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1. 发明授权

EP1362984B1 Gas turbine engine 有权
公开(公告)号：EP1362984B1
公开(公告)日：2007-04-25
申请号：EP03252779.8
申请日：2003-05-02
申请人： ROLLS-ROYCE PLC
发明人： Walsh, Philip Patrick , Fletcher, Paul
IPC分类号： F02C3/13 , F02C3/113 , F01D17/16 , F02C3/10 , F02C7/08 , F02C6/18 , F02C3/30
CPC分类号： F02C3/305 , F01D17/162 , F01D17/165 , F02C3/10 , F02C3/107 , F02C3/113 , F02C3/13 , F02C6/18 , F02C7/08 , Y02T50/671

2. 发明授权

EP1365127B1 Gas turbine engine and method of operating such a gas turbine engine 有权
标题翻译：操作这样一种发动机的燃气涡轮发动机和方法
公开(公告)号：EP1365127B1
公开(公告)日：2008-08-13
申请号：EP03252858.0
申请日：2003-05-07
申请人： ROLLS-ROYCE PLC
发明人： Walsh, Philip Patrick , Fletcher, Paul
IPC分类号： F02C3/30
CPC分类号： F02C7/10 , F02C3/305 , F02C7/1435

3. 发明公开

EP1362984A2 Gas turbine engine 有权
标题翻译：燃气轮机
公开(公告)号：EP1362984A2
公开(公告)日：2003-11-19
申请号：EP03252779.8
申请日：2003-05-02
申请人： ROLLS-ROYCE plc
发明人： Walsh, Philip Patrick , Fletcher, Paul
IPC分类号： F01D17/14 , F02C3/13 , F02C7/057
CPC分类号： F02C3/305 , F01D17/162 , F01D17/165 , F02C3/10 , F02C3/107 , F02C3/113 , F02C3/13 , F02C6/18 , F02C7/08 , Y02T50/671
摘要： A gas turbine engine (10) comprises a first compressor (16), a combustor (22) and a first turbine (24) arranged in flow series. The first turbine (24) is arranged to drive the first compressor (16). The first compressor (16) has variable inlet guide vanes (38) and the first turbine (24) has variable inlet guide vanes (42). A second compressor (48) is arranged upstream of the first compressor (16). An auxiliary intake (12) is arranged upstream of the first compressor (16) and downstream of the second compressor (48). A valve (54) is arranged upstream of the first compressor (16) and downstream of the second compressor (48). The valve (54) is movable between a first position in which the second compressor (48) supplies air to the first compressor (16) and a second position in which the second compressor (48) does not supply fluid to the second compressor (16) and the auxiliary intake (12) supplies fluid to the first compressor (16). A drive means (60,62,64,66) is arranged to selectively drive the second compressor (48).
摘要翻译：燃气涡轮发动机（10）包括以流动系列布置的第一压缩机（16），燃烧器（22）和第一涡轮机（24）。第一涡轮（24）布置成驱动第一压缩机（16）。第一压缩机（16）具有可变的入口导向叶片（38），并且第一涡轮机（24）具有可变的入口导向叶片（42）。第二压缩机（48）布置在第一压缩机（16）的上游。辅助进气口（12）布置在第一压缩机（16）的上游并且在第二压缩机（48）的下游。阀（54）布置在第一压缩机（16）的上游和第二压缩机（48）的下游。阀54可以在第二压缩机48向第一压缩机16供应空气的第一位置和第二压缩机48不向第二压缩机16供应流体的第二位置之间移动）和辅助进气口（12）向第一压缩机（16）供应流体。驱动装置（60,66,66,66）布置成有选择地驱动第二压缩机（48）。

4. 发明公开

EP1362984A3 Gas turbine engine 有权
标题翻译：燃气轮机
公开(公告)号：EP1362984A3
公开(公告)日：2006-09-06
申请号：EP03252779.8
申请日：2003-05-02
申请人： ROLLS-ROYCE PLC
发明人： Walsh, Philip Patrick , Fletcher, Paul
IPC分类号： F02C3/13 , F02C3/113 , F01D17/16 , F02C3/10 , F02C7/08 , F02C6/18 , F02C3/30
CPC分类号： F02C3/305 , F01D17/162 , F01D17/165 , F02C3/10 , F02C3/107 , F02C3/113 , F02C3/13 , F02C6/18 , F02C7/08 , Y02T50/671
摘要： A gas turbine engine (10) comprises a first compressor (16), a combustor (22) and a first turbine (24) arranged in flow series. The first turbine (24) is arranged to drive the first compressor (16). The first compressor (16) has variable inlet guide vanes (38) and the first turbine (24) has variable inlet guide vanes (42). A second compressor (48) is arranged upstream of the first compressor (16). An auxiliary intake (12) is arranged upstream of the first compressor (16) and downstream of the second compressor (48). A valve (54) is arranged upstream of the first compressor (16) and downstream of the second compressor (48). The valve (54) is movable between a first position in which the second compressor (48) supplies air to the first compressor (16) and a second position in which the second compressor (48) does not supply fluid to the second compressor (16) and the auxiliary intake (12) supplies fluid to the first compressor (16). A drive means (60,62,64,66) is arranged to selectively drive the second compressor (48).

5. 发明公开

EP1055809A3 A gas turbine engine and a method of controlling a gas turbine engine 有权
标题翻译：燃气轮机及其控制
公开(公告)号：EP1055809A3
公开(公告)日：2002-11-27
申请号：EP00303481.6
申请日：2000-04-25
申请人： ROLLS-ROYCE PLC
发明人： Willis, Jeffrey Douglas , Melville, James , Fletcher, Paul , Walsh, Philip Patrick
IPC分类号： F02C9/20 , F02C3/08 , F02C7/08 , F02C6/20 , F02C3/10 , F23R3/28
CPC分类号： F02C7/08 , F02C3/08 , F02C9/20
摘要： A gas turbine engine comprises a centrifugal compressor (4), an air diffuser (8), a heat exchanger (10), combustion apparatus (12), and first and second turbines (14,18). The combustion chamber assembly (22) comprises a primary, a secondary and a tertiary fuel and air mixing ducts (54,78,98). The compressor (4), diffuser (8), primary and secondary fuel and air mixing ducts (54,78) and turbines (14,18) all comprise means (6,8,16,20) for varying the mass flow area at their inlets such that in operation the amount of air mass through each component may be independently variable. Under part power conditions the mass flow is reduced and under full power conditions the mass flow is increased thereby maintaining a substantially constant gas cycle throughout the engine.

6. 发明公开

EP0765998A2 Turbine engine control system 失效
标题翻译： Kraftstoffregelsystemfüreine Gasturbine
公开(公告)号：EP0765998A2
公开(公告)日：1997-04-02
申请号：EP96306574.3
申请日：1996-09-10
申请人： ROLLS-ROYCE plc
发明人： Walsh, Philip Patrick , Corbett, Nicholas Charles , Rowe, Arthur Laurence
IPC分类号： F02C9/28
CPC分类号： F02C9/28 , F02C9/34
摘要： A fuel control system (300) for a premixed lean burn combustor (36) in a combustion turbine engine (10), the combustor (36) having at least two stages (P,S,T), the control system (300) including;

an air flow evaluation module (28) having means utilising an iterative algorithm (29) to derive an accurate value of total air flow to the combustor (W31), the evaluation module (28) further having means (31) dividing the derived total air flow value into the proportions (Mp, Ms, Mt) required by the combustor stages (p, s, t) and outputting signals in parallel representing the air flow to respective combustor stages (p, s, t), and
a control module (317, 322, 327, 352) associated with each stage (p, s, t) of the combustor (36) and responsible for setting the fuel demand signal for the associated combustor stage (p, s, t), each control module (317, 322, 327, 352) being adapted to set the fuel demand signal with reference to an appropriate one of said output signals.
摘要翻译：一种用于燃气涡轮发动机（10）中的预混稀燃燃烧器（36）的燃料控制系统（300），所述燃烧器（36）具有至少两级（P，S，T），所述控制系统（300）包括 ; 具有利用迭代算法（29）导出到燃烧器（W31）的总空气流的准确值的装置的空气流评估模块（28），所述评估模块（28）还具有将导出的总空气将流量值分配为燃烧器级（p，s，t）所需的比例（Mp，Ms，Mt）并且并行地输出表示到各个燃烧器级（p，s，t）的空气流的信号，以及控制模块与燃烧器（36）的每个级（p，s，t）相关联并且负责设置用于相关联的燃烧器级（p，s，t）的燃料需求信号，每个控制模块（317,322,327,352） 317,322,327,352）适于根据所述输出信号中的适当一个来设置燃料需求信号。

7. 发明授权

EP1055809B1 A gas turbine engine and a method of controlling a gas turbine engine 有权
标题翻译：燃气轮机及其控制
公开(公告)号：EP1055809B1
公开(公告)日：2006-03-01
申请号：EP00303481.6
申请日：2000-04-25
申请人： ROLLS-ROYCE PLC
发明人： Willis, Jeffrey Douglas , Melville, James , Fletcher, Paul , Walsh, Philip Patrick
IPC分类号： F02C9/20 , F02C3/08 , F02C7/08 , F02C6/20 , F02C3/10 , F23R3/28
CPC分类号： F02C7/08 , F02C3/08 , F02C9/20

8. 发明公开

EP1521037A1 Method and system for controlling fuel supply in a combustion turbine engine 有权
标题翻译： Verfahren und System zur Regelung der Brennstoffversorgung in einer Gurburbine
公开(公告)号：EP1521037A1
公开(公告)日：2005-04-06
申请号：EP04255353.7
申请日：2004-09-03
申请人： ROLLS-ROYCE plc
发明人： Fletcher, Paul , Walsh, Philip Patrick
IPC分类号： F23R3/34 , F02C9/28
CPC分类号： F23R3/286 , F02C9/263 , F02C9/28 , F23N1/00 , F23N2041/20 , F23R3/346
摘要： In order to regulate fuel flow to the combustor (36) of the combustion turbine engine (10) having a primary combustion zone (64) and at least one further combustion zone, the temperature of the inlet and outlet of the combustor (36) are determined, as are first and second values representing first and second properties, with the first property being one of: the total enthalpy rise in the combustor (36), the equivalence ratio of the combustor (36), the fuel/air ratio of said combustor (36), the fuel flow through the combustor, and the second property being one of: the enthalpy rise in the primary zone (64), the equivalence ratio of said primary zone (64), the fuel/air ratio of the primary zone(64); the temperature rise across the primary zone(64), or the fuel flow through the primary zone (64). The second property is determined from the first value and the current value of the ratio of the fuel to the primary zone (64) to the total fuel to the combustor (36). The temperature of the outlet of the primary zone (64) is thus determined from the inlet temperature and the second value, are compared with a predetermined temperature to generate a control signal dependent on the difference. The fuel to the primary zone (64) is then varied, to vary the control signal to reduce the difference. This use of ratios eliminates the need for a gas chromatograph, flow ratios and humidity sensors to determine the properties of the gas.
摘要翻译：为了调节到具有主燃烧区（64）和至少一个另外的燃烧区的燃气涡轮发动机（10）的燃烧器（36）的燃料流，燃烧器（36）的入口和出口的温度为确定，以及表示第一和第二属性的第一值和第二值，其中第一属性是以下之一：燃烧器（36）中的总焓升高，燃烧器（36）的当量比，所述燃烧器（36）的燃料/空气比燃烧器（36），通过燃烧器的燃料流动，第二特性是以下之一：初级区域（64）中的焓升高，所述初级区域（64）的当量比，初级区域（64）的燃料/空气比区（64）; 主区域（64）的温度上升，或通过主区域（64）的燃料流。第二特性根据燃料与主要区域（64）与燃烧器（36）的总燃料的比率的第一值和当前值确定。因此，从入口温度和第二值确定主区域（64）的出口的温度与预定温度进行比较，以根据差异产生控制信号。然后改变到主区域（64）的燃料以改变控制信号以减小差异。这种比例的使用消除了气相色谱仪，流量比和湿度传感器的需要，以确定气体的性质。

9. 发明公开

EP1365127A3 Gas turbine engine and method of operating such a gas turbine engine 有权
标题翻译：操作这样一种发动机的燃气涡轮发动机和方法
公开(公告)号：EP1365127A3
公开(公告)日：2004-11-17
申请号：EP03252858.0
申请日：2003-05-07
申请人： ROLLS-ROYCE plc
发明人： Walsh, Philip Patrick , Fletcher, Paul
IPC分类号： F02C3/30
CPC分类号： F02C7/10 , F02C3/305 , F02C7/1435
摘要： A gas turbine engine (10) comprises a second compressor (14), a first compressor (16), a heat exchanger (18), a combustor (20), a first turbine (22), a second turbine (24) and a third turbine (26) arranged in flow series. The first turbine (22) is arranged to drive the first compressor (16). The second turbine (24) is arranged to drive the second compressor (14). There are means to inject liquid into the gas turbine engine (10). The means to inject liquid is arranged to inject liquid upstream (46) of the second compressor (14), within (48) the second compressor (14), between (50) the second compressor (14) and the first compressor (16), within (52) the first compressor (16), between (54) the first compressor (16) and the heat exchanger (18) or within (56) the combustor (20) to boost the power of the gas turbine engine (10). The means to inject liquid is arranged to inject liquid between (70) the combustor (20) and the first turbine (22), within (68) the first turbine (22), between (66) the first turbine (22) and the second turbine (24), within (64) the second turbine (24), between (62) the second turbine (24) and the third turbine (26), within (60) the third turbine (26) or between (72) the third turbine (26) and the heat exchanger (18) to reduce the power of the gas turbine engine (10).

10. 发明授权

EP1521037B1 Method and system for controlling fuel supply in a combustion turbine engine 有权
标题翻译：一种用于控制燃气涡轮机的燃料供给的方法和系统
公开(公告)号：EP1521037B1
公开(公告)日：2011-11-16
申请号：EP04255353.7
申请日：2004-09-03
申请人： ROLLS-ROYCE PLC
发明人： Fletcher, Paul , Walsh, Philip Patrick
IPC分类号： F23R3/34 , F02C9/28
CPC分类号： F23R3/286 , F02C9/263 , F02C9/28 , F23N1/00 , F23N2041/20 , F23R3/346

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