which the arms are rotatably mounted.

5. The turbofan according to claim 1 , wherein the operating system comprises: a cam secured to one of the arms of the pair of adjacent arms, the cam having a tooth, the mobile cowl having a groove 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 arm, a transmission system which transmits the movement of the arm to the adjacent arm.

6. The turbofan according to claim 5 , wherein the transmission system comprises, for two adjacent arms, a connecting rod mounted articulated between said two arms, and wherein a point of articulation of the connecting rod to each arm is offset with respect to the axis of rotation of the arm.

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

Assignees

• Airbus Operations Sas

Inventors

• Czapla Lionel
• Thubert Benjamin
• Le Fanic Julien

Classifications

• 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

• F02K1/763

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

• B64D29/06

  Attaching of nacelles, fairings or cowlings · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• B64D29/02

  associated with wings · CPC title