公开(公告)号：US20170240288A1

公开(公告)日：2017-08-24

申请号：US15437698

申请日：2017-02-21

Applicant: Airbus Operations SAS

Inventor： Olivier PAUTIS ,  Laurent LAFONT ,  Pascal Gougeon

IPC: B64D29/06 ,  B64D27/26

CPC classification number: B64D29/06 ,  B64D27/16 ,  B64D27/26 ,  B64D2027/262 ,  B64D2027/264

Abstract: In order to reduce the size of the attachment arrangement between an aircraft engine and its attachment device, an engine assembly is provided for which the primary structure of the attachment device includes a central box and two movable structural cowls. Further the arrangement for attaching the engine on the structure comprises a group of main ties laid out in a main transverse plane for absorbing forces crossing a front end of the movable structural cowls, this group comprising three main shearing pins radially oriented and distributed around a longitudinal axis of the engine, each pin crossing a first shearing orifice provided on a fitting secured to the hub of the intermediate case on the one hand, and a second shearing orifice provided on one of the movable cowls or on its connecting structure to the central box on the other hand.

公开(公告)号：US11359542B2

公开(公告)日：2022-06-14

申请号：US17199960

申请日：2021-03-12

Applicant: Airbus Operations SAS

Inventor： Pascal Gardes ,  Fabien Menou ,  Pascal Gougeon ,  Simon Vanderbauwede

IPC: F02C6/20 ,  F02C9/18 ,  F04D29/52 ,  F02K1/72 ,  F02K1/64 ,  F02K1/70

Abstract: An engine including a motor and a nacelle and a duct between the nacelle and the motor. The nacelle includes a fixed structure, a mobile assembly that is mobile between an advanced position and a retracted position to define a window between the duct and the outside, and a plurality of blades that are mobile in rotation between a stowed position and a deployed position, each one extending on either side of its axis of rotation with a first arm and a second arm. In the stowed position, the first arm is outside the duct and the second arm is inside the nacelle, and where, in the deployed position, the first arm is across the duct and the second arm projects out of the nacelle. With such blades, the flow of air is optimally directed towards the front without it being necessary to provide cascades.

公开(公告)号：US11255293B2

公开(公告)日：2022-02-22

申请号：US16832344

申请日：2020-03-27

Applicant: Airbus Operations SAS

Inventor： Pascal Gardes ,  Frédéric Ridray ,  Benoit Orteu ,  Pascal Gougeon ,  Frédéric Piard

IPC: F02K1/72

Abstract: A turbofan with a secondary duct and including a fixed structure and a mobile assembly including a frame with openwork regions. The mobile assembly is translatable between advanced and extended positions. The openwork regions are positioned across the window in the extended position. A plurality of blocking doors is provided, each being mobile between stowed and deployed positions. An array of rams move the mobile assembly. A cascade grille mounts on the frame across the openwork region. The grille slides on the frame parallel to the translational direction. For each grille, a rear stop limits rearward movement, and a compression spring pushes the grille to the rear for abutment against a rear stop. For each grille, the fixed structure comprises a stop element against which the grille abuts upon movement from the advanced position to the extended position.