公开(公告)号：US4604030A

公开(公告)日：1986-08-05

申请号：US675214

申请日：1984-11-27

申请人： Jacky Naudet

发明人： Jacky Naudet

IPC分类号： F04D29/56 ,  F01D9/04 ,  F01D11/00 ,  F01D17/16 ,  H02K15/02 ,  F01D11/02

CPC分类号： F04D29/563 ,  F01D11/001 ,  F01D17/162 ,  F05D2230/644

摘要： The invention relates to a turbo-machine incorporating a compressor with stator vanes of which the angle of incidence is adjustable. In order to enable adjustment in the position of the internal ring of a stator of the compressor, each of the sectors of the ring is provided with adjustment locations constituted by the bushes of pivot bearings for the roots of the vanes which roots comprise an external screw thread cooperating with a complementary internal screw thread of their seating and these come into abutment against a shoulder of the pivot of each vane so that the radial position of each of the sectors can be adjusted by rotation of the bushes in their respective seating.

摘要翻译： 本发明涉及一种包含具有定子叶片的压缩机的涡轮机，其中入射角可调。 为了能够调整压缩机的定子的内环的位置，环的每个扇区都设置有由叶片根部的枢转轴承的衬套构成的调​​节位置，根部包括外螺纹 螺纹与其座的互补内螺纹配合，并且它们抵靠每个叶片的枢轴的肩部，使得每个扇区的径向位置可以通过其各自的座中的衬套的旋转来调节。

公开(公告)号：US07018173B2

公开(公告)日：2006-03-28

申请号：US10489867

申请日：2002-10-24

申请人： Serge Bongrand ,  Alain Henri Daniel Bouron ,  Sébastien Georges Roger Goux ,  Fabrice Marois ,  Jacky Naudet ,  Gabriel Radeljak ,  Dominique Raulin

发明人： Serge Bongrand ,  Alain Henri Daniel Bouron ,  Sébastien Georges Roger Goux ,  Fabrice Marois ,  Jacky Naudet ,  Gabriel Radeljak ,  Dominique Raulin

IPC分类号： F01D9/02

CPC分类号： F01D25/246 ,  F01D9/042 ,  F05B2260/301

摘要： A device for stopping rotation of a fixed blade bearing sector in a gas turbine casing. Sectors of synchronizing ring blades are maintained against tangential rotational movements by sliding into grooves of a casing by pins passing through perforations in an extension of the two parts. The pins are prevented from accidental removal either by a flexible lock ring or by a locking tab maintained between the two parts when they have been completely assembled.

摘要翻译： 一种用于停止燃气轮机壳体中的固定叶片轴承部分的旋转的装置。 通过在两个部分的延伸部分穿过穿孔的销通过滑入壳体的凹槽来保持同步环形叶片的扇形体相切的旋转运动。 通过柔性锁环或两个部件完全组装后保持的锁定突出部分可以防止销的意外移除。

公开(公告)号：US20050129521A1

公开(公告)日：2005-06-16

申请号：US10868781

申请日：2004-06-17

申请人： Jacky Naudet

发明人： Jacky Naudet

IPC分类号： F01D5/14 ,  F04D29/32 ,  F01D5/30

CPC分类号： F01D5/143 ,  F05D2240/80 ,  Y02T50/673

摘要： The blade of gas turbine engine compressor of the invention includes a hammer type root to be inserted into a circumferential groove of the rotor of the compressor, a platform (12) integral with the root (11) and supporting an airfoil portion (13), the platform including two edges perpendicular to the axis of the rotor (20, 21) and two curved flanks (22, 23), the curve of the flanks being made out of at least one curve defined by an equation, the curvature centre of the point in the curve whereof the curvature radius is the smallest, being situated within a band (B) central to the platform and accounting for 60% of the width (D) of the platform (12) measured between its parallel rectilinear edges (20, 21), the equation defining the curve being, in the sense of mathematic functions, continuous and with continuous first derivative.

摘要翻译： 本发明的燃气涡轮发动机压缩机的叶片包括插入压缩机的转子的圆周槽中的锤式根部，与根部（11）成一体并支撑翼型部分（13）的平台（12） 所述平台包括垂直于所述转子（20,21）的轴线的两个边缘和两个弯曲的侧面（22,23），所述侧面的曲线由至少一个由方程定义的曲线制成，所述曲率中心 位于曲线半径最小的曲线上，位于平台中心的带（B）内，并且占平台（12）在其平行直线边缘（20,28）之间测量的宽度（D）的60％ 21），在数学函数意义上，定义曲线的方程是连续的和连续的一阶导数。

公开(公告)号：US06011617A

公开(公告)日：2000-01-04

申请号：US199492

申请日：1998-11-25

申请人： Jacky Naudet

发明人： Jacky Naudet

IPC分类号： A61B1/00 ,  F02C7/00 ,  G02B23/26 ,  G01N21/00

CPC分类号： G02B23/2492 ,  G02B23/26

摘要： A system for inspecting internal zones of a machine, such as an engine, comprises an observation device having an optical fiber endoscope, and distribution and guide means including a network of flexible guide sheaths placed in the machine to define a number of different inspection routes along which the endoscope can be guided from an aperture in the machine wall to various predetermined critical internal zones. Preferably the system includes first electrical means implanted in each guide sheath and co-operable with second electrical means secured to the endoscope in order to detect the position thereof in the network and to transmit the position to a monitoring device outside the machine for monitoring and assisting the guidance of the endoscope in the network.

摘要翻译： 用于检查诸如发动机的机器的内部区域的系统包括具有光纤内窥镜的观察装置，以及分配和引导装置，其包括放置在机器中的柔性引导护套网络，以限定沿着 内窥镜可以从机器壁中的孔引导到各种预定的关键内部区域。 优选地，系统包括植入每个引导护套中的第一电气装置，并且可与固定到内窥镜的第二电气装置协同操作，以便检测其在网络中的位置并将该位置传送到机器外部的监视装置，以便监视和辅助 内窥镜在网络中的引导。

公开(公告)号：US5277544A

公开(公告)日：1994-01-11

申请号：US947541

申请日：1992-09-21

申请人： Jacky Naudet

发明人： Jacky Naudet

IPC分类号： F01D17/16

CPC分类号： F01D17/162 ,  F04D29/563

摘要： A blade control rod system for controlling blades of a gas turbine stator is provided with at least one rod for controlling an associated blade. The blade includes a shaft about which the blade pivots with one end of the rod being engaged on the blade. The control rod system includes a projection which extends beneath a portion of at least one adjacent rod, so that the accidental loosening of a nut which secures the rod on the shaft of the blade is not sufficient to allow the rod to become detached.

摘要翻译： 用于控制燃气轮机定子的叶片的叶片控制杆系统设置有用于控制相关叶片的至少一个杆。 叶片包括轴，刀片围绕该轴枢转，杆的一端接合在叶片上。 控制杆系统包括在至少一个相邻杆的一部分下方延伸的突起，使得将杆固定在刀片的轴上的螺母的意外松动不足以允许杆脱离。

公开(公告)号：US4787820A

公开(公告)日：1988-11-29

申请号：US140992

申请日：1988-01-05

申请人： Jacques M. P. Stenneler ,  Jacky Naudet

发明人： Jacques M. P. Stenneler ,  Jacky Naudet

IPC分类号： F01D5/08 ,  F02C7/18

CPC分类号： F02C7/18 ,  F01D5/08 ,  F01D5/087 ,  F04D29/321

摘要： A turbine plant compressor disc is formed from two halves which are welded together near the rim and define an internal cavity in which a centripetal accelerator is mounted for inducing cooling air to flow from the compressor through inclined passages in the rim on the downstream side of the blades carried by the rim, through the cavity of the disc, and towards the turbine to be cooled in the vicinity of the turbine shaft. The centripetal accelerator is composed of sectors which are removably mounted in the cavity of the disc, the sectors forming a perforated ring disposed in the central bore of the disc and each sector having a flat web extending radially outwards in the inner cavity of the disc to form radial centripetal channels communicating with the air passages in the rim.

摘要翻译： 涡轮机压缩机盘由两个半部形成，两个半部在边缘附近焊接在一起，并且限定内部空腔，其中安装有向心加速器，其中冷却空气通过来自压缩机的倾斜通道在边缘的下游侧 由轮辋承载的叶片通过盘的空腔并且朝向涡轮机在涡轮机轴附近被冷却。 向心加速器由可移除地安装在盘的空腔中的扇区组成，扇形部形成设置在盘的中心孔中的穿孔环，并且每个扇形体具有在盘的内腔中径向向外延伸的扁平腹板， 形成与边缘中的空气通道连通的径向向心通道。

公开(公告)号：US4750746A

公开(公告)日：1988-06-14

申请号：US91451

申请日：1987-08-31

申请人： Jean Claude M. Boudot ,  Jacky Naudet

发明人： Jean Claude M. Boudot ,  Jacky Naudet

IPC分类号： F01D11/00 ,  F02C7/28 ,  F16J15/18 ,  F16J15/30 ,  F04D29/12

CPC分类号： F16J15/184 ,  F01D11/00 ,  F01D11/005 ,  F02C7/28

摘要： A device for attaching a seal to a shaft wherein the seal is mounted on a hoop which, in turn, is mounted on the end of a shaft. A second, resilient hoop member is interposed between the seal and a flange on the shaft to exert a compressive force on the seal. A split ring member engages circumferential grooves formed on the shaft and the first hoop member to prevent relative axial movement. A pin attached to the hoop member engages a notch on the split ring member to prevent any relative circumferential motion between these elements.

摘要翻译： 用于将密封件附接到轴的装置，其中所述密封件安装在环上，所述环又安装在轴的端部上。 第二弹性环构件插入在密封件和轴之间的凸缘之间，以在密封件上施加压缩力。 开口环构件接合形成在轴和第一环构件上的周向槽，以防止相对的轴向运动。 附接到环形构件的销与开口环构件上的凹口接合以防止这些元件之间的任何相对圆周运动。

公开(公告)号：US4730983A

公开(公告)日：1988-03-15

申请号：US89414

申请日：1987-08-26

申请人： Jacky Naudet ,  Jean-Louis Bertrand

发明人： Jacky Naudet ,  Jean-Louis Bertrand

IPC分类号： F01D5/30 ,  F01D5/32 ,  F01D11/00

CPC分类号： F01D5/3015 ,  F01D11/006

摘要： A locking and sealing system is disclosed for attaching a rotor blade to a rotor blade disk in a turbojet engine. The system has a first split ring member which locks the rotor blade foot portion onto the rotor blade disk. A second split ring member is inserted between the first split ring member in a downstream flange of the rotor blade foot portions to provide a positive seal to prevent air leakage between the foot portions and the notches formed in the rotor disk.

摘要翻译： 公开了用于将转子叶片附接到涡轮喷气发动机中的转子叶片盘的锁定和密封系统。 该系统具有第一开口环构件，其将转子叶片脚部分锁定到转子叶片盘上。 第二开口环构件插入在转子叶片脚部的下游凸缘中的第一开口环构件之间，以提供正密封，以防止脚部和形成在转子盘中的凹口之间的空气泄漏。

公开(公告)号：US4595339A

公开(公告)日：1986-06-17

申请号：US647635

申请日：1984-09-06

申请人： Jacky Naudet

发明人： Jacky Naudet

IPC分类号： F01D5/04 ,  F01D5/08 ,  F02C7/18

CPC分类号： F01D5/048 ,  F01D5/085 ,  F02C7/18 ,  F04D29/321

摘要： A compressor disc assembly with an integral centripetal accelerator for the exhaustion of air for use in a cooling device of a gas turbine, the bleeding of air at the surface of the compressor drum being effected by orifices situated in the platforms of the blades and in the median plane of the compressor disc. The assembly is formed from two half discs. The centripetal accelerator includes several sectors detachably mounted in the space defined between the two half discs of the compressor, each sector being formed from two half shells having on their internal face ribs in the form of centripetal blades by which the half shells are assembled together. The invention is utilized for cooling a gas turbine by bleeding air from the compressor.

摘要翻译： 一种具有整体向心加速器的压缩机盘组件，其用于在燃气轮机的冷却装置中用于空气的排气，压缩机鼓的表面处的空气的渗透由位于叶片的平台中的孔和 压缩机盘的中间平面。 组件由两个半圆盘形成。 向心加速器包括可拆卸地安装在压缩机的两个半圆盘之间的空间中的几个扇区，每个扇区由两个半壳形成，两个半壳在其内表面上形成向心式叶片形式的肋，半壳体组装在一起。 本发明用于通过从压缩机排出空气来冷却燃气轮机。