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31. 发明申请

WO2011161371A1 ROUE MOBILE A AUBES EN MATERIAU COMPOSITE POUR MOTEUR A TURBINE A GAZ A LIAISON PIED D'AUBE/DISQUE PAR SERRAGE 审中-公开
标题翻译：用于具有夹紧叶片根/盘连接的气体涡轮发动机的复合材料的叶片转子盘
公开(公告)号：WO2011161371A1
公开(公告)日：2011-12-29
申请号：PCT/FR2011/051424
申请日：2011-06-21
申请人： SNECMA , BLANCHARD, Stéphane, Pierre, Guillaume , RICOU, Laurent, Pierre, Joseph
发明人： BLANCHARD, Stéphane, Pierre, Guillaume , RICOU, Laurent, Pierre, Joseph
IPC分类号： F01D5/28 , F01D5/30
CPC分类号： F01D5/3023 , F01D5/282 , F01D5/3046 , F01D5/3053 , F01D5/3069 , F05D2250/25 , Y02T50/672
摘要： L'invention concerne une roue mobile (10) pour moteur à turbine à gaz, comprenant un disque métallique de maintien (100) ayant à sa périphérie une pluralité de dents s'étendant radialement vers l'extérieur du disque, une pluralité d'aubes en matériau composite (300), chaque aube comprenant un pied (304) qui est engagé entre deux dents adjacentes du disque de maintien et qui est maintenu entre ces dents par une liaison pivot, un disque de serrage (200) ayant à sa périphérie une pluralité de dents s'étendant selon une direction axiale, le disque de serrage étant fixé coaxialement sur le disque de maintien avec ses dents venant chacune se positionner circonférentiellement entre un pied d'aube et une dent du disque de maintien, et des moyens (400) pour exercer un effort serrage selon une direction circonférentielle des dents du disque de serrage contre les pieds des aubes.
摘要翻译：本发明涉及一种用于燃气涡轮发动机的转子盘（10），其包括金属保持盘（100），该金属保持盘在其周边具有径向朝向盘的外部延伸的多个齿，多个叶片（300）制成每个叶片包括根部（304），所述根部（304）接合在所述保持盘的两个相邻的齿之间并且通过枢转连接保持在所述齿之间;夹紧盘（200），其在其周边具有多个齿沿轴向方向延伸，所述夹紧盘同轴地固定在所述保持盘上，其每个齿周向位于所述保持盘的刀根和齿之间，以及用于沿圆周方向施加夹紧力的装置（400）将夹紧盘的齿部夹紧在叶片的根部上。

33. 发明专利

JP2005098300A Turbine wheel for turbomachinery, and assembly method of the wheel 有权
标题翻译：用于涡轮机的涡轮轮，以及轮的组装方法
公开(公告)号：JP2005098300A
公开(公告)日：2005-04-14
申请号：JP2004269316
申请日：2004-09-16
申请人： Snecma Moteurs , スネクマ・モトウール
发明人： LARDELLIER ALAIN
IPC分类号： F01D5/02 , F01D5/00 , F01D5/30
CPC分类号： F01D5/3046 , F01D5/00 , F01D5/3023 , F01D5/3069
摘要： PROBLEM TO BE SOLVED: To provide a turbine wheel for turbomachinery essentially unrestricted in maximum number of blades disposed to each segment, and remarkably improving overall sealability.
SOLUTION: A disk 4 of the turbine wheel 1 has an upstream rib 14a and a downstream rib 14b which extend in an annular direction around a shaft 2 as the center. Each segment 6 attached to the disk is held in an outside diameter direction by the disk by means of an upstream engagement means 16a which constitutes a part of a root part 8 and is cooperated with a complementary upstream engagement means 18a forming an external radial end part of the upstream rib, and a downstream engagement means 18b forming a part of the root part 8 and capable of cooperating with complementary downstream engagement means 18b forming an external radial end part of the downstream rib. The upstream rib and the downstream rib are movable in a direction from an engagement position to a close position which are spaced from each other, or vice versa, and each blade part is assembled on the turbine disk.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：提供一种用于涡轮机械的涡轮机叶轮，其基本上不受限制地设置在每个段上的最大数量的叶片，并且显着提高总体密封性。解决方案：涡轮机叶轮1的盘4具有围绕作为中心的轴2以环形方向延伸的上游肋14a和下游肋14b。通过构成根部8的一部分的上游接合装置16a，将附接到盘的每个段6通过盘保持在外径方向上，并且与形成外部径向端部的互补上游接合装置18a配合以及形成根部8的一部分并且能够与形成下游肋的外部径向端部的互补的下游接合装置18b配合的下游接合装置18b。上游肋和下游肋可以在从接合位置到彼此间隔开的关闭位置的方向上移动，反之亦然，并且每个叶片部分组装在涡轮盘上。版权所有（C）2005，JPO＆NCIPI

34. 发明专利

JPS59203809A Mounting structure of moving vane for axial-flow type turbo-machine 失效
标题翻译：轴流式涡轮机移动风门安装结构
公开(公告)号：JPS59203809A
公开(公告)日：1984-11-19
申请号：JP7831883
申请日：1983-05-06
申请人： Asahi Glass Co Ltd
发明人： TAKAHASHI SHIROU , TORIYAMA AKIRA , SHINOHARA NOBUHIRO
IPC分类号： F01D5/30
CPC分类号： F01D5/3069
摘要： PURPOSE:To prevent the generation of a backlash between a moving vane and a disk by holding heat-resisting heat-insulating pads among the indentations of the disk divided into two by a surface vertical to a shaft and a moving vane mounting section connected to the indentations. CONSTITUTION:Heat-resisting heat-insulating pads 3, 5 are held among the indentations 28 of disks 25 divided into two by surfaces vertical to a shaft 24 and the mounting sections 2 of moving vanes 26 connected and mounted to the indentations 28. Differences among thermal expansions of the moving vanes 26 and the disks 25 can be absorbed by the pads 3, 5. Accordingly, the generation of backlashes among the moving vanes 26 and the disks 25 can be prevented even when a turbo-machine is operated under high centrifugal force at a high temperature.
摘要翻译：目的：为了防止在移动叶片和盘之间产生间隙，通过在垂直于轴的表面上分隔成两个的盘的凹陷之间保持耐热隔热垫，以及连接到轴的移动叶片安装部压痕。构成：将耐热绝热垫3,5保持在与轴24垂直的两个分开的盘25的凹口28和连接并安装到凹痕28的移动叶片26的安装部分2之间。差异移动叶片26和盘25的热膨胀可以被垫片3,5吸收。因此，即使当涡轮机在高离心力下操作时，也可以防止活动叶片26和盘25之间产生间隙强力在高温下。

35. 发明专利

JP2012097601A Turbine and method for manufacturing turbine 有权
标题翻译：用于制造涡轮的涡轮机和方法
公开(公告)号：JP2012097601A
公开(公告)日：2012-05-24
申请号：JP2010244290
申请日：2010-10-29
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： ONISHI TOMOYUKI , WAKI YUICHIRO , YAMASHITA SHOSEI , MATSUO TAKAAKI , MATSUO ASAHARU
IPC分类号： F01D11/00 , F01D9/04 , F01D25/24
CPC分类号： F01D5/12 , F01D5/3069 , F01D9/042 , F01D11/001 , F01D11/003
摘要： PROBLEM TO BE SOLVED: To improve the efficiency of a turbine because a flow of the main flow flowing out from a row of stator blades is designed in a manner hardly generating turbulence of the main flow in the row of stator blades.SOLUTION: The turbine includes: a shaft 30 supported rotatably; rotor blade members provided on the outer periphery of the shaft 30 and forming a row of rotor blades in the circumferential direction of the shaft 30; a casing surrounding the shaft 30 and the row of rotor blades; an outer ring member 72 provided to the inner periphery of the casing and including an inner periphery 72a of which the cross-section having irregular shapes continues in the circumferential direction; stator blade members 41 provided in the circumferential direction, the stator blade members respectively having shrouds 43 which are engaged with the inner periphery 72a of the outer ring member 72 and also respectively having stator blade bodies 42 which are extended inward from the shrouds 72a in the radial direction, the stator blade members forming a row of stator blades with circumferentially adjacent shrouds 43 provided close to each other; and a plate-shaped member 71 for connecting at least some of the stator blade members 41 and covering the shrouds 43 of the connected stator blade members 41 from one side in the axial direction to seal shroud gaps formed between the shrouds 43 adjacent to each other in the circumferential direction.
摘要翻译：要解决的问题：为了提高涡轮机的效率，因为从一排定子叶片流出的主流的流动被设计成几乎不产生定子叶片排中的主流的湍流的方式。涡轮机包括：可旋转地支撑的轴30; 设置在轴30的外周的转子叶片构件，在轴30的圆周方向上形成一列转子叶片; 围绕轴30和转子叶片排的壳体; 设置在壳体的内周的外圈构件72，其内周72a具有不规则形状的横截面沿圆周方向延伸; 定子叶片构件41设置在圆周方向上，定子叶片构件分别具有与外圈构件72的内周72a接合的护罩43，并且还具有定子叶片体42，其中定子叶片构件42从护罩72a向内延伸定子叶片构件形成一排具有彼此靠近设置的周向相邻的罩43的定子叶片; 以及板状构件71，用于连接至少一些定子叶片构件41并且从轴向的一侧覆盖连接的定子叶片构件41的护罩43，以密封形成在彼此相邻的护罩43之间的护罩间隙在圆周方向。版权所有（C）2012，JPO＆INPIT

36. 发明专利

JP2011511900A Multiple-piece wing with rotor for a fluid institution 有权
公开(公告)号：JP2011511900A
公开(公告)日：2011-04-14
申请号：JP2010546221
申请日：2008-12-11
申请人：マン・ディーゼル・アンド・ターボ・エスイー
发明人：アンドレアス・クライネフェルト , ウィリアム・エフ・クライン , エミール・アシェンブルック , ミハエル・ブラスヴィヒ
IPC分类号： F01D5/30 , F01D5/06
CPC分类号： F01D5/3038 , F01D5/06 , F01D5/066 , F01D5/3069 , F05D2240/20 , F05D2260/30 , F05D2260/36
摘要： A multipart bladed rotor (1) for a flow machine, particularly a gas turbine or steam turbine or an axial compressor, has at least two disks (2) whose front sides, which face one another, are connected to one another, particularly by positive engagement, in a separating plane (7) so as to be fixed with respect to rotation relative to one another, wherein a groove (10) for receiving a blade root (14) of at least one rotor blade is formed in the separating plane.

37. 发明专利

JPS59170494A Blade holding hub for axial flow fan 失效
标题翻译：用于轴流风扇的叶片保持架
公开(公告)号：JPS59170494A
公开(公告)日：1984-09-26
申请号：JP4059184
申请日：1984-03-05
申请人： Kofuimuko Spa
发明人： ANTONIO MOJIEBITSUTSU
IPC分类号： F04D29/32 , F01D5/30 , F04D29/34
CPC分类号： F04D29/34 , F01D5/3069 , Y10T29/49327 , Y10T29/49995

38. 发明授权

US10633986B2 Platform with axial attachment for blade with circumferential attachment 有权
公开(公告)号：US10633986B2
公开(公告)日：2020-04-28
申请号：US16119561
申请日：2018-08-31
申请人： Rolls-Royce Corporation , Rolls-Royce North American Technologies Inc.
发明人： Aaron D. Sippel , Ted J. Freeman , Loic Fabries
IPC分类号： F01D5/30 , F04D29/32 , F01D11/00 , B23P15/00
CPC分类号： F01D5/3069 , B23P15/006 , F01D5/3038 , F01D11/008 , F04D29/322 , F05D2220/323 , F05D2230/60 , F05D2240/30 , F05D2240/80 , Y10T29/49321
摘要： A wheel assembly for a gas turbine engine includes a disk, a plurality of blades, and a plurality of platforms. The disk is configured to rotate about an axis during operation of the gas turbine engine. The blades each include a circumferentially extending attachment feature that is received in the disk. The platforms each have an axially extending attachment feature that is received in the disk.

39. 发明申请

US20180080332A1 INTERMEDIATE CASING GUIDE VANE WHEEL 审中-公开
公开(公告)号：US20180080332A1
公开(公告)日：2018-03-22
申请号：US15707428
申请日：2017-09-18
申请人： Safran Aircraft Engines
发明人： Marc-Antoine Anatole GOT , Cédric ZACCARDI
IPC分类号： F01D9/04 , F01D5/28
CPC分类号： F01D9/041 , F01D5/282 , F01D5/3069 , F01D9/042 , F01D25/246 , F05D2220/36 , F05D2240/12 , F05D2260/31 , F05D2300/603 , Y02T50/672
摘要： An OGV wheel comprising guide vanes made of polymer matrix composite material reinforced by fibers, each having a vane root and a vane tip, the vane roots being fastened on a hub of the wheel by first connection means and the vane tip being fastened on an outer shroud of the wheel by second connection means, the first connection means including a bearing plane secured to the hub and a first backing plate for securing to the hub, the vane roots being sandwiched between the bearing plane and the first backing plate, and the second connection means including a second backing plate for securing to the shroud, the vane tip being sandwiched between the shroud and the second backing plate.

40. 发明授权

US09896949B2 Bonded fan platform 有权
公开(公告)号：US09896949B2
公开(公告)日：2018-02-20
申请号：US14862390
申请日：2015-09-23
申请人： United Technologies Corporation
发明人： Thomas J. Robertson
IPC分类号： F01D5/14 , F01D5/30 , F01D5/12 , F04D29/02 , F04D29/32 , F02K3/06 , F01D5/28 , F01D11/00
CPC分类号： F01D5/3069 , F01D5/12 , F01D5/147 , F01D5/282 , F01D5/3053 , F01D11/005 , F01D11/008 , F02K3/06 , F04D29/023 , F04D29/324 , F05D2220/36 , F05D2240/80 , F05D2240/81 , F05D2260/30 , F05D2260/36 , F05D2300/603 , Y02T50/676
摘要： A fan is provided. The fan may comprise a fan blade and a blade platform coupled to the fan blade. The blade platform may be a thermoplastic. A fan blade platform is also provided. The fan blade platform may comprise a first platform half comprising a slot at a first end of the first platform half and a first receiving member at a second end of the first platform half opposite the first end of the first platform half. A second platform half may comprise a hook. The second platform half may also include a second receiving member at a second end of the second platform half opposite the first end of the second platform half with the hook configured to interface with the slot. A pin may be configured to pass through the first receiving member and the second receiving member.

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