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25 条记录 (耗时 0.027 秒)

    Sealing structure for a pivoting blade of a gas turbine
    5.
    发明授权
    Sealing structure for a pivoting blade of a gas turbine 失效
    燃气轮机枢转叶片的密封结构

    公开(公告)号：US5324165A

    公开(公告)日：1994-06-28

    申请号：US58760

    申请日：1993-05-10

    申请人： Jean-Louis Charbonnel ,  Jacky S. Naudet

    发明人： Jean-Louis Charbonnel ,  Jacky S. Naudet

    IPC分类号： F01D9/02 ,  F01D11/00 ,  F01D17/16 ,  F02C7/28 ,  F04D29/08 ,  F04D29/32

    CPC分类号： F04D29/083 ,  F01D11/003 ,  F01D17/162 ,  F04D29/323

    摘要： A sealing structure for a gas turbine blade which pivots about a pivot shaft. A split ring is located in a groove on the shaft, in which the ring can be embedded and held by a bush. When the blade is fitted, the bush abuts against a wall of the stator, slides on the pivot shaft and frees the ring, which expands and forms the seal. The invention relates to gas turbines where the stator blades have a variable setting.

    摘要翻译： 一种用于围绕枢轴枢转的燃气轮机叶片的密封结构。 开口环位于轴上的凹槽中，环可以由衬套嵌入和保持。 当叶片安装时，衬套抵靠定子的壁，在枢轴上滑动并释放环，该环膨胀并形成密封。 本发明涉及一种定子叶片具有可变设定值的燃气轮机。

    Axial fixing arrangement for rotor blades of a turbomachine
    8.
    发明授权
    Axial fixing arrangement for rotor blades of a turbomachine 失效
    涡轮机转子叶片的轴向固定装置

    公开(公告)号：US5622476A

    公开(公告)日：1997-04-22

    申请号：US572045

    申请日：1995-12-14

    申请人： Danielle C. R. Adde ,  Jean-Louis Charbonnel ,  Philippe F. P. Gougeon ,  Gerard G. Miraucourt

    发明人： Danielle C. R. Adde ,  Jean-Louis Charbonnel ,  Philippe F. P. Gougeon ,  Gerard G. Miraucourt

    IPC分类号： F01D5/30 ,  F01D5/32

    CPC分类号： F01D5/323 ,  Y02T50/671

    摘要： A fixing arrangement for axially fixing a blade in position on a rotor disk of a turbomachine rotor includes a relatively flexible locking wedge inserted between the root of the blade and the bottom of the axial groove in the periphery of the rotor disk in which the root is received in a radially interlocking manner, the locking wedge having a retaining hook which is received in a groove in the blade root to hold the locking wedge in position. In one embodiment the locking wedge holds a plate in position in the recesses defined by undercut projections on the upstream face of the blade root and the rotor disk to prevent axial movement the blade relative to the disk. In an alternative embodiment the downstream end of the locking wedge has a stop which engages the downstream faces of the blade root and the rotor disk to prevent axial movement of the blade in the upstream direction, and the upstream face of the blade root has a projection which overlaps and bears against an upstream face of the disk to prevent axial movement of the blade in the downstream direction.

    摘要翻译： 用于将叶片轴向固定在涡轮机转子的转子盘上的位置的固定装置包括插入叶片根部和转子盘周边中的轴向槽底部之间的相对柔性的锁定楔，其中根部是 以径向互锁的方式接收，所述锁定楔具有保持钩，所述保持钩被容纳在所述叶片根部中的凹槽中以将所述锁定楔保持在适当位置。 在一个实施例中，锁定楔将板固定在由叶片根部和转子盘的上游面上的切削突起限定的凹部中，以防止叶片相对于盘的轴向移动。 在替代实施例中，锁定楔的下游端具有止动件，其与叶片根部和转子盘的下游面接合，以防止叶片沿上游方向的轴向移动，并且叶片根部的上游面具有突起 其与盘的上游面重叠并抵靠，以防止叶片在下游方向上的轴向移动。

    Turbine engine equipped with means for controlling the play between the rotor and stator
    9.
    发明授权
    Turbine engine equipped with means for controlling the play between the rotor and stator 失效
    涡轮发动机配备有用于控制转子和定子之间的间隙的装置

    公开(公告)号：US5616003A

    公开(公告)日：1997-04-01

    申请号：US330072

    申请日：1994-10-26

    申请人： Jean-Louis Charbonnel ,  Daniel J. Marey ,  Fabrice Marois ,  Gerard G. Miraucourt

    发明人： Jean-Louis Charbonnel ,  Daniel J. Marey ,  Fabrice Marois ,  Gerard G. Miraucourt

    IPC分类号： F01D25/24 ,  F01D25/26 ,  F03B11/02

    CPC分类号： F01D25/265 ,  F01D25/246

    摘要： A turbine engine includes a ferrule formed of a plurality of ferrule elements in the shape of circular sectors, each bearing on one internal face thereof fixed vanes and a circular housing surrounding the ferrule. The turbine has a support ring including a plurality of circular ring sectors each secured to the housing and having a U-shaped section whose opening is directed towards the ferrule, each ferrule element includes a hooking mechanism (9a) to be introduced into the opening of at least one ring sector so as to integrally connect the ring sector and the ferrule element.

    摘要翻译： 涡轮发动机包括由圆形扇形的多个套圈元件形成的套圈，每个套圈元件的一个内表面上具有固定叶片和围绕套圈的圆形壳体。 涡轮机具有支撑环，该支撑环包括多个圆环部分，每个环形部分均固定到壳体上，并具有一个U形部分，其开口指向套圈，每个套圈元件包括一个钩子机构（9a） 至少一个环形部分，以便一体地连接环形部分和套圈元件。

    Sealing and retaining device for a rotor notched with pin settings receiving blade roots
    10.
    发明授权
    Sealing and retaining device for a rotor notched with pin settings receiving blade roots 失效
    用于接收叶片根部的针脚设计的转子的密封和保持装置

    公开(公告)号：US5320492A

    公开(公告)日：1994-06-14

    申请号：US87903

    申请日：1993-07-09

    申请人： Michel A. Bouru ,  Jean-Louis Charbonnel ,  Jean-Claude Prato

    发明人： Michel A. Bouru ,  Jean-Louis Charbonnel ,  Jean-Claude Prato

    IPC分类号： F01D5/30 ,  F01D5/32 ,  F01D11/00

    CPC分类号： F01D11/006 ,  F01D5/3015 ,  F05D2250/182

    摘要： A sealing and retention device for the blades of a rotor which engage with axial pin settings of the rotor wherein the device includes, in a first embodiment, a flange in the shape of a circular collar which engages the rotor and a locking ring which engages the blades and the flange wherein the locking ring has a conical portion which engages a first protuberance portion of the blades such that upon centrifugal sliding of the locking ring in a radially outward direction, the locking ring is axially displaced toward the flange. The device may also include a conical crest located on the rotor and the flange may have a conical surface for engaging the conical crest of the rotor.

    摘要翻译： 一种用于转子叶片的密封和保持装置，其与转子的轴向销设置接合，其中，在第一实施例中，该装置包括与转子接合的圆形轴环形状的凸缘和接合转子的锁定环 叶片和凸缘，其中锁定环具有与叶片的第一突起部分接合的锥形部分，使得当锁定环沿径向向外的方向离心滑动时，锁定环朝向凸缘轴向移位。 该装置还可以包括位于转子上的圆锥形突起，并且凸缘可以具有锥形表面，用于接合转子的锥形顶端。