公开(公告)号：EP3385504A1

公开(公告)日：2018-10-10

申请号：EP18160507.2

申请日：2018-03-07

申请人： Rolls-Royce plc

发明人： Pitt, Simon

IPC分类号： F01D9/02 ,  F01D9/06 ,  F01D25/12

CPC分类号： F01D5/186 ,  F01D9/041 ,  F01D9/065 ,  F01D11/10 ,  F01D11/24 ,  F01D25/12 ,  F02C7/18 ,  F05D2230/23 ,  F05D2240/11 ,  F05D2240/122 ,  F05D2240/123 ,  F05D2240/81 ,  F05D2260/201 ,  F05D2260/202 ,  F05D2260/205 ,  F05D2260/60 ,  Y02T50/676

摘要： A vane cooling system for a gas turbine engine comprises a vane (20a) arranged on a stator and having a chamber (27,28) extending continuously from a radially inner end to a radially outer end of the vane. The vane (20a) has a first inlet (41) and a second inlet (42). A first cooling fluid feed (54) in communication with the first inlet (41) and a second cooling fluid feed (43) in communication with the second inlet (42). The first cooling fluid feed (54) has a higher pressure than the second cooling fluid feed (43). A flow adjustment device (45) is arranged for adjusting a flow of the second cooling fluid feed (43) into the second inlet (42). The chamber is divided by a restrictor plate (25, 26) to provide an inner chamber (27) and a wall-side chamber (28) bordering the inner chamber (27). The first inlet (41) enters the wall-side chamber (28) and the second inlet (42) enters the central chamber (27).

公开(公告)号：EP2864614B1

公开(公告)日：2018-10-10

申请号：EP13809658.1

申请日：2013-06-04

申请人： United Technologies Corporation

发明人： GRILLO, Joseph

IPC分类号： F01M1/16 ,  B64D37/22 ,  F01D25/20 ,  F01M11/06

CPC分类号： F02C7/00 ,  F01D25/20 ,  F01M11/067 ,  F05D2250/51 ,  F05D2250/75 ,  F05D2260/60 ,  F05D2260/98

摘要： An exemplary valve device for controlling flow of a turbomachine fluid includes a housing having a first inlet at a first elevation, a second inlet at a second elevation higher than the first elevation, and an outlet. A flow control member is within the housing. The flow control member in a positive g-force environment is biased toward a first position that permits flow through the first inlet to the outlet. The flow control member in a negative g-force environment is biased toward a second position that restricts flow through the first inlet to the outlet.

公开(公告)号：EP3211177B1

公开(公告)日：2018-10-03

申请号：EP17156984.1

申请日：2017-02-20

申请人： General Electric Company

发明人： SREERAM, Kiran ,  DIMMICK, John Herbert III ,  LIOTTA, Gary Charles ,  SECH, John Robert ,  BONINI, Eric Richard ,  REILLY, Patrick Shawn

IPC分类号： F01D5/08 ,  F01D5/18 ,  F01D25/12 ,  F01D5/04 ,  F04D29/32 ,  F04D29/52 ,  F04D29/64

CPC分类号： F04D29/322 ,  F01D5/046 ,  F01D5/048 ,  F01D5/087 ,  F01D5/187 ,  F01D5/188 ,  F01D25/12 ,  F04D29/522 ,  F04D29/644 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/232 ,  F05D2260/30 ,  F05D2260/60 ,  Y02T50/671 ,  Y02T50/673 ,  Y02T50/676

摘要： A rotor wheel for an engine includes a plurality of impeller vanes (40) and a plurality of fluid passages (36) defined by adjacent impeller vanes. The fluid passages are radially disposed across at least a portion of the rotor wheel. One or more impeller inserts (44, 4A, 44B, 44C) may be disposed within one or more of the plurality of fluid passages (36), respectively. The impeller inserts (44, 4A, 44B, 44C) define an impeller passage (46) with a passage shape that controls a flow of fluid through the one or more of the plurality of fluid passages (36).

公开(公告)号：EP2943668B1

公开(公告)日：2018-04-04

申请号：EP13870696.5

申请日：2013-06-07

申请人： United Technologies Corporation

发明人： SUCIU, Gabriel L. ,  CHANDLER, Jesse M.

IPC分类号： F02C7/12 ,  F02C7/20 ,  F01D25/16

CPC分类号： F01D25/162 ,  F02C7/12 ,  F02C7/20 ,  F02C7/32 ,  F05D2220/325 ,  F05D2260/60 ,  Y02T50/675

摘要： A gas turbine engine has a turbine section, and a housing enclosing the turbine section, with a mount structure secured to the housing for mounting and including internal flow passages for delivering air to remote locations.

公开(公告)号：EP3211177A1

公开(公告)日：2017-08-30

申请号：EP17156984.1

申请日：2017-02-20

申请人： General Electric Company

发明人： SREERAM, Kiran ,  DIMMICK, John Herbert III ,  LIOTTA, Gary Charles ,  SECH, John Robert ,  BONINI, Eric Richard ,  REILLY, Patrick Shawn

IPC分类号： F01D5/08 ,  F01D5/18 ,  F01D25/12 ,  F01D5/04

CPC分类号： F04D29/322 ,  F01D5/046 ,  F01D5/048 ,  F01D5/087 ,  F01D5/187 ,  F01D5/188 ,  F01D25/12 ,  F04D29/522 ,  F04D29/644 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/232 ,  F05D2260/30 ,  F05D2260/60 ,  Y02T50/671 ,  Y02T50/673 ,  Y02T50/676

摘要： A rotor wheel for an engine includes a plurality of impeller vanes (40) and a plurality of fluid passages (36) defined by adjacent impeller vanes. The fluid passages are radially disposed across at least a portion of the rotor wheel. One or more impeller inserts (44, 4A, 44B, 44C) may be disposed within one or more of the plurality of fluid passages (36), respectively. The impeller inserts (44, 4A, 44B, 44C) define an impeller passage (46) with a passage shape that controls a flow of fluid through the one or more of the plurality of fluid passages (36).

摘要翻译： 一种用于发动机的转子叶轮包括多个叶轮叶片（40）和由相邻的叶轮叶片限定的多个流体通道（36）。 流体通道径向地设置在转子叶轮的至少一部分上。 一个或多个叶轮插入件（44,4A，44B，44C）可以分别设置在多个流体通道（36）中的一个或多个内。 叶轮插入件（44,4A，44B，44C）限定具有通道形状的叶轮通道（46），该通道形状控制流体通过多个流体通道（36）中的一个或多个流体通道。

公开(公告)号：EP3156595A1

公开(公告)日：2017-04-19

申请号：EP15189271.8

申请日：2015-10-12

申请人： Siemens Aktiengesellschaft

发明人： Mugglestone, Jonathan ,  Nilsson, Ulf

IPC分类号： F01D5/18

CPC分类号： F01D9/065 ,  F05D2230/54 ,  F05D2250/15 ,  F05D2260/231 ,  F05D2260/60

摘要： The present invention relates to a method of manufacture of a channelling tube (10) with an insulating air gap (44) for transferring coolant from the outer platform to the inner platform of a hollow stator vane of a turbine. The purpose is to minimize heat transfer even at low flow rates of coolant in order to supply said coolant at the lowest possible temperature to the inner platform.
The tube is realized by tight rolling a flat metal sheet (16) in order to obtain a tight spiral defining a tube with an outer diameter d; said tube is then released so that it expands via a spring effect to an outer diameter D; the circumferential ends of the spiral are attached to the adjacent layer to define a central passage (42) for the coolant and the spiral gap (44) that creates insulation layer(s) around the central passage.

摘要翻译： 本发明涉及一种制造具有绝缘气隙（44）的导流管（10）的方法，用于将冷却剂从外平台传送到涡轮机的中空定子叶片的内平台。 目的是尽可能在低流量的冷却剂下尽量减少传热，以便将最低可能的温度的所述冷却剂供应到内部平台。 通过紧密轧制平板金属板（16）来实现管，以获得限定具有外径d的管的紧密螺旋; 所述管然后被释放，使得其经由弹簧效应膨胀到外径D; 螺旋的周向端部附接到相邻的层，以限定用于冷却剂的中心通道（42）和围绕中心通道产生绝缘层的螺旋间隙（44）。

公开(公告)号：EP2943668A4

公开(公告)日：2016-01-20

申请号：EP13870696

申请日：2013-06-07

申请人： UNITED TECHNOLOGIES CORP

发明人： SUCIU GABRIEL L ,  CHANDLER JESSE M

IPC分类号： F02C7/12 ,  F01D25/16 ,  F02C7/20

CPC分类号： F01D25/162 ,  F02C7/12 ,  F02C7/20 ,  F02C7/32 ,  F05D2220/325 ,  F05D2260/60 ,  Y02T50/675

摘要： A gas turbine engine has a turbine section, and a housing enclosing the turbine section, with a mount structure secured to the housing for mounting and including internal flow passages for delivering air to remote locations.

公开(公告)号：EP2943668A1

公开(公告)日：2015-11-18

申请号：EP13870696.5

申请日：2013-06-07

申请人： United Technologies Corporation

发明人： SUCIU, Gabriel L. ,  CHANDLER, Jesse M.

IPC分类号： F02C7/00 ,  F02C9/16 ,  F02C3/00

CPC分类号： F01D25/162 ,  F02C7/12 ,  F02C7/20 ,  F02C7/32 ,  F05D2220/325 ,  F05D2260/60 ,  Y02T50/675

摘要： A gas turbine engine has a turbine section, and a housing enclosing the turbine section, with a mount structure secured to the housing for mounting and including internal flow passages for delivering air to remote locations.

公开(公告)号：EP2694781A1

公开(公告)日：2014-02-12

申请号：EP12717412.6

申请日：2012-03-29

申请人： SNECMA

发明人： POUZET, Emilie ,  CASALIGGI, Pascal ,  PASQUIET, Didier

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

CPC分类号： F01D11/006 ,  F01D5/3015 ,  F01D5/323 ,  F01D11/005 ,  F05D2260/30 ,  F05D2260/60 ,  Y02T50/673 ,  Y10T29/49995

摘要： The invention relates to a sealing ring (60) intended to be pressed against a rotor disc of a turbine stage for an aircraft turbomachine, the ring being equipped with a plurality of anti-rotation pegs (66) for preventing it from rotating in relation to the rotor disc, each peg (66) protruding axially from a ring body (63) and having two opposite circumferential-end surfaces (72) which are intended respectively to be located facing two directly consecutive blades carried on the rotor disc. According to the invention, an axially opening slot (70) passes radially through at least one of the anti-rotation pegs (66).

公开(公告)号：EP2497924A2

公开(公告)日：2012-09-12

申请号：EP12157991.6

申请日：2012-03-02

申请人： General Electric Company

发明人： Nenmeni, Vijay Raghavendran ,  Rozdolski, Michael John ,  Chillar, Rahul

IPC分类号： F02C9/40

CPC分类号： F02C9/40 ,  F02C7/232 ,  F05D2260/60 ,  F05D2260/602

摘要： A system includes a turbine fuel controller (14). The turbine fuel controller (14) includes a purge control logic (40) configured to control a purge sequence of mixing an inert purge gas (36) with a first fuel (18) during a first fuel shutdown, wherein the purge sequence is configured to open a purge valve (34, 92, and 94) for the inert purge gas (36) before fully closing a fuel valve (26) for the first fuel (18).

摘要翻译： 一种系统包括涡轮燃料控制器（14）。 涡轮燃料控制器（14）包括构造成控制第一燃料关闭期间与第一燃料（18）的惰性吹扫气体（36）的混合，worin清洗程序的清洗程序的清洗控制逻辑（40）被配置为 完全关闭燃料阀（26），用于所述第一燃料（18）之前，打开用于惰性吹扫气体（36）净化阀（34，92，和94）。