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公开(公告)号：US20050276690A1
公开(公告)日：2005-12-15
申请号：US11151452
申请日：2005-06-14
CPC分类号： F02C6/08 , F01D11/24 , F05D2270/00 , F05D2270/64
摘要： A system for controlling a flow of air applied to a gas turbine shroud in an airplane engine, the air flow being adjusted by a regulator valve of position that is controlled by a first control signal calculated on the basis of a first setpoint value corresponding to predetermined clearance between the rotor and the turbine shroud. The system further comprises means for calculating at least one second control signal based on a second setpoint value different from the first value representative of clearance in the turbine, and selector means for-selecting the second control signal to control the regulator valve in response to one or more engine parameters. With such a system, it is possible to control the air flow applied to the shroud in application of a plurality of control logic systems.
摘要翻译： 一种用于控制施加到飞机发动机中的燃气涡轮机护罩的空气流的系统，所述空气流由调节阀调节，所述调节阀由通过基于对应于预定的第一设定值计算的第一控制信号控制 转子与涡轮机罩之间的间隙。 该系统还包括用于基于与代表涡轮机中的间隙的第一值不同的第二设定点值来计算至少一个第二控制信号的装置，以及用于响应于一个控制信号控制第二控制信号以控制调节阀的选择器装置 或更多的发动机参数。 利用这种系统，可以在施加多个控制逻辑系统的同时控制施加到护罩的气流。
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公开(公告)号：US07584618B2
公开(公告)日：2009-09-08
申请号：US11151452
申请日：2005-06-14
IPC分类号： F02C6/08
CPC分类号： F02C6/08 , F01D11/24 , F05D2270/00 , F05D2270/64
摘要： A system for controlling a flow of air applied to a gas turbine shroud in an airplane engine, the air flow being adjusted by a regulator valve of position that is controlled by a first control signal calculated on the basis of a first setpoint value corresponding to predetermined clearance between the rotor and the turbine shroud. The system further comprises means for calculating at least one second control signal based on a second setpoint value different from the first value representative of clearance in the turbine, and selector means for-selecting the second control signal to control the regulator valve in response to one or more engine parameters. With such a system, it is possible to control the air flow applied to the shroud in application of a plurality of control logic systems.
摘要翻译： 一种用于控制施加到飞机发动机中的燃气涡轮机护罩的空气流的系统，所述空气流由调节阀调节，所述调节阀由通过基于对应于预定的第一设定值计算的第一控制信号控制 转子与涡轮机罩之间的间隙。 该系统还包括用于基于与代表涡轮机中的间隙的第一值不同的第二设定点值来计算至少一个第二控制信号的装置，以及用于响应于一个控制信号控制第二控制信号以控制调节阀的选择器装置 或更多的发动机参数。 利用这种系统，可以在施加多个控制逻辑系统的同时控制施加到护罩的气流。
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公开(公告)号：US07287955B2
公开(公告)日：2007-10-30
申请号：US11031128
申请日：2005-01-10
申请人： Denis Amiot , Anne-Marie Arraitz , Thierry Fachat , Alain Gendraud , Pascal Lefebvre , Delphine Roussin-Moynier
发明人： Denis Amiot , Anne-Marie Arraitz , Thierry Fachat , Alain Gendraud , Pascal Lefebvre , Delphine Roussin-Moynier
IPC分类号： F01D11/18
CPC分类号： F01D11/24 , F05D2230/13
摘要： A clearance control device for controlling clearance between rotary blade tips and a stationary bushing of a gas turbine having a casing that is provided with at least two annular ridges, the clearance control device including a circular tuning unit that includes air circulation means for circulating air, said means being made up of at least three ducts; air supply means for supplying air to the air flow ducts; and air discharge means for discharging air on the ridges in order to modify the temperature, the air discharge means for each duct being made up of at least one top row having a number N of perforations disposed facing one of the side faces of the ridges and of at least one bottom row having a number 2N of perforations disposed facing a connection radius that connects the ridges to the casing.
摘要翻译： 一种间隙控制装置，用于控制旋转叶片尖端和具有设置有至少两个环形脊的壳体的燃气轮机的固定衬套之间的间隙，所述间隙控制装置包括圆形调谐单元，所述圆形调谐单元包括用于循环空气的空气循环装置， 所述装置由至少三个管道组成; 用于向空气流动管道供应空气的供气装置; 以及空气排出装置，用于排出脊上的空气以改变温度，每个管道的排气装置由至少一个顶排组成，其具有面向脊的一个侧面设置的N个穿孔， 至少一个底行，其具有数目2N的穿孔，所述穿孔面向连接脊与壳体的连接半径。
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公开(公告)号：US20050158169A1
公开(公告)日：2005-07-21
申请号：US11031128
申请日：2005-01-10
申请人： Denis Amiot , Anne-Marie Arraitz , Thierry Fachat , Alain Gendraud , Pascal Lefebvre , Delphine Roussin-Moynier
发明人： Denis Amiot , Anne-Marie Arraitz , Thierry Fachat , Alain Gendraud , Pascal Lefebvre , Delphine Roussin-Moynier
CPC分类号： F01D11/24 , F05D2230/13
摘要： A clearance control device for controlling clearance between rotary blade tips and a stationary bushing of a gas turbine having a casing that is provided with at least two annular ridges, the clearance control device including a circular tuning unit that includes air circulation means for circulating air, said means being made up of at least three ducts; air supply means for supplying air to the air flow ducts; and air discharge means for discharging air on the ridges in order to modify the temperature, the air discharge means for each duct being made up of at least one top row having a number N of perforations disposed facing one of the side faces of the ridges and of at least one bottom row having a number 2N of perforations disposed facing a connection radius that connects the ridges to the casing.
摘要翻译： 一种间隙控制装置，用于控制旋转叶片尖端和具有设置有至少两个环形脊的壳体的燃气轮机的固定衬套之间的间隙，所述间隙控制装置包括圆形调谐单元，所述圆形调谐单元包括用于循环空气的空气循环装置， 所述装置由至少三个管道组成; 用于向空气流动管道供应空气的供气装置; 以及空气排出装置，用于排出脊上的空气以改变温度，每个管道的排气装置由至少一个顶排组成，其具有面向脊的一个侧面设置的N个穿孔， 具有至少一个底行，其具有面向连接所述脊与所述壳体的连接半径设置的数目为2N的穿孔。
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公开(公告)号：US07201559B2
公开(公告)日：2007-04-10
申请号：US11110885
申请日：2005-04-21
IPC分类号： F01D11/14
CPC分类号： F01D11/005
摘要： A stationary ring assembly forming a rotor shroud for a gas turbine including a plurality of segments having adjacent side faces that are placed end to end with sealing means interposed therebetween. The sealing means include at least one axial sealing strip and at least one radial sealing strip respectively received in axial slots and in radial slots formed facing one another in the adjacent side faces of the segments. At least one end of each radial slot opens out into the corresponding axial slot, each axial slot of a segment presents a depth that is greater than the depth of the corresponding radial slot, and the axial sealing strip presents a width that is greater than the width of the radial strip.
摘要翻译： 一种形成用于燃气轮机的转子护罩的固定环组件，包括多个段，所述多个段具有相邻的侧面，所述相邻的侧面以其间插入的密封装置端对端设置。 密封装置包括至少一个轴向密封条和至少一个径向密封条，其分别容纳在轴向槽中和在相邻侧面中彼此面对的径向槽中。 每个径向槽的至少一端开口到对应的轴向槽中，一段的每个轴向槽呈现出比相应的径向槽的深度大的深度，并且轴向密封条的宽度大于 径向条的宽度。
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公开(公告)号：US20050248100A1
公开(公告)日：2005-11-10
申请号：US11110885
申请日：2005-04-21
CPC分类号： F01D11/005
摘要： A stationary ring assembly forming a rotor shroud for a gas turbine, the stationary ring assembly comprising a plurality of segments having adjacent side faces that are placed end to end with sealing means interposed therebetween, the sealing means comprising at least one axial sealing strip and at least one radial sealing strip respectively received in axial slots and in radial slots formed facing one another in the adjacent side faces of the segments, at least one end of each radial slot opening out into the corresponding axial slot, each axial slot of a segment presenting a depth that is greater than the depth of the corresponding radial slot, and the axial sealing strip presenting a width that is greater than the width of the radial strip.
摘要翻译： 一种固定环组件，其形成用于燃气轮机的转子罩，所述固定环组件包括多个段，所述多个段具有相邻的侧面，所述相邻的侧面以插入其间的密封装置端对端设置，所述密封装置包括至少一个轴向密封条， 至少一个径向密封条分别容纳在轴向槽中和在所述段的相邻侧面中彼此面对的径向槽中，每个径向槽的至少一端开口到相应的轴向槽中， 大于相应的径向槽的深度的深度，以及轴向密封条的宽度大于径向条的宽度。
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