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11. 发明申请

US20130239582A1 CONSTANT SPEED PUMP SYSTEM FOR ENGINE ECS LOSS ELIMINATION 有权
标题翻译：恒定速度泵系统用于发动机ECS损失消除
公开(公告)号：US20130239582A1
公开(公告)日：2013-09-19
申请号：US13419660
申请日：2012-03-14
申请人： Gabriel L. Suciu , Brian D. Merry , Jorn A. Glahn , Christopher M. Dye
发明人： Gabriel L. Suciu , Brian D. Merry , Jorn A. Glahn , Christopher M. Dye
IPC分类号： F02C6/08
CPC分类号： F02C6/08 , F01D15/08 , F02C7/32 , F02C7/36 , F02K3/06 , Y02T50/671
摘要： A gas turbine engine has an impeller pump for delivering air to an environmental control system and a speed control pump connected to the impeller pump for driving the impeller pump at a constant speed.
摘要翻译：燃气涡轮发动机具有用于将空气输送到环境控制系统的叶轮泵和连接到叶轮泵的速度控制泵，用于以恒定速度驱动叶轮泵。

12. 发明申请

US20130086922A1 Combined Pump System for Engine TMS AOC Reduction and ECS Loss Elimination 有权
标题翻译：发动机TMS AOC减少和ECS丢失消除的组合泵系统
公开(公告)号：US20130086922A1
公开(公告)日：2013-04-11
申请号：US13253144
申请日：2011-10-05
申请人： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye
发明人： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye
IPC分类号： F02C6/04 , F04B35/00
CPC分类号： F02C7/32 , F02C3/09 , F02C3/103 , F02C3/107 , F02C6/04 , F02C7/14 , F02C7/36 , F02C9/16 , Y02T50/675
摘要： A compression pump for an engine is provided. The pump may include a first impeller operatively coupled to a main shaft of the engine, a first inlet configured to at least partially receive bypass airflow, and a first outlet configured to direct compressed air to a thermal management system.
摘要翻译：提供一种用于发动机的压缩泵。泵可以包括可操作地联接到发动机的主轴的第一叶轮，构造成至少部分地接收旁路气流的第一入口和被配置为将压缩空气引导到热管理系统的第一出口。

13. 发明授权

US09151224B2 Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination 有权
标题翻译：恒速泵系统用于发动机热管理系统AOC减排和环境控制系统损耗消除
公开(公告)号：US09151224B2
公开(公告)日：2015-10-06
申请号：US13419695
申请日：2012-03-14
申请人： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye
发明人： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye
IPC分类号： F02C7/14 , F02C3/09 , F02C9/16 , F02C3/10 , F02C7/32 , F02C7/36 , F02C6/08 , F01D15/08 , F02C6/04
CPC分类号： F02C6/08 , F01D15/08 , F02C7/32 , F02K3/06 , Y02T50/671
摘要： A gas turbine engine has a spool, a towershaft connected to the spool and an impeller pump. An integrated drive pump is connected to the towershaft and to the impeller pump for driving the impeller pump at a constant speed. The integrated drive pump is positioned on an engine core. The gas turbine engine includes a fan and a bypass duct located between a cowl and the engine core. The gas turbine engine includes an intake manifold for the impeller pump, and the intake manifold receives air from the bypass duct.
摘要翻译：燃气涡轮发动机具有阀芯，连接到阀芯的塔轴和叶轮泵。集成的驱动泵连接到塔轴和叶轮泵，以恒定的速度驱动叶轮泵。集成驱动泵位于发动机芯上。燃气涡轮发动机包括位于罩和发动机芯之间的风扇和旁通管。燃气涡轮发动机包括用于叶轮泵的进气歧管，并且进气歧管从旁路管道接收空气。

14. 发明授权

US09121346B2 Pump system for TMS AOC reduction 有权
标题翻译：用于TMS AOC的泵系统
公开(公告)号：US09121346B2
公开(公告)日：2015-09-01
申请号：US13419649
申请日：2012-03-14
申请人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Jorn A. Glahn
发明人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Jorn A. Glahn
IPC分类号： F02K99/00 , F02C7/14 , F02C7/224 , F04D29/58
CPC分类号： F02C7/14 , F01D25/12 , F02C7/224 , F02K3/06 , F04D29/5826 , F05D2250/36
摘要： An engine includes a duct containing a flow of cool air and a pump system having an impeller with an inlet for receiving air from the duct and an outlet for discharging air into a discharge manifold. The discharge manifold containing at least one heat exchanger which forms part of a thermal management system.
摘要翻译：发动机包括含有冷空气流的管道和具有叶轮的泵系统，叶轮具有用于从管道接收空气的入口和用于将空气排放到排放歧管中的出口。排放歧管包含形成热管理系统的一部分的至少一个热交换器。

15. 发明授权

US09080511B2 Integrated thermal system for a gas turbine engine 有权
标题翻译：燃气轮机的集成热系统
公开(公告)号：US09080511B2
公开(公告)日：2015-07-14
申请号：US13278279
申请日：2011-10-21
申请人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Christopher M. Dye , Nathan Snape
发明人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Christopher M. Dye , Nathan Snape
IPC分类号： F02C7/12 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/18
CPC分类号： F02C7/185 , F02C7/08 , F02C7/14 , F02C7/18 , Y02T50/671
摘要： An integrated thermal system for a gas turbine engine includes an Air-Oil Cooler and an Air-Air PreCooler within a housing, the Air-Air PreCooler downstream of the Air-Oil Cooler.
摘要翻译：用于燃气涡轮发动机的集成热系统包括在壳体内的空气 - 油冷却器和空气预冷器，空气 - 油冷却器下游的空气预制冷器。

16. 发明申请

US20130098046A1 INTEGRATED THERMAL SYSTEM FOR A GAS TURBINE ENGINE 有权
标题翻译：用于气体涡轮发动机的集成热系统
公开(公告)号：US20130098046A1
公开(公告)日：2013-04-25
申请号：US13278279
申请日：2011-10-21
申请人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Christopher M. Dye , Nathan Snape
发明人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Christopher M. Dye , Nathan Snape
IPC分类号： F02C9/00 , F23R3/26
CPC分类号： F02C7/185 , F02C7/08 , F02C7/14 , F02C7/18 , Y02T50/671
摘要： An integrated thermal system for a gas turbine engine includes an Air-Oil Cooler and an Air-Air PreCooler within a housing, the Air-Air PreCooler downstream of the Air-Oil Cooler.
摘要翻译：用于燃气涡轮发动机的集成热系统包括在壳体内的空气 - 油冷却器和空气预冷器，空气 - 油冷却器下游的空气预制冷器。

17. 发明授权

US08602717B2 Compression system for turbomachine heat exchanger 有权
标题翻译：涡轮机热交换器压缩系统
公开(公告)号：US08602717B2
公开(公告)日：2013-12-10
申请号：US12914976
申请日：2010-10-28
申请人： Gabriel L. Suciu , Jorn A. Glahn , Christopher M. Dye
发明人： Gabriel L. Suciu , Jorn A. Glahn , Christopher M. Dye
IPC分类号： F01D5/18 , F01D5/08
CPC分类号： F02C7/14 , F02C7/32 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine cooling arrangement includes a pump configured to pressurize a first turbomachine fluid that is then communicated through a heat exchanger assembly to remove thermal energy from a second turbomachine fluid. A portion of the pump is configured to be housed within a gearbox housing of a turbomachine.
摘要翻译：示例性涡轮机冷却装置包括泵，所述泵构造成对第一涡轮机液进行加压，所述第一涡轮机流体然后通过热交换器组件连通以从第二涡轮机流体去除热能。泵的一部分被配置为容纳在涡轮机的齿轮箱壳体内。

18. 发明申请

US20120107104A1 COMPRESSION SYSTEM FOR TURBOMACHINE HEAT EXCHANGER 有权
标题翻译：涡轮换热器压缩系统
公开(公告)号：US20120107104A1
公开(公告)日：2012-05-03
申请号：US12914976
申请日：2010-10-28
申请人： Gabriel L. Suciu , Jorn A. Glahn , Christopher M. Dye
发明人： Gabriel L. Suciu , Jorn A. Glahn , Christopher M. Dye
IPC分类号： F04D29/58
CPC分类号： F02C7/14 , F02C7/32 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine cooling arrangement includes a pump configured to pressurize a first turbomachine fluid that is then communicated through a heat exchanger assembly to remove thermal energy from a second turbomachine fluid. A portion of the pump is configured to be housed within a gearbox housing of a turbomachine.
摘要翻译：示例性涡轮机冷却装置包括泵，所述泵构造成对第一涡轮机液进行加压，所述第一涡轮机流体然后通过热交换器组件连通以从第二涡轮机流体去除热能。泵的一部分被配置为容纳在涡轮机的齿轮箱壳体内。

19. 发明申请

US20130291514A1 GAS TURBINE ENGINE OIL TANK 有权
标题翻译：气体涡轮发动机油箱
公开(公告)号：US20130291514A1
公开(公告)日：2013-11-07
申请号：US13465637
申请日：2012-05-07
申请人： Gabriel L. Suciu , Nathan Snape , Christopher M. Dye
发明人： Gabriel L. Suciu , Nathan Snape , Christopher M. Dye
IPC分类号： F02C7/06
CPC分类号： F02C3/04 , F01D25/12 , F01D25/18 , F02C7/06 , F02C7/12 , F02C7/14 , F02C7/32
摘要： A gas turbine engine includes an engine static structure housing that includes a compressor section and a turbine section. A core nacelle encloses the engine static structure to provide a core compartment. An oil tank is arranged in the core compartment and is axially aligned with the compressor section. Fan and core nacelles define an annular bypass flow path. The core nacelle provides a core compartment and includes an opening into the core compartment. The oil tank is arranged in the core compartment and includes a portion aligned with the opening that is exposed to the bypass flow path. The engine static structure is supported relative to a fan case by a radial structure. The oil tank is mounted to the engine static structure. An oil fill tube is mounted to the fan case and is fluidly connected to the oil tank.
摘要翻译：燃气涡轮发动机包括包括压缩机部分和涡轮部分的发动机静态结构壳体。一个核心机舱包围发动机静态结构以提供一个核心隔间。油箱布置在芯部隔室中并与压缩机部分轴向对准。风扇和核心机舱定义一个环形旁路流动路径。核心机舱提供一个核心隔间，并包括一个通向核心隔间的开口。油箱布置在核心舱中，并且包括与暴露于旁路流路的开口对准的部分。发动机静态结构通过径向结构相对于风扇壳体被支撑。油箱安装在发动机静态结构上。加油管安装在风扇壳体上，并与油箱流体连接。

20. 发明授权

US08347637B2 Accessory gearbox with internal layshaft 有权
标题翻译：配有内置副轴的齿轮箱
公开(公告)号：US08347637B2
公开(公告)日：2013-01-08
申请号：US12787385
申请日：2010-05-25
申请人： Gabriel L. Suciu , Christopher M. Dye , Nathan Snape , Hung Duong
发明人： Gabriel L. Suciu , Christopher M. Dye , Nathan Snape , Hung Duong
IPC分类号： F16H57/00
CPC分类号： F02C7/32 , F05D2240/60 , F05D2250/70 , F05D2250/72 , F05D2260/4031 , F05D2260/53 , Y02T50/671 , Y10T74/2186
摘要： An engine accessory system for a gas turbine engine includes a first accessory component mountable to an accessory gearbox along a first accessory axis transverse to a layshaft axis of rotation.
摘要翻译：用于燃气涡轮发动机的发动机附件系统包括第一辅助部件，其可沿横向于副轴旋转轴线的第一附件轴线安装到附件齿轮箱。

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