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公开(公告)号：US20130248041A1
公开(公告)日：2013-09-26
申请号：US13992124
申请日：2011-12-15
IPC分类号： F16L55/07
CPC分类号： F16L55/07 , B64C25/02 , H02G3/28 , H02G3/32 , Y10T29/49826
摘要： The invention provides a device (2) for guiding a cable (8a, 8b) in a duct (4), the device (2) being characterized in that it comprises at least one guide tube (12) receiving the cable (8a, 8b) and at least one expandable clamp (13) secured to one end (12a) of the tube (12), the expandable clamp (13) being deployed so as to be blocked against the inside wall of the duct (4) in order to hold the tube (12) in the duct (4). The device serves to guide and hold the cable in the duct without damaging the duct.
摘要翻译： 本发明提供了一种用于将电缆（8a，8b）引导到管道（4）中的装置（2），该装置（2）的特征在于，其包括至少一个接纳电缆（8a，8b）的导管 ）和固定到所述管（12）的一端（12a）的至少一个可膨胀夹具（13），所述可膨胀夹具（13）被展开以便阻挡在所述管道（4）的内壁上，以便 将管（12）保持在管道（4）中。 该装置用于引导和保持电缆在管道中而不损坏管道。
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公开(公告)号：US09488306B2
公开(公告)日：2016-11-08
申请号：US13992124
申请日：2011-12-15
CPC分类号： F16L55/07 , B64C25/02 , H02G3/28 , H02G3/32 , Y10T29/49826
摘要： The invention provides a device (2) for guiding a cable (8a, 8b) in a duct (4), the device (2) being characterized in that it comprises at least one guide tube (12) receiving the cable (8a, 8b) and at least one expandable clamp (13) secured to one end (12a) of the tube (12), the expandable clamp (13) being deployed so as to be blocked against the inside wall of the duct (4) in order to hold the tube (12) in the duct (4). The device serves to guide and hold the cable in the duct without damaging the duct.
摘要翻译： 本发明提供了一种用于将电缆（8a，8b）引导到管道（4）中的装置（2），该装置（2）的特征在于，其包括至少一个接纳电缆（8a，8b）的导管 ）和固定到所述管（12）的一端（12a）的至少一个可膨胀夹具（13），所述可膨胀夹具（13）被展开以便阻挡在所述管道（4）的内壁上，以便 将管（12）保持在管道（4）中。 该装置用于引导和保持电缆在管道中而不损坏管道。
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公开(公告)号：US20190382102A1
公开(公告)日：2019-12-19
申请号：US16445013
申请日：2019-06-18
摘要： A method of moving a door of a well for an aircraft undercarriage during sequences of deploying or retracting the undercarriage includes: using a temporary mechanical connection between the door and the undercarriage that is effective when the undercarriage is close to its retracted position, causing the door to be opened by the undercarriage while the undercarriage is being deployed and causing the door to be closed by the undercarriage while the undercarriage is being retracted, but releasing the door from the undercarriage when the undercarriage is close to its deployed position, and using a door actuator acting on the door to close and open the door when the undercarriage is in its deployed position and the temporary mechanical connection is interrupted.
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4.发明授权Device for coupling an actuator for controlling the landing gear of an aircraft 有权用于联接用于控制飞行器的起落架的致动器的装置公开(公告)号：US09511852B2
公开(公告)日：2016-12-06
申请号：US14238534
申请日：2012-09-07
摘要： A device for coupling an actuator for operating an aircraft undercarriage to an aircraft structure. The device comprises a lever having a first end for hinging to the structure of the aircraft, and a second end to which the actuator is hinged, a pre-loading structure acting on the lever to urge it towards a stable rest position that is occupied by the lever in the absence of any force transiting through the actuator; and an abutment structure defining at least one working position for the lever when the actuator is activated.
摘要翻译： 一种用于将用于操作飞行器起落架的致动器联接到飞机结构的装置。 该装置包括杠杆，其具有用于铰接到飞行器的结构的第一端和致动器铰接的第二端，作用在杠杆上的预加载结构，以将其推向稳定的休止位置，该静止位置由 没有任何力通过致动器的杠杆; 以及当所述致动器被致动时限定所述杠杆的至少一个工作位置的邻接结构。
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5.发明申请DEVICE FOR COUPLING AN ACTUATOR FOR CONTROLLING THE LANDING GEAR OF AN AIRCRAFT 有权用于联接执行机构以控制飞机的起落架的装置公开(公告)号：US20140209738A1
公开(公告)日：2014-07-31
申请号：US14238534
申请日：2012-09-07
IPC分类号： B64C25/20
摘要： A device for coupling an actuator for operating an aircraft undercarriage to an aircraft structure. The device comprises a lever having a first end for hinging to the structure of the aircraft, and a second end to which the actuator is hinged, a pre-loading structure acting on the lever to urge it towards a stable rest position that is occupied by the lever in the absence of any force transiting through the actuator; and an abutment structure defining at least one working position for the lever when the actuator is activated.
摘要翻译： 一种用于将用于操作飞行器起落架的致动器联接到飞机结构的装置。 该装置包括杠杆，其具有用于铰接到飞行器的结构的第一端和致动器铰接的第二端，作用在杠杆上的预加载结构，以将其推向稳定的休止位置，该静止位置由 没有任何力通过致动器的杠杆; 以及当所述致动器被致动时限定所述杠杆的至少一个工作位置的邻接结构。
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