Device for guiding and holding a cable within a pipe
    1.
    发明授权
    Device for guiding and holding a cable within a pipe 有权
    用于引导和保持管道内的电缆的装置

    公开(公告)号:US09488306B2

    公开(公告)日:2016-11-08

    申请号:US13992124

    申请日:2011-12-15

    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。

    DEVICE FOR GUIDING AND HOLDING A CABLE WITHIN A PIPE
    2.
    发明申请
    DEVICE FOR GUIDING AND HOLDING A CABLE WITHIN A PIPE 有权
    用于在管道中引导和保持电缆的装置

    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

    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。

    Raisable landing gear
    3.
    发明授权
    Raisable landing gear 失效
    可升降起落架

    公开(公告)号:US5263664A

    公开(公告)日:1993-11-23

    申请号:US019896

    申请日:1993-02-19

    IPC分类号: B64C25/02 B64C25/66 B64C25/10

    CPC分类号: B64C25/02 B64C25/66

    摘要: The invention relates to raisable landing gear having a shock absorber strut and a sliding rod. According to the invention, the landing gear includes a lateral stabilizer hinged to the strut and fitted with a wheel at its free end, together with mechanical coupling means associated with said lateral stabilizer, in such a manner that: firstly lowering the landing gear deploys the lateral stabilizer so that its wheel, when the landing gear is in its lowered position, provides support additional to that provided by the wheels of the wheel set, and also constitutes a lateral stabilizer proper during taxiing of the airplane; and secondly raising the landing gear folds the lateral stabilizer so as to enable the entire landing gear assembly to be housed when in the raised position. It then becomes possible to organize the landing gear beneath the fuselage of the airplane, thereby making it possible to obtain landing gear that is extremely short.

    摘要翻译: 本发明涉及具有减震器支柱和滑动杆的可抬升起落架。 根据本发明,起落架包括侧向稳定器,该侧向稳定器铰接到支柱并且在其自由端处装配有车轮以及与所述侧向稳定器相关联的机械联接装置,其方式为:首先降低起落架部署 侧向稳定器,使得当起落架处于其降低位置时,其轮子提供额外的轮子组件所提供的支撑,并且还在飞机滑行期间构成侧向稳定器; 并且其次升起起落架折叠横向稳定器,以使整个起落架组件能够在处于升高位置时被容纳。 然后可以将起落架组装在飞机的机身下方,从而可以获得极短的起落架。

    Laterally-raisable aircraft landing gear
    4.
    发明授权
    Laterally-raisable aircraft landing gear 失效
    可升降的飞机起落架

    公开(公告)号:US5478030A

    公开(公告)日:1995-12-26

    申请号:US266643

    申请日:1994-06-28

    IPC分类号: B64C25/12

    CPC分类号: B64C25/12 B64C2025/125

    摘要: The invention relates to aircraft landing gear of the type that is laterally-raisable and that has twin wheels in a side-by-side configuration. According to the invention, the leg is constituted by an upside-down L-shaped strut whose two branches are hinged together, comprising a beam-forming first branch that is hinged to the structure of the aircraft and a second branch having a wheel lever hinged to the end thereof. The wheel lever is also connected to the first branch via a shock absorber. A controlling guide bar connects the second branch to the structure of the aircraft via a fork swivel-mounted on said second branch, in such a manner as to cause said second branch to move forwards while the landing ger is being raised, such forwards movement causing the wheels to be folded in because the shock absorber then acts as a second guide bar.

    摘要翻译: 本发明涉及一种横向可升高的类型的飞机起落架,并且具有并排配置的双轮。 根据本发明,腿由倒置的L形支柱构成,其两个分支铰接在一起,包括铰接到飞行器结构的梁形成第一分支和具有铰链的轮杆的第二分支 到最后。 车轮杆还通过减震器连接到第一分支。 控制引导杆通过安装在所述第二分支上的叉子将所述第二分支连接到所述飞行器的结构,以使得所述第二分支在所述着陆台升高时向前移动,这样的向前运动导致 因为减震器然后用作第二导杆,所以要折叠的轮子。