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1.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
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。
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公开(公告)号：US5224820A
公开(公告)日：1993-07-06
申请号：US950138
申请日：1992-09-24
申请人： Christophe Brichet , Jean-Louis Charbonnel , Gerard G. Miraucourt , Jacky Naudet , Jean-Francois Van De Voorde
发明人： Christophe Brichet , Jean-Louis Charbonnel , Gerard G. Miraucourt , Jacky Naudet , Jean-Francois Van De Voorde
IPC分类号： F01D17/16
CPC分类号： F01D17/162 , Y02T50/671
摘要： In a turbomachine in which the stator includes at least one stage of pivole blades and a ring which is movable axially to operate the levers which rotate the blades, the ring is moved by varying the pressure of gas which is contained in sealed chambers and which exerts a force between the movable ring and another fixed ring. This arrangement enables a better distribution of the forces to be achieved than purely mechanical movement control systems.
摘要翻译： 在涡轮机中，其中定子包括至少一个可转动叶片级和一个可轴向移动以操作转动叶片的杆的环，该环通过改变密封室中容纳的气体压力而移动， 可动环与另一固定环之间的力。 这种布置使得能够比纯机械运动控制系统更好地分配要实现的力。
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公开(公告)号：US5636968A
公开(公告)日：1997-06-10
申请号：US508169
申请日：1995-07-27
CPC分类号： F04D29/563 , F01D17/162 , F05D2250/141
摘要： A device for assembling a circular stage of pivoting vanes and composed of a ring for retaining bushes in which the pivots of the vanes rotate. The ring is composed of sectors extending between the pivots and connected together by a circular rail. A further ring separate from the rail or integrated with the latter is engaged in throats of the pivots so as to retain them against an axial movement.
摘要翻译： 一种用于组装枢转叶片的圆台的装置，由用于保持衬套的环组成，其中叶片的枢轴旋转。 环由在枢轴之间延伸并通过圆形轨连接在一起的扇区组成。 与轨道分离或与后者集成的另一个环接合在枢轴的喉部中，以便将其保持抵抗轴向运动。
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公开(公告)号：US5407322A
公开(公告)日：1995-04-18
申请号：US125753
申请日：1993-09-24
申请人： Jean-Louis Charbonnel , Jean-Luc C. Y. Goga , Gerard G. Miraucourt , Jacky S. Naudet , Denis B. Pottier
发明人： Jean-Louis Charbonnel , Jean-Luc C. Y. Goga , Gerard G. Miraucourt , Jacky S. Naudet , Denis B. Pottier
CPC分类号： F01D17/162 , F16B4/00 , F05D2300/505 , Y02T50/672
摘要： Variable phase vane provided with a composite pivot having a joining piece for receiving the control pieces. The joining piece is made of a material less dense than the actual pivot. These two elements are force-fitted without using any weld or mechanical linking device. The vane finally obtained is thus rendered lighter in weight
摘要翻译： 具有复合枢轴的可变相叶片具有用于接收控制件的接合件。 连接件由比实际枢轴密度小的材料制成。 这两个元件是强制安装的，不使用任何焊接或机械连接装置。 因此，最终获得的叶片的重量更轻
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公开(公告)号：US5622476A
公开(公告)日：1997-04-22
申请号：US572045
申请日：1995-12-14
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。
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6.发明授权Annular gasket disposed at one axial extremity of a rotor and covering blade feet 失效环形垫片设置在转子的一个轴向末端并且覆盖叶片脚部
公开(公告)号：US5330324A
公开(公告)日：1994-07-19
申请号：US106632
申请日：1993-08-16
申请人： Daniel Agram , Jean-Louis Charbonnel , Philippe G. E. Joly , Gerard G. Miraucourt , Jacky S. Naudet , Jean-Claude Prato
发明人： Daniel Agram , Jean-Louis Charbonnel , Philippe G. E. Joly , Gerard G. Miraucourt , Jacky S. Naudet , Jean-Claude Prato
CPC分类号： F01D5/3015 , F01D11/006 , Y02T50/671
摘要： An annular gasket includes, at least partially conically shaped portion and is supported on a rotor via three bearing surfaces. The conical shape makes it possible to reject the center of gravity of the sections of the rotor which provokes substantial rotational movement when centrifugal forces exist and allows for an improved imperviousness via the internal and external bearings. This invention is applicable for the rotors of aircraft engines provided with axial broachings in which blade feet are able to slide.
摘要翻译： 环形垫圈包括至少部分圆锥形的部分，并通过三个支承表面支撑在转子上。 锥形形状使得有可能拒绝转子部分的重心，当离心力存在时会引起相当大的旋转运动，并允许通过内外轴承改善不透水性。 本发明适用于具有叶片脚能够滑动的轴向拉刀的飞机发动机的转子。
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7.发明授权Method of fixing stemmed blade for a flow-straightening stage of a gas turbine engine 失效固定用于燃气涡轮发动机的流动整流级的叶片的方法
公开(公告)号：US5319850A
公开(公告)日：1994-06-14
申请号：US45224
申请日：1993-04-13
CPC分类号： F01D9/044 , Y10T29/49321 , Y10T29/49323
摘要： A stemmed blade for flow-straightener blading of a gas turbine engine includes at least one shank at the head of the blade forming a stem for use in fixing the blade. The shank has a notched portion situated adjacent the head of the blade and an end portion separated from the notched portion by a zone of lower tensile strength. Fixing of the blade to the engine casing is carried out by fitting the blade in position with the shank projecting radially outwards through a hole in the casing and then crimping a bush on to the notched portion of the shank using a suitable crimping tool which exerts a compressive force on the bush while exerting a traction force on the end of the shank until the zone of lower tensile strength breaks.
摘要翻译： 用于燃气涡轮发动机的流动整流器叶片的干叶片包括在叶片头部处的至少一个柄部，形成用于固定叶片的杆。 柄部具有邻近刀片头部的切口部分，以及与切口部分分离具有较低拉伸强度的区域的端部。 通过将刀片通过壳体中的孔径向向外突出的杆将刀片固定在适当位置，然后使用合适的压接工具将衬套压紧到柄的切口部分来实现刀片到发动机壳体的固定，该压接工具施加 在衬套的端部施加牵引力直到较低拉伸强度的区域破裂时，衬套上的压缩力。
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8.发明授权Stemmed blade for a flow-straightening stage of a gas turbine engine and method of fixing said blade 失效气体涡轮发动机的流动阶段的直角叶片和固定刀片的方法
公开(公告)号：US5236304A
公开(公告)日：1993-08-17
申请号：US806269
申请日：1991-12-13
IPC分类号： F01D9/04
CPC分类号： F01D9/044 , Y10T29/49321 , Y10T29/49323
摘要： A stemmed blade for flow-straightener blading of a gas turbine engine comprises at least one shank at the head of the blade forming a stem for use in fixing the blade. The shank has a notched portion situated adjacent the head of the blade and an end portion separated from the notched portion by a zone of lower tensile strength. The fixing of the blade to the engine casing is carried out by fitting the blade in position with the shank projecting radially outwards through a hole in the casing and then crimping a bush on to the notched portion of the shank using a suitable crimping tool which exerts a compressive force on the bush while exerting a traction on the end of the shank until the zone of lower tensile strength breaks.
摘要翻译： 用于燃气涡轮发动机的流动整流器叶片的干叶片包括在叶片头部处的至少一个柄部，形成用于固定叶片的杆。 柄部具有邻近刀片头部的切口部分，以及与切口部分分离具有较低拉伸强度的区域的端部。 通过将刀片通过套管中的孔径向向外突出的柄将刀片固定在适当位置，然后使用合适的压接工具将衬套压紧到柄的切口部分上来实现刀片到发动机壳体的固定， 在衬套的端部施加牵引力直到较低的拉伸强度断裂的区域上的衬套上的压缩力。
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