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公开(公告)号:US20170028947A1
公开(公告)日:2017-02-02
申请号:US15222703
申请日:2016-07-28
发明人: Jack BLANCHARD , Anthony BRYANT
摘要: A vehicle fairing including an electrical routing for conducting power and/or control signals between spaced-apart components of a vehicle structure. The vehicle fairing includes an outer surface configured to form part of an outer surface of a vehicle body. The electrical routing includes a printed circuit board having a substrate and a first conductive path for conduction of electrical current or signals provided on the substrate. The substrate is substantially rigid and forms at least a portion of the outer surface of the vehicle fairing.
摘要翻译: 一种车辆整流罩,其包括用于在车辆结构的间隔开的部件之间进行动力和/或控制信号的电气路线。 车辆整流罩包括构造成形成车身的外表面的一部分的外表面。 电路由包括具有衬底和用于传导电流的第一导电路径的印刷电路板或设置在衬底上的信号。 衬底基本上是刚性的并且形成车辆整流罩外表面的至少一部分。
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公开(公告)号:US20150060612A1
公开(公告)日:2015-03-05
申请号:US14517198
申请日:2014-10-17
发明人: Jack BLANCHARD , David ROUTLEDGE
CPC分类号: B64C1/406 , F16L3/123 , F16L3/127 , F16L3/13 , F16L3/221 , F16L3/227 , F16L3/237 , F16M13/02 , H02G3/32
摘要: A conduit harness retention system has a base, a first spacer, a second spacer and a cap which snap-fit together to retain P-clip harnesses in position spaced from an aircraft fuselage.
摘要翻译: 导管线束保持系统具有底座,第一间隔件,第二间隔件和帽,其卡扣配合在一起以将P形夹子线束保持在与飞机机身间隔开的位置。
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公开(公告)号:US20130206926A1
公开(公告)日:2013-08-15
申请号:US13755410
申请日:2013-01-31
发明人: Andreas YIASOUMI , Jack BLANCHARD
IPC分类号: H02G3/38
CPC分类号: H02G3/38 , H02G3/0437
摘要: An electrical cable raceway for an aircraft, the electrical cable raceway being formed at least in part from a ceramic material.
摘要翻译: 一种用于飞行器的电缆滚道,所述电缆滚道至少部分地由陶瓷材料形成。
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公开(公告)号:US20130192892A1
公开(公告)日:2013-08-01
申请号:US13755364
申请日:2013-01-31
发明人: Jack BLANCHARD , Anthony BRYANT
IPC分类号: H02G3/04
CPC分类号: H02G3/0437 , H02G3/0608
摘要: A cable protector for connection to an aircraft electrical cable raceway, comprising a flexible conductive body defining a conduit through which an electrical cable can pass and an electrically conductive connection arrangement configured to enable connection of the body of the protector to a raceway in an electrically conductive manner.
摘要翻译: 用于连接到飞机电缆轨道的电缆保护器,包括限定电缆可以通过的导管的柔性导电体,以及导电连接装置,该导电连接装置被配置为能够将保护器的主体连接到导轨 方式。
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公开(公告)号:US20140263828A1
公开(公告)日:2014-09-18
申请号:US14264453
申请日:2014-04-29
发明人: Jack BLANCHARD , Andreas YIASOUMI
CPC分类号: B64C13/28 , B64C9/22 , H01B7/065 , H02G11/006 , Y02T50/44
摘要: A telescopic strut for electrically connecting a fixed structure of an aircraft to a movable structure mounted to the fixed structure, wherein the strut is adapted to be mechanically connected to the fixed structure by its one end and to be mechanically connected to the movable structure by its opposite end, the strut comprising a plurality of telescopic elements and containing a helically coiled electrical cable, wherein the cable is adapted to move between retracted and extended positions with the telescoping of the strut. Also, a method of operating an aircraft having a movable structure mounted to a fixed structure, and one or more of the telescopic struts mechanically and electrically connected between the fixed and movable structures.
摘要翻译: 一种用于将飞行器的固定结构电连接到安装到固定结构的可移动结构的伸缩支柱,其中所述支柱适于通过其一端机械连接到所述固定结构,并且通过其固定结构与所述可移动结构机械连接 所述支柱包括多个伸缩元件并且包含螺旋状卷绕的电缆,其中所述电缆适于在所述支柱的伸缩状态下在缩回位置和延伸位置之间移动。 而且,一种操作具有安装到固定结构的可移动结构的飞行器的方法,以及机械地和电连接在固定结构和可移动结构之间的一个或多个伸缩支柱。
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