公开(公告)号：US5000659A

公开(公告)日：1991-03-19

申请号：US533770

申请日：1990-06-06

申请人： Philippe P. Catte ,  Jacky Naudet

发明人： Philippe P. Catte ,  Jacky Naudet

IPC分类号： F01D25/28

CPC分类号： F04D29/563 ,  F01D17/162 ,  F01D25/285 ,  Y10T403/645

摘要： In a turbomachine, such as a turboshaft aero-engine, having a compressor casing composed of upstream and downstream casing rings, and a variably settable stage of stator blades which is mounted in one of said casing rings near the junction therebetween so that, in normal operation, the blades have their leading (or trailing) edges projecting into the other casing ring, the setting of the blades being adjusted by a control ring surrounding the casing, there is provided a locking system for temporarily locking the blades in an angular setting in which the leading (or trailing) edges are retracted clear of said other casing when the casing is to be dismantled or assembled. The locking system comprises at least one locking member which is held captive on one of the screws securing the two casing rings together, the member being movable in the axial direction by the screw and having axially extending wings which engage in slots in the control ring to effect the locking of the stator blades when the screw is unscrewed.

摘要翻译： 在具有由上游和下游壳环构成的压缩机壳体的涡轮机，例如涡轮轴航空发动机，以及可变地设置的定子叶片级，其安装在靠近其间的接合处的一个所述壳体环中，使得在正常情况下 叶片的前缘（或后缘）突出到另一壳体环中，叶片的设置由围绕壳体的控制环进行调节，提供了一种用于将叶片临时锁定在角度设置中的锁定系统 当外壳要被拆卸或组装时，引导（或拖尾）边缘从所述另一壳体缩回。 所述锁定系统包括至少一个锁定构件，所述至少一个锁定构件保持在将所述两个套管环固定在一起的所述螺钉中的一个上，所述螺钉将所述螺栓固定在所述轴向上，并且具有轴向延伸的翼，所述翼与所述控制环中的槽接合， 当拧下螺丝时，会影响定子叶片的锁定。

公开(公告)号：US5096377A

公开(公告)日：1992-03-17

申请号：US626551

申请日：1990-12-12

申请人： Philippe P. Catte ,  Jacky Naudet

发明人： Philippe P. Catte ,  Jacky Naudet

IPC分类号： F01D25/26 ,  F04D29/52

CPC分类号： F04D29/522 ,  F01D25/265 ,  Y02T50/671 ,  Y10T403/645 ,  Y10T403/7094

摘要： The casing of a turboshaft engine, particularly a turbojet engine with a high speed propeller, comprises axially successive shells which are fixed firmly to each other end to end by bolted coupling flanges, at least one of the shells comprising an additional mechanical axial retaining joint enabling the connection between the shells to withstand any exceptional stresses such as those caused by the loss of a propeller blade of the turbojet engine. Preferably the retaining joint comprises a radially inwardly directed tongue carried by one of the shells and received in a radially outwardly open groove provided in a portion of the other shell or a member securely fixed thereto.

摘要翻译： 涡轮轴发动机的壳体，特别是具有高速螺旋桨的涡轮喷气发动机的壳体包括轴向连续的壳体，其通过螺栓联接凸缘彼此牢固地固定到彼此的端部，至少一个壳体包括附加的机械轴向保持接头，使能 壳体之间的连接以承受诸如由涡轮喷气发动机的螺旋桨叶片的损失引起的任何异常应力。 优选地，保持接头包括由一个壳体承载的径向向内指向的舌片，并被接纳在设置在另一壳体的一部分中的径向向外开放的凹槽中或固定到其上的构件。

公开(公告)号：US5052893A

公开(公告)日：1991-10-01

申请号：US543717

申请日：1990-07-17

申请人： Philippe P. Catte

发明人： Philippe P. Catte

IPC分类号： F01D5/30

CPC分类号： F01D5/3015

摘要： A device for locking the blade roots (3) in rotor disk alveoli (2) consists of a single split ring (9) with a Y shaped cross-section of which a radial upstream arm (9a) is inserted in the groove (7) of the downstream blade lips (6) the radial downstream arm (9b) of the ring (9) being pressed against the downstream part of the blade lips (6).

摘要翻译： PCT No.PCT / FR89 / 00588 Sec。 371日期1990年7月17日第 102（e）日期1990年7月17日PCT提交1989年11月16日PCT公布。 公开号WO90 / 05837 日期：1990年5月31日。一种用于将叶片根部（3）锁定在转子盘肺泡（2）中的装置由具有Y形横截面的单个开口环（9）组成，其中径向上游臂（9a）插入其中 在下游叶片（6）的凹槽（7）中，环（9）的径向下游臂（9b）被压靠在叶片唇缘（6）的下游部分。