公开(公告)号：US20240424684A1

公开(公告)日：2024-12-26

申请号：US18734340

申请日：2024-06-05

Applicant: Airbus SAS ,  Airbus Operations S.L. ,  Airbus Operations GmbH

Inventor： Wladislav LAGUTIN ,  Juan Francisco GARCIA AMADO ,  Boris MORINIERE

IPC: B25J11/00

Abstract: A painting device including at least one guide system, at least a first movable support configured to move along the guide system, a robotic arm secured to the first movable support, at least a first tool connected to the free end of the robotic arm, and at least a first piece of equipment connected to the first tool by at least one umbilical connection, the first piece of equipment being movable and connected to the first movable support. This configuration makes it possible to reduce the length of the umbilical connection. A painting installation having at least one such painting device is also provided.

公开(公告)号：US20240424517A1

公开(公告)日：2024-12-26

申请号：US18751620

申请日：2024-06-24

Applicant: Airbus SAS ,  Airbus Operations S.L. ,  Airbus Operations GmbH

Inventor： Wladislav LAGUTIN ,  Juan Francisco GARCIA AMADO ,  Boris MORINIERE

IPC: B05B16/80 ,  B05B16/40

Abstract: A painting system suitable for painting a fuselage of an aircraft, including a paint booth which is positioned on a platform. This paint booth includes at least first and second lateral openings which are configured to permit the wings of the aircraft to pass through the paint booth, in addition to at least two elements, at least one thereof being mobile between an adjacent position corresponding to a closed state of the paint booth in which the two elements are joined together, in addition to a spaced-apart position corresponding to an open state of the paint booth in which the fuselage can be positioned between the two elements.

公开(公告)号：US12162245B2

公开(公告)日：2024-12-10

申请号：US18489143

申请日：2023-10-18

Applicant: Airbus Operations SAS ,  Airbus Operations S.L.

Inventor： Richard Murillo ,  Matilde De La Mota Mendiola ,  Nathan Lagache

IPC: B32B3/10 ,  B32B3/08 ,  B32B5/02 ,  B32B15/092 ,  B32B15/14 ,  B32B27/12 ,  B32B27/38 ,  B32B37/18 ,  B32B38/00 ,  B64C1/12 ,  B64F5/10 ,  H01B5/16

Abstract: A resin film configured to hold a conductive metallic track against a panel. The resin film partially covers the conductive metallic track, such that the conductive metallic track has at least one region which does not have the resin film, so as to allow an electrical connection by contact. Thus, in the context of assembly on a panel, the metallic track incorporated between the panel and the resin film is protected, thus rendering this technical solution particularly robust. Furthermore, the resin film electrically insulates the metallic track from surrounding elements, and the regions which do not have resin film allow an electrical connection by contact.

公开(公告)号：US11952134B2

公开(公告)日：2024-04-09

申请号：US17737134

申请日：2022-05-05

Applicant: Airbus SAS ,  Airbus Operations SAS ,  Airbus Operations GmbH ,  Airbus Operations S.L.

Inventor： Jorge Carretero Benignos ,  Benedikt Bammer ,  Olivier Verseux ,  Maria Del Sagrario Juanas Fernandez ,  Jorge Molano Rembiasz ,  Thomas Scherer ,  Alexander Solntsev

IPC: B64D27/24 ,  B64D33/08

CPC classification number: B64D27/24 ,  B64D33/08

Abstract: An electric propulsion unit of an aircraft including a nacelle housing an electric power system, an electric motor and a cooling system for the electric power system; the nacelle including a central fairing, a front fairing which extends from the central fairing to a front end and a rear fairing which extends from the central fairing to a rear end. The front fairing includes a protrude positioned in a lower part of the front fairing, the protrude having a front face in a transverse plane, a main air inlet of the cooling system being positioned on the front face.

公开(公告)号：US11745848B2

公开(公告)日：2023-09-05

申请号：US16999198

申请日：2020-08-21

Applicant: AIRBUS OPERATIONS S.L.

Inventor： Raul Olmo Mora ,  Tamara Blanco Varela

IPC: B64C1/40 ,  B29C70/22 ,  B32B5/02 ,  G10K11/168 ,  B29K307/04 ,  B29K309/08 ,  B64C1/00

CPC classification number: B64C1/40 ,  B29C70/228 ,  B32B5/024 ,  G10K11/168 ,  B29K2307/04 ,  B29K2309/08 ,  B32B2250/03 ,  B32B2250/05 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/102 ,  B32B2605/18 ,  B64C2001/0072

Abstract: A sound wave absorbing laminate composite material structure for an aircraft including stacked plies of a hybrid composite material, wherein each of the hybrid composite material plies includes first polymer material tows parallel to a warp direction, second polymer material tows parallel to a weft direction, and sound absorbent material tows parallel to the warp direction, wherein the first and second polymer material tows carbon or glass fiber reinforcing polymer.

公开(公告)号：US11643222B2

公开(公告)日：2023-05-09

申请号：US16502436

申请日：2019-07-03

Applicant: Airbus Operations, S.L.

Inventor： Francisco Javier Honorato Ruiz ,  Jesús Javier Vázquez Castro ,  Enrique Guinaldo Fernández ,  Carlos García Nieto ,  Iker Vélez De Mendizábal Alonso

IPC: B64F5/10 ,  B64C3/18 ,  B29L31/30 ,  B64C9/02

CPC classification number: B64F5/10 ,  B64C3/187 ,  B29L2031/3085 ,  B64C9/02

Abstract: A method for manufacturing the trailing edge ribs and the bearing ribs of trailing edges of aircraft lifting surfaces, in which the trailing edge ribs and the bearing ribs are made by joining simple C-shaped parts and/or simple L-shaped parts so as to obtain the final trailing edge ribs and bearing ribs. The manufacturing of the simple C-shaped parts uses the same tooling both for the trailing edge ribs and the bearing ribs, and the manufacturing of the simple L-shaped parts uses the same tooling both for the trailing edge ribs and the bearing ribs.

公开(公告)号：US11623752B2

公开(公告)日：2023-04-11

申请号：US16916549

申请日：2020-06-30

Applicant: Airbus Operations S.L.

Inventor： Angel Garcia Zuazo ,  Serafin Escudero Fraile ,  Esteban Martino-Gonzalez ,  Juan Tomas Prieto Padilla ,  Diego Barron Vega

IPC: B64D13/06 ,  B64D13/02 ,  B64D13/08 ,  F02C6/04 ,  F02C6/08 ,  F02C7/18 ,  B64D27/12 ,  B64D41/00

Abstract: An aircraft installation of a pneumatic system of an aircraft with different compressed air sources for supplying pressurized air to air consumer equipment. Either an air bleed system, electrical compressors, or a combination thereof may perform such supplying of compressed air depending on the aircraft operation condition, for instance the flight altitude or specific flight phases. Also, a turbofan engine, and a method for supplying compressed air to air consumer equipment are disclosed.

公开(公告)号：US20230024567A1

公开(公告)日：2023-01-26

申请号：US17867911

申请日：2022-07-19

Applicant: Airbus Operations S.L.

Inventor： Asuncion BUTRAGUENO-MARTINEZ ,  Veronica BARCELO CASTELLO ,  Matilde DE LA MOTA MENDIOLA ,  Jesus Javier VAZQUEZ CASTRO

IPC: B29C70/34

Abstract: A method for manufacturing an aeronautical panel with improved impact and damping behaviors. The method is applicable not only to flat panels but also to curved or highly curved panels, whatever their size and the shape of their core. The manufactured sandwich panels comprise dry fiber mats made from fabric material and/or non-crimp fabric material. In a particular embodiment, the fabric material and/or the non-crimp fabric material comprise dry fibers which are recycled and/or reused fibers.

公开(公告)号：US20230014715A1

公开(公告)日：2023-01-19

申请号：US17861371

申请日：2022-07-11

Applicant: Airbus Operations S.L.

Inventor： Cesar MARTIN BLAZQUEZ ,  Carlos FLORES HERNANDEZ

IPC: B64F5/10 ,  B64C1/06

Abstract: A method for the assembly of frames in an aircraft shell, wherein the aircraft shell comprises a skin and a plurality of stringers co-cured with the skin, wherein the skin has a plurality of reference marks. Identifying the reference marks on the skin using a first robot with artificial vision, establishing a local reference for the positioning of each frame based on a reference mark, grabbing a frame using the first robot, establishing a relative position between the first robot and the frame based on the reference mark, positioning the frame on an inner side of the aircraft shell using the first robot, and with a second robot, drilling holes through the frame and skin, and attaching the frame to the skin with fasteners.

公开(公告)号：US11555448B2

公开(公告)日：2023-01-17

申请号：US16440301

申请日：2019-06-13

Applicant: Airbus Operations S.L.

Inventor： Carlos Casado-Montero ,  Pio Fernandez-Lopez

IPC: F02C7/057 ,  B64D13/02 ,  B64D33/02 ,  B64D13/06

Abstract: An air intake system comprising an air duct suitable for providing airflow to the inside of an aircraft, preferably to an auxiliary power unit; an inlet arranged at one end of the air duct; a skin surrounding the inlet; a plurality of slots arranged on the skin; a driving arrangement, a flap door connected to the driving arrangement, and a plurality of fins connected to the driving means. The driving arrangement is configured for moving the flap door between at least two positions, the positions being a closed position wherein the flap door closes the inlet, and an opened position wherein the flap door is driven away from the closed position. The driving arrangement is also configured for moving the plurality of fins such that the plurality of fins protrudes through the slots.