公开(公告)号：US07946811B2

公开(公告)日：2011-05-24

申请号：US11625967

申请日：2007-01-23

申请人： Olivier Abgrall ,  Yvon Cloarec

发明人： Olivier Abgrall ,  Yvon Cloarec

IPC分类号： F01D9/04

CPC分类号： F01D9/041 ,  F01D25/246 ,  F04D29/542

摘要： An assembly of sectorized fixed compressors for a turbomachine compressor is disclosed. The assembly is a single piece and includes two coaxial rings connected by radial airfoils. The outer ring includes two annular mounting lugs on a casing of the compressor. At least one of these annular lugs is connected to the outer ring in a zone axially separate from the zone for connecting the leading edges or trailing edges of the airfoils to the outer ring.

摘要翻译： 公开了一种用于涡轮机压缩机的扇形固定式压缩机组件。 该组件是单件，并且包括通过径向翼型件连接的两个同轴环。 外环在压缩机的壳体上包括两个环形安装凸耳。 这些环形凸耳中的至少一个在与用于将翼型件的前缘或后缘连接到外圈的区域轴向分离的区域中连接到外环。

公开(公告)号：US20070172349A1

公开(公告)日：2007-07-26

申请号：US11625967

申请日：2007-01-23

申请人： Olivier Abgrall ,  Yvon Cloarec

发明人： Olivier Abgrall ,  Yvon Cloarec

IPC分类号： F01D9/00

CPC分类号： F01D9/041 ,  F01D25/246 ,  F04D29/542

摘要： An assembly of sectorized fixed compressors (50) for a turbomachine compressor, this assembly being made in a single piece and comprising two coaxial rings (20, 52) connected by radial airfoils (24), the outer ring comprising two annular mounting lugs (56, 66) on a casing of the compressor, at least one of these annular lugs being connected to the outer ring in a zone axially separate from the zone for connecting the leading edges (26) or trailing edges (28) of the airfoils to the outer ring.

摘要翻译： 用于涡轮机械压缩机的扇形固定压缩机（50）的组件，该组件制成单件并且包括由径向翼型件（24）连接的两个同轴环（20,52），外环包括两个环形安装凸耳（56 ，66）在所述压缩机的壳体上，所述环形凸耳中的至少一个在与所述区域轴向分离的区域中连接到所述外环，用于将所述翼型件的前缘（26）或后缘（28）连接到 外圈。

公开(公告)号：US08585369B2

公开(公告)日：2013-11-19

申请号：US12937894

申请日：2009-04-24

申请人： Stephan Yves Aubin ,  Erick Jacques Boston ,  Yvon Cloarec

发明人： Stephan Yves Aubin ,  Erick Jacques Boston ,  Yvon Cloarec

IPC分类号： F01D5/02

CPC分类号： F04D29/322 ,  F01D5/3015

摘要： A device for axial retention of mobile vanes mounted on a rotor disc includes two open rings, superimposed. At least one of the rings includes a rotating stop mechanism configured to cooperate with at least one hook of the disc. The two open rings are mounted in a discontinuous groove formed in the hooks, at the end of teeth situated on the periphery of the rotor disc, such that the rotating stop mechanism of the first ring is placed in the opening of the second ring. The significance of contact surfaces between the two rings allows a damping of vibrations during operation.

摘要翻译： 安装在转子盘上的用于轴向保持移动叶片的装置包括叠加的两个开环。 至少一个环包括被配置为与盘的至少一个钩配合的旋转止动机构。 两个敞开的环安装在形成在钩中的不连续的槽中，位于转子盘的周边的齿的端部，使得第一环的旋转止动机构被放置在第二环的开口中。 两个环之间的接触表面的意义允许在操作期间阻尼振动。

公开(公告)号：US08858181B2

公开(公告)日：2014-10-14

申请号：US13224774

申请日：2011-09-02

申请人： Yvon Cloarec

发明人： Yvon Cloarec

IPC分类号： F01D5/30 ,  F01D5/32

CPC分类号： F01D5/3038 ,  F01D5/32 ,  F05D2230/64 ,  Y10T29/49321

摘要： The invention relates to a device (30) for blockage of vanes in a circumferential groove (10) of a turbine engine disc, the device being intended to deploy in a radial direction to be locked in the circumferential groove open radially. According to the invention, the blocking device comprises a first and a second piece (32, 34) designed to deploy in the radial direction by relative displacement of these pieces in the circumferential direction (23).

摘要翻译： 本发明涉及一种用于在涡轮发动机盘的周向槽（10）中阻塞叶片的装置（30），该装置旨在沿径向方向展开以锁定在径向开口的周向槽中。 根据本发明，阻挡装置包括第一和第二部件（32,34），其被设计成沿圆周方向（23）通过这些部件的相对位移沿径向展开。

公开(公告)号：US20130202423A1

公开(公告)日：2013-08-08

申请号：US13805142

申请日：2011-06-16

申请人： Yvon Cloarec

发明人： Yvon Cloarec

IPC分类号： F01D9/00

CPC分类号： F01D9/00 ,  F01D5/225 ,  F01D5/26 ,  F01D9/041 ,  F01D9/042 ,  F01D25/04 ,  F01D25/06 ,  F01D25/246 ,  F04D29/542 ,  F04D29/668 ,  F05D2240/80 ,  F05D2260/36 ,  F05D2260/96 ,  Y02T50/671

摘要： A stator angular sector for a turbine engine compressor and including: an outer shroud and an inner shroud; and at least one vane extending radially between the shrouds and connected thereto at its radial ends. At one of its axial ends the outer shroud includes a cavity opening out to the axial end and extending between a radially-inner tongue of the outer shroud to which the radially-outer end of the vane is connected, and a radially-outer tongue of the outer shroud carrying a mounting mechanism for mounting the stator angular sector to a casing of the engine. An abutment-forming insert is housed at least in part in the cavity, the abutment-forming insert configured to limit radial movements of the radially-inner tongue by contact and thus to modify vibratory behavior of the radially-inner tongue.

摘要翻译： 一种用于涡轮发动机压缩机的定子角扇形件，包括：外护罩和内护罩; 以及至少一个叶片，其径向延伸在护罩之间并且在其径向端部处与其连接。 在其一个轴向端部处，外护罩包括通向轴向端部并且在外护罩的径向内部舌部之间延伸的空腔，叶片的径向外端连接到该外部舌部和径向外部舌部 该外护罩具有用于将定子角扇区安装到发动机壳体的安装机构。 邻接形成插入件至少部分地容纳在空腔中，邻接形成插入件构造成通过接触来限制径向内部舌片的径向运动，并且因此改变径向内部舌部的振动特性。

公开(公告)号：US09222363B2

公开(公告)日：2015-12-29

申请号：US13805142

申请日：2011-06-16

申请人： Yvon Cloarec

发明人： Yvon Cloarec

IPC分类号： F01D9/00 ,  F01D25/04 ,  F01D5/22 ,  F01D25/06 ,  F01D5/26 ,  F01D25/24 ,  F04D29/54 ,  F04D29/66 ,  F01D9/04

CPC分类号： F01D9/00 ,  F01D5/225 ,  F01D5/26 ,  F01D9/041 ,  F01D9/042 ,  F01D25/04 ,  F01D25/06 ,  F01D25/246 ,  F04D29/542 ,  F04D29/668 ,  F05D2240/80 ,  F05D2260/36 ,  F05D2260/96 ,  Y02T50/671

摘要： A stator angular sector for a turbine engine compressor and including: an outer shroud and an inner shroud; and at least one vane extending radially between the shrouds and connected thereto at its radial ends. At one of its axial ends the outer shroud includes a cavity opening out to the axial end and extending between a radially-inner tongue of the outer shroud to which the radially-outer end of the vane is connected and a radially-outer tongue of the outer shroud carrying a mounting mechanism for mounting the stator angular sector to a casing of the engine. An abutment-forming insert is housed at least in part in the cavity, the abutment-forming insert configured to limit radial movements of the radially-inner tongue by contact and thus to modify vibratory behavior of the radially-inner tongue.

摘要翻译： 一种用于涡轮发动机压缩机的定子角扇形件，包括：外护罩和内护罩; 以及至少一个叶片，其径向延伸在护罩之间并且在其径向端部处与其连接。 在其一个轴向端部处，外护罩包括通向轴向端部并且在外护罩的径向内部舌部之间延伸的空腔，叶片的径向外端与其连接，径向外部舌部 外护罩带有用于将定子角扇区安装到发动机壳体的安装机构。 邻接形成插入件至少部分地容纳在空腔中，邻接形成插入件构造成通过接触来限制径向内部舌片的径向运动，并且因此改变径向内部舌部的振动特性。

公开(公告)号：US07029227B2

公开(公告)日：2006-04-18

申请号：US10477234

申请日：2002-05-10

申请人： Marc Berthillier ,  Yvon Cloarec ,  Eric Seinturier

发明人： Marc Berthillier ,  Yvon Cloarec ,  Eric Seinturier

IPC分类号： F03D1/02

CPC分类号： F01D5/10 ,  F04D29/544 ,  F04D29/666 ,  F16F15/20

摘要： A method of reducing vibration in a structure comprising at least one rotor (101j) and a fixed set of sources of disturbance (102j) liable to give rise to disturbances in the fluid flow (11) that cause the rotor to vibrate, the method comprising a step of distributing the fixed sources of disturbance angularly in non-uniform manner so as to reduce the amplitude of excitation as seen by the rotor, and a step which consists in verifying that the maximum amplitude of a response of the rotor to the excitation is obtained by: determining a first signal whose Fourier transform corresponds to the frequency spectrum of the excitation in the event of the fixed sources of disturbance being distributed in a predetermined angular distribution; by modifying the first signal into a second signal adapted to said selected angular distribution for the fixed sources of disturbance; by determining the frequency spectrum of the excitation by calculating the Fourier transform of the second signal; and by calculating the response of the rotor to the excitation on the basis of the frequency spectrum of the excitation.

摘要翻译： 一种降低结构中的振动的方法，该结构包括至少一个转子（101）和一组固定的干扰源（102），易于引起干扰源 导致转子振动的流体流动（11），该方法包括以不均匀的方式角度地分布固定的干扰源的步骤，以减小由转子看到的激励振幅，以及包括 在验证转子对激励的响应的最大振幅是通过以下方式获得的：确定在固定的干扰源以预定的角度分布分布的情况下，傅里叶变换对应于激励的频谱的第一信号 ; 通过将所述第一信号修改为适于所述固定干扰源的所述选定角分布的第二信号; 通过计算第二信号的傅立叶变换来确定激励的频谱; 并且通过基于激励的频谱计算转子对激励的响应。

公开(公告)号：US08206090B2

公开(公告)日：2012-06-26

申请号：US12194650

申请日：2008-08-20

申请人： Yvon Cloarec

发明人： Yvon Cloarec

IPC分类号： F01D17/12

CPC分类号： F01D11/001 ,  F01D17/162 ,  F04D29/102 ,  F04D29/563 ,  F05D2250/312 ,  F05D2260/56 ,  Y02T50/671

摘要： A stator stage of a compressor of a turbomachine including an annular row of variable-pitch vanes is disclosed. Each vane includes an external cylindrical pivot defining the axis of rotation of the vane, and an internal cylindrical pivot mounted in a housing of an internal ring. The internal pivot of each vane extends along an axis substantially parallel to the axis of rotation of the vane and at a distance from this axis, and is mounted in the housing of the ring by a swiveling or a tilting system.

摘要翻译： 公开了一种涡轮机的压缩机的定子级，该涡轮机包括环形排的可变节流叶片。 每个叶片包括限定叶片的旋转轴线的外部圆柱形枢轴和安装在内部环的壳体中的内部圆柱形枢轴。 每个叶片的内部枢轴沿基本上平行于叶片的旋转轴线的轴线延伸并且距离该轴线一定距离，并且通过旋转或倾斜系统安装在环的壳体中。

公开(公告)号：US07850430B2

公开(公告)日：2010-12-14

申请号：US11835117

申请日：2007-08-07

申请人： Yvon Cloarec

发明人： Yvon Cloarec

IPC分类号： F01D5/30

CPC分类号： F01D5/3015 ,  Y02T50/671

摘要： A turbomachine rotor blade comprising a root (14) mounted in a channel of the periphery of a disk and held by an annular flange (18) which presses on the root (14) of the blade (12), this root comprising a stop (44) engaging in a matching cavity of the flange in order to stop it rotating about the axis of the disk, the central portion of the stop having a thickness less than that of the ends of the stop.

摘要翻译： 一种涡轮机械转子叶片，其包括安装在盘的周边的通道中并由压在叶片（12）的根部（14）上的环形凸缘（18）保持的根部（14），该根部包括止动件 44）接合凸缘的匹配腔以便使其围绕盘的轴线旋转，止动件的中心部分的厚度小于止动件端部的厚度。

公开(公告)号：US09228449B2

公开(公告)日：2016-01-05

申请号：US13805211

申请日：2011-06-16

申请人： Yvon Cloarec

发明人： Yvon Cloarec

IPC分类号： F01D25/04 ,  F01D25/06 ,  F04D29/66 ,  F01D5/26 ,  F01D9/04 ,  F01D25/24 ,  F01D5/22

CPC分类号： F01D25/04 ,  F01D5/225 ,  F01D5/26 ,  F01D9/042 ,  F01D25/06 ,  F01D25/246 ,  F04D29/542 ,  F04D29/668 ,  F05D2240/80 ,  F05D2260/38 ,  F05D2260/96 ,  Y02T50/671

摘要： A stator angular sector for a turbine engine compressor including: an outer shroud and an inner shroud, and at least one vane extending radially between the shrouds. The outer shroud includes first and second mounting mechanisms for mounting the stator angular sector on a casing of the engine, which mechanisms are oriented parallel to the axis in opposite directions and connected together by an intermediate portion. The outer shroud includes at least one axial end portion extending from the intermediate portion with which at least one damper-forming insert is configured to come into contact, such that beyond a given value for amplitude of vibration of the end portion, the damper insert and the end portion are configured to move relative to each other to vary total moving mass moving with the end portion, thereby modifying vibratory behavior of the end portion.

摘要翻译： 一种用于涡轮发动机压缩机的定子角扇区，包括：外护罩和内护罩，以及在护罩之间径向延伸的至少一个叶片。 外护罩包括用于将定子角扇区安装在发动机的壳体上的第一和第二安装机构，这些机构在相反方向上平行于轴线定向并通过中间部分连接在一起。 外护罩包括从中间部分延伸的至少一个轴向端部，通过该至少一个轴向端部，至少一个阻尼器形成插入件构造成接触，使得超过端部振动的给定值，阻尼器插入件和 端部构造成相对于彼此移动以改变随着端部移动的总运动质量，从而改变端部的振动特性。