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71. 发明授权

US11492821B2 Emergency exit system 有权
公开(公告)号：US11492821B2
公开(公告)日：2022-11-08
申请号：US16440435
申请日：2019-06-13
申请人： Airbus Operations GmbH
发明人： Uwe Papenroth , Hermann Benthien , Torsten Witt
IPC分类号： E05B65/10 , B64C1/14 , B64C1/34
摘要： An emergency exit system comprising a first primary structure frame, a second primary structure frame extending substantially parallel to the first primary structure frame, a door opening arranged between the first primary structure frame and the second primary structure frame, and a door shiftable substantially parallel to the first primary structure frame and the second primary structure frame between a closed position and an open position. In the closed position, the door closes the door opening. In the open position, the door opens up the door opening. At least one of the primary structure frames comprises a primary structure guide element for guiding the door when the door is shifted between the closed position and the open position.

72. 发明申请

US20220055771A1 Deformable shim and mounting arrangement 有权
公开(公告)号：US20220055771A1
公开(公告)日：2022-02-24
申请号：US17454115
申请日：2021-11-09
申请人： Airbus Operations GmbH
发明人： Mika Bots , Matthias Hegenbart , Hermann Benthien
IPC分类号： B64F5/10 , B64C1/06 , B23P19/02 , B23P19/04
摘要： A method of providing a deformable shim that comprises a main structure of an at least partly cellular region. The main structure is compressible by plastic deformation from an initial volume to a deformed volume, wherein the deformed volume is smaller than the initial volume. In a deformed state, the main structure maintains the deformed volume without further or continuing compression force. Further, the main structure is arrangeable between a first aircraft component and a second aircraft component to create a predefined distance between the first and the second aircraft component.

73. 发明授权

US11198521B2 Deformable shim and mounting arrangement 有权
公开(公告)号：US11198521B2
公开(公告)日：2021-12-14
申请号：US15879642
申请日：2018-01-25
申请人： Airbus Operations GmbH
发明人： Mika Bots , Matthias Hegenbart , Hermann Benthien
IPC分类号： B64C1/14 , B64F5/10 , B64C1/06 , B23P19/02 , B23P19/04
摘要： In order to improve and facilitate shimming between two parts, a deformable shim is provided that comprises a main structure of an at least partly cellular region. The main structure is compressible by plastic deformation from an initial volume to a deformed volume, wherein the deformed volume is smaller than the initial volume. In a deformed state, the main structure maintains the deformed volume without further or continuing compression force. Further, the main structure is arrangeable between a first aircraft component and a second aircraft component to create a predefined distance between the first and the second aircraft component.

74. 发明授权

US11137011B2 Fastening system for fastening a first component at a variable spacing on a second component 有权
公开(公告)号：US11137011B2
公开(公告)日：2021-10-05
申请号：US16218593
申请日：2018-12-13
申请人： Airbus Operations GmbH
发明人： Niklas Lehmensieck , Hermann Benthien
IPC分类号： F16B21/02 , F16B5/02 , F16B37/08 , F16B21/07
摘要： A fastening system for fastening a first component variably spaced on a second component has a main body, a slide, and an elongate locking element. The main body has a mounting surface for mounting on the first component and a locating surface, through which an elongate depression passes, for fastening to the second component. The main body has a slideway to movably support the slide along the depression and the locating surface. Facing sides of the slide and the depression each have a first tooth system. The locking element fits into the elongate depression and has a second tooth system on two mutually opposite longitudinal sides and engages between the depression first tooth system and the locking element and between the slide and the locking element in a first alignment within the depression and releases it in a second alignment. The mounting surface and locating surfaces are not parallel.

75. 发明授权

US11136124B2 Fastening system for fastening a component on a fuselage structure 有权
公开(公告)号：US11136124B2
公开(公告)日：2021-10-05
申请号：US16222457
申请日：2018-12-17
申请人： Airbus Operations GmbH
发明人： Hermann Benthien
IPC分类号： B64D11/00 , B64F5/00 , F16B33/00
摘要： 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.

76. 发明授权

US10773782B2 Interior component carrier system and method for mounting an interior component carrier system 有权
公开(公告)号：US10773782B2
公开(公告)日：2020-09-15
申请号：US15639854
申请日：2017-06-30
申请人： Airbus Operations GmbH
发明人： Martin Metten , Hermann Benthien , Marcus Hinrichs , Michael Telkamp , Florian Mueller , Tancredi Tincani
IPC分类号： B64D11/00 , B64C1/06 , B64F5/00
摘要： An interior component carrier system comprises a first and second installation rail. Each rail includes at least one connecting portion connectable to an associated primary structure component to fasten the rail to the component, and a carrier portion extending from the connecting portion in a direction along a longitudinal axis of the system. The system further comprises a first carrier element having a first end connected to a first carrier rod extending in a direction along the longitudinal axis and a second end connectable to a first interior component, wherein the first carrier rod is fastened to the carrier portion of the first rail, and a second carrier element having a first end connected to a second carrier rod extending in the longitudinal axis direction and a second end connected to the first carrier element, wherein the second carrier rod is fastened to the second rail carrier portion.

77. 发明授权

US10343344B2 Connection system, connection arrangement and method 有权
公开(公告)号：US10343344B2
公开(公告)日：2019-07-09
申请号：US15486949
申请日：2017-04-13
申请人： AIRBUS OPERATIONS GMBH
发明人： Hermann Benthien , Matthias Hegenbart
IPC分类号： B29C65/54 , B29C65/00 , B29C65/56 , B29C65/48 , A44B18/00 , B64C1/12 , F16B11/00 , B29L31/30
摘要： A connection system has a first adhesion segment, on which a first connection region is formed, a second adhesion segment, on which a second connection region is formed, and a solidifiable liquid connection substance for connecting the two adhesion segments in a material fit, wherein at least one of the two connection regions is formed flexibly, such that, when the liquid connection substance is introduced between the two connection regions which are opposite one another in an assembly arrangement of the two adhesion segments, a material connection is formed between the two connection regions automatically as a result of the elastocapillary effect via the liquid connection substance.

78. 发明申请

US20190092473A1 PIVOTABLE LUGGAGE LOCKER, AND VEHICLE HAVING A LUGGAGE LOCKER 审中-公开
公开(公告)号：US20190092473A1
公开(公告)日：2019-03-28
申请号：US16143091
申请日：2018-09-26
申请人： Airbus Operations GmbH
发明人： Hermann Benthien
IPC分类号： B64D11/00
摘要： A pivotable luggage locker for a vehicle, the luggage locker including a luggage compartment which has a bottom and the rear wall, and a first holder. The first holder is attached on an outer side of the rear wall and is set up to hold the luggage compartment rotatably. In addition, the luggage locker includes a second holder which is attached in a region of an upper side of the luggage compartment, and an actuating mechanism which is coupled rotatably to the luggage compartment on the second holder and is set up to rotate the luggage compartment about the first holder. Furthermore, a vehicle having a pivotable luggage locker of this type is disclosed.

79. 发明申请

US20180079171A1 BONDING ARRANGEMENT AND PRODUCTION METHOD 审中-公开
公开(公告)号：US20180079171A1
公开(公告)日：2018-03-22
申请号：US15706919
申请日：2017-09-18
申请人： Airbus Operations GmbH
发明人： Matthias Hegenbart , Hermann Benthien , Mika Bots
IPC分类号： B32B7/02 , B32B7/12 , B32B37/12 , B32B37/14 , B32B3/12 , B32B3/30
CPC分类号： B32B7/02 , B32B1/04 , B32B3/00 , B32B3/02 , B32B3/06 , B32B3/12 , B32B3/22 , B32B3/26 , B32B3/28 , B32B3/30 , B32B5/18 , B32B7/04 , B32B7/05 , B32B7/12 , B32B7/14 , B32B15/00 , B32B15/046 , B32B15/08 , B32B15/20 , B32B25/00 , B32B25/14 , B32B37/1292 , B32B37/144 , B32B2255/205 , B32B2255/26 , B32B2255/28 , B32B2605/00 , B32B2605/18 , F16B11/006
摘要： In order to provide a new and improved bonding arrangement, especially for use in an aircraft or spacecraft, which is designed to overcome problems of bonding arrangements under Mode I loading stress and which is designed or configured particularly to create a bond design which is incapable of locally loading the adhesive bond above the peel strength, a bonding arrangement is disclosed with a coating structure, which is split into a plurality of neighboring structural elements spatially separated from each other, and at least one supporting member is provided, which comprises a plurality of recesses receiving the structural elements in operating position.

80. 发明授权

US09415552B2 Method for the manufacture of a fibre composite component, a supporting core, and also a fibre composite component 有权
标题翻译：用于制造纤维复合材料组件，支撑芯以及纤维复合材料组件的方法
公开(公告)号：US09415552B2
公开(公告)日：2016-08-16
申请号：US13886415
申请日：2013-05-03
申请人： Airbus Operations GmbH
发明人： Hermann Benthien , Axel Soeffker
IPC分类号： B29D22/00 , B29C70/44 , B29D99/00
CPC分类号： B29D22/00 , B29C70/446 , B29D99/0014 , Y10T428/13
摘要： A method for the manufacture of a fiber composite component reinforcement section, which bounds a cavity, whereby a supporting core, with an elastic sleeve bounding an interior space, is temporarily positioned in the cavity. The steps include: laying down fibrous material on a base molding tool to form a base element of the fiber composite component, draping fibrous material in a negative mold, arranging the supporting core on an inner surface of the fibrous material in the negative mold, positioning the negative mold fitted with the fibrous material and the supporting core, on the base element to form the reinforcement section, forming a vacuum chamber accommodating the negative mold and the base element by covering with a vacuum film, evacuating the vacuum chamber, and curing the fibrous material, whereby when using a dry fibrous material, a matrix material is injected into the fibrous material after the evacuation.
摘要翻译：一种制造纤维复合材料部件增强部分的方法，该部分限定空腔，由此具有限定内部空间的弹性套筒的支撑芯暂时定位在空腔中。步骤包括：将纤维材料铺设在基底模具上以形成纤维复合材料部件的基底元件，将纤维材料包覆在阴模中，将支撑芯布置在负模具中的纤维材料的内表面上，定位在基体元件上装有纤维材料和支撑芯的负模具以形成加强部分，通过用真空膜覆盖形成容纳负模和真空室的真空室，抽空真空室，并固化纤维材料，其中当使用干燥的纤维材料时，抽真空后将基质材料注入纤维材料中。

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