Micro miniature air gap inspection crawler
    2.
    发明公开
    Micro miniature air gap inspection crawler 审中-公开
    微科 - 小型Luftspalt-Inspektionsraupe

    公开(公告)号:EP1862381A2

    公开(公告)日:2007-12-05

    申请号:EP07108514.6

    申请日:2007-05-21

    IPC分类号: B62D55/00 H02K15/00

    CPC分类号: B62D63/02 G01R31/34 H02K15/00

    摘要: An air gap inspection device (100). The air gap inspection device (100) may include a substantially rigid rail (110), a cart (150) positioned on the rail (110), a drive system (180) for maneuvering the cart (150) along the rail (110), and an inspection head (200) positioned on the cart (150).

    摘要翻译: 气隙检查装置(100)。 气隙检查装置(100)可以包括基本上刚性的轨道(110),定位在轨道(110)上的手推车(150),用于沿着轨道(110)操纵推车(150)的驱动系统(180) 和位于推车(150)上的检查头(200)。

    Ultrasonic miniature air gap inspection crawler
    3.
    发明公开
    Ultrasonic miniature air gap inspection crawler 有权
    Ultraschall-迷你Luftspalt-Inspektionskriecher

    公开(公告)号:EP1772949A1

    公开(公告)日:2007-04-11

    申请号:EP06255188.2

    申请日:2006-10-09

    IPC分类号: H02K15/00 H02K11/00

    CPC分类号: H02K15/00 G01R31/34

    摘要: A miniature air gap inspection crawler (100). The miniature air gap inspection crawler (100) may include a base (110), a linear drive mechanism (200, 210) and a circumferential drive mechanism (330, 340) such that either the linear drive mechanism (200, 210) or the circumferential drive mechanism (330, 340) may be employed, and an inspection module (500) connected to the base (110).

    摘要翻译: 小型气隙检查履带(100)。 微型气隙检查履带(100)可以包括基部(110),线性驱动机构(200,210)和周向驱动机构(330,340),使得线性驱动机构(200,210)或 圆周驱动机构(330,340),以及连接到基座(110)的检查模块(500)。

    Method and apparatus for robotically inspecting gas turbine combustor components
    6.
    发明公开
    Method and apparatus for robotically inspecting gas turbine combustor components 审中-公开
    Verfahren und Vorrichtung zur robotgesteuerten Inspektion der Gasturbinenbrennkammerteile

    公开(公告)号:EP1900906A2

    公开(公告)日:2008-03-19

    申请号:EP07115646.7

    申请日:2007-09-04

    IPC分类号: F01D9/02 F01D25/00

    摘要: Apparatus for inspecting in situ a wear pad gap in a gas turbine engine combustor, wherein the wear pad gap is defined between a wear pad of a transition piece impingement sleeve and a forward ring of a flow duct of the combustor. The apparatus includes an elongate guide, a mount for coupling the guide to the combustor such that the guide at least partially extends within a space between the impingement sleeve and a body of the transition piece and such that a portion of the guide extends adjacent the wear pad. A cam follower is coupled to the guide for movement along the guide and an inspection head (48) is carried by the cam follower. An actuator is coupled to the cam follower for displacing the cam follower along the guide.

    摘要翻译: 用于在燃气涡轮发动机燃烧器中原位检查磨损垫间隙的装置,其中所述磨损垫间隙限定在过渡件冲击套筒的磨损垫和所述燃烧器的流动管道的前环之间。 该装置包括细长引导件,用于将引导件连接到燃烧器的安装件,使得引导件至少部分地在冲击套筒和过渡件的主体之间的空间内延伸,并且使得引导件的一部分在磨损 垫。 凸轮从动件联接到引导件以沿着引导件移动,并且检查头(48)由凸轮从动件承载。 致动器联接到凸轮从动件,用于沿着引导件移动凸轮从动件。