公开(公告)号：US07591594B2

公开(公告)日：2009-09-22

申请号：US11072260

申请日：2005-03-07

申请人： Gilles Charier ,  Guy Dusserre-Telmon ,  Marc Marchi ,  Jean-Pierre Mourlan ,  Patrice Rosset ,  Zoltan Zsiga

发明人： Gilles Charier ,  Guy Dusserre-Telmon ,  Marc Marchi ,  Jean-Pierre Mourlan ,  Patrice Rosset ,  Zoltan Zsiga

IPC分类号： F16C43/04 ,  F16C33/58 ,  F01D25/16

CPC分类号： F01D5/026 ,  F01D25/166 ,  F16C2360/23

摘要： A turbomachine roller bearing that supports a shaft constituted by a trunnion of a shaft line of a high-pressure spool of a turbomachine to rotate relative to a stationary support that is connected to a casing of the turbomachine, said bearing comprising rollers inserted between an outer ring disposed adjacent to the stationary support and an inner ring disposed adjacent to the high-pressure trunnion, the inner ring extending along the axis beyond a downstream end of the high-pressure trunnion to which it is secured by clamping means, and being provided with anti-rotation means for preventing said inner ring from rotating relative to the high-pressure trunnion.

摘要翻译： 一种涡轮机滚子轴承，其支撑由涡轮机的高压线轴的轴线的耳轴构成的轴，以相对于连接到涡轮机的壳体的固定支撑件旋转，所述轴承包括插入在外部 环设置成邻近固定支撑件和邻近高压耳轴设置的内环，内环沿着轴线延伸超过高压耳轴的下游端，其通过夹紧装置固定到该下端，并且设置有 用于防止所述内圈相对于高压耳轴旋转的防旋转装置。

公开(公告)号：US20050196088A1

公开(公告)日：2005-09-08

申请号：US11072260

申请日：2005-03-07

申请人： Gilles Charier ,  Guy Dusserre-Telmon ,  Marc Marchi ,  Jean-Pierre Mourlan ,  Patrice Rosset ,  Zoltan Zsiga

发明人： Gilles Charier ,  Guy Dusserre-Telmon ,  Marc Marchi ,  Jean-Pierre Mourlan ,  Patrice Rosset ,  Zoltan Zsiga

IPC分类号： F01D5/02 ,  F01D25/16 ,  F02C7/06 ,  F16C33/58 ,  F16K25/00

CPC分类号： F01D5/026 ,  F01D25/166 ,  F16C2360/23

摘要： A turbomachine roller bearing that supports a shaft constituted by a trunnion of a shaft line of a high-pressure spool of a turbomachine to rotate relative to a stationary support that is connected to a casing of the turbomachine, said bearing comprising rollers inserted between an outer ring disposed adjacent to the stationary support and an inner ring disposed adjacent to the high-pressure trunnion, the inner ring extending along the axis beyond a downstream end of the high-pressure trunnion to which it is secured by clamping means, and being provided with anti-rotation means for preventing said inner ring from rotating relative to the high-pressure trunnion.

摘要翻译： 一种涡轮机滚子轴承，其支撑由涡轮机的高压线轴的轴线的耳轴构成的轴，以相对于连接到涡轮机的壳体的固定支撑件旋转，所述轴承包括插入在外部 环设置成邻近固定支撑件和邻近高压耳轴设置的内环，内环沿着轴线延伸超过高压耳轴的下游端，其通过夹紧装置固定到该下端，并且设置有 用于防止所述内圈相对于高压耳轴旋转的防旋转装置。

公开(公告)号：US07128529B2

公开(公告)日：2006-10-31

申请号：US10876693

申请日：2004-06-28

申请人： Pascal Le Jeune ,  Gilles Charier

发明人： Pascal Le Jeune ,  Gilles Charier

IPC分类号： F04D29/04 ,  F03B11/06

CPC分类号： F01D5/066 ,  F01D5/025 ,  F01D25/16 ,  F16C19/06 ,  F16C35/073 ,  F16C2360/23 ,  F16D1/06

摘要： A device (D) is dedicated to securing a machine shaft (AIP) on a bearing support (SP). This device (D) comprises i) a locknut (19) provided with a stop, comprising a front face (23), a thread (20) intended to interact with a thread (7) of the bearing support (SP), and first coupling means (22), ii) an extraction nut (11) comprising a thread (12) intended to interact with a thread (1) of the shaft (AIP), inverted in relation to the thread (7) of the bearing support (SP), two coupling means (17) and a stop (13) provided with a front face, intended to be supported on a rear face (8) of a stop of the bearing support (SP), and a rear face (14) on which butts the front face (23) of the locknut stop (19) when it is located in an immobilisation position, and iii) a nut lock (24) provided with third (29) and fourth (26) coupling means, designed so as to interact respectively with the first (22) and second (17) coupling means, in order to couple in rotation the extraction nut (11) and the locknut (19) once they have been located in an immobilisation position.

摘要翻译： 设备（D）专用于将机轴（AIP）固定在轴承座（SP）上。 该装置（D）包括i）设置有止动件的锁紧螺母（19），包括前表面（23），用于与轴承支撑件（SP）的螺纹（7）相互作用的螺纹（20） 联接装置（22），ii）提取螺母（11），其包括用于与轴（AIP）的螺纹（1）相互作用的螺纹（12），其相对于轴承支撑件的螺纹（7） SP），两个联接装置（17）和设置有前表面的止动件（13），其被设置为支撑在轴承支撑件（SP）的止动件的后表面（8）上，以及后表面（14） 当其位于固定位置时，所述锁紧螺母止动器（19）的前表面（23）与所述锁定螺母止动器（19）的前表面（23）接合，以及iii）设置有第三（29）和第四（26）联接装置的螺母锁（24） 以便分别与第一（22）和第二（17）联接装置相互作用，以便一旦它们位于一个im中，就将旋转抽出螺母（11）和锁紧螺母（19）联接在一起 动员职位。

公开(公告)号：US20070212226A1

公开(公告)日：2007-09-13

申请号：US11625041

申请日：2007-01-19

申请人： Frederic Guihard ,  Gilles Charier

发明人： Frederic Guihard ,  Gilles Charier

IPC分类号： F04D29/00

CPC分类号： F01D5/026 ,  F02C7/36 ,  F05B2260/301 ,  F05D2250/182

摘要： The invention relates to an assembly between a turbine shaft and a stub axle of a turbomachine compressor shaft, the assembly comprising a substantially cylindrical compressor shaft stub axle, a substantially cylindrical turbine shaft disposed coaxially inside the compressor shaft stub axle, means for transmitting torque between the turbine shaft and the compressor shaft stub axle, and clamping means for clamping a downstream end of the turbine shaft to the compressor shaft stub axle. The compressor shaft stub axle has a plurality of teeth extending radially from its inside surface, and the turbine shaft is provided at its downstream end with a plurality of axial slots, the teeth of the stub axle co-operating with the slots of the turbine shaft.

摘要翻译： 本发明涉及涡轮机轴和涡轮机械压缩机轴的短轴之间的组件，该组件包括基本上圆柱形的压缩机轴短轴，同轴地设置在压缩机轴短轴内的基本上圆柱形的涡轮轴，用于在压缩机轴短轴之间传递扭矩的装置 涡轮轴和压缩机轴短轴，以及用于将涡轮轴的下游端紧固到压缩机轴短轴的夹紧装置。 压缩机轴短轴具有从其内表面径向延伸的多个齿，并且涡轮轴在其下游端设有多个轴向槽，短轴的齿与涡轮轴的槽配合 。

公开(公告)号：US20060233479A1

公开(公告)日：2006-10-19

申请号：US11402974

申请日：2006-04-13

申请人： Philippe Bouiller ,  Gilles Charier ,  Daniel Plona

发明人： Philippe Bouiller ,  Gilles Charier ,  Daniel Plona

IPC分类号： F16C43/04

CPC分类号： F01D25/16 ,  F02C7/06 ,  F05D2260/30 ,  F16C19/26 ,  F16C33/58 ,  F16C33/6651 ,  F16C33/6677 ,  F16C35/063 ,  F16C2360/23

摘要： The assembly arrangement between an inner race 6 of a bearing and a journal 2 supported in rotation in this bearing comprises: a journal annular groove 36 and a race annular groove 26 which interact to form an annular channel 52 when they are placed opposite one another, a retaining ring 40 placed in the said annular channel 52, which prevents a relative movement in translation between the said journal 2 and the said inner race 6, and at least one recess 38 of the said journal 2 and at least one tooth 32 of the said inner race 6, which interact to prevent a relative movement in rotation between the said journal 2 and the said inner race 6.

摘要翻译： 轴承的内圈6和轴承2之间的组合布置在该轴承中被支承为旋转的轴颈2包括：轴颈环形槽36和座圈环形槽26，当它们彼此相对放置时相互作用以形成环形通道52， 设置在所述环形通道52中的保持环40，其防止在所述轴颈2和所述内座圈6之间平移的相对运动，以及所述轴颈2的至少一个凹部38和所述轴颈2的至少一个齿32 所述内圈6相互作用以防止在所述轴颈2和所述内座圈6之间旋转的相对运动。

公开(公告)号：US20080063515A1

公开(公告)日：2008-03-13

申请号：US11755934

申请日：2007-05-31

申请人： Eric BIL ,  Gilles Charier ,  Philippe Fessou ,  Patrick Morel

发明人： Eric BIL ,  Gilles Charier ,  Philippe Fessou ,  Patrick Morel

IPC分类号： F04D27/00

CPC分类号： F02K3/075 ,  F01D17/105 ,  F04D27/0215 ,  F04D27/023 ,  F04D29/545 ,  F05D2240/55 ,  F05D2260/50

摘要： The bypass turbomachine comprises, between a primary flowpath (2) and a secondary flowpath (3), a structural intermediate casing (14). A bleed passage (29) allows the diversion of a portion of the gas stream toward the secondary flowpath (3), downstream of support arms (18) situated at the periphery of the intermediate casing. A bleed opening (28) emerges upstream of the support arms (18). A slide valve (22) slides between three positions, namely a closed position in which the slide valve (22) completely blocks off the bleed passage and opening, an intermediate position in which the bleed opening (28) emerging upstream of the support arms (18) is blocked off, while the bleed passage (29) for diverting a portion of the gas stream downstream of the support arms (18) is open, and an open position in which the bleed opening (28) emerging upstream of the support arms (18) and the bleed passage (29) emerging downstream of the support arms are both open.

摘要翻译： 旁通涡轮机在主流路（2）和次流路（3）之间包括结构中间壳体（14）。 排放通道（29）允许气流的一部分朝着位于中间壳体的周边的支撑臂（18）的下游侧向二级流路（3）转向。 出血口（28）出现在支撑臂（18）的上游。 滑阀（22）在三个位置之间滑动，即关闭位置，其中滑阀（22）完全阻止排放通道和打开;中间位置，其中出现在支撑臂上游的排气口（28） 18）被阻止，而用于将支撑臂（18）下游的气流的一部分转向的排放通道（29）是打开的，并且打开位置，其中出口开口（28）出现在支撑臂 （18）和出现在支撑臂下游的排出通道（29）都是开放的。

公开(公告)号：US20070137221A1

公开(公告)日：2007-06-21

申请号：US11551560

申请日：2006-10-20

申请人： Gilles Charier ,  Stephane Rousselin ,  Philippe Bouiller

发明人： Gilles Charier ,  Stephane Rousselin ,  Philippe Bouiller

IPC分类号： F02C7/12

CPC分类号： F02C7/12 ,  F01D5/082 ,  F05D2220/3212 ,  F05D2260/60

摘要： The present invention relates to a device for ventilating turbine components in a gas turbine engine comprising two turbine rotors mechanically independent of each other, each with at least one turbine disk, an HP turbine disk and an LP turbine disk respectively, and with a first circuit for ventilating the LP turbine. The device comprises an air compression wheel arranged downstream of the HP turbine disk especially between said two turbine disks, HP and LP in order to assist the circulation of the air in said first circuit. The invention also relates to the wheel.

摘要翻译： 本发明涉及一种用于在燃气涡轮发动机中通风涡轮机部件的装置，其包括机械上彼此独立的两个涡轮转子，每个具有至少一个涡轮盘，HP涡轮盘和LP涡轮盘，并且具有第一回路 用于使LP涡轮机通风。 该装置包括布置在HP涡轮盘的下游的空气压缩轮，特别是在所述两个涡轮盘HP和LP之间，以帮助空气在所述第一回路中循环。 本发明还涉及车轮。

公开(公告)号：US20060188369A1

公开(公告)日：2006-08-24

申请号：US11355884

申请日：2006-02-17

申请人： Gilles Charier ,  Claude Nottin ,  Stephane Rousselin

发明人： Gilles Charier ,  Claude Nottin ,  Stephane Rousselin

IPC分类号： F01D9/00

CPC分类号： F01D17/141 ,  F01D17/14 ,  F05D2300/50212

摘要： A device for varying the section of the throat of a turbine nozzle, the nozzle being formed by a plurality of stationary vanes extending radially between outer and inner annular platforms and spaced apart from one another in order to define a throat presenting a minimum flow section. The device comprises an annular element having a coefficient of expansion that is less than that of the platforms of the nozzle, the annular element being secured to the outer platform and being capable of taking up two positions: one position corresponding to no expansion of the platforms, in which the element provides continuity for the profile of the flow passage; and another position corresponding to the platforms having expanded, in which position the element projects into the flow passage so as to reduce its section.

公开(公告)号：US20050013696A1

公开(公告)日：2005-01-20

申请号：US10876693

申请日：2004-06-28

申请人： Pascal Le Jeune ,  Gilles Charier

发明人： Pascal Le Jeune ,  Gilles Charier

IPC分类号： F01D5/02 ,  F01D5/06 ,  F01D25/16 ,  F16B39/02 ,  F16B39/12 ,  F16B39/16 ,  F16C35/073 ,  F16D1/06 ,  F16B43/00

CPC分类号： F01D5/066 ,  F01D5/025 ,  F01D25/16 ,  F16C19/06 ,  F16C35/073 ,  F16C2360/23 ,  F16D1/06

摘要： A device (D) is dedicated to securing a machine shaft (AIP) on a bearing support (SP). This device (D) comprises i) a locknut (19) provided with a stop, comprising a front face (23), a thread (20) intended to interact with a thread (7) of the bearing support (SP), and first coupling means (22), ii) an extraction nut (11) comprising a thread (12) intended to interact with a thread (1) of the shaft (AIP), inverted in relation to the thread (7) of the bearing support (SP), two coupling means (17) and a stop (13) provided with a front face, intended to be supported on a rear face (8) of a stop of the bearing support (SP), and a rear face (14) on which butts the front face (23) of the locknut stop (19) when it is located in an immobilisation position, and iii) a nut lock (24) provided with third (29) and fourth (26) coupling means, designed so as to interact respectively with the first (22) and second (17) coupling means, in order to couple in rotation the extraction nut (11) and the locknut (19) once they have been located in an irnmobilisation position.

摘要翻译： 设备（D）专用于将机轴（AIP）固定在轴承座（SP）上。 该装置（D）包括i）设置有止动件的锁紧螺母（19），包括前表面（23），用于与轴承支撑件（SP）的螺纹（7）相互作用的螺纹（20） 联接装置（22），ii）提取螺母（11），其包括用于与轴（AIP）的螺纹（1）相互作用的螺纹（12），其相对于轴承支撑件的螺纹（7） SP），两个联接装置（17）和设置有前表面的止动件（13），其被设置为支撑在轴承支撑件（SP）的止动件的后表面（8）上，以及后表面（14） 当其位于固定位置时，所述锁紧螺母止动器（19）的前表面（23）与所述锁定螺母止动器（19）的前表面（23）接合，以及iii）设置有第三（29）和第四（26）联接装置的螺母锁（24） 以便分别与第一（22）和第二（17）联接装置相互作用，以便一旦它们位于不饱和位置，就将旋转抽出螺母（11）和锁紧螺母（19）联接在一起。