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31. 发明公开

EP2778372A2 Gas turbine engine fuel system with ecology valve 有权
标题翻译： Gasturbinentriebwerks- Brennstoffsystem mitÖkoventil
公开(公告)号：EP2778372A2
公开(公告)日：2014-09-17
申请号：EP14159598.3
申请日：2014-03-13
申请人： PRATT & WHITNEY CANADA CORP.
发明人： Belleville, Francois
IPC分类号： F02C7/232
CPC分类号： F02C7/232 , F01D21/00 , F02C7/228 , F05D2260/602
摘要： A gas turbine engine fuel system (20) has an ecology valve (52) for withdrawing residual fuel from primary and secondary fuel manifolds (22, 24) upon engine shut-down. The ecology valve (52) has primary and secondary reservoirs (66, 72) respectively connected in fluid flow communication with the primary and secondary fuel manifolds (22, 24) and a reciprocating piston (54) movable from a retracted position when engine start-up is initiated to an extended position under normal engine running conditions. The movement of the reciprocating piston (54) between the retracted and extended positions controls the flow of fuel from and to the primary and secondary reservoirs (66, 72). A cross-bleed passage (90) is defined in the reciprocating piston (54) and connects the primary and secondary reservoirs (66, 72) in fluid flow communication only when the piston (54) is in its extended position.
摘要翻译：燃气涡轮发动机燃料系统（20）具有生态阀（52），用于在发动机关闭时从主燃料歧管（22）和第二燃料歧管（22,24）中抽出残余燃料。生态阀（52）具有分别连接到主燃料歧管（22,24）和主燃料歧管（22,24）的流体流动连通的主要和次要储存器（66,72）以及当发动机起动时可从缩回位置移动的往复活塞（54）在正常的发动机运行条件下启动到延伸位置。往复活塞（54）在缩回位置和伸展位置之间的移动控制来自主要和辅助储存器（66,72）的燃料流。交叉排放通道（90）限定在往复活塞（54）中，并且仅当活塞（54）处于其延伸位置时，才将流体流动连通并连接主储液器（66,72）。

32. 发明公开

EP2700878A3 Method for mixing a dilution air in a sequential combustion system of a gas turbine 有权转让
标题翻译：一种用于在燃气涡轮机的连续燃烧系统混合的稀释空气的方法
公开(公告)号：EP2700878A3
公开(公告)日：2014-03-26
申请号：EP13180967.5
申请日：2013-08-20
申请人： Alstom Technology Ltd
发明人： Eroglu, Adnan , Freitag, Ewald
IPC分类号： F23R3/34 , F23R3/20 , F23R3/06
CPC分类号： F23R3/34 , F02C7/22 , F02C7/228 , F23R3/06 , F23R3/20 , F23R3/26 , F23R3/346 , F23R3/42 , F23R2900/00014 , F23R2900/03042 , F23R2900/03341 , Y02E20/14
摘要： The invention relates a method for mixing a dilution air with a hot main flow in a sequential combustion system of a gas turbine (100), wherein the gas turbine essentially comprises at least one compressor, a first combustor which is connected downstream to the compressor The hot gases of the first combustor are admitted to at least one intermediate turbine or directly or indirectly to at least one second combustor, wherein the hot gases of the second combustor are admitted to a further turbine or directly or indirectly to an energy recovery. The method comprising a coaxial injection of first combustor liner cooling air (104) with second combustor liner cooling air (105) having a sufficient excess pressure margin with respect to the second combustor liner cooling air

33. 发明公开

EP1988267A3 Fuel supply system 有权
公开(公告)号：EP1988267A3
公开(公告)日：2014-03-19
申请号：EP08250751.8
申请日：2008-03-05
申请人： Rolls-Royce plc
发明人： Scully, Mark , Rowe, Arthur Laurence
IPC分类号： F02C7/22 , F02C9/28 , F02C9/34 , F02C9/38
CPC分类号： F02C7/228 , F02C7/222 , F02C7/236 , F02C9/263 , F02C9/34 , F05D2270/3015 , F23K5/04 , F23K2301/206
摘要： A turbine fuel supply system is disclosed as including a first sub-system having: a first nozzle for injecting fuel into a combustor of a turbine engine; a first valve controllable to communicate fuel to the first nozzle; and a first fuel manifold for communicating fuel to the first valve from a fuel source; the system further including a controller assembly for raising the pressure of fuel in the first fuel manifold; and the system being characterized in that the first valve is adapted to open in response to a predetermined pressure difference between the first fuel manifold and the pressure in the combustor, thereby allowing fuel to be communicated from the first fuel manifold to the first nozzle. The system may include a first recirculating conduit in fluid communication with the first fuel manifold and the fuel source, the first recirculating conduit allowing fuel not communicated by the first valve to be returned to the fuel source.

34. 发明公开

EP2634395A1 GAS TURBINE AND GAS TURBINE PLANT PROVIDED WITH SAME 有权转让
标题翻译：燃气轮机
公开(公告)号：EP2634395A1
公开(公告)日：2013-09-04
申请号：EP11836415.7
申请日：2011-10-27
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： MURAKAMI, Masayuki , HIGASHI, Kazuya , NAKAMOTO, Yukimasa , FUJII, Satoko , SHIMIZU, Takeyuki , MATSUMOTO, Keigo
IPC分类号： F02C7/232 , F02C7/22 , F02C9/40 , F23R3/28 , F23R3/34 , F23R3/36
CPC分类号： F02C7/232 , F01D25/12 , F02C3/30 , F02C7/14 , F02C7/222 , F02C7/228 , F02C9/40 , F05D2260/213 , F05D2260/2214 , F05D2260/608 , F23D2209/30 , F23K2301/203 , F23R3/283 , F23R3/343 , F23R3/36
摘要： The invention provides a gas-turbine fuel nozzle (1) that includes a plurality of fuel supply channels (3a) to which fuel is supplied, a plurality of fuel/scavenging-fluid supply channels (3b) to which fuel or a scavenging fluid for scavenging the fuel is supplied, and a plurality of injection holes (7a, 7b) that are provided at downstream ends of the fuel supply channels (3a) or the fuel/scavenging-fluid supply channels (3b) and that inject the fuel guided from the fuel supply channels (3a) or the fuel/scavenging-fluid supply channels (3b); a scavenging-fluid supply channel (21) that is connected to the fuel/scavenging-fluid supply channels (3b) to guide the scavenging fluid; and scavenging-fluid cooling means (23) for cooling the scavenging fluid to a temperature lower than a self-ignition temperature of the fuel.
摘要翻译：本发明提供了一种燃气轮机燃料喷嘴（1），其包括多个供应燃料的燃料供应通道（3a），多个燃料/清扫流体供应通道（3b），燃料或清除流体供应通道供给清除燃料的多个喷射孔（7a，7b），设置在燃料供给流路（3a）的下游侧或燃料/扫气流体供给流路（3b）的喷出孔（7a，7b）燃料供应通道（3a）或燃料/清除液供应通道（3b）; 与所述燃料/清扫液供给通道（3b）连接以引导所述清扫流体的扫气流体供应通道（21）以及用于将清扫流体冷却至低于燃料的自燃温度的温度的扫气流体冷却装置（23）。

35. 发明公开

EP2597285A2 Fuel-air mixture distribution for gas turbine engine combustors 有权转让
标题翻译： Kraftstoff-Luft-GemischverteilungfürGasturbinenbrennkammern
公开(公告)号：EP2597285A2
公开(公告)日：2013-05-29
申请号：EP12193572.0
申请日：2012-11-21
申请人： United Technologies Corporation
发明人： Hoke, James B. , Proscia, William
IPC分类号： F02C7/228 , F02C9/28
CPC分类号： F02C9/28 , F02C7/22 , F02C7/228 , F02C7/232 , F05D2260/964 , F05D2270/14 , F23R3/28 , F23R3/34
摘要： A method of noise control from a combustor (56) of a gas turbine engine (20) includes selectively forming a plurality of local circumferential zones with different fuel-air ratios within the combustor (56).
摘要翻译：来自燃气涡轮发动机（20）的燃烧器（56）的噪声控制的方法包括在燃烧器（56）内选择性地形成具有不同燃料 - 空气比的多个局部周向区域。

36. 发明公开

EP2551470A1 Verfahren zum Hochfahren einer stationären Gasturbine 审中-公开
标题翻译：维尔法赫恩zum Hochfahren einerstationärenGasturbine
公开(公告)号：EP2551470A1
公开(公告)日：2013-01-30
申请号：EP11175342.2
申请日：2011-07-26
申请人： SIEMENS AKTIENGESELLSCHAFT
发明人： Deuker, Eberhard , Köstlin, Berthold , Meisl, Jürgen , Nehlsen, Dennis , Schildmacher, Kai-Uwe
IPC分类号： F01D19/00 , F02C3/20 , F02C3/22 , F02C3/24 , F02C3/26 , F02C7/228 , F02C7/26
CPC分类号： F02C7/26 , F01D19/00 , F02C3/20 , F02C3/22 , F02C3/24 , F02C3/26 , F02C7/228 , F02C9/28 , F02C9/34 , F02C9/40 , F05D2260/85 , F05D2270/08 , F05D2270/31
摘要： Die Erfindung betrifft ein Verfahren zum Hochfahren einer stationären Gasturbine (10) mit zumindest einer Brennkammer (14), deren Brenner einen Pilotbrenner und einen Hauptbrenner umfassen und durch die unterschiedliche Brennstoffarten in die Brennkammer (14) zur Verbrennung eingebracht werden, wobei während des Beschleunigens eines Rotors (18) der Gasturbine (10) aus dem Stand bis auf eine Nenndrehzahl die Schritte durchgeführt werden:
- Zuführen von Brennstoff einer ersten Brennstoffart zu den Pilotbrennern und
- Zuführen von Brennstoff der ersten Brennstoffart zu den
Hauptbrennern.
Um ein Verfahren bereitzustellen, bei dem ein vergleichsweise geringer Versorgungsdruck im Brennstoffversorgungssystem erforderlich ist und bei dem während des Hochfahrens maschinengefährdende Verbrennungsschwingungen vermieden werden, wird vorgeschlagen, dass vor dem Erreichen der Nenndrehzahl dem Brenner Brennstoff einer zweiten Brennstoffart zugeführt wird.
摘要翻译：用于启动固定式燃气轮机的方法包括向先导燃烧器供应燃料，并向主燃烧器供应燃料。在实现燃烧器燃料的额定速度之前，提供不同类型的燃料。不同类型的燃料供应给引燃燃烧器。不同类型的燃料被供应到主燃烧器，其中前一类燃料的初始量减少。前一种类型的燃料是气体燃料类型，后一类燃料是液体燃料。

37. 发明公开

EP2511499A2 Fuel flow divider and ecology system for a gas turbine engine fuel flow control system 失效转让
标题翻译：燃料流分离器和生态系统，用于燃气涡轮发动机的燃料流控制系统
公开(公告)号：EP2511499A2
公开(公告)日：2012-10-17
申请号：EP12162915.8
申请日：2012-04-02
申请人： Honeywell International Inc.
发明人： Futa, Paul , McRoberts, Brad , Lafferty, Greg
IPC分类号： F02C7/232 , F02C9/26
CPC分类号： F02C9/263 , F02C7/228 , F02C7/232 , F02C9/34 , Y10T137/2524
摘要： A flow divider valve for a gas turbine engine fuel supply system is provided. The flow divider valve is configured, whenever fuel pressure at its inlet port is between a first predetermined pressure and a second predetermined pressure, to supply the fuel to a start nozzle manifold outlet port at a substantially constant flow rate, and to direct any fuel flow in excess of the substantially constant flow rate to a run nozzle manifold outlet port.

38. 发明公开

EP2475858A1 METHOD FOR SWITCHING OVER A GAS TURBINE BURNER OPERATION FROM LIQUID TO GAS FUEL AND VICE-VERSA 有权转让
标题翻译：一种用于开关的液体燃气涡轮机燃烧器操作，以气体燃料的方法，并且反之亦然
公开(公告)号：EP2475858A1
公开(公告)日：2012-07-18
申请号：EP10760279.9
申请日：2010-09-06
申请人： Alstom Technology Ltd
发明人： MEEUWISSEN, Thiemo , LACHNER, Rudolf , KOKANOVIC, Stanka , SCHELL, Susanne
IPC分类号： F02C3/22 , F02C3/24 , F02C7/228 , F23R3/28 , F23R3/34 , F23D17/00
CPC分类号： F02C3/22 , F02C3/24 , F02C7/228 , F23D17/002 , F23R3/286 , F23R3/343
摘要： The method for switching over a gas turbine burner operation from liquid fuel (21) to gas fuel (22, 23) and vice-versa, with the burner (1) comprising nozzles (6) for feeding a premixed gas fuel, nozzles (8) for injecting a pilot gas fuel (23) and nozzles (9) for injecting a liquid fuel (21). According to the method, while the liquid fuel (21) and the premix gas fuel (22) are regulated to switch over from liquid fuel to gas fuel operation or vice-versa, the pilot gas fuel (23) is controlled at a substantially constant flow rate.

39. 发明授权

EP2075440B1 Method and device for controlling a gas-turbine plant 有权
标题翻译：的方法和装置用于控制燃气轮机设备
公开(公告)号：EP2075440B1
公开(公告)日：2012-05-30
申请号：EP07425849.2
申请日：2007-12-31
申请人： ANSALDO ENERGIA S.P.A.
发明人： Cacciacarne, Stefano , De Micheli, Emanuele , Ferrera, Flavio , Gatti, Roberta
IPC分类号： F02C9/26 , F02C9/28 , F23R3/26 , F23R3/28
CPC分类号： F02C9/28 , F02C7/22 , F02C7/228 , F02C7/232 , F02C9/26 , F02C9/34 , F02C9/40 , F05D2270/083 , F23N1/022 , F23N2037/02 , F23N2041/20 , F23R3/26 , F23R3/34

40. 发明授权

EP1300566B1 Fuel ratio control method in a gas turbine combustor 有权
标题翻译：在燃气轮机燃烧器用于空燃比控制的量的方法
公开(公告)号：EP1300566B1
公开(公告)日：2012-04-04
申请号：EP02021189.2
申请日：2002-09-24
申请人： MITSUBISHI HEAVY INDUSTRIES, LTD.
发明人： Aoyama, Kuniaki, Mitsubishi Heavy Ind. Ltd.
IPC分类号： F02C7/228 , F02C9/26
CPC分类号： F02C7/228 , F01D17/02 , F05D2270/14 , F23D2900/00015 , F23N5/184 , F23N2041/20

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