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1.发明授权公开(公告)号：US08356483B2
公开(公告)日：2013-01-22
申请号：US12100470
申请日：2008-04-10
申请人： Dale William Petty , Shawn M. McMahon , Michael Joseph Murphy , Sean P. Zamora , Timothy A. Swanson
发明人： Dale William Petty , Shawn M. McMahon , Michael Joseph Murphy , Sean P. Zamora , Timothy A. Swanson
IPC分类号： F02K1/06
摘要： A nozzle assembly for a gas turbine engine includes a door axially slidable relative to a passage in communication with a secondary flow path to regulate the secondary flow though the passage.
摘要翻译： 用于燃气涡轮发动机的喷嘴组件包括相对于与二次流动路径连通的通道可轴向滑动的门，以调节通过通道的二次流。
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2.发明授权Gas turbine engine systems involving variable nozzles with flexible panels 有权包括具有柔性板的可变喷嘴的燃气涡轮发动机系统公开(公告)号：US09267463B2
公开(公告)日：2016-02-23
申请号：US12054762
申请日：2008-03-25
CPC分类号： F02K1/1207 , F02K1/10 , F02K1/82 , F05D2300/501 , F05D2300/603 , F05D2300/604 , Y02T50/672
摘要： A flexible panel assembly for a gas turbine engine selectively exhibits a range of positions to regulate exhaust of the engine.
摘要翻译： 用于燃气涡轮发动机的柔性面板组件选择性地展现一定范围的位置以调节发动机的排气。
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3.发明申请公开(公告)号：US20090241550A1
公开(公告)日：2009-10-01
申请号：US12054762
申请日：2008-03-25
IPC分类号： F02K1/06
CPC分类号： F02K1/1207 , F02K1/10 , F02K1/82 , F05D2300/501 , F05D2300/603 , F05D2300/604 , Y02T50/672
摘要： Gas turbine engine systems involving flexible panels are provided. In this regard, a representative flexible panel assembly for a gas turbine engine includes: a flexible panel operative to define at least one of a throat area and an exit area of a nozzle of a gas turbine engine, the panel being further operative to selectively exhibit a range of positions to regulate exhaust of the engine.
摘要翻译： 提供涉及柔性板的燃气涡轮发动机系统。 在这方面，用于燃气涡轮发动机的代表性的柔性面板组件包括：柔性面板，其可操作以限定燃气涡轮发动机的喷嘴的喉部区域和出口区域中的至少一个，所述面板还可操作以选择性地展现 一系列位置来调节发动机的排气。
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4.发明申请公开(公告)号：US20090255269A1
公开(公告)日：2009-10-15
申请号：US12100470
申请日：2008-04-10
申请人： Dale William Petty , Shawn M. McMahon , Michael Joseph Murphy , Sean P. Zamora , Timothy A. Swanson
发明人： Dale William Petty , Shawn M. McMahon , Michael Joseph Murphy , Sean P. Zamora , Timothy A. Swanson
IPC分类号： F02K1/06
摘要： Gas turbine engine systems involving variable nozzles with sliding doors are provided. In this regard, a representative door assembly for a gas turbine engine includes: a door configured for alignment with an exit area of a nozzle and operative to variably open and close the nozzle exit area such that gas directed along a gas path defined, at least in part, by the nozzle exit area is regulated
摘要翻译： 提供了包括具有滑动门的可变喷嘴的燃气涡轮发动机系统。 在这方面，用于燃气涡轮发动机的代表性门组件包括：门，其被配置为与喷嘴的出口区域对准并且可操作地可变地打开和关闭喷嘴出口区域，使得沿着气体路径定向的气体至少 部分由喷嘴出口区域进行调节
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公开(公告)号：US08733107B2
公开(公告)日：2014-05-27
申请号：US12970478
申请日：2010-12-16
IPC分类号： F02K1/00
CPC分类号： F02K1/1223
摘要： A mechanism included in a convergent-divergent nozzle connected to an aft portion of a gas turbine engine, which mechanism includes a convergent flap configured to be kinematically connected to the aft portion of the gas turbine engine, a divergent flap pivotally connected to the convergent flap and configured to be kinematically connected to the aft portion of the gas turbine engine, at least one actuator configured to be connected to the aft portion of the gas turbine engine and to mechanically prescribe the position of the convergent flap and the divergent flap by moving through one or more positions, and at least one biasing apparatus. The biasing apparatus is configured to position at least one of the convergent flap and the divergent flap independent of the positions of the actuator by substantially balancing a force on the at least one of the convergent flap and the divergent flap produced by a gas pressure on the nozzle.
摘要翻译： 包括在连接到燃气涡轮发动机的后部的会聚扩散喷嘴中的机构，该机构包括构造成运动学地连接到燃气涡轮发动机的后部的会聚挡板，枢转地连接到会聚挡板 并且构造成运动学地连接到燃气涡轮发动机的后部，至少一个致动器，其构造成连接到燃气涡轮发动机的后部并且通过移动通过机械方式规定会聚翼片和发散翼片的位置 一个或多个位置，以及至少一个偏置装置。 偏置装置构造成通过基本上平衡在会聚翼片上的至少一个上的力和由气体压力产生的发散翼片上的力而使收敛翼片和发散片片中的至少一个独立于致动器的位置 喷嘴。
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公开(公告)号：US07871242B2
公开(公告)日：2011-01-18
申请号：US11755925
申请日：2007-05-31
IPC分类号： F01D9/00
CPC分类号： F02K1/822 , F01D17/148 , F02C6/08 , F05D2260/50 , Y02T50/675
摘要： A rotational flow balance system includes an actuator system which controls operation of both a fan duct blocker ring and a modulated exhaust cooling ring through a kinematic system. The kinematic system is controlled by the single actuator system such that the modulated exhaust cooling ring will remain in a fixed position while the fan duct blocker ring can be moved to satisfy operational requirements.
摘要翻译： 旋转流量平衡系统包括致动器系统，其通过运动系统控制风扇阻塞环和调制排气冷却环的操作。 运动系统由单个致动器系统控制，使得调节的排气冷却环将保持在固定位置，同时风扇管道阻塞环可以移动以满足操作要求。
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公开(公告)号：US20110088403A1
公开(公告)日：2011-04-21
申请号：US12970478
申请日：2010-12-16
IPC分类号： F02K1/12
CPC分类号： F02K1/1223
摘要： A mechanism included in a convergent-divergent nozzle connected to an aft portion of a gas turbine engine, which mechanism includes a convergent flap configured to be kinematically connected to the aft portion of the gas turbine engine, a divergent flap pivotally connected to the convergent flap and configured to be kinematically connected to the aft portion of the gas turbine engine, at least one actuator configured to be connected to the aft portion of the gas turbine engine and to mechanically prescribe the position of the convergent flap and the divergent flap by moving through one or more positions, and at least one biasing apparatus. The biasing apparatus is configured to position at least one of the convergent flap and the divergent flap independent of the positions of the actuator by substantially balancing a force on the at least one of the convergent flap and the divergent flap produced by a gas pressure on the nozzle.
摘要翻译： 包括在连接到燃气涡轮发动机的后部的会聚扩散喷嘴中的机构，该机构包括构造成运动学地连接到燃气涡轮发动机的后部的会聚挡板，枢转地连接到会聚挡板 并且构造成运动学地连接到燃气涡轮发动机的后部，至少一个致动器，其构造成连接到燃气涡轮发动机的后部并且通过移动通过机械方式规定会聚翼片和发散片的位置 一个或多个位置，以及至少一个偏置装置。 偏置装置构造成通过基本上平衡在会聚翼片上的至少一个上的力和由气体压力产生的发散翼片上的力而使收敛翼片和发散片片中的至少一个独立于致动器的位置 喷嘴。
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公开(公告)号：US07874160B2
公开(公告)日：2011-01-25
申请号：US11894313
申请日：2007-08-21
IPC分类号： F02K1/00
CPC分类号： F02K1/1223
摘要： A mechanism included in a convergent-divergent nozzle connected to an aft portion of a gas turbine engine, which mechanism includes a convergent flap configured to be kinematically connected to the aft portion of the gas turbine engine, a divergent flap pivotally connected to the convergent flap and configured to be kinematically connected to the aft portion of the gas turbine engine, at least one actuator configured to be connected to the aft portion of the gas turbine engine and to mechanically prescribe the position of the convergent flap and the divergent flap by moving through one or more positions, and at least one biasing apparatus. The biasing apparatus is configured to position at least one of the convergent flap and the divergent flap independent of the positions of the actuator by substantially balancing a force on the at least one of the convergent flap and the divergent flap produced by a gas pressure on the nozzle.
摘要翻译： 包括在连接到燃气涡轮发动机的后部的会聚扩散喷嘴中的机构，该机构包括构造成运动学地连接到燃气涡轮发动机的后部的会聚挡板，枢转地连接到会聚挡板 并且构造成运动学地连接到燃气涡轮发动机的后部，至少一个致动器，其构造成连接到燃气涡轮发动机的后部并且通过移动通过机械方式规定会聚翼片和发散片的位置 一个或多个位置，以及至少一个偏置装置。 偏置装置构造成通过基本上平衡在会聚翼片上的至少一个上的力和由气体压力产生的发散翼片上的力而使收敛翼片和发散片片中的至少一个独立于致动器的位置 喷嘴。
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公开(公告)号：US20090097965A1
公开(公告)日：2009-04-16
申请号：US11755925
申请日：2007-05-31
IPC分类号： F02C9/16
CPC分类号： F02K1/822 , F01D17/148 , F02C6/08 , F05D2260/50 , Y02T50/675
摘要： A rotational flow balance system includes an actuator system which controls operation of both a fan duct blocker ring and a modulated exhaust cooling ring through a kinematic system. The kinematic system is controlled by the single actuator system such that the modulated exhaust cooling ring will remain in a fixed position while the fan duct blocker ring can be moved to satisfy operational requirements.
摘要翻译： 旋转流量平衡系统包括致动器系统，其通过运动系统控制风扇阻塞环和调制排气冷却环的操作。 运动系统由单个致动器系统控制，使得调节的排气冷却环将保持在固定位置，同时风扇管道阻塞环可以移动以满足操作要求。
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公开(公告)号：US20090072049A1
公开(公告)日：2009-03-19
申请号：US11894313
申请日：2007-08-21
IPC分类号： B64C9/38
CPC分类号： F02K1/1223
摘要： A mechanism included in a convergent-divergent nozzle connected to an aft portion of a gas turbine engine, which mechanism includes a convergent flap configured to be kinematically connected to the aft portion of the gas turbine engine, a divergent flap pivotally connected to the convergent flap and configured to be kinematically connected to the aft portion of the gas turbine engine, at least one actuator configured to be connected to the aft portion of the gas turbine engine and to mechanically prescribe the position of the convergent flap and the divergent flap by moving through one or more positions, and at least one biasing apparatus. The biasing apparatus is configured to position at least one of the convergent flap and the divergent flap independent of the positions of the actuator by substantially balancing a force on the at least one of the convergent flap and the divergent flap produced by a gas pressure on the nozzle.
摘要翻译： 包括在连接到燃气涡轮发动机的后部的会聚扩散喷嘴中的机构，该机构包括构造成运动学地连接到燃气涡轮发动机的后部的会聚挡板，枢转地连接到会聚挡板 并且构造成运动学地连接到燃气涡轮发动机的后部，至少一个致动器，其构造成连接到燃气涡轮发动机的后部并且通过移动通过机械方式规定会聚翼片和发散片的位置 一个或多个位置，以及至少一个偏置装置。 偏置装置构造成通过基本上平衡在会聚翼片上的至少一个上的力和由气体压力产生的发散翼片上的力而使收敛翼片和发散片片中的至少一个独立于致动器的位置 喷嘴。
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