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1. 发明授权

EP2372105B1 Rotor blade tip clearance control 有权转让
公开(公告)号：EP2372105B1
公开(公告)日：2019-05-22
申请号：EP11157430.7
申请日：2011-03-09
申请人： Rolls-Royce plc
发明人： Lewis, Leo Vivian , Bacic, Marko
IPC分类号： F01D11/24

2. 发明授权

EP2722489B1 Fluidic actuator 有权转让
公开(公告)号：EP2722489B1
公开(公告)日：2018-07-18
申请号：EP13185175.0
申请日：2013-09-19
申请人： Rolls-Royce plc
发明人： Bacic, Marko , Daniel, Ronald
IPC分类号： F01D11/06 , F01D11/10 , F01D11/20
CPC分类号： F04D29/16 , F01D11/06 , F01D11/10 , F01D11/20 , F05D2270/62
摘要： A fluidic actuator (64) comprising: a fluid nozzle (52) for delivering fluid and a tube (56) having an open end (58) and a closed end (60), the open end (58) spaced from the fluid nozzle (52). Also a pair of electrodes (66) mounted in the tube (56) and spaced apart to create a spark gap therebetween. A voltage source (68) is arranged to supply a voltage across the pair of electrodes (66) wherein the voltage causes plasma formation in the spark gap thereby shortening the effective length (x) of the tube (56).

3. 发明公开

EP2599969A3 Method of detecting shaft break and system 有权转让
标题翻译：检测轴断裂和系统的方法
公开(公告)号：EP2599969A3
公开(公告)日：2017-11-29
申请号：EP12191015.2
申请日：2012-11-02
申请人： Rolls-Royce plc
发明人： Bacic, Marko
IPC分类号： F01D21/04
CPC分类号： F01D21/04 , F01D17/04 , F01D17/06 , F01D17/08 , F01D17/085 , F01D21/003 , F01D21/045
摘要： The present invention provides a method of detecting shaft break in a shaft system comprising a shaft coupled between two masses. The method comprises a number of steps. Firstly, to define a time-dependent rotational speed equation for the shaft in terms of system inertia for an engine transient event. Then to discretize the rotational speed equation in terms of a discrete time constant in the discrete domain. Then to recursively define the discretized equation to give a recursive equation and to solve the recursive equation to determine the discrete time constant. Then to define a threshold as a function of engine power and then to set a shaft break signal to TRUE if the discrete time constant is greater than the threshold. A shaft break detection system is also provided by the present invention.
摘要翻译：本发明提供了一种检测轴系统中轴断裂的方法，该轴系统包括连接在两个质量块之间的轴。该方法包括多个步骤。首先，根据发动机瞬态事件的系统惯性来定义轴的时间相关旋转速度方程。然后根据离散区域中的离散时间常数离散旋转速度方程。然后递归地定义离散方程以给出递归方程并求解递归方程以确定离散时间常数。然后，将阈值定义为发动机功率的函数，然后如果离散时间常数大于阈值，则将轴断裂信号设置为TRUE。本发明还提供了一种轴断裂检测系统。

4. 发明公开

EP2620601A3 Improvements in or relating to gas turbine engine control 无效转让
标题翻译：燃气涡轮发动机控制或有关的改进
公开(公告)号：EP2620601A3
公开(公告)日：2017-08-23
申请号：EP13150398.9
申请日：2013-01-07
申请人： Rolls-Royce plc
发明人： Beecroft, Peter , Bacic, Marko , Lewis, Leo Vivian
IPC分类号： F01D11/20 , G05B23/02 , F02C9/00 , F02C9/28
CPC分类号： F02C9/00 , F01D11/08 , F01D11/20 , F02C9/28 , F05D2260/80 , F05D2260/82
摘要： A gas turbine engine control apparatus comprises a controller (34), a memory (36) associated with the controller (34) and inputs (38) for measurement data from an engine. The controller (34) determines the start of a monitoring cycle at (73), receives measurement data at the inputs (38) during the monitoring cycle, manipulates the measurement data to provide an incremental deterioration value representing deterioration occurring within the engine and during the monitoring cycle, and uses the incremental deterioration value at (72) to update a deterioration value (74) stored in the memory (36), and determines the start of a further monitoring cycle.
摘要翻译：燃气涡轮发动机控制设备包括控制器（34），与控制器（34）相关联的存储器（36）以及用于来自发动机的测量数据的输入（38）。控制器（34）在（73）处确定监测周期的开始，在监测周期期间在输入端（38）接收测量数据，操纵测量数据以提供表示发动机内发生劣化的增量劣化值，并且在监视周期，并使用（72）处的增量恶化值来更新存储器（36）中存储的恶化值（74），并确定另一监视周期的开始。

5. 发明授权

EP2273168B1 Valve failure detection 有权转让
标题翻译：阀故障检测
公开(公告)号：EP2273168B1
公开(公告)日：2017-08-23
申请号：EP10167135.2
申请日：2010-06-24
申请人： Rolls-Royce plc
发明人： Bacic, Marko
IPC分类号： F04D27/00 , F04D27/02 , F16K37/00
CPC分类号： F16K37/0083 , F04D27/001 , F04D27/0215

6. 发明授权

EP2604825B1 Controller for cooling the turbine section of a gas turbine engine 有权转让
标题翻译：用于冷却燃气轮机发动机的涡轮部分的控制器
公开(公告)号：EP2604825B1
公开(公告)日：2017-04-26
申请号：EP12193315.4
申请日：2012-11-20
申请人： Rolls-Royce plc
发明人： Bacic, Marko
IPC分类号： F02C7/18 , F02C6/08 , F01D5/08
CPC分类号： F02C7/185 , F01D5/08 , F01D5/081 , F01D5/082 , F01D5/085 , F01D5/087 , F01D5/088 , F01D11/24 , F01D17/02 , F01D17/085 , F02C3/13 , F02C6/08 , F02C7/12 , F02C7/125 , F02C9/18 , F05D2260/213 , F05D2260/81 , F05D2270/112 , F05D2270/114 , F05D2270/303 , F05D2270/3032 , F05D2270/44 , Y02T50/675 , Y02T50/676

7. 发明公开

EP2843198A1 Method and control system for active rotor tip control clearance 有权转让
标题翻译： Verfahren und Steuerungssystem zur aktiven Kontrolle des Schaufelspitzenspalts
公开(公告)号：EP2843198A1
公开(公告)日：2015-03-04
申请号：EP14180787.5
申请日：2014-08-13
申请人： Rolls-Royce plc
发明人： Bacic, Marko , Tooke, James
IPC分类号： F01D11/20 , F04D29/16
CPC分类号： F01D19/02 , F01D5/02 , F01D7/02 , F01D11/20 , F01D21/003 , F01D21/14 , F01D25/12 , F04D27/001 , F04D29/164 , F04D29/526 , F05D2220/32 , F05D2260/81 , F05D2260/821 , F05D2270/114 , F05D2270/301 , F05D2270/305 , F05D2270/44 , F05D2270/80
摘要： A method of controlling a rotor tip clearance arrangement of a gas turbine engine and a control system configured to control rotor tip clearance. Steps include measuring at least one engine parameter; determining engine power demand from the at least one engine parameter; and calculating rotor tip clearance given the determined engine power demand. The rotor tip clearance arrangement is controlled to increase or decrease the rotor tip clearance based on the difference between the calculated clearance and a predefined target clearance.
Corresponding control system for controlling a rotor tip clearance arrangement.
摘要翻译：一种控制燃气涡轮发动机的转子顶端间隙布置的方法和被配置为控制转子尖端间隙的控制系统。步骤包括测量至少一个引擎参数; 从所述至少一个发动机参数确定发动机功率需求; 并根据确定的发动机功率需求计算转子叶片间隙。基于计算出的间隙和预定义的目标间隙之间的差异，控制转子顶端间隙布置以增加或减小转子顶端间隙。用于控制转子顶端间隙布置的相应控制系统。

8. 发明公开

EP2604825A2 Controller for cooling the turbine section of a gas turbine engine 有权转让
标题翻译：控制器用于冷却燃气涡轮发动机的涡轮部分
公开(公告)号：EP2604825A2
公开(公告)日：2013-06-19
申请号：EP12193315.4
申请日：2012-11-20
申请人： Rolls-Royce plc
发明人： Bacic, Marko
IPC分类号： F02C7/18 , F02C6/08
CPC分类号： F02C7/185 , F01D5/08 , F01D5/081 , F01D5/082 , F01D5/085 , F01D5/087 , F01D5/088 , F01D11/24 , F01D17/02 , F01D17/085 , F02C3/13 , F02C6/08 , F02C7/12 , F02C7/125 , F02C9/18 , F05D2260/213 , F05D2260/81 , F05D2270/112 , F05D2270/114 , F05D2270/303 , F05D2270/3032 , F05D2270/44 , Y02T50/675 , Y02T50/676
摘要： A gas turbine engine has, in flow series, a compressor section, a combustor, and a turbine section. The engine further has a cooling system which diverts a cooling air flow received from the compressor section to a heat exchanger and then to the turbine section to cool a component thereof. The cooling air flow by-passes the combustor and is cooled in the heat exchanger. The cooling system has a valve arrangement which regulates the cooling air flow. The engine further has a closed-loop controller (56) which estimates and/or measures one or more temperatures (50) of the cooled component, compares values (54) derived from the estimated and/or measured temperatures with one or more corresponding targets, and issues a demand signal to the valve arrangement based on the comparison and a value of the demand signal at a previous time step.

9. 发明公开

EP2273168A2 Valve failure detection 有权转让
标题翻译：阀门故障检测
公开(公告)号：EP2273168A2
公开(公告)日：2011-01-12
申请号：EP10167135.2
申请日：2010-06-24
申请人： Rolls-Royce plc
发明人： Bacic, Marko
IPC分类号： F16K37/00
CPC分类号： F16K37/0083 , F04D27/001 , F04D27/0215
摘要： A method and arrangement for detecting failure of an actuated component, particularly a valve. The method comprises determining a calibration step response (50) and an in-use step response (58) for the actuated component, determining any difference between the responses and comparing the difference to a pre-determined threshold indicating failure.

10. 发明公开

EP4249738A1 GAS TURBINE ENGINE SYSTEM 审中-实审
公开(公告)号：EP4249738A1
公开(公告)日：2023-09-27
申请号：EP23157955.8
申请日：2023-02-22
申请人： Rolls-Royce plc
发明人： Bacic, Marko , Holt, Jonathan
IPC分类号： F02C3/22 , F02C7/232
摘要： A gas turbine engine system 100 comprises a hydrogen-burning gas turbine engine and a fuel system comprising (i) a fuel line 114 arranged to receive gaseous hydrogen at an input 115 thereof and provide the gaseous hydrogen to combustion apparatus 106 of the hydrogen-burning gas turbine engine and (ii) a vent line 116 including a vent valve 104 and having a first end coupled to the fuel line and a second end disposed remotely from the hydrogen-burning gas turbine engine. A controller 112 is arranged to switch the vent valve from a closed state to an open state upon detection of an engine shaft-break or similar condition, thus providing rapid evacuation of gaseous hydrogen from the fuel line and hence rapid shut-down of the engine. The engine may be shut down more rapidly than is possible by means of a shut-off valve within the fuel line.

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