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公开(公告)号：US20150004834A1
公开(公告)日：2015-01-01
申请号：US13930024
申请日：2013-06-28
Applicant: The Boeing Company
Inventor： Ty Aaby Larsen , Todd Burton Brouwer , Robert T. Johnson , Mark Eugene Liffring , Mark Stephen Shander , Robert Dennis Holley , Margaret L. Douglas
CPC classification number: H01H19/62 , B64C1/18 , B64D2221/00 , Y02T50/43
Abstract: An interconnect for transferring signals herein includes one or more signal contacts to transfer the power or data to or from an integrated truss system. An interconnect may be configured to transfer power or data between layers of the integrated truss system or within the same layer of the integrated truss system. An interconnect may be configured with one or more compression mechanisms that secure the interconnect in the integrated truss system.
Abstract translation: 用于在这里传送信号的互连包括一个或多个信号触点，用于将功率或数据传送到集成桁架系统或从集成桁架系统传输。 互连可以被配置为在集成桁架系统的层之间或在集成桁架系统的相同层内传递功率或数据。 互连可以配置有一个或多个压缩机构，其将互连固定在集成桁架系统中。
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公开(公告)号：US09406462B2
公开(公告)日：2016-08-02
申请号：US13930024
申请日：2013-06-28
Applicant: The Boeing Company
Inventor： Ty Aaby Larsen , Todd Burton Brouwer , Robert T Johnson , Mark Eugene Liffring , Mark Stephen Shander , Robert Dennis Holley , Margaret L. Douglas
CPC classification number: H01H19/62 , B64C1/18 , B64D2221/00 , Y02T50/43
Abstract: An interconnect for transferring signals herein includes one or more signal contacts to transfer the power or data to or from an integrated truss system. An interconnect may be configured to transfer power or data between layers of the integrated truss system or within the same layer of the integrated truss system. An interconnect may be configured with one or more compression mechanisms that secure the interconnect in the integrated truss system.
Abstract translation: 用于在这里传送信号的互连包括一个或多个信号触点，用于将功率或数据传送到集成桁架系统或从集成桁架系统传输。 互连可以被配置为在集成桁架系统的层之间或在集成桁架系统的相同层内传递功率或数据。 互连可以配置有一个或多个压缩机构，其将互连固定在集成桁架系统中。
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公开(公告)号：US10060355B2
公开(公告)日：2018-08-28
申请号：US14617640
申请日：2015-02-09
Applicant: THE BOEING COMPANY
Inventor： Christopher Wheaton , Mark Stephen Shander
CPC classification number: F02C7/24 , B64D13/00 , F01D25/00 , F02C7/00 , F02C7/32 , F05D2300/2102 , F05D2300/614 , F16L57/00 , Y02T50/672
Abstract: Apparatus and system for containing a rupture of a duct. The apparatus includes an air-permeable sheet, such as a wide-weave fiberglass sheet. The air-permeable sheet includes a strap arranged on a first side of the sheet such that it forms diamond-shaped patterns along a longitudinal axis. The strap can be made of a tight-weave fiberglass. Laterally-spaced corners of the diamond-shaped patterns include connection members that can be engaged to affix the strap and the air-permeable sheet around a duct. Various aspects include an air-impermeable air barrier surrounding the wide-weave fiberglass sheet and strap. The air barrier can include a window that directs air from a ruptured duct. Various aspects can be used on a bleed-air duct of an aircraft. The window of the air barrier can be aimed at a temperature sensor. A valve can close the bleed-air duct if the temperature sensor detects a high temperature leak.
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