-
11.发明授权公开(公告)号：US09212680B2
公开(公告)日：2015-12-15
申请号：US13654851
申请日：2012-10-18
Applicant: AIRBUS OPERATIONS GMBH
Inventor： Uwe Schneider
CPC classification number: F16B21/12 , B64D11/003 , F16B5/0241 , F16B19/02
Abstract: A tie bar for connecting an equipment fitting of an equipment module to a structure fitting of a fuselage cell structure. At each end the tie bar has a fork head each with a fork head hole for a bolt. The spacing between the fork heads can be continuously adjusted. A captive bushing is utilized for sound and vibration decoupling. The bushings which are a press fit in the fork head holes can no longer fall out during the handling of the tie bars 10. The dimensions of the bushings made of plastic are adapted to the respective application scenario by a tolerance calculation and guarantee an effective sound and vibration decoupling between the structure fitting and the equipment fitting.
Abstract translation: 用于将设备模块的设备配件连接到机身单元结构的结构配件的连接杆。 在每个端部，连接杆具有一个叉头，每个叉头具有用于螺栓的叉头孔。 叉头之间的间距可以连续调节。 隔音衬套用于声音和振动解耦。 在接头杆10的处理期间，压配合在叉头孔中的衬套不能再脱落。由塑料制成的衬套的尺寸通过公差计算适应于相应的应用场景，并保证有效的声音 和结构配件与设备配件之间的振动解耦。
-
公开(公告)号：US20140065937A1
公开(公告)日：2014-03-06
申请号：US14010756
申请日：2013-08-27
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Witaliy Kotnow , Gordon Konieczny
IPC: B64D13/02
CPC classification number: B64D13/02 , B64D13/00 , B64D2013/0625
Abstract: A system for supplying passengers with air comprises an air supply line and an individual air panel with at least one air nozzle. The air supply line can be fitted with a plurality of laterally situated air outlets, which are spaced apart at uniform distances from each other. The individual air panel comprises an air tap opening with a width and length, wherein the length is several times greater than the width. The individual air panel can be variably positioned in the longitudinal direction on the air supply line in such a way that the air tap opening in the longitudinal direction is arranged parallel to the air supply line, and that the air tap opening covers at least one air outlet. In this way, air can flow out of the air supply line through the air outlet and air tap opening to the air nozzle.
Abstract translation: 用于向乘客提供空气的系统包括空气供应管线和具有至少一个空气喷嘴的单独的空气面板。 供气管线可以装配有彼此间隔开的多个横向设置的空气出口。 单独的空气面板包括具有宽度和长度的空气抽头开口，其中长度是宽度的几倍。 各个空气面板可以沿空气供应管线沿长度方向可变地定位，使得沿长度方向的分接开口平行于空气供应管线布置，并且空气抽头开口覆盖至少一个空气 出口。 以这种方式，空气可以通过空气出口从空气供应管线流出并且空气抽头通向空气喷嘴。
-
公开(公告)号：US10377462B2
公开(公告)日：2019-08-13
申请号：US15349244
申请日：2016-11-11
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
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.
-
公开(公告)号：US09810249B2
公开(公告)日：2017-11-07
申请号：US14613463
申请日：2015-02-04
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Peter Bielik , Hristo Margov , Raj Kotian
CPC classification number: F16B1/02 , B64C1/00 , B64D11/003 , Y02T50/46 , Y10T29/49826
Abstract: An attachment structure for an equipment unit of an aircraft includes a first attachment device extending in a longitudinal direction of the aircraft, wherein the first attachment device is attached to a stringer and to a frame and wherein the first attachment device has a first engagement element and a second attachment device attachable to the equipment unit, wherein the second attachment device has a second engagement element adapted for engaging into the first engagement element, such that a force from the equipment unit in the longitudinal direction on the second attachment device is transferred via the second engagement element to the first engagement element and via the first attachment device to the stringer and the frame.
-
公开(公告)号：US09688406B2
公开(公告)日：2017-06-27
申请号：US14622029
申请日：2015-02-13
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Patrick Rollfink , Diana Siehndel
CPC classification number: B64D11/00 , B64D11/0015 , B64D13/00 , B64D13/06 , B64D25/00 , B64D2011/0046 , B64D2011/0053
Abstract: An interior component for an interior room of an aircraft is provided. The interior component includes a body having a first surface and a second surface and a multitude of functional modules which form a passenger service unit. The second surface is arranged opposite to the first surface and comprises a recess. The multitude of functional modules are arranged one after another in the recess in the longitudinal direction of the interior component, such that a first front surface of the functional module arranged frontally in the longitudinal direction closes flush with a first front surface of the body.
-
Patent Agency Ranking
公开(公告)号：US09527479B2
公开(公告)日：2016-12-27
申请号：US14208369
申请日：2014-03-13
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: B60R99/00 , A47C7/62 , A47C7/72 , A47C13/00 , B64D11/0015 , B64D11/06 , B64D11/0624 , B64D11/0626
Abstract: A passenger seat and a passenger service supply system is provided, comprising a seat with a seating and a backrest, and a passenger service module providing a passenger service such as conditioned air, a personal light, data network access or a similar service. A passenger service module supply line is connected to the passenger service module with a first end, and comprises an interface, which is adapted to connect a second end of the passenger service module supply line to a central supply line of a means of transport. The passenger service module supply line is thereby at least partly integrated into the seating.
Abstract translation: 提供乘客座椅和乘客服务供应系统，其包括具有座位和靠背的座椅，以及提供诸如调节空气，个人照明，数据网络接入或类似服务的乘客服务的乘客服务模块。 乘客服务模块供应线路连接到具有第一端的乘客服务模块，并且包括适于将乘客服务模块供应线的第二端连接到运输工具的中央供应线的接口。 乘客服务模块供应线由此至少部分地集成在座位中。
-
公开(公告)号：US10569879B2
公开(公告)日：2020-02-25
申请号：US15487983
申请日：2017-04-14
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
Abstract: An aircraft ceiling liner element comprises a load-bearing carrier platform, configured to form a part of an aircraft ceiling liner, and a mounting mounted on the carrier platform, connectable to a primary structure of the aircraft. An electrical connection mounted on the carrier platform is connectable to an electrical supply network of the aircraft. Furthermore, the aircraft ceiling liner element comprises a mechanical interface mounted on the carrier platform, configured to attach various interchangeable modular units detachably and in a load-transferring manner to the carrier platform, and an electrical interface mounted on the carrier platform, which interface is configured to create an electrical connection between the modular unit and the carrier platform.
-
18.发明授权公开(公告)号：US10450068B2
公开(公告)日：2019-10-22
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
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.
-
公开(公告)号：US20170297714A1
公开(公告)日：2017-10-19
申请号：US15487983
申请日：2017-04-14
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider
CPC classification number: B64D11/003 , B64C1/066 , B64C1/22 , B64D11/0015 , B64D45/00
Abstract: An aircraft ceiling liner element comprises a load-bearing carrier platform, configured to form a part of an aircraft ceiling liner, and a mounting mounted on the carrier platform, connectable to a primary structure of the aircraft. An electrical connection mounted on the carrier platform is connectable to an electrical supply network of the aircraft. Furthermore, the aircraft ceiling liner element comprises a mechanical interface mounted on the carrier platform, configured to attach various interchangeable modular units detachably and in a load-transferring manner to the carrier platform, and an electrical interface mounted on the carrier platform, which interface is configured to create an electrical connection between the modular unit and the carrier platform.
-
公开(公告)号：US09630721B2
公开(公告)日：2017-04-25
申请号：US14010756
申请日：2013-08-27
Applicant: Airbus Operations GmbH
Inventor： Uwe Schneider , Witaliy Kotnow , Gordon Konieczny
CPC classification number: B64D13/02 , B64D13/00 , B64D2013/0625
Abstract: A system for supplying passengers with air comprises an air supply line and an individual air panel with at least one air nozzle. The air supply line can be fitted with a plurality of laterally situated air outlets, which are spaced apart at uniform distances from each other. The individual air panel comprises an air tap opening with a width and length, wherein the length is several times greater than the width. The individual air panel can be variably positioned in the longitudinal direction on the air supply line in such a way that the air tap opening in the longitudinal direction is arranged parallel to the air supply line, and that the air tap opening covers at least one air outlet. In this way, air can flow out of the air supply line through the air outlet and air tap opening to the air nozzle.
-
-
-
-
-
-
-
-
-
Search Results
23
records
(took 0.016 seconds)
