公开(公告)号：US11548659B2

公开(公告)日：2023-01-10

申请号：US16195977

申请日：2018-11-20

Applicant: AIRBUS OPERATIONS GMBH

Inventor： Peter Linde ,  Albrecht Kluge

IPC: B64F5/10 ,  B64C1/14 ,  B29C65/00 ,  B29C65/44 ,  B29C65/16 ,  B23K13/02 ,  B23K20/10 ,  B23K26/24 ,  B29L31/30 ,  B29L31/00 ,  B29C65/08 ,  B29C65/46 ,  B23K101/24

Abstract: A method for producing a frame component for a door frame structure of an aircraft. A connecting zone is generated on a first and a second assembly surface of a connecting component in each case by generating a surface texture on the assembly surfaces, wherein the connecting component is formed from a metal material. The assembly surfaces of the connecting component are placed against a door frame member and against an attachment member, wherein the door frame member and the attachment member are each formed from a fiber-reinforced thermoplastics material. Furthermore, the connecting component and the door frame member are welded, and the connecting component and the attachment member are welded. A frame component and a door frame structure are also described.

公开(公告)号：US12060157B2

公开(公告)日：2024-08-13

申请号：US17853265

申请日：2022-06-29

Applicant: AIRBUS OPERATIONS GMBH

Inventor： Markus Müller ,  Albrecht Kluge

IPC: B64D37/30 ,  B64D37/06 ,  F17C13/08 ,  B60K15/03

CPC classification number: B64D37/30 ,  B64D37/06 ,  F17C13/086 ,  B60K2015/03065 ,  F17C2201/0109 ,  F17C2201/054 ,  F17C2201/056 ,  F17C2203/012 ,  F17C2203/014 ,  F17C2203/032 ,  F17C2203/0391 ,  F17C2203/0629 ,  F17C2203/0663 ,  F17C2221/012 ,  F17C2223/0169 ,  F17C2223/033 ,  F17C2260/033 ,  F17C2270/0189

Abstract: A mount for a double-walled vessel includes a first support to support the mount against an outer wall of the double-walled vessel, a second support to support the mount against an inner wall of the double-walled vessel, and a flexible member connecting the first support and the second support. The first support and can be arranged at a first end of the flexible member and the second support can be arranged at a second end of the flexible member opposite to the first end. Further described are a vessel including at least one such mount as well as a vehicle including such vessel.

公开(公告)号：US20190193344A1

公开(公告)日：2019-06-27

申请号：US16214737

申请日：2018-12-10

Applicant: Airbus Operations GmbH

Inventor： Claus Hanske ,  Benjamin Leohold ,  Remo Hinz ,  Albrecht Kluge

IPC: B29C70/34 ,  B29C70/44 ,  B29C37/00 ,  B29C33/38

CPC classification number: B29C70/342 ,  B29C33/38 ,  B29C33/3828 ,  B29C37/005 ,  B29C70/40 ,  B29C70/446

Abstract: A tool for use in consolidation of a fibre-reinforced component has an outer casing supported by an internal structure. The outer casing has a first contact surface, which is provided for the purpose of resting flat against the component during the consolidation of the component and predetermining a shape of the component in some section or sections. The internal structure and the outer casing are configured in such a way that, when the tool is heated from an initial temperature to a consolidation temperature required for the consolidation of the component, the tool expands in such a way perpendicularly to the first contact surface that a defined first pressure is exerted on the component by the first contact surface. The use of a component of this kind is furthermore claimed and described.

公开(公告)号：US20190030646A1

公开(公告)日：2019-01-31

申请号：US16044841

申请日：2018-07-25

Applicant: Airbus Operations GmbH

Inventor： Albrecht Kluge ,  Peter Linde

IPC: B23K26/36 ,  G02B6/42 ,  B23K26/00 ,  B23K26/064 ,  B23K26/08 ,  B32B3/02 ,  B32B27/08 ,  B32B7/04 ,  B32B3/26

Abstract: A device for reducing a stress concentration at an edge of a laminated composite material has an optical element, an actuator element, and a receptacle space for a first component of a laminated composite material which can be or is connected to a second component via a contact face and has an edge element above the contact face. The optical element defines a focus face for laser radiation for vaporizing laminated composite material. The actuator element is designed to move the optical element around a first component arranged in the receptacle space. and orients the optical element in such a way that an angle, including the first component, between the contact face and the focus face is smaller than 90°. The angle is selected such that after vaporization of the laminated composite material at the focus face the stress concentration at the edge element is reduced under load.