公开(公告)号：EP1923633A2

公开(公告)日：2008-05-21

申请号：EP07020923.4

申请日：2007-10-25

申请人： Delavan Inc. ,  ROSEMOUNT AEROSPACE INC.

发明人： Cornwell, Michael D. ,  Goeke, Jerry L. ,  Myhre, Douglas C. ,  Eriksen, Harald O.

IPC分类号： F23N1/00

CPC分类号： F23N1/002 ,  F01D17/02 ,  F01D21/003 ,  F02C9/28 ,  F05D2270/301 ,  F05D2270/303 ,  F23N5/082 ,  F23N5/16 ,  F23N2029/04 ,  F23N2029/08 ,  F23N2029/16 ,  F23N2041/20 ,  F23N2900/05005 ,  F23R2900/00013 ,  Y02T50/677

摘要： A system is disclosed for actively controlling combustion in a gas turbine engine (10), which includes a fuel injector (110) for issuing fuel into a combustion chamber of the gas turbine engine. The fuel injector has a dynamic pressure sensor (130) for measuring acoustic pressure within the combustion chamber and a flame sensor (140) for observing flame characteristics within the combustion chamber. The system further includes a high speed valve assembly (112) for controlling flow of fuel to the injector and an electronic controller associated with the fuel injector for commanding the valve assembly to deliver fuel to the fuel injector at a commanded flow rate, based upon input from the sensors in the fuel injector.

摘要翻译： 公开了一种用于主动控制燃气涡轮发动机（10）中的燃烧的系统，该燃气涡轮发动机（10）包括用于将燃料释放到燃气涡轮发动机（10）的燃烧室中的燃料喷射器（110）。 燃料喷射器（110）具有用于测量燃烧室内的声压的动态压力传感器（130）和用于观察燃烧室内的火焰特性的火焰传感器（140）。 该系统还包括用于控制燃料流向喷射器（110）的高速阀组件（112）和与燃料喷射器（110）相关联的电子控制器，用于指示阀组件（112）将燃料输送到燃料喷射器 （110），其根据来自燃料喷射器（110）中的传感器（130,140）的输入以指令的流量进行控制。

公开(公告)号：EP1923633A3

公开(公告)日：2013-02-27

申请号：EP07020923.4

申请日：2007-10-25

申请人： Delavan Inc. ,  Rosemount Aerospace Inc.

发明人： Cornwell, Michael D. ,  Goeke, Jerry L. ,  Myhre, Douglas C. ,  Eriksen, Harald O.

IPC分类号： F01D17/02 ,  F01D21/00 ,  F02C9/28 ,  F23N1/00 ,  F23N5/08 ,  F23N5/16 ,  F23R3/00

CPC分类号： F23N1/002 ,  F01D17/02 ,  F01D21/003 ,  F02C9/28 ,  F05D2270/301 ,  F05D2270/303 ,  F23N5/082 ,  F23N5/16 ,  F23N2029/04 ,  F23N2029/08 ,  F23N2029/16 ,  F23N2041/20 ,  F23N2900/05005 ,  F23R2900/00013 ,  Y02T50/677

摘要： A system is disclosed for actively controlling combustion in a gas turbine engine (10), which includes a fuel injector (110) for issuing fuel into a combustion chamber of the gas turbine engine (10). The fuel injector (110) has a dynamic pressure sensor (130) for measuring acoustic pressure within the combustion chamber and a flame sensor (140) for observing flame characteristics within the combustion chamber. The system further includes a high speed valve assembly (112) for controlling flow of fuel to the injector (110) and an electronic controller associated with the fuel injector (110) for commanding the valve assembly (112) to deliver fuel to the fuel injector (110) at a commanded flow rate, based upon input from the sensors (130,140) in the fuel injector (110).

公开(公告)号：EP2028422A2

公开(公告)日：2009-02-25

申请号：EP08014915.6

申请日：2008-08-22

申请人： Delavan Inc.

发明人： Cornwell, Michael D. ,  Goeke, Jerry L.

IPC分类号： F23N5/24 ,  F23R3/28

CPC分类号： F23R3/28 ,  F02C7/232 ,  F02C9/266 ,  F05D2270/083 ,  F23N5/242 ,  F23N2035/18 ,  F23N2041/20 ,  F23R2900/00013

摘要： A method of controlling combustion stability in a turbine engine having combustion stability control capability includes the steps of providing at least one pair of pulsating valves, mutually arranged in parallel with respect to fuel flow provided to a combustor of the turbine engine, detecting an amplitude and frequency of a pressure wave of at least one periodic combustion instability, selecting an amplitude, frequency and first phase shift, with respect to the pressure wave, of resultant fuel pulsations to reduce the amplitude of the pressure wave, translating the selected amplitude into a second, relative phase shift between each pulsating valve of at least one pair of pulsating valves, and commanding each pulsating valve of at least one pair of pulsating valves to operate at the selected frequency and a relative second phase shift with respect to one another, to yield a resultant fuel pulsation at the selected amplitude, frequency and first phase shift, with respect to the detected pressure wave of combustion instability.

摘要翻译： 一种控制具有燃烧稳定性控制能力的涡轮发动机的燃烧稳定性的方法包括以下步骤：提供至少一对相对于提供给涡轮发动机的燃烧器的燃料流平行布置的脉动阀，检测振幅和 至少一个周期性燃烧不稳定性的压力波的频率，相对于压力波选择合成燃料脉动的振幅，频率和第一相移以减小压力波的幅度，将所选择的幅度转换为第二 ，至少一对脉动阀的每个脉动阀之间的相对相移，以及指令至少一对脉动阀的每个脉动阀以选定的频率和相对于彼此的相对第二相移进行操作，以产生 在所选择的振幅，频率和第一相移相对于检测器的结果燃料脉动 d压力波的燃烧不稳定。

公开(公告)号：EP2028422A3

公开(公告)日：2013-03-27

申请号：EP08014915.6

申请日：2008-08-22

申请人： Delavan Inc.

发明人： Cornwell, Michael D. ,  Goeke, Jerry L.

IPC分类号： F23N5/24 ,  F23R3/28 ,  F02C7/232 ,  F02C7/22

CPC分类号： F23R3/28 ,  F02C7/232 ,  F02C9/266 ,  F05D2270/083 ,  F23N5/242 ,  F23N2035/18 ,  F23N2041/20 ,  F23R2900/00013

摘要： A method of controlling combustion stability in a turbine engine having combustion stability control capability includes the steps of providing at least one pair of pulsating valves, mutually arranged in parallel with respect to fuel flow provided to a combustor of the turbine engine, detecting an amplitude and frequency of a pressure wave of at least one periodic combustion instability, selecting an amplitude, frequency and first phase shift, with respect to the pressure wave, of resultant fuel pulsations to reduce the amplitude of the pressure wave, translating the selected amplitude into a second, relative phase shift between each pulsating valve of at least one pair of pulsating valves, and commanding each pulsating valve of at least one pair of pulsating valves to operate at the selected frequency and a relative second phase shift with respect to one another, to yield a resultant fuel pulsation at the selected amplitude, frequency and first phase shift, with respect to the detected pressure wave of combustion instability.