公开(公告)号：US08100635B2

公开(公告)日：2012-01-24

申请号：US12254518

申请日：2008-10-20

申请人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Nicolas Pommier

发明人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Nicolas Pommier

IPC分类号： F01D5/14 ,  F03D11/00 ,  F04D29/38

CPC分类号： F01D11/005 ,  F01D11/24 ,  F05D2240/11 ,  Y02T50/671

摘要： A turbine stage in a turbine engine, including a wheel with blades rotating inside a sealing ring held by a casing of the turbine, and an annular thermal protection sheet mounted between the casing and the sealing ring is disclosed. The annular thermal protection sheet is formed by a plurality of curved plates mounted end-to-end and attached by pins to the casing.

摘要翻译： 公开了一种涡轮发动机中的涡轮级，包括在由涡轮机的壳体保持的密封环内旋转的叶片的叶片，以及安装在壳体和密封环之间的环形热保护片。 环形热保护片由端对端安装的多个弯曲板形成，并通过销附接到壳体。

公开(公告)号：US08403636B2

公开(公告)日：2013-03-26

申请号：US12038422

申请日：2008-02-27

申请人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Vincent Philippot

发明人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Vincent Philippot

IPC分类号： F01D9/04

CPC分类号： F01D11/12 ,  F01D9/04 ,  F01D25/246 ,  F05D2240/11

摘要： A turbine stage in a turbomachine including ring sectors arranged about a turbine impeller, and an annular support supporting the ring sectors and attached to a turbine casing is disclosed. The annular support is able to be deformed elastically in the radial direction to cushion at least a portion of the deformations of the turbine casing in operation.

摘要翻译： 公开了一种涡轮机中的涡轮级，包括围绕涡轮机叶轮布置的环形部分，以及支撑环形部分并附接到涡轮壳体的环形支撑件。 环形支撑件能够在径向方向上弹性变形以在运行中缓冲涡轮机壳体的至少一部分变形。

公开(公告)号：US08133018B2

公开(公告)日：2012-03-13

申请号：US12038604

申请日：2008-02-27

申请人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Vincent Philippot

发明人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Vincent Philippot

IPC分类号： F01D9/00

CPC分类号： F01D25/246 ,  F01D9/042

摘要： A high-pressure turbine of a turbomachine, including at least one upstream guide vane element and an impeller mounted so as to rotate inside ring sectors attached to an annular support which is suspended from an outer casing, the upstream guide vane element including, at its radially inner end, a mechanism for attachment to an inner casing and, at its radially outer end, a mechanism for pressing axially on a fixed element of the turbine that is suspended from the outer casing independently of the annular support for attachment of the ring sectors.

摘要翻译： 涡轮机的高压涡轮机，包括至少一个上游引导叶片元件和叶轮，其安装成在附接到从外壳悬挂的环形支撑件的环形部分内旋转，所述上游引导叶片元件包括在其上 径向内端，用于附接到内壳体的机构，并且在其径向外端处具有用于轴向地按压在涡轮机的固定元件上的机构，所述机构与所述环形支撑件独立于所述环形支撑件悬挂， 。

公开(公告)号：US20080267768A1

公开(公告)日：2008-10-30

申请号：US12038604

申请日：2008-02-27

申请人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Vincent Philippot

发明人： Mathieu Dakowski ,  Claire Dorin ,  Alain Dominique Gendraud ,  Vincent Philippot

IPC分类号： F01D5/02

CPC分类号： F01D25/246 ,  F01D9/042

摘要： High-pressure turbine of a turbomachine A high-pressure turbine (10) of a turbomachine, comprising at least one upstream guide vane element (16) and an impeller (18) mounted so as to rotate inside ring sectors (20) attached to an annular support (24) which is suspended from an outer casing (22), the upstream guide vane element comprising, at its radially inner end, means of attachment to an inner casing and, at its radially outer end, means (102, 104) for pressing axially on a fixed element (90) of the turbine that is suspended from the outer casing independently of the annular support for attachment of the ring sectors.

摘要翻译： 涡轮机的高压涡轮机涡轮机的高压涡轮机（10），包括至少一个上游引导叶片元件（16）和叶轮（18），所述至少一个上游引导叶片元件（16）和叶轮（18）安装成在环形部分（20）内旋转， 环形支撑件（24），其从外壳（22）悬挂，所述上游引导叶片元件在其径向内端包括附接到内壳的装置，并且在其径向外端处包括装置（102,104） 用于轴向地压在涡轮机的固定元件（90）上，所述固定元件（90）独立于环形支撑件从外壳悬挂以附接环形部分。

公开(公告)号：US20110229314A1

公开(公告)日：2011-09-22

申请号：US13059350

申请日：2009-08-24

申请人： Mathieu Dakowski ,  Alain Dominique Gendraud

发明人： Mathieu Dakowski ,  Alain Dominique Gendraud

IPC分类号： F01D9/00

CPC分类号： F02C3/045 ,  F01D9/042 ,  F01D25/246 ,  F05D2250/41 ,  F05D2270/114 ,  Y02T50/671

摘要： An assembling of a guide vane assembly of a turbomachine turbine, formed by an annular row of stationary flow-stabilizing vanes. An outer edge of the guide vane assembly is axially bearing on a line of an external casing of the turbine and an inner edge of the guide vane assembly is in axial sliding connection with the line of the internal casing of the turbine, the axial sliding connection allowing the inner edge to be free along the motor axis with the axial stop being achieved by the axial bearing of the outer edge of the vane.

摘要翻译： 一种涡轮机涡轮机的导叶组件的组装，由一组固定的流动稳定叶片形成。 导向叶片组件的外边缘轴向地轴承在涡轮机的外壳的一条线上，并且导向叶片组件的内边缘与涡轮机的内壳线的轴向滑动连接，轴向滑动连接 允许内边缘沿着马达轴线自由，其中轴向止动通过叶片的外边缘的轴向轴承来实现。

公开(公告)号：US08858169B2

公开(公告)日：2014-10-14

申请号：US13059350

申请日：2009-08-24

申请人： Mathieu Dakowski ,  Alain Dominique Gendraud

发明人： Mathieu Dakowski ,  Alain Dominique Gendraud

IPC分类号： F01D1/02 ,  F01D25/24

CPC分类号： F02C3/045 ,  F01D9/042 ,  F01D25/246 ,  F05D2250/41 ,  F05D2270/114 ,  Y02T50/671

摘要： An assembling of a guide vane assembly of a turbomachine turbine, formed by an annular row of stationary flow-stabilizing vanes. An outer edge of the guide vane assembly is axially bearing on a line of an external casing of the turbine and an inner edge of the guide vane assembly is in axial sliding connection with the line of the internal casing of the turbine, the axial sliding connection allowing the inner edge to be free along the motor axis with the axial stop being achieved by the axial bearing of the outer edge of the vane.

摘要翻译： 一种涡轮机涡轮机的导叶组件的组装，由一组固定的流动稳定叶片形成。 导向叶片组件的外边缘轴向地轴承在涡轮机的外壳的一条线上，并且导向叶片组件的内边缘与涡轮机的内壳线的轴向滑动连接，轴向滑动连接 允许内边缘沿着马达轴线自由，其中轴向止动通过叶片的外边缘的轴向轴承来实现。

公开(公告)号：US07533533B2

公开(公告)日：2009-05-19

申请号：US11236576

申请日：2005-09-28

申请人： Daniel Olivier Bainachi ,  Mathieu Dakowski ,  Olivier Kreder ,  Romain Lunel ,  Daniel Georges Plona

发明人： Daniel Olivier Bainachi ,  Mathieu Dakowski ,  Olivier Kreder ,  Romain Lunel ,  Daniel Georges Plona

IPC分类号： F02K1/00

CPC分类号： F02K1/12 ,  F05D2240/128 ,  F05D2240/50 ,  F05D2250/241 ,  F05D2250/411 ,  F05D2260/30

摘要： The jet engine of the invention comprises an exhaust nozzle of variable section, comprising at least one flap pivot mounted about a pin, the pin being joined to the fixed structure of the jet engine via two braces each comprising a bore for housing the pin, the flap being pivot commanded by an actuating cylinder, connected to two fasteners which each comprise a bore through which the pin passes and about which they rotate. The jet engine is characterized by the fact that the pin, the bores of the braces and bores of the fasteners are arranged so that the contacts between the pin with the bore walls of the braces and with the bore walls of the fasteners are made over convex surfaces. Therefore, when in operation, in the event of pin bending the contact surfaces follow this convex shape and are suitably distributed.

摘要翻译： 本发明的喷气发动机包括可变部分的排气喷嘴，包括至少一个围绕销安装的挡板枢轴，该销通过两个支架连接到喷气发动机的固定结构，每个支架包括用于容纳销的孔， 翼片由致动筒指示，连接到两个紧固件，每个紧固件包括销穿过的孔，并且它们绕它们旋转。 喷气式发动机的特征在于，销，支架的孔和孔的孔被布置成使得销与支架的孔壁之间的接触以及紧固件的孔壁被制成凸起 表面。 因此，当操作时，在销弯曲的情况下，接触表面遵循该凸形并且适当地分布。

公开(公告)号：US20060090470A1

公开(公告)日：2006-05-04

申请号：US11248330

申请日：2005-10-13

申请人： Mathieu Dakowski ,  Guy Lapergue ,  Romain Lunel ,  Guillaume Sevi

发明人： Mathieu Dakowski ,  Guy Lapergue ,  Romain Lunel ,  Guillaume Sevi

IPC分类号： F02K1/12

CPC分类号： F02K1/1207

摘要： A variable-section turbomachine nozzle comprises a plurality of moving flaps, and a moving flap control system comprising control levers each associated with a respective moving flap, the control levers comprising both controlled levers that are actuated directly by actuators, and follower levers that are actuated by the controlled levers via transmission links. When the nozzle is at rest, the flaps associated with the follower levers present a radial offset relative to the flaps associated with the controlled levers.

公开(公告)号：US09004852B2

公开(公告)日：2015-04-14

申请号：US13125154

申请日：2009-10-16

申请人： Mathieu Dakowski ,  Fabrice Garin ,  Delphine Roussin-Leroux ,  Wilfried Schweblen

发明人： Mathieu Dakowski ,  Fabrice Garin ,  Delphine Roussin-Leroux ,  Wilfried Schweblen

IPC分类号： F01D5/08 ,  F02C7/18

CPC分类号： F01D5/082 ,  F01D5/087 ,  F02C7/18 ,  F05D2260/205 ,  Y02T50/671 ,  Y02T50/676

摘要： A turbomachine high-pressure turbine including a rotor disc with upstream and downstream annular flanges separating a radially internal annular cavity in which the hub of the disc extends from two radially external annular cavities, of which one is upstream of the disc and receives a ventilation air flow and of which the other is downstream of the disc, the upstream flange of the disc including a mechanism connecting to the upstream eternal cavity and the internal cavity for ventilating the hub of the disc.

摘要翻译： 一种涡轮机高压涡轮，包括具有上游和下游环形凸缘的转子盘，所述转子盘分开径向内部的环形空腔，其中盘的轮毂从两个径向外部的环形空腔延伸，其中一个在盘的上游并且接收通风空气 流动，另一个在盘的下游，盘的上游凸缘包括连接到上游永恒腔的机构和用于使盘的毂通风的内腔。

公开(公告)号：US08757966B2

公开(公告)日：2014-06-24

申请号：US13059790

申请日：2009-08-25

申请人： Stéphane Pierre Guillaume Blanchard ,  Fabrice Marcel Noël Garin ,  Laurent Pierre Joseph Ricou ,  Mathieu Dakowski

发明人： Stéphane Pierre Guillaume Blanchard ,  Fabrice Marcel Noël Garin ,  Laurent Pierre Joseph Ricou ,  Mathieu Dakowski

IPC分类号： F01D9/02 ,  F01D9/04

CPC分类号： F01D9/023 ,  F01D9/04 ,  F01D9/042 ,  F05D2230/64 ,  F05D2260/30 ,  Y02T50/671

摘要： A stationary vane assembly of a turbine engine including an inner casing and a high-pressure turbine guide vane assembly including at least two angular sectors including blades, the angular sectors being fixed on the casing, each angular sector including a platform and a fastening tab. The fastening tab protrudes from the platform radially inwardly. The casing includes a first annular groove receiving the fastening tabs, radial retaining pins for the angular sectors being introduced into bores made in the casing and the fastening tabs, the axial retaining pins being axially stopped by a ring mounted in a second annular groove of the casing.

摘要翻译： 包括涡轮发动机的固定叶片组件，其包括内壳和包括至少两个包括叶片的角扇区的高压涡轮导叶组件，角扇区固定在壳体上，每个角扇区包括平台和紧固翼片。 紧固片从平台径向向内突出。 壳体包括容纳紧固突片的第一环形凹槽，用于角部分的径向保持销引入到壳体和紧固突片中形成的孔中，轴向保持销由安装在第二环形凹槽 套管。