公开(公告)号：US20220228541A1

公开(公告)日：2022-07-21

申请号：US17580110

申请日：2022-01-20

Applicant: Airbus Operations SAS

Inventor： Alain PORTE ,  Lionel CZAPLA ,  Benjamin THUBERT

IPC: F02K3/02

Abstract: A turbofan engine with a nacelle and a flow path, in which the nacelle comprises a movable cowl that makes it possible to define a window between the flow path and the outside, veils with a first edge fixed to the movable cowl and alternately assuming a folded position or a deployed position across the flow path, and a pneumatic system displacing a second edge of the veils from the folded position to the deployed position and vice versa. The pneumatic system comprises a rigid main roll, for each veil, at least one extendable secondary roll fixed to a second edge of the veil, and a pressurization and depressurization system which, alternately, generates a pressure or a depression in each secondary roll. Replacing the reverse doors and their driving mechanisms with flexible veils and a pneumatic system allows for a weight reduction.

公开(公告)号：US11377224B2

公开(公告)日：2022-07-05

申请号：US16778950

申请日：2020-01-31

Applicant: Airbus Operations SAS

Inventor： Jean-Marc Cantin ,  Olivier Dubois

IPC: B64D33/02 ,  B64F5/10

Abstract: A system comprising a trolley which comprises a platform and wheels attached beneath the platform, an air intake of an aircraft engine, where the air intake rests on the platform so as to have its narrowest part at the top and its widest part at the bottom, and an inflatable protection item in the form of a closed envelope which is placed around the widest part of the air intake. A system of this kind makes it possible to protect the air intake from collisions that it might experience during movement of the trolley, and to increase safety by avoiding collisions between operators and the air intake.

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：US11348565B2

公开(公告)日：2022-05-31

申请号：US16664995

申请日：2019-10-28

Applicant: Airbus Operations SAS

Inventor： Florian Ravise ,  Lionel Czapla

IPC: G10K11/168 ,  G10K11/172 ,  B32B3/12 ,  B32B3/26

Abstract: An assembly forming an acoustic insulator having a first sheet, a pierced second sheet, and a plurality of first and second structures. Each first structure comprises a first and a second strip, wherein each is shaped to form half of the wall of a cage and wherein, for two successive halves, each strip comprises a facet of a joining wall. Each second structure is made up of a first and a second strip, wherein each is shaped to form half of the wall of a cone, wherein. For each strip, at least one of the wall halves of each cone is pierced. For two successive halves, each strip comprises one facet of the connecting wall. Each cone is located in a cell and each connecting wall is located between the two facets of a joining wall, and, between two adjacent first structures, a second structure is likewise fitted.

公开(公告)号：US11345479B2

公开(公告)日：2022-05-31

申请号：US16363513

申请日：2019-03-25

Applicant: Airbus Operations SAS

Inventor： Jean Geliot ,  Thomas Deforet ,  Adeline Soulie ,  Olivier Dubois

IPC: B64D27/26

Abstract: An engine attachment configured to link an engine and an aircraft pylon comprising a first end fitting having two mutually parallel wings, a joining piece positioned between the first end fitting wings and linked to the first end fitting by a link system, fixing elements, linking the first end fitting and the pylon, including first and second fixing elements positioned between the first end fitting wings which are inclined by an angle of between 10 and 45° to be able to be put in place and removed in the presence of the joining piece linked to the first end fitting by the link system. The inclined fixing elements absorb lateral loads. The joining piece and the first end fitting are linked by the link system before the engine is fixed to the pylon. The engine is fixed to the pylon by putting the fixing elements in place.

公开(公告)号：US11325715B2

公开(公告)日：2022-05-10

申请号：US16807351

申请日：2020-03-03

Applicant: Airbus Operations SAS

Inventor： Thomas Deforet ,  Rémi Lansiaux ,  Olivier Dubois ,  Anthony Mertes ,  David Alric ,  Stéphane Nogues

IPC: B64D27/26

Abstract: A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader, extending between first and second ends that has a central part connected to the support by a principal link comprising a principal rotation axis, at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops, secured to a fitting secured to the support, between which the extension is positioned.

公开(公告)号：US11325214B2

公开(公告)日：2022-05-10

申请号：US16580949

申请日：2019-09-24

Applicant: Airbus Operations SAS ,  Airbus SAS

Inventor： Jean-Marc Datas ,  Jacques Bouriquet ,  Jean-Mickael Brindeau ,  André Aquila ,  Patrick Guibert ,  Nicolas Darbonville ,  Thomas Autret

IPC: B23Q1/26

Abstract: A transport trolley for transporting a load comprising a base mounted on motorized wheels, a deck mounted to be translationally mobile on the base in a direction of translation, a first motorized system displacing the deck, a hexapod platform comprising a platform and a set of six jacks in which each is mounted articulated between the deck and the platform. The platform comprises a plurality of bearing points configured to come under the load and each bearing point takes the form of a receptacle with its opening oriented upwards. A control unit controls each motorized wheel, the first motorized system and each jack. The use of a hexapod platform makes it possible to finely position the wing at its position of fixing onto the fuselage and the use of a mobile deck supporting the hexapod platform allows for adjustability of the position despite a smaller footprint around the aircraft.

公开(公告)号：US20220139240A1

公开(公告)日：2022-05-05

申请号：US17515952

申请日：2021-11-01

Applicant: Airbus Operations SAS

Inventor： Nicolas MARCONNET

IPC: G08G5/02 ,  G08G5/00

Abstract: A system for assisting in the landing of an aircraft including a processing unit configured to: during a first phase of a landing runway approach procedure, when the aircraft flies above a predetermined height with respect to a landing runway threshold, determine a bias of position and speed information from an inertia unit of the aircraft, as a function of the merged position and speed information determined as a function of information from a receiver of ILS guidance signals and of information from a signal receiver of a satellite navigation system, then, during a second phase of the approach procedure, when the aircraft flies below the predetermined height, determine so-called adjusted aircraft position and speed information by applying, to information from the inertial unit, a correction corresponding to the bias determined during the first phase of the approach procedure.

公开(公告)号：US20220135236A1

公开(公告)日：2022-05-05

申请号：US17512188

申请日：2021-10-27

Applicant: Airbus Operations SAS

Inventor： Antoine ABELE ,  Maxime ZEBIAN

IPC: B64D13/08 ,  B64D37/32 ,  F25B13/00 ,  F25B31/02

Abstract: An aircraft having an engine, a cabin, an air conditioning system collecting the hot air from the engine, so as to treat the hot air, regulate a temperature of the hot air and send the hot air towards the cabin via a main line, an air line channeling the air leaving the cabin, and an arrangement for cooling the engine using the air thus drawn off by the air line. By drawing off the air at the outlet of the cabin, the performance of the engine is improved and the fuel consumption is reduced.

公开(公告)号：US20220106056A1

公开(公告)日：2022-04-07

申请号：US17488469

申请日：2021-09-29

Applicant: Airbus Operations SAS

Inventor： Patrick OMS

IPC: B64D41/00 ,  H02H3/33 ,  H02H1/04

Abstract: A device includes a current difference measurement module for measuring the difference between a current flowing in a positive contact of the electrical installation and a current flowing in a negative contact of the electrical installation, a low-pass filter for filtering the differential current, a full-wave rectifier without threshold module for rectifying the filtered current and a trip module for emitting a trip command when the rectified current is greater than or equal to a predetermined threshold for a predetermined duration. The device thus makes it possible to protect a DC-voltage electrical installation in a noisy environment.