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公开(公告)号：US20190193872A1
公开(公告)日：2019-06-27
申请号：US16205504
申请日：2018-11-30
发明人： Hermann Benthien , Martin Metten , Florian Müller , Michael Telkamp , Marcus Hinrichs , Tancredi Tincani , Ralph Schmitt
摘要： A system for installing modules on a fuselage structure has modules with holders arranged thereon for fastening on a fuselage structure, assembly stands, which can be moved on a floor level, and a flexible connecting element, extending via all the modules and coupling them together. Each assembly stand has a base for supporting the stand on the floor level and a holding device, designed to support the module. The assembly stands, the modules and the at least one connecting element are designed to form a chain of assembly stands, such that two successive groups of assembly stands enclose a pivot point at which the mutually facing modules have a larger spacing relative to one another than the modules within the respective groups. The connecting element allows the pivoting of the groups relative to one another at the pivot point through an angle of at least 90°.
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2.发明授权公开(公告)号：US10773782B2
公开(公告)日：2020-09-15
申请号：US15639854
申请日：2017-06-30
发明人： Martin Metten , Hermann Benthien , Marcus Hinrichs , Michael Telkamp , Florian Mueller , Tancredi Tincani
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.
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公开(公告)号：US09902483B2
公开(公告)日：2018-02-27
申请号：US14469146
申请日：2014-08-26
发明人： Pierre C. Zahlen , Johannes Born , Lars Meyer , Gregor Baumbach , Claus Hanske , Jens Prowe , Johan Oentoro , M. Ichwan Zuardy , Wouter Brok , Martin Metten
IPC分类号： B32B3/24 , B32B3/26 , B32B5/18 , B32B5/24 , B32B5/26 , B32B5/28 , B32B7/04 , B60J1/00 , B64C1/14 , B29C70/02 , B32B3/08 , B32B37/16 , B32B37/30 , B32B37/12 , B32B38/04 , B29C70/30 , B29L7/00 , B32B3/02 , B29C70/54 , B29L9/00 , B29L31/30 , B29L31/00 , B64C1/12 , B64C1/00
CPC分类号： B64C1/1484 , B29C70/023 , B29C70/026 , B29C70/30 , B29C70/545 , B29C2793/0018 , B29C2793/0081 , B29L2007/002 , B29L2009/00 , B29L2031/005 , B29L2031/30 , B29L2031/3082 , B32B3/02 , B32B3/08 , B32B3/263 , B32B3/266 , B32B5/18 , B32B5/245 , B32B5/26 , B32B5/28 , B32B7/04 , B32B37/16 , B32B37/30 , B32B38/04 , B32B2250/03 , B32B2250/24 , B32B2250/40 , B32B2250/44 , B32B2260/00 , B32B2266/08 , B32B2305/022 , B32B2305/07 , B32B2605/00 , B32B2605/006 , B32B2605/18 , B60J1/00 , B60J1/004 , B60J1/006 , B64C1/12 , B64C1/14 , B64C1/1492 , B64C2001/0072 , Y02T50/43 , Y10T29/49163 , Y10T29/49165 , Y10T428/12667 , Y10T428/239 , Y10T428/24322 , Y10T428/24521 , Y10T428/25 , Y10T428/256 , Y10T428/257 , Y10T428/26 , Y10T428/2982
摘要： The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.
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公开(公告)号：US10960981B2
公开(公告)日：2021-03-30
申请号：US16006530
申请日：2018-06-12
发明人： Martin Metten
摘要： An aircraft region comprising an aisle section extending in a longitudinal direction of the aircraft region, a bench seat oriented transversely with respect to the longitudinal direction and having a first seat adjacent to the aisle section and a second seat arranged remote from the aisle section, and an aircraft stowage bin system having a first stowage bin arranged at least in part above the first seat and a second stowage bin arranged at least in part above the second seat. The first stowage bin has a first rear side facing away from the aisle section, and the second stowage bin has a second rear side facing away from the aisle section. The second stowage bin is arranged above the second seat such that it is accessible for a person sitting on the second seat or standing in the longitudinal direction in front of the second seat.
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5.发明申请SHELL STRUCTURE OF A FUSELAGE AT A DOOR OPENING AND METHOD OF FORMING THE SHELL STRUCTURE 审中-公开门开口处的外壳结构和形成壳结构的方法公开(公告)号：US20140367521A1
公开(公告)日：2014-12-18
申请号：US14295035
申请日：2014-06-03
发明人： Paul Joern , Wouter Brok , Martin Metten
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B64D11/00 , B64D11/02 , Y02T50/46 , Y10T29/49622
摘要： A shell structure of a fuselage at a door opening of the fuselage comprising a main door frame arranged on a cross-sectional plane of the fuselage. A wall portion of the main door frame extends into the fuselage and forms at least part of a first monument wall.
摘要翻译： 机身的门开口处的机身的外壳结构包括设置在机身的横截面上的主门框。 主门框的壁部分延伸到机身中并形成第一纪念墙的至少一部分。
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公开(公告)号：US11046218B2
公开(公告)日：2021-06-29
申请号：US16450126
申请日：2019-06-24
发明人： Martin Metten , Michael Telkamp , Hermann Benthien , Surya Utomo
摘要： A seat frame fastening assembly for laterally fastening a seat frame in a vehicle, wherein the seat frame fastening assembly comprises a holding rail arranged in a longitudinal direction of the vehicle, and a lateral element laterally fastened to a seat frame and coupled to the holding rail. The holding rail comprises a first power- and/or data-transfer interface and the lateral holding element comprises a second power- and/or data-transfer interface. The second power- and/or data-transfer interface is furthermore arranged in the lateral holding element such that a position of the second power- and/or data-transfer interface corresponds to a position of the first power- and/or data-transfer interface when the lateral holding element is coupled to the holding rail. Furthermore, a seat frame has such a seat frame fastening assembly, a vehicle portion has a corresponding seat frame and a vehicle has such a vehicle portion.
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公开(公告)号：US09580176B2
公开(公告)日：2017-02-28
申请号：US14278118
申请日：2014-05-15
发明人： Bernd Ehlers , Martin Metten , Stefan Behrens
CPC分类号： B64D11/06 , B64D11/00 , B64D11/0629 , B64D11/0691 , B64D2011/0092
摘要： An aircraft region comprising a main aisle extending along a longitudinal axis of an aircraft cabin, a door aisle extending along a transverse axis of the aircraft cabin substantially perpendicularly to the main aisle and an aircraft monument arranged in the door aisle and comprising at least one flight attendant seat facing a section of the main aisle adjoining the door aisle.
摘要翻译： 飞机区域，包括沿着飞机机舱的纵向轴线延伸的主通道，大门垂直于主通道的飞机机舱的横向轴线延伸的门通道和布置在门通道中的飞机纪念碑，并且包括至少一个飞行 伴随座位面临着与主通道相邻的一段主通道。
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公开(公告)号：US20150064389A1
公开(公告)日：2015-03-05
申请号：US14469146
申请日：2014-08-26
发明人： Pierre C. Zahlen , Johannes Born , Lars Meyer , Gregor Baumbach , Claus Hanske , Jens Prowe , Johan Oentoro , M. Ichwan Zuardy , Wouter Brok , Martin Metten
CPC分类号： B64C1/1484 , B29C70/023 , B29C70/026 , B29C70/30 , B29C70/545 , B29C2793/0018 , B29C2793/0081 , B29L2007/002 , B29L2009/00 , B29L2031/005 , B29L2031/30 , B29L2031/3082 , B32B3/02 , B32B3/08 , B32B3/263 , B32B3/266 , B32B5/18 , B32B5/245 , B32B5/26 , B32B5/28 , B32B7/04 , B32B37/16 , B32B37/30 , B32B38/04 , B32B2250/03 , B32B2250/24 , B32B2250/40 , B32B2250/44 , B32B2260/00 , B32B2266/08 , B32B2305/022 , B32B2305/07 , B32B2605/00 , B32B2605/006 , B32B2605/18 , B60J1/00 , B60J1/004 , B60J1/006 , B64C1/12 , B64C1/14 , B64C1/1492 , B64C2001/0072 , Y02T50/43 , Y10T29/49163 , Y10T29/49165 , Y10T428/12667 , Y10T428/239 , Y10T428/24322 , Y10T428/24521 , Y10T428/25 , Y10T428/256 , Y10T428/257 , Y10T428/26 , Y10T428/2982
摘要： The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.
摘要翻译： 本公开涉及一种用于车辆的车体结构的窗板，特别是飞机或航天器的机身，包括在面板的第一侧上延伸以形成车身结构的外皮的第一皮肤; 第二皮肤，其在所述面板的第二侧上延伸以形成所述车身结构的内表皮; 以及位于三明治结构中的第一和第二表层之间并覆盖的核心，特别是泡沫芯。 窗口面板包括通过第一层，芯部和第二层形成的至少一个窗孔。 芯可以限制在或限制在面板的有限程度，区域或部分上。 因此，第一皮肤和/或第二皮肤可以延伸超过或覆盖面板的比芯的更大的面积。
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公开(公告)号：US20140339364A1
公开(公告)日：2014-11-20
申请号：US14278118
申请日：2014-05-15
发明人： Bernd Ehlers , Martin Metten , Stefan Behrens
IPC分类号： B64D11/06
CPC分类号： B64D11/06 , B64D11/00 , B64D11/0629 , B64D11/0691 , B64D2011/0092
摘要： An aircraft region comprising a main aisle extending along a longitudinal axis of an aircraft cabin, a door aisle extending along a transverse axis of the aircraft cabin substantially perpendicularly to the main aisle and an aircraft monument arranged in the door aisle and comprising at least one flight attendant seat facing a section of the main aisle adjoining the door aisle.
摘要翻译： 飞机区域，包括沿着飞机机舱的纵向轴线延伸的主通道，大门垂直于主通道的飞机机舱的横向轴线延伸的门通道和布置在门通道中的飞机纪念碑，并且包括至少一个飞行 伴随座位面临着与主通道相邻的一段主通道。
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