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公开(公告)号：US20250002175A1
公开(公告)日：2025-01-02
申请号：US18740136
申请日：2024-06-11
Applicant: Airbus Operations GmbH
Inventor： Andreas POPPE , Hermann BENTHIEN
Abstract: A connector for truss work members to a support structure for a mounting interface of a trusswork. The connector has a body with a first portion and a second portion. A central opening is provided in the body having an inner wall configured for receiving a connection end of a truss member. The first portion and the second portion are arranged concentrically. The first portion has first circumferential edge sections, and the second portion has second circumferential edge sections. The first and second circumferential edge sections are spaced apart by gap sections that are configured to receive connecting flanges of a support structure. The gap sections are forming segments along a virtual surface that is curved at least in one direction.
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公开(公告)号：US20240400208A1
公开(公告)日：2024-12-05
申请号：US18677348
申请日：2024-05-29
Applicant: Airbus Operations GmbH
Inventor： Hermann BENTHIEN , Andreas POPPE
Abstract: A mounting rail interface comprises an elongate body. The body comprises two elongate lateral portions; and an elongate central portion arranged between the two lateral portions. The lateral portions are defined for providing a transition portion to an adjacent surface. The central portion comprises a plurality of openings with a respective circumferential edge flange. The openings are defined as elongate openings configured to allow a range of different orientations of a connector. The edge flange is defined with a concave curved contour on its bottom side. The concave curved contour provides an abutting surface for a connector configured to engage with the edge flange of the opening. The curved contour provides an abutting surface over at least an angular range.
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公开(公告)号：US20230264802A1
公开(公告)日：2023-08-24
申请号：US18172645
申请日：2023-02-22
Applicant: Airbus Operations GmbH
Inventor： Hermann BENTHIEN , Andreas POPPE
CPC classification number: B64C1/066 , F16F1/3732 , F16B5/02
Abstract: A connection assembly for connecting a first element to a second element is provided. The connection assembly has a male element and a female element. The female element has a barrel nut. The barrel nut has a conical inner portion positioned at a first longitudinal region and a cylindrical inner portion positioned at a second longitudinal region. The barrel nut has a first engaging element portion and a first plain portion arranged alternatingly around a circumferential direction of the barrel nut. The male element has a cylindrical bolt-like shape and has a second engaging element portion and a second plain portion arranged alternatingly around a circumferential direction of the male element. The male element further has flattened sides at the second plain portion. The second engaging element portion of the male element is configured to engage with a respective one of the first engaging element portion of the barrel nut.
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公开(公告)号：US20190193871A1
公开(公告)日：2019-06-27
申请号：US16222457
申请日：2018-12-17
Applicant: Airbus Operations GmbH
Inventor： Hermann BENTHIEN
CPC classification number: B64F5/00 , B64D11/003 , F16B33/00
Abstract: A system has a frame with first and second spaced apart edges, a first holder couplable to the fuselage structure and embodied for articulated connection to a first region of the frame that is close to the first edge, a second holder couplable to the fuselage structure, and a strut. A first end of the strut is connectable in an articulated manner to the second holder. A second end of the strut is connectable in an articulated manner to a second region of the frame near the second edge and remote from the first edge. The frame and the strut form a triangular structure with the first and second holders. The strut and the frame form two sides of the triangular structure. A length of the first and/or second side is variable to adjust the position of the frame.
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5.发明申请公开(公告)号：US20190135453A1
公开(公告)日：2019-05-09
申请号：US16172564
申请日：2018-10-26
Applicant: Airbus Operations GmbH
Inventor： Hermann BENTHIEN , Matthias HEGENBART , Thomas LERCHE , Tobias-Valentin MAYER
Abstract: Disclosed here is a transfer system for transferring luggage into a vehicle having a freight hold opening and a passenger compartment opening arranged at the same level outside the vehicle. The system has a luggage transfer element and a passenger bridge, wherein the passenger bridge has a transition zone that can be simultaneously connected to the freight hold opening and the passenger compartment opening. The luggage transfer element has a housing module for receiving luggage, and a movement module for transferring the luggage transfer element. The luggage transfer element can be transferred through the transition zone and the freight hold opening by way of the movement module. The system avoids delays as the passengers are boarding and simplifies the transfer of luggage into a freight hold.
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Patent Agency Ranking
公开(公告)号：US20150102168A1
公开(公告)日：2015-04-16
申请号：US14487727
申请日：2014-09-16
Applicant: Airbus Operations GmbH
Inventor： Hermann BENTHIEN , Cord HAACK , Andreas POPPE , Michael BURRICHTER , Torsten ABRAHAM , Michael BRINCKMANN , Christoph DIERKER , Frank WERTH , Wulf BINDEWALD
IPC: B64C1/06
Abstract: An aircraft fuselage structure is disclosed herein and includes an outer skin, with circumferential ribs, such that a recess is provided for receiving a wing torsion box in the outer skin, and the ribs are interrupted in the region of the recess. An object of the disclosure includes providing an aircraft fuselage structure designed such that the wing torsion box is able to extend at least partially through the upper region of the fuselage, without the stability of the fuselage being significantly reduced. This can include providing first longitudinal members which are adjacent to the recess and which extend along the longitudinal edges beyond the entire length thereof. End regions of the first longitudinal members are connected to ribs which extend circumferentially at intervals from the transverse edges of the recess along the outer skin over the vertical longitudinal central plane.
Abstract translation: 本文公开了一种飞机机身结构，并且包括具有周向肋的外皮，使得设置用于在外皮中接收翼扭转盒的凹部，并且肋在凹部的区域中断。 本公开的目的包括提供一种设计成使得机翼扭转箱能够至少部分地延伸穿过机身的上部区域的飞行器机身结构，而不会显着减小机身的稳定性。 这可以包括提供与凹部相邻并且沿着纵向边缘延伸超过其整个长度的第一纵向构件。 第一纵向构件的端部区域连接到肋，其沿垂直纵向中心平面沿着外皮从凹部的横向边缘周向延伸。
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公开(公告)号：US20250042532A1
公开(公告)日：2025-02-06
申请号：US18787420
申请日：2024-07-29
Applicant: Airbus Operations GmbH
Inventor： Jens LOHMAR , Hermann BENTHIEN , Janes PEIMANN
Abstract: An aircraft cabin floor arrangement with air distribution. The arrangement comprises a plurality of floor panels and at least one air supply. The at least one air supply is configured for being arranged in a longitudinal direction of an aircraft. The plurality of floor panels are configured for being arranged in a spanning direction transverse to the longitudinal direction of the aircraft. The plurality of floor panels each comprise a plurality of elongate cavities aligned with the spanning direction of the floor panels. The at least one air supply is fluidly connected to at least a part of the elongate cavities of the floor panels for supplying air from the at least one air supply to the elongate cavities. The fluidly connected elongate cavities are providing supply air to passenger seat areas in an aircraft cabin.
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公开(公告)号：US20240308642A1
公开(公告)日：2024-09-19
申请号：US18594422
申请日：2024-03-04
Applicant: Airbus Operations GmbH
Inventor： Matthias HEGENBART , Hermann BENTHIEN
Abstract: A vehicle with a cabin comprising an adaptive rail system. The cabin includes a connection area adapted to hold the adaptive rail system. The adaptive rail system includes a rail interface, configured to be attachable to the connection area, at least one installation rail, configured to be attachable to the rail interface, and a jig. The jig is connected to the at least one installation rail in a moveable manner, such that a module attached to the jig is movable inside the cabin.
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9.发明公开公开(公告)号：US20240102503A1
公开(公告)日：2024-03-28
申请号：US18468373
申请日：2023-09-15
Applicant: Airbus Operations GmbH
Inventor： Hermann BENTHIEN , Andreas POPPE , Stefan BENTHIEN
IPC: F16B21/06
CPC classification number: F16B21/065
Abstract: A fastening device (1) for fastening mechanical element (2) with support structure (3) to fasten a cabin fitting element to a frame of an aircraft, fastening device (1) includes: enclosure (4) mountable to support structure (3); locator bush (5) in enclosure (4 and slidable along longitudinal axis (X) in an unlocked position of the fastening device (1); retaining element (6) around the longitudinal axis (X) and mechanically coupled to locator bush (5); and locking bolt (7) with a bolt head (8) mounting mechanical element (2) between bolt head (8) and enclosure (4), wherein locking bolt (7) is slidable into locator bush (5), and locking bolt (7) has a recess (9) on at least a section of a shell surface of locking bolt (7) and is positively-locking connectable with retaining element (6).
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公开(公告)号：US20230234776A1
公开(公告)日：2023-07-27
申请号：US17919041
申请日：2021-04-13
Applicant: Airbus Operations GmbH
Inventor： Ralf SCHLIWA , Thomas GRABOW , Hermann BENTHIEN , Lars Uwe HANSEN , Dirk MEIRANKE , Lucas GLEIXNER , Paul WICHTMANN
IPC: B65D88/14
CPC classification number: B65D88/14
Abstract: A freight container configured to fit in an aircraft cargo hold includes a floor element. First and second parallel side walls extend away from first and second opposite edges of the floor element base surface. A top wall, parallel to a floor element resting surface, extends between edges of the first and second side walls, which edges are remote from the first and second edges. A front wall extends between the first and second side walls from a base surface third edge to a top wall front edge. The front wall has a first front wall portion, extending from the base surface third edge at a first angle of at least 90° to the resting surface. The front wall has a second front wall portion, extending from the top wall front edge at a second angle of less than 180° and more than 90° to the top wall.
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