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公开(公告)号：US20050201859A1
公开(公告)日：2005-09-15
申请号：US10517613
申请日：2003-06-25
CPC分类号： F01D5/081 , F01D5/3015 , F01D11/02 , F02C7/28 , Y02T50/671 , Y02T50/676
摘要： A ventilation circuit of a turbomachine turbine rotor having a turbine disk and an upstream flange disposed upstream from a combustion chamber from which it is spaced apart by a cavity. A first cooling air circuit delivers air into the cavity via main injectors and holes in the flange. A second cooling air circuit delivers air through enclosures delimited by the combustion chamber inner casing and the rotor via a discharge labyrinth, an under-injector labyrinth, and at least one labyrinth downstream from the main injectors between an annular structure and the flange. Three single-wiper labyrinths delimiting two cavities upstream from the venting cavity of the turbine disk are provided downstream from the main injectors. One of the cavities is fed with air from the second circuit upstream from the under-injector labyrinth by bore holes in the annular structure sloping tangentially in the rotation direction of the rotor.
摘要翻译： 具有涡轮机涡轮机转子的通风回路，其具有涡轮盘和设置在燃烧室上游的上游凸缘，所述燃烧室被空腔间隔开。 第一个冷却空气回路通过主注射器和法兰中的孔将空气输送到空腔中。 第二冷却空气回路通过排气迷宫，下注射器迷宫和至少一个迷宫在主喷射器下游的环形结构和凸缘之间的空气通过燃烧室内壳和转子限定的空气。 在主喷射器的下游设置有将涡轮盘的通气腔上游限定两个空腔的三个单刮水器迷宫。 其中一个空腔通过在转子的旋转方向上切向倾斜的环形结构中的钻孔而从喷射器迷宫的上游的第二回路供给空气。
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2.发明授权公开(公告)号：US07766574B2
公开(公告)日：2010-08-03
申请号：US11107854
申请日：2005-04-18
申请人： Jean-Philippe Maffre
发明人： Jean-Philippe Maffre
CPC分类号： F01D25/243 , F01D5/066 , F05B2260/301 , F16B2200/506 , F16L23/036 , Y10T403/1691 , Y10T403/75
摘要： A fastener system is configured to fasten together at least two parts, one of which includes at least one flange that is caused to bear against a surface of the other part by a plurality of pins each presenting a collar having a non-circular outline. The collar is received in a groove formed in a bearing surface of one of the parts, and is designed to prevent the pins from turning by abutment against a wall, wherein the outline of each collar includes two substantially opposite plane surfaces that serve as mutual abutments against two adjacent collars.
摘要翻译： 紧固件系统被配置成将至少两个部件紧固在一起，其中一个部件包括至少一个凸缘，所述凸缘通过多个销钉而承受抵靠另一部件的表面，每个销子具有非圆形轮廓的轴环。 套环被容纳在形成在其中一个部件的支承表面中的凹槽中，并且被设计成防止销通过抵靠壁而转动，其中每个轴环的轮廓包括用作相互邻接的两个基本上相对的平面 对着两个相邻的衣领。
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公开(公告)号：US20060291955A1
公开(公告)日：2006-12-28
申请号：US11181885
申请日：2005-07-15
申请人： Jean-Philippe Maffre
发明人： Jean-Philippe Maffre
IPC分类号： B25G3/28
CPC分类号： F01D25/16 , F05D2230/60 , Y10T403/7026
摘要： The present invention relates to an assembly composed of a rotary shaft and of a roller bearing supporting said shaft, the bearing including a ring interconnected with the shaft and forming a raceway. The assembly is characterised in that the ring is immobilised in rotation on the shaft by a coupling formed by a plurality of teeth on the shaft co-operating with lugs interconnected with the ring, the lugs being received between said teeth, and in axial direction by a snap ring transversal in the form of a ring portion. The invention applies in particular to the installation of a ring of a roller bearing on a turbine shaft.
摘要翻译： 本发明涉及一种由旋转轴和支撑所述轴的滚子轴承组成的组件，该轴承包括与轴相互连接并形成滚道的环。 该组件的特征在于，所述环通过由与所述环相互连接的凸耳配合的所述轴上的多个齿形成的联接器固定在所述轴上，所述凸耳被接收在所述齿之间，并且在轴向方向上通过 以环形部分形式横切的卡环。 本发明特别适用于在涡轮轴上安装滚子轴承的环。
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公开(公告)号：US06520743B2
公开(公告)日：2003-02-18
申请号：US09907679
申请日：2001-07-19
IPC分类号： B63H120
CPC分类号： F01D11/006 , F01D5/3015
摘要： An apparatus for axially retaining rotor blades to an annular radially extending disk having a recess and a flange. An annular retaining ring is disposed in the recess and includes an axially extending lip and an axially outer side forming an annular bevel surface along a radially outer edge. A retaining plate having an axially extending base, a radially extending outward arm and a radially extending inward leg having an annular bevel surface along an axially inner, radially inner edge is affixed to the disk and the leg cooperates with the lip of the ring. Wherein, the bevel surfaces of the retaining plate and retaining ring are arranged outwardly opposite to one another so that the bevel surfaces are radially compressed along each other as the base slidably engages with the recess walls.
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5.发明申请公开(公告)号：US20050238423A1
公开(公告)日：2005-10-27
申请号：US11107854
申请日：2005-04-18
申请人： Jean-Philippe Maffre
发明人： Jean-Philippe Maffre
IPC分类号： F01D5/02 , F01D5/06 , F01D25/24 , F16B5/02 , F16B33/00 , F16B35/04 , F16B39/28 , F16L23/036 , H01R13/213
CPC分类号： F01D25/243 , F01D5/066 , F05B2260/301 , F16B2200/506 , F16L23/036 , Y10T403/1691 , Y10T403/75
摘要： The invention relates to a fastener system for fastening together at least two parts, one of which includes at least one flange that is caused to bear against a surface of the other part by means of a plurality of pins each presenting a collar having a non-circular outline, said collar being received in a groove formed in a bearing surface of one of said parts, and being designed to prevent said pins from turning by abutment against a wall, wherein the outline of each collar includes two substantially opposite plane surfaces that serve as mutual abutments against two adjacent collars.
摘要翻译： 本发明涉及一种用于将至少两个部件紧固在一起的紧固件系统，其中的一个部件包括至少一个凸缘，该凸缘通过多个销而承受抵靠另一部分的表面， 所述套环被容纳在形成在所述部件之一的轴承表面中的凹槽中，并且被设计成通过抵靠壁来防止所述销转动，其中每个轴环的轮廓包括两个基本上相对的平面， 作为与两个相邻套环的相互邻接。
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公开(公告)号：US07048497B2
公开(公告)日：2006-05-23
申请号：US10491438
申请日：2002-11-07
IPC分类号： F01D25/12
CPC分类号： F01D11/001 , F01D5/081 , F05D2260/6022 , Y02T50/673 , Y02T50/676
摘要： A gas turbine stator including at least a first injector providing a passage for a main cooling air stream into a pressurized chamber. An evacuation mechanism discharges air coming from an internal labyrinth gland of a first cavity towards a lower-pressure second cavity. A second injector evacuates the air contained in the second cavity towards a main duct. The stator further includes a third injector designed to generate an overpressure close to the internal labyrinth gland in the pressurized chamber.
摘要翻译： 一种燃气轮机定子，其至少包括第一喷射器，该第一喷射器提供用于主冷却空气流进入加压室的通道。 排气机构将来自第一腔的内部迷宫密封的空气排出到较低压力的第二腔。 第二喷射器将包含在第二空腔中的空气朝向主管排出。 定子还包括第三喷射器，其被设计成在加压室内靠近内部迷宫压盖产生过压。
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