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1.发明申请POWER DRIVE UNIT AND AIRCRAFT CARGO COMPARTMENT FLOOR WITH POWER DRIVE UNITS 有权动力驱动单元和飞机货架地板与动力驱动单元公开(公告)号：US20140367227A1
公开(公告)日：2014-12-18
申请号：US14296585
申请日：2014-06-05
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: B64C1/22 , B64C1/20 , B64D9/00 , B64D2009/006 , B65G13/06 , B65G13/10 , Y02T50/46
Abstract: A power drive unit, including a plurality of diagonal rollers arranged at a circumference around a central roller axis and each of the plurality of diagonal rollers having a respective diagonal roller axis, a first drive motor coupled to a roller carrier and configured to rotate the plurality of diagonal rollers around the central roller axis, and a second drive motor coupled to a gear carrier and configured to rotate each of the diagonal rollers around the respective diagonal roller axis. The diagonal roller axes are tilted by a common skew angle with respect to the central roller axis.
Abstract translation: 一种动力驱动单元，包括布置在围绕中心滚轴轴线的圆周上的多个对角滚子，并且所述多个对角滚子中的每一个具有相应的对角滚子轴线;第一驱动马达，其联接到滚轮托架并且构造成使多个 围绕中心辊轴线的对角滚子和耦合到齿轮架的第二驱动马达，并且构造成围绕相应的对角滚子轴线旋转每个对角滚子。 倾斜滚子轴线相对于中心滚子轴线倾斜一个共同的倾斜角度。
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公开(公告)号：US11840871B2
公开(公告)日：2023-12-12
申请号：US17209321
申请日：2021-03-23
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: E05C3/16 , B60R5/003 , E05C3/008 , E05F3/04 , B64D11/003 , E05Y2201/21 , E05Y2201/654 , E05Y2900/502 , E05Y2900/54
Abstract: A closing aid for a luggage compartment flap is described, which closing aid comprises an actuating element, a movement element and a connecting element. The actuating element is integrated in a locking mechanism of the luggage compartment flap. The connecting element connects the actuating element to the movement element and transmits a movement of the actuating element to the movement element such that the luggage compartment flap fastened to the movement element is moved at least part of the way from an open position to a closed position. A luggage compartment and a vehicle having a closing aid of this type are also described.
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公开(公告)号：US09834309B2
公开(公告)日：2017-12-05
申请号：US14548426
申请日：2014-11-20
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Vladimir Berger , Andreas Wietzke
CPC classification number: B64D13/00 , B64D11/00 , B64D2013/003
Abstract: An air supply system for passengers includes an air supply line with a plurality of laterally situated air outlets, an individual air panel with at least one air nozzle and an air inlet opening. The individual air panel can be variably positioned along the air supply line in such a way that the air inlet opening faces one of the air outlets. A plurality of magnetic valves is arranged at the air outlets of the air supply line. One of the magnetic valves may be magnetically actuated by the individual air panel, when the air inlet opening of the individual air panel faces said one magnetic valve, so that air can flow out of the air supply line through the air outlet and the air inlet opening to the air nozzle.
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公开(公告)号：US20170144745A1
公开(公告)日：2017-05-25
申请号：US15349244
申请日：2016-11-11
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: B64C1/14 , B64C1/066 , B64C1/18 , B64C2001/009 , B64D13/04
Abstract: A decompression assembly for use in an aircraft comprises a cabin lining element, an opening formed in the element, and an air channel arranged adjacent to a rear face of the element and connected to the opening. The air channel is provided with an air outlet which, during normal operation of the assembly, discharges air exiting a cabin region delimited by the element through the opening into an area located between the element and an aircraft outer skin, a first decompression opening, and a first decompression flap which, during normal operation of the decompression assembly, closes the first decompression opening in the air channel and which, in the event of a rapid decompression, opens the first decompression opening to allow a pressure equalization between the aircraft cabin region and the aircraft area located between the cabin lining element and the aircraft outer skin.
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公开(公告)号：US09511863B2
公开(公告)日：2016-12-06
申请号：US14160966
申请日：2014-01-22
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Andreas Jespersen
CPC classification number: B64D11/003 , A47B46/00 , Y02T50/46
Abstract: A storage compartment for a passenger cabin of an aircraft is provided. The storage compartment comprises a storage compartment body, a mounting, a fixing brace and a pull rod. The fixing brace is connected to a frame of the primary structure of an aircraft and to the mounting and takes up forces transversely to the direction of flight. The pull rod is connected to a stringer of the aircraft primary structure and also to the mounting and takes up forces in the direction of flight in such a way that even in the event of an impact event, only low torques are to be taken up by the supporting primary structure of the aircraft.
Abstract translation: 提供了一种用于飞机客舱的储藏室。 储藏室包括储藏室主体，安装件，固定支架和拉杆。 固定支架连接到飞行器的主要结构的框架并且安装并横向于飞行方向承受力。 拉杆连接到飞机初级结构的纵梁，并且还以安装方式并且沿着飞行方向占据力，使得即使在碰撞事件的情况下，只有低扭矩将被 飞机的辅助主体结构。
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Patent Agency Ranking
6.发明授权Power drive unit and aircraft cargo compartment floor with power drive units 有权电力驱动单元和飞机货舱地板与动力传动单元公开(公告)号：US09340276B2
公开(公告)日：2016-05-17
申请号：US14296585
申请日：2014-06-05
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: B64C1/22 , B64C1/20 , B64D9/00 , B64D2009/006 , B65G13/06 , B65G13/10 , Y02T50/46
Abstract: A power drive unit, including a plurality of diagonal rollers arranged at a circumference around a central roller axis and each of the plurality of diagonal rollers having a respective diagonal roller axis, a first drive motor coupled to a roller carrier and configured to rotate the plurality of diagonal rollers around the central roller axis, and a second drive motor coupled to a gear carrier and configured to rotate each of the diagonal rollers around the respective diagonal roller axis. The diagonal roller axes are tilted by a common skew angle with respect to the central roller axis.
Abstract translation: 一种动力驱动单元，包括布置在围绕中心滚轴轴线的圆周上的多个对角滚子，并且所述多个对角滚子中的每一个具有相应的对角滚子轴线;第一驱动马达，其联接到滚轮托架并且构造成使多个 围绕中心辊轴线的对角滚子和耦合到齿轮架的第二驱动马达，并且构造成围绕相应的对角滚子轴线旋转每个对角滚子。 倾斜滚子轴线相对于中心滚子轴线倾斜一个共同的倾斜角度。
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公开(公告)号：US09308996B2
公开(公告)日：2016-04-12
申请号：US14271499
申请日：2014-05-07
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Patrick Rollfink
CPC classification number: B64D11/003 , B60R5/00
Abstract: A luggage compartment for a means of transport and a means of transport with a luggage compartment are provided. The luggage compartment comprises a housing with a pivotably attached connecting element and with a sliding element. The connecting element is adapted for being pivotably attached to a first structural element and the sliding element is adapted for moving along a rail connected to a second structural element. The luggage compartment is easy to manufacture and to maintain.
Abstract translation: 提供了一个用于运输工具的行李箱和一个带有行李箱的运输工具。 行李箱包括具有可枢转地连接的连接元件和滑动元件的壳体。 连接元件适于可枢转地附接到第一结构元件，并且滑动元件适于沿着连接到第二结构元件的轨道移动。 行李箱容易制造和维护。
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公开(公告)号：US20170144744A1
公开(公告)日：2017-05-25
申请号：US15349254
申请日：2016-11-11
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: B64C1/14 , B64C1/066 , B64C1/18 , B64C2001/009 , B64D13/04
Abstract: An aircraft decompression assembly, comprising a cabin lining element, an element opening and an air channel adjacent to an element rear face and connected to the opening. A channel outlet, during normal assembly operation, discharges air exiting a cabin region delimited by the element through the opening into a secluded area between the element and an aircraft outer skin. A first decompression opening has a first decompression flap, which during normal operation, closes the first decompression opening and, in the event of a rapid decompression, opens the first decompression opening equalizing a pressure between the cabin region and the secluded area. A second decompression opening in the lining element has a second decompression flap which, during normal operation, closes the second decompression opening and which, in the event of a rapid decompression, opens the second decompression opening equalizing a pressure between the cabin region and the secluded area.
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公开(公告)号：US09522735B2
公开(公告)日：2016-12-20
申请号：US14567330
申请日：2014-12-11
Applicant: Airbus Operations GmbH
Inventor： Sabrina Moje , Matthias Breuer , Paul Vine , Uwe Schneider
IPC: B64D11/00
CPC classification number: B64D11/003 , B64D11/00
Abstract: An aircraft area comprises a first rib forming a component of an aircraft primary structure and extending in an arc shape along an outer contour of the aircraft area. A second rib is arranged at a distance from the first rib and parallel to the first rib, also forms a component of the aircraft primary structure and extends in an arc shape along the outer contour of the aircraft area. A luggage compartment is arranged between the first and the second rib such that a portion of a first side face of the luggage compartment that faces the first rib is arranged opposite a side face of the first rib that faces the luggage compartment, and/or that a portion of a second side face of the luggage compartment that faces the second rib is arranged opposite a side face of the second rib that faces the luggage compartment.
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10.发明申请AIRCRAFT LUGGAGE SYSTEM HAVING A LUGGAGE COMPARTMENT AND AN ADDITIONAL LUGGAGE COMPARTMENT 审中-公开具有行李舱和附加行李舱的飞机运输系统公开(公告)号：US20160288908A1
公开(公告)日：2016-10-06
申请号：US15177937
申请日：2016-06-09
Applicant: Airbus Operations GmbH
Inventor： Sabrina Moje , Matthias Breuer , Paul Vine , Uwe Schneider
IPC: B64D11/00
CPC classification number: B64D11/003
Abstract: An aircraft luggage system comprising a luggage compartment which comprises an upper side directed towards a ceiling of an aircraft when the luggage compartment is assembled in the aircraft, a lower side directed towards a floor of the aircraft, a rear side directed towards an outer contour of the aircraft, and two side faces connect the upper side to the lower side. The lower side of the luggage compartment is rigidly connected to the side faces and the rear side of the luggage compartment. A flap, movable between a closed position and an open position, is configured to make an inner space of the luggage compartment accessible or to close it. At least one additional luggage compartment is arranged adjacent to at least one of the upper side and the lower side of the luggage compartment.
Abstract translation: 一种飞行器行李系统，包括行李舱，当行李舱组装在飞行器中时，该行李舱包括朝向飞行器的天花板的上侧，朝向飞行器的地板的下侧，指向外部轮廓的外侧轮廓的后侧 飞机和两个侧面将上侧连接到下侧。 行李箱的下侧刚性地连接到行李箱的侧面和后侧。 可在关闭位置和打开位置之间移动的挡板构造成使得行李箱的内部空间可接近或闭合。 至少一个额外的行李箱被布置成与行李箱的上侧和下侧中的至少一个相邻。
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