-
11.发明授权System for controlling variable geometry equipment of a gas turbine engine especially comprising a guiding track connection 有权用于控制燃气涡轮发动机的可变几何设备的系统，特别地包括导轨连接公开(公告)号：US08690520B2
公开(公告)日：2014-04-08
申请号：US13121706
申请日：2009-09-29
IPC分类号： F04D29/56
摘要： A system for controlling at least two sets of variable geometry equipment of a gas turbine engine including at least one first body and a second body, the first set of equipment being a stage of variable stator vanes of a compressor of the first body moving between a closed position during idling and an open position at high speed, and the second set of equipment being at least one bleed valve of a compressor of the second body moving between an open position during idling and a closed position at high speed. An actuator actuates the two sets of equipment.
摘要翻译： 一种用于控制包括至少一个第一主体和第二主体的燃气涡轮发动机的至少两组可变几何设备的系统，所述第一组设备是所述第一主体的压缩机的可变定子叶片的阶段， 在空转期间的关闭位置和高速的打开位置，第二组设备是第二机构的压缩机的至少一个放气阀，其在空转期间的打开位置和高速关闭位置之间移动。 执行器致动两组设备。
-
12.发明授权System for controlling at least two variable-geometry equipments of a gas turbine engine, particularly by rack 有权用于控制燃气涡轮发动机，特别是机架的至少两个可变几何设备的系统公开(公告)号：US08337140B2
公开(公告)日：2012-12-25
申请号：US12566211
申请日：2009-09-24
IPC分类号： F04D29/56
CPC分类号： F01D17/16 , F01D17/20 , F02C6/08 , F02C9/18 , F02C9/22 , F04D29/563 , F05D2270/58
摘要： A system for controlling at least two variable-geometry equipments of a gas turbine engine is disclosed. The engine includes at least a first core rotating at a first speed and a second core rotating at a second speed. The first equipment includes at least one variable-pitch stator blade of a compressor of the first core and the second equipment includes at least one air bleed valve of a compressor of the second engine core moving between an open position at idle speed and a closed position at high speed. The system includes an actuator which actuates both equipments.
摘要翻译： 公开了一种用于控制燃气涡轮发动机的至少两个可变几何设备的系统。 发动机至少包括以第一速度旋转的第一铁心和以第二速度旋转的第二铁芯。 第一设备包括至少一个第一芯的压缩机的可变间距定子叶片，第二设备包括至少一个第二发动机芯的压缩机的排气阀，其在空转速度的打开位置和关闭位置之间移动 高速 该系统包括致动器两个设备的致动器。
-
13.发明授权System for controlling variable-geometry equipments of a turbomachine, particularly by articulated bellcranks 有权用于控制涡轮机的可变几何设备的系统，特别是通过铰接的曲拐公开(公告)号：US08328500B2
公开(公告)日：2012-12-11
申请号：US12566400
申请日：2009-09-24
IPC分类号： F04D29/56
摘要： A system for controlling at least two variable-geometry equipments of a turbomachine, in which the first equipment is a variable pitch stator blade stage of a compressor of a first core moving between a closed position at idle speed and an open position at high speed, and the second equipment is at least one bleed valve of a compressor of a second core moving between an open position at idle speed and a closed position at high speed, is disclosed. The actuator operates over a portion of its travel a first branch of an angle transmission member which actuates the first equipment and leaves this branch at rest on an abutment over the rest of its travel. The actuator operates the second equipment via a sliding junction member arranging a free travel in the actuation of said second equipment.
摘要翻译： 一种用于控制涡轮机的至少两个可变几何设备的系统，其中所述第一设备是在怠速的关闭位置和高速打开位置之间移动的第一铁芯的压缩机的变桨距定子叶片级， 并且第二设备是至少一个在怠速的打开位置和高速关闭位置之间移动的第二芯片的压缩机的排放阀。 致动器在其行程的一部分上操作角度传递构件的第一分支，该第一分支致动第一设备，并使该分支静止在其行程的其余部分上的基台上。 致动器通过滑动接合构件操作第二设备，该滑动接合构件在所述第二设备的致动中布置自由行程。
-
公开(公告)号：US20110246151A1
公开(公告)日：2011-10-06
申请号：US13133790
申请日：2009-12-08
IPC分类号： G06F17/10
CPC分类号： G01K7/42 , G01K13/02 , G01K2013/024
摘要： An estimation method that can estimate a stream temperature in a turbojet including: digitally modeling the stream temperature with help of a modeled signal; and correcting the modeled signal with help of an error signal, a signal obtained after correction representing an estimate of the stream temperature. When predetermined conditions relating to at least one operating stage of a turbojet and to temperature stability are satisfied, the error signal is updated from the modeled signal and from a measurement signal of the stream temperature as delivered by a temperature sensor.
摘要翻译： 可以估计涡轮喷气发动机中的气流温度的估计方法，其包括：借助于建模信号对气流温度进行数字建模; 以及通过误差信号校正建模信号，校正后获得的信号表示流温度的估计。 当满足关于涡轮喷气发动机的至少一个操作阶段和温度稳定性的预定条件时，从建模的信号和由温度传感器传送的流温度的测量信号更新误差信号。
-
15.发明申请SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE PARTICULARLY COMPRISING A BARREL LINK 有权用于控制气瓶涡轮发动机的可变几何设备的系统，特别包括一个气缸连杆公开(公告)号：US20110229310A1
公开(公告)日：2011-09-22
申请号：US13121752
申请日：2009-09-29
IPC分类号： F04D29/56
CPC分类号： F01D17/16 , F01D17/20 , F02C6/08 , F02C9/18 , F02C9/22 , F05D2270/58 , Y02T50/671
摘要： A system for controlling at least two variable geometry apparatuses of a gas turbine engine that includes at least a first body and a second body, the first apparatus including a stator blade stage with a variable setting angle of a compressor of the first body capable of switching between a closed position in an idle mode and an open position in a high-speed mode, and the second apparatus including at least one discharge valve of a compressor of the second body capable of switching between an open position in an idle mode and a closed position in a high-speed mode. The system further includes an actuator for actuating the two apparatuses.
摘要翻译： 一种用于控制燃气涡轮发动机的至少两个可变几何装置的系统，所述至少两个可变几何装置至少包括第一主体和第二主体，所述第一装置包括具有能够切换的第一主体的压缩机的可变的设定角度的定子叶片台 在空闲模式的关闭位置和高速模式的打开位置之间，所述第二装置包括能够在空闲模式的打开位置和关闭状态之间切换的所述第二主体的压缩机的至少一个排出阀 位置在高速模式。 该系统还包括用于致动这两个装置的致动器。
-
公开(公告)号：US08936429B2
公开(公告)日：2015-01-20
申请号：US13363763
申请日：2012-02-01
IPC分类号： F01D11/24
CPC分类号： F01D11/24
摘要： A method and system for controlling clearance between the tips of blades of a turbine rotor in a gas turbine airplane engine and a turbine ring of a casing surrounding the blades. A valve is controlled to act on a flow rate and/or a temperature of air directed against the casing. The valve is of the on/off type for switching between an open state and a closed state in a determined reaction time, the valve control module including a corrector for determining a first binary control signal that can take a first value corresponding to an open state and a second value corresponding to a closed state of the valve. The corrector includes a time-delay module for determining a binary control signal, with the duration between two successive changes of state in the control signal being not less than the reaction time of the valve.
摘要翻译： 一种用于控制燃气轮机飞机发动机中的涡轮转子的叶片的尖端与围绕叶片的壳体的涡轮环之间的间隙的方法和系统。 控制阀作用于流向壳体的流量和/或空气的温度。 所述阀具有在确定的反应时间内在打开状态和关闭状态之间切换的开/关型，所述阀控制模块包括校正器，用于确定第一二进制控制信号，该第一二进制控制信号可以采取对应于打开状态的第一值 以及对应于阀的关闭状态的第二值。 校正器包括用于确定二进制控制信号的时间延迟模块，控制信号中两个连续的状态变化之间的持续时间不小于阀的反应时间。
-
17.发明申请公开(公告)号：US20130323016A1
公开(公告)日：2013-12-05
申请号：US13984979
申请日：2012-02-02
IPC分类号： G01B7/14
CPC分类号： G01B7/14 , F01D11/24 , F05D2260/85 , F05D2270/303
摘要： A method controlling a clearance between tips of blades of a turbine rotor of a gas turbine aircraft engine and a ring-shaped turbine shroud of a housing surrounding the blades, the method including: controlling flow and/or temperature of air directed toward the housing according to an estimate of the clearance, the estimate of the clearance is determined upon start-up of the aircraft engine, according to a temperature measured by a temperature sensor including a sensitive element positioned in a free space of the aircraft engine.
摘要翻译： 一种控制燃气轮机飞机发动机的涡轮机转子的叶片的尖端与围绕叶片的壳体的环形涡轮机罩之间的间隙的方法，该方法包括：控制朝向壳体的空气的流动和/或温度， 根据由包括位于飞机发动机的自由空间中的敏感元件的温度传感器测量的温度，飞行器发动机起动时确定间隙的估计。
-
公开(公告)号：US20130213053A1
公开(公告)日：2013-08-22
申请号：US13880997
申请日：2011-10-14
申请人： Bruno Robert Gaully , Cecile Marot
发明人： Bruno Robert Gaully , Cecile Marot
IPC分类号： F02C9/26
摘要： A control of a fuel metering device for a turbine engine as a function of a weight flow rate setpoint includes responding to at least one validity criterion to select a weight flow rate from among: a weight flow rate calculated as a function of a position signal; a weight flow rate calculated as a function of the position signal and of at least one temperature measurement signal; a weight flow rate calculated as a function of the position signal and of at least one permittivity measurement signal; a weight flow rate calculated as a function of the position signal, of at least one temperature measurement signal, and of at least one permittivity measurement signal; and a weight flow rate calculated as a function of a temperature measurement signal, of a permittivity measurement signal, and of a volume flow rate measurement signal.
摘要翻译： 作为重量流量设定点的函数的用于涡轮发动机的燃料计量装置的控制包括响应至少一个有效性标准，以从以下各项中选择重量流量：根据位置信号计算的重量流量; 作为位置信号和至少一个温度测量信号的函数计算的重量流量; 作为位置信号和至少一个介电常数测量信号的函数计算的重量流量; 至少一个温度测量信号和至少一个介电常数测量信号的作为位置信号的函数计算的重量流量; 以及作为温度测量信号，介电常数测量信号和体积流量测量信号的函数计算的重量流量。
-
19.发明申请公开(公告)号：US20120279334A1
公开(公告)日：2012-11-08
申请号：US13509388
申请日：2010-11-16
申请人： Bruno Robert Gaully
发明人： Bruno Robert Gaully
IPC分类号： F16H3/08
CPC分类号： F16D11/10 , F02C7/275 , F02C7/32 , F02C7/36 , F05D2220/50 , F05D2260/40311 , F05D2260/85 , F16D2011/008 , F16H2063/3093 , Y02T50/671
摘要： A device for changing a transmission ratio between a turbine shaft and a shaft of a starter-generator of an aeroengine, the device including: first and second fixed gear wheels carried by the shaft of the starter-generator; first and second idler gearwheels carried by the turbine shaft, and meshing respectively with the first and second fixed gearwheels to define different gear ratios; a changeover sleeve interposed between the idler gearwheels and mechanically coupled to the turbine shaft, the changeover sleeve being movable in translation on the turbine shaft between two coupling positions; and a mechanism causing the changeover sleeve to move in translation automatically from either one of its coupling positions to the other one when the sum of torques between the turbine shaft and the starter-generator shaft changes sign.
摘要翻译： 一种用于改变涡轮轴与航空发动机起动发电机的轴之间的传动比的装置，该装置包括：起动发电机的轴承载的第一和第二固定齿轮; 由涡轮轴承载的第一和第二空转齿轮，分别与第一和第二固定齿轮啮合以限定不同的传动比; 插入在所述空转齿轮之间并机械地联接到所述涡轮轴的转换套筒，所述转换套筒可在所述涡轮机轴上在两个联接位置之间平移地运动; 以及当涡轮轴和起动器 - 发电机轴之间的转矩之和改变标志时，使得切换套筒从其联接位置之一自动地平移移动到另一个联接位置的机构。
-
20.发明申请SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE ESPECIALLY COMPRISING A GUIDING TRACK CONNECTION 有权用于控制气体涡轮发动机的可变几何设备的系统特别包括导向轨道连接公开(公告)号：US20110190950A1
公开(公告)日：2011-08-04
申请号：US13121706
申请日：2009-09-29
IPC分类号： G06F1/26
摘要： A system for controlling at least two sets of variable geometry equipment of a gas turbine engine including at least one first body and a second body, the first set of equipment being a stage of variable stator vanes of a compressor of the first body moving between a closed position during idling and an open position at high speed, and the second set of equipment being at least one bleed valve of a compressor of the second body moving between an open position during idling and a closed position at high speed. An actuator actuates the two sets of equipment.
摘要翻译： 一种用于控制包括至少一个第一主体和第二主体的燃气涡轮发动机的至少两组可变几何设备的系统，所述第一组设备是所述第一主体的压缩机的可变定子叶片的阶段， 在空转期间的关闭位置和高速的打开位置，第二组设备是第二机构的压缩机的至少一个放气阀，其在空转期间的打开位置和高速关闭位置之间移动。 执行器致动两组设备。
-
-
-
-
-
-
-
-
-
搜索结果
36 条记录 (耗时 0.025 秒)
