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    • 2. 发明申请
    • ATTACHMENT BRACKET AND SUPPORT ASSEMBLY
    • 附件支架和支撑总成
    • WO2017029569A1
    • 2017-02-23
    • PCT/IB2016/054622
    • 2016-08-01
    • BOMBARDIER INC.SHORT BROTHERS PLC
    • GALLIEN, RenéDESHAIES, Martin
    • F16B11/00H02G3/00
    • H02G3/32F16B5/0685F16B7/0433F16B11/006F16B37/044F16B37/048
    • A support assembly (10) having a structural element (12) having first and second non-parallel adjoining surfaces (18), a bracket (14) attached to the structural element (12), and a component support (16). The bracket (14) has a first flange (20) including a first attachment surface (24) adhesively bonded to the first surface (18) of the structural element (12), a second flange (20) including a second attachment surface (24) adhesively bonded to the second surface (18) of the structural element (12), and a connection portion (48) interconnecting the first and second flanges (20), the connection portion (48) extending spaced from the structural element (12) such that a gap (52) is defined therebetween. The component support (16) is engaged to the first flange (20). The connection portion (48) may have a lower resistance to rupture than that of the first and second flanges (20). A method of removably securing a component to a structural element is also discussed.
    • 具有具有第一和第二非平行相邻表面(18)的结构元件(12)的支撑组件(10),附接到结构元件(12)的支架(14)和部件支撑件(16)。 支架(14)具有第一凸缘(20),第一凸缘(20)包括粘合地结合到结构元件(12)的第一表面(18)的第一附接表面(24);第二凸缘(20),包括第二附接表面 )连接到所述结构元件(12)的第二表面(18),以及连接所述第一和第二凸缘(20)的连接部分(48),所述连接部分(48)与所述结构元件(12)间隔开延伸, 使得它们之间限定间隙(52)。 部件支撑件(16)接合到第一法兰(20)。 连接部分(48)可以具有比第一和第二凸缘(20)的抗破坏性更低的抗破坏性。 还讨论了将组件可移除地固定到结构元件的方法。
    • 3. 发明公开
    • STANDOFF DEVICE AND METHOD OF INSTALLATION OF HARNESS
    • VERFAHREN ZUR EINRICHTUNG EINES KABELBAUMS的ABSTANDSHALTER
    • EP2684266A1
    • 2014-01-15
    • EP11718486.1
    • 2011-03-10
    • Bombardier Inc.SHORT BROTHERS PLC
    • PAUZÉ, MartinWOOD, Keith, AntonyDESHAIES, MartinLANDRY, Pierre
    • H02G3/30B60R16/02
    • H01B17/16F16L3/221F16L3/237H01B17/14H02G3/30H02G3/32
    • A device connects a wire harness to a structure. A fixation portion of the device is secured to the structure. A spacing portion is connected to the fixation portion and to a connector portion. A retaining clip on the connector portion deforms when a wire harness connector component moves axially toward the fixation portion. The clip opposes an abutment edge against the component into engagement position when the component is past the clip to prevent it from moving back onto the clip. An abutment surface contacts another portion of the component in engagement position to prevent further axial movement of the component toward the fixation portion. The component is held captive between the edge and the abutment surface. Also provided are a cable support for connecting the wire harness to the device, a method for connecting and disconnecting the wire harness to a structure with the device, and an aircraft.
    • 设备将线束连接到结构。 该装置的固定部分固定在该结构上。 间隔部分连接到固定部分和连接器部分。 当线束连接器部件沿固定部分轴向移动时,连接器部分上的固定夹变形。 当组件经过夹子以防止其回到夹子上时,夹子将抵靠部件的抵接边缘与接合位置相对。 邻接表面接合部件的接合位置的另一部分以防止部件朝着固定部分进一步轴向移动。 该部件保持在边缘和邻接表面之间。 还提供了用于将线束连接到装置的电缆支撑件,用于将线束连接和断开到具有该装置的结构的方法以及飞行器。