公开(公告)号：EP3109433B1

公开(公告)日：2018-08-15

申请号：EP16174191.3

申请日：2016-06-13

申请人： Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

发明人： Vaisman, Igor ,  Armstrong, Michael James

IPC分类号： F02C1/00 ,  F02C1/10 ,  F02C6/20 ,  F02C7/08 ,  F02C7/141 ,  F02C7/18 ,  F01K23/10 ,  F02K3/077

CPC分类号： F02K3/00 ,  F01K23/10 ,  F01K25/103 ,  F02C1/007 ,  F02C1/10 ,  F02C3/04 ,  F02C3/10 ,  F02C3/13 ,  F02C6/206 ,  F02C7/08 ,  F02C7/141 ,  F02C7/143 ,  F02C7/18 ,  F02K3/077 ,  F02K99/00 ,  F05D2210/10 ,  F05D2210/13 ,  F05D2250/311 ,  F05D2260/213 ,  F22B3/08 ,  Y02T50/676

摘要： A gas turbine engine (10, 200, 300, 400, 500, 600, 700, 800) includes a first shaft (202) coupled to a first turbine (204, 506) and a first compressor (206, 608), a second shaft (208) coupled to a second turbine (210) and a second compressor (212), and a third shaft (214) coupled to a third turbine (216) and a fan assembly (218, 306, 318, 414, 416). The turbine engine includes a heat rejection heat exchanger (220, 402) configured to reject heat from a closed loop system (222, 314) with air passed from the fan assembly (218, 306, 318, 414, 416), and a combustor (224) positioned to receive compressed air from the second compressor (212) as a core stream (226, 320, 418). The closed-loop system (222, 314) includes the first, second, and third turbines (204, 210, 216, 506) and the first compressor (206, 608) and receives energy input from the combustor (224).

公开(公告)号：EP3147219A1

公开(公告)日：2017-03-29

申请号：EP16190031.1

申请日：2016-09-22

申请人： Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

发明人： Armstrong, Michael James ,  Vaisman, Igor

IPC分类号： B64D27/02 ,  F02K3/06 ,  F02K3/077 ,  F02C1/10 ,  F01K23/10 ,  F01K25/10 ,  F02K3/12 ,  F02C6/18

CPC分类号： F02K5/00 ,  B64D27/02 ,  B64D2027/026 ,  F01K23/10 ,  F01K25/103 ,  F02C1/105 ,  F02C6/18 ,  F02C6/206 ,  F02K3/06 ,  F02K3/077 ,  F02K3/12 ,  F05D2210/12 ,  F05D2210/13 ,  F05D2240/40 ,  F05D2250/311 ,  F05D2260/213 ,  Y02T50/675

摘要： A power and propulsion system (400, 500, 600, 700) includes an air compressor (712, 718), a combustor (724) positioned to receive compressed air from the air compressor (712, 718) as a core stream (726), and a closed-loop system (404, 504, 722) having carbon dioxide as a working fluid that receives heat from the combustor (724) and rejects heat to a cooling stream. The closed-loop system (404, 504, 722) configured to provide power to a fan (718, 732) that provides the cooling stream, and to one or more distributed propulsors (406, 506, 606, 608) that provide thrust to an aircraft.

摘要翻译： 动力和推进系统（400,500,600,700）包括空气压缩机（712,718），定位成将来自空气压缩机（712,718）的压缩空气作为核心流（726）接收的燃烧器（724） 以及具有二氧化碳作为工作流体的闭环系统（404,504,722），其接收来自燃烧器（724）的热量并将热量排除到冷却流。 闭环系统（404,504,722）被配置为向提供冷却流的风扇（718,732）以及向一个或多个分布式推进器（406,506,606,608）提供动力，所述推进器提供推力 一架飞机

公开(公告)号：EP3109433A1

公开(公告)日：2016-12-28

申请号：EP16174191.3

申请日：2016-06-13

申请人： Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

发明人： Vaisman, Igor ,  Armstrong, Michael James

IPC分类号： F02C1/00 ,  F02C1/10 ,  F02C6/20 ,  F02C7/08 ,  F02C7/141 ,  F02C7/18 ,  F01K23/10 ,  F02K3/077

CPC分类号： F02K3/00 ,  F01K23/10 ,  F01K25/103 ,  F02C1/007 ,  F02C1/10 ,  F02C3/04 ,  F02C3/10 ,  F02C3/13 ,  F02C6/206 ,  F02C7/08 ,  F02C7/141 ,  F02C7/143 ,  F02C7/18 ,  F02K3/077 ,  F02K99/00 ,  F05D2210/10 ,  F05D2210/13 ,  F05D2250/311 ,  F05D2260/213 ,  F22B3/08 ,  Y02T50/676

摘要： A gas turbine engine (10, 200, 300, 400, 500, 600, 700, 800) includes a first shaft (202) coupled to a first turbine (204, 506) and a first compressor (206, 608), a second shaft (208) coupled to a second turbine (210) and a second compressor (212), and a third shaft (214) coupled to a third turbine (216) and a fan assembly (218, 306, 318, 414, 416). The turbine engine includes a heat rejection heat exchanger (220, 402) configured to reject heat from a closed loop system (222, 314) with air passed from the fan assembly (218, 306, 318, 414, 416), and a combustor (224) positioned to receive compressed air from the second compressor (212) as a core stream (226, 320, 418). The closed-loop system (222, 314) includes the first, second, and third turbines (204, 210, 216, 506) and the first compressor (206, 608) and receives energy input from the combustor (224).

摘要翻译： 一种燃气涡轮发动机（10，200，300，400，500，600，700，800）包括耦合到第一涡轮机（204，506）和第一压缩机（206，608），第二的第一轴（202） 耦合到耦合到第三涡轮机（216）和一个风扇组件（218，306，318，414，416）的第二涡轮（210）和第二压缩机（212）和第三轴（214）的轴（208） ， 该涡轮发动机包括排热换热器（220，402）被配置为从一个闭环系统（222，314）与来自风扇组件（218，306，318，414，416）通过空气排出热，和燃烧器 （224）设置成从所述第二压缩机（212），其为核心流（226，320，418）接收压缩空气。 闭环系统（222，314）包括第一，第二和第三涡轮机（204，210，216，506）和所述第一压缩机（206，608）和来自所述燃烧器（224）接收的能量输入。

公开(公告)号：EP3092387A1

公开(公告)日：2016-11-16

申请号：EP15701551.2

申请日：2015-01-07

申请人： Finno Energy Oy

发明人： ERÄMAA, Timo ,  SALMINEN, Heikki J.

IPC分类号： F02C5/12 ,  F01K23/10 ,  F02C9/16 ,  F01D15/10

CPC分类号： F01K21/04 ,  F01D15/10 ,  F01K21/047 ,  F01K23/10 ,  F02C5/12 ,  F02C9/16 ,  F02C9/50 ,  F05D2210/12 ,  F05D2210/13 ,  F05D2220/76 ,  F05D2260/964 ,  F05D2270/14 ,  F05D2270/16 ,  H02K7/1823 ,  Y02E20/16

摘要： An object of the present invention is to provide a method and a system for implementing the method so as to alleviate the disadvantages of a reciprocating combustion engine and gas turbine in electric energy production. The invention is based on the idea of arranging a combustion chamber outside a gas turbine and providing compressed air to the combustion chamber in order to carry out a combustion process supplemented with high pressure steam pulses.

摘要翻译： 本发明的一个目的是提供一种实现该方法的方法和系统，以减轻往复式内燃机和燃气轮机在电能生产中的缺点。 本发明基于这样的想法：在燃气轮机外部布置燃烧室并向燃烧室提供压缩空气以实施补充有高压蒸汽脉冲的燃烧过程。

公开(公告)号：EP3019746A1

公开(公告)日：2016-05-18

申请号：EP14745209.8

申请日：2014-07-09

申请人： Storewatt

发明人： FAVY, Claude

IPC分类号： F03G7/05

CPC分类号： F03G7/05 ,  F01D1/026 ,  F01D1/32 ,  F05D2210/13 ,  F05D2240/241 ,  F05D2240/242 ,  Y02E10/34

摘要： The invention relates to a two-phase expansion device (106) capable of maximizing the amount of movement produced by a two-phase flow. The two-phase expansion device (106) is characterized in that it includes at least: one dispenser (105) for dispensing the fluid to a plurality of two-phase expansion nozzles (60); a plurality of adjacent two-phase expansion nozzles (60) with substantially parallel axes, each two-phase expansion nozzle (60) including sequentially at least one diffuser (65), one neck (66), and one tube (67), the two-phase expansion nozzles (60) being arranged to each receive a portion of the flow from the hot source; and means for supporting the plurality of two-phase expansion nozzles (60) and including means for sealably separating the two-phase expansion nozzles (60).

摘要翻译： 能够使由两相流产生的运动量最大化的两相膨胀装置（106）。 两相膨胀装置（106）至少包括：用于将流体分配到多个两相膨胀喷嘴（60）的一个分配器（105）; 多个具有基本上平行的轴的相邻的两相膨胀喷嘴（60），每个两相膨胀喷嘴（60）依次包括至少一个扩散器（65），一个颈部（66）和一个管（67）， 两相膨胀喷嘴（60）被布置成每个接收来自热源的流的一部分; 以及用于支撑多个两相膨胀喷嘴（60）并包括用于密封地分离两相膨胀喷嘴（60）的元件的元件。

公开(公告)号：EP2873838A1

公开(公告)日：2015-05-20

申请号：EP14190227.0

申请日：2014-10-24

申请人： Rolls-Royce Deutschland Ltd & Co KG

发明人： Beier, Jürgen ,  Venter, Gideon

IPC分类号： F02C3/30 ,  F02C7/06 ,  F01D25/18 ,  B01D46/00 ,  B01D47/06 ,  B01D51/04

CPC分类号： F01D25/18 ,  B01D45/12 ,  B01D46/0086 ,  B01D46/429 ,  B01D47/06 ,  F02C3/30 ,  F02C7/06 ,  F05D2210/13 ,  F05D2260/609 ,  F05D2260/98

摘要： Es wird ein Strahltriebwerk (1) mit einer Einrichtung (29) zum Einsprühen von Öl in einen in einem von einem Wandungsbereich (33) begrenzten Strömungsquerschnitt (34) geführten Luft-Öl-Volumenstrom beschrieben. Der Luft-Öl-Volumenstrom ist zum Abscheiden von Öl durch einen Ölabscheider führbar. Erfindungsgemäß ist das Öl im Bereich der Einrichtung (29) über einen bewegbar gegenüber dem Wandungsbereich (33) ausgeführten Auslassbereich (35) in den Luft-Öl-Volumenstrom einsprühbar.

摘要翻译： 它被描述（34）引导的空气 - 油流，具有喷气发动机（1）的装置（29）用于注入油成的壁区域（33）的流动横截面的一个密闭。 空气 - 油流可被引导到的油通过油分离器的分离。 据经由可相对于运行所述出口（35）到空气油流einsprühbar壁区域（33）本发明的油在所述装置（29）的面积。

公开(公告)号：EP2082959A2

公开(公告)日：2009-07-29

申请号：EP09150886.1

申请日：2009-01-19

申请人： Honeywell International Inc.

发明人： Dwyer, Michael D., Honeywell International Inc. ,  Wessels, Richard F., Honeywell International Inc. ,  Hollingsworth, D. R., Honeywell International Inc.

IPC分类号： B64D11/02 ,  F02C3/30 ,  F02C7/143 ,  F02C3/24

CPC分类号： B64D11/02 ,  F02C3/24 ,  F02C3/30 ,  F02C3/305 ,  F02C7/1435 ,  F05D2210/13 ,  F05D2220/60 ,  F05D2260/602 ,  Y02T50/46 ,  Y02T50/671 ,  Y02T50/675

摘要： A disposal system is provided. In an embodiment, by way of example, the disposal system can include a first tank (22) adapted to be at least partially filled with waste fluid. The disposal system can also include a waste processing device (28) adapted to receive waste fluid and adjust one or more properties of the waste fluid. Additionally, the waste disposal system can include a jet engine (38) comprising a first chamber adapted to contain a fluid undergoing compression. The jet engine can be in fluid communication with the waste processing device to receive the waste fluid from the waste processing device.

摘要翻译： 提供处置系统。 在一个实施例中，举例来说，处理系统可以包括适于至少部分地填充有废液的第一箱（22）。 处理系统还可以包括废物处理装置（28），其适于接收废弃流体并调整废弃流体的一种或多种性质。 另外，废物处理系统可以包括喷气发动机（38），该喷气发动机（38）包括适于容纳经受压缩的流体的第一室。 喷气发动机可以与废物处理装置流体连通以从废物处理装置接收废物流体。

公开(公告)号：EP1836378A1

公开(公告)日：2007-09-26

申请号：EP05818424.3

申请日：2005-12-23

申请人： Renewable Energy Systems Limited

发明人： DRYSDALE, Kenneth, William, Patterson

IPC分类号： F01D9/06 ,  F01D9/02 ,  F01K21/04 ,  F01K23/04 ,  F01K27/02 ,  F25B41/00 ,  F25B30/02 ,  H02K7/18 ,  H02M7/02

CPC分类号： H02K7/1823 ,  F01D15/005 ,  F01K21/005 ,  F02C1/002 ,  F02C1/007 ,  F05D2210/13 ,  F25B11/02 ,  F25B29/003 ,  F25B2339/047 ,  F25B2400/14 ,  F28C3/08 ,  H02M7/10

摘要： A refrigeration apparatus (7200) includes a heat pump circuit (7201) and a power generation circuit (7100). The power generation circuit (7100) includes an evaporator (701) including a first and a second heat exchanger (710a, 710b), a turbine (702), a condenser (703) and a pump (704). The first heat exchanger (710a) absorbs heat rejected from the heat pump circuit (7201) into a power generation circuit (7100) while the second heat exchanger (710b) further heats the fluid. The power generation circuit (7100) includes a bypass (707) which allows a portion of working liquid to enter the turbine (702) without passing through the evaporator (701). A heat pump (704) with similar bypass is also disclosed. Also disclosed are dual stage turbine design and a nozzle (10300) for a turbine which includes two fluid paths (1011, 1014) that adapted to receive and mix the liquid and vapour streams of working fluid, so that the liquid working fluid is vaporized by the heat from the vapour working fluid.

公开(公告)号：EP0839278A4

公开(公告)日：2000-02-23

申请号：EP96918409

申请日：1996-06-07

申请人： BIPHASE ENERGY COMPANY

发明人： HAYS LANCE G

IPC分类号： F03G4/00 ,  B01D17/00 ,  B01D19/00 ,  F01D1/00 ,  F01D1/32 ,  F01D15/00 ,  F01D25/32 ,  F01K21/00 ,  F01K25/04 ,  F03G7/04 ,  F03G7/00 ,  F01D1/36 ,  F01K25/06 ,  F01K27/00

CPC分类号： F01K21/005 ,  B01D17/00 ,  B01D17/0217 ,  B01D17/044 ,  B01D19/0052 ,  F01D1/00 ,  F01D1/32 ,  F01D15/00 ,  F01D25/32 ,  F05D2210/13 ,  F05D2240/36

摘要： A multistage two-phase turbine having multiple stages to receive fluid, each stage having an inlet and outlet comprising nozzles at the inlet to each stage to accelerate the fluid that consists of a mixture of gas and liquid, to form two-phase jets; a rotating separator structure to receive and separate the two-phase jets into gas streams and liquid stream in each stage; the turbine having a rotating output shaft, and there being structure to convert the kinetic energy of the liquid streams into shaft power; structure to remove the separated liquid from at least one stage and transfer it to nozzles at the next stage; structure to remove the separated liquid from the last stage and transfer it to primary outlet structure; and structure to remove the separated gas from at least one stage and transfer it to a secondary outlet structure.

公开(公告)号：EP0032815B1

公开(公告)日：1986-01-08

申请号：EP81300172.4

申请日：1981-01-15

申请人： TRANSAMERICA DELAVAL INC.

发明人： Ritzi, Emil W.

IPC分类号： F01K21/00 ,  F01D1/00

CPC分类号： F01D1/32 ,  F01K21/005 ,  F05D2210/13 ,  F05D2240/36