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1. 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。

2. 发明申请

US20120117982A1 AXIAL ACCESSORY GEARBOX 有权
标题翻译：轴附件齿轮箱
公开(公告)号：US20120117982A1
公开(公告)日：2012-05-17
申请号：US13103152
申请日：2011-05-09
申请人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
发明人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
IPC分类号： F02C6/00
CPC分类号： F02C7/32 , F05D2250/31 , F05D2260/4031
摘要： An accessory system for a gas turbine engine includes a main case which defines an accessory gearbox axis. A cover is removably mountable to the main case and a first gear set at least partially within the cover along a first accessory axis transverse to the accessory gearbox axis.
摘要翻译：用于燃气涡轮发动机的附件系统包括限定附件齿轮箱轴线的主壳体。盖子可移除地安装到主壳体上，并且第一齿轮组沿着与附件齿轮箱轴线横向的第一附件轴线至少部分地设置在盖子内。

3. 发明申请

US20120117981A1 AXIAL ACCESSORY GEARBOX 有权
标题翻译：轴附件齿轮箱
公开(公告)号：US20120117981A1
公开(公告)日：2012-05-17
申请号：US12948051
申请日：2010-11-17
申请人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
发明人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
IPC分类号： F02C6/00
CPC分类号： F02C7/32 , F05D2250/31 , F05D2260/4031 , F16H1/222
摘要： An accessory system for a gas turbine engine includes an accessory gearbox which defines an accessory gearbox axis. A crossover gear set generally along the accessory gearbox axis interconnects a first gear set and a second gear set.
摘要翻译：用于燃气涡轮发动机的附件系统包括限定附件齿轮箱轴的附件齿轮箱。大体上沿着附件齿轮箱轴的交叉齿轮组将第一齿轮组和第二齿轮组相互连接。

4. 发明申请

US20110289936A1 ACCESSORY GEARBOX WITH INTERNAL LAYSHAFT 有权
标题翻译：配件齿轮箱，内置LAYSHAFT
公开(公告)号：US20110289936A1
公开(公告)日：2011-12-01
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： F02C6/00
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。

5. 发明授权

US08490411B2 Axial accessory gearbox 有权
标题翻译：轴向配件齿轮箱
公开(公告)号：US08490411B2
公开(公告)日：2013-07-23
申请号：US13103152
申请日：2011-05-09
申请人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
发明人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
IPC分类号： F02C7/275
CPC分类号： F02C7/32 , F05D2250/31 , F05D2260/4031
摘要： An accessory system for a gas turbine engine includes a main case which defines an accessory gearbox axis. A cover is removably mountable to the main case and a first gear set at least partially within the cover along a first accessory axis transverse to the accessory gearbox axis.
摘要翻译：用于燃气涡轮发动机的附件系统包括限定附件齿轮箱轴线的主壳体。盖子可移除地安装到主壳体上，并且第一齿轮组沿着与附件齿轮箱轴线横向的第一附件轴线至少部分地设置在盖子内。

6. 发明授权

US08490410B2 Axial accessory gearbox 有权
标题翻译：轴向配件齿轮箱
公开(公告)号：US08490410B2
公开(公告)日：2013-07-23
申请号：US12948051
申请日：2010-11-17
申请人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
发明人： Gabriel L. Suciu , Christopher M. Dye , Hung Duong , Nathan Snape
IPC分类号： F02C7/275
CPC分类号： F02C7/32 , F05D2250/31 , F05D2260/4031 , F16H1/222
摘要： An accessory system for a gas turbine engine includes an accessory gearbox which defines an accessory gearbox axis. A crossover gear set generally along the accessory gearbox axis interconnects a first gear set and a second gear set.
摘要翻译：用于燃气涡轮发动机的附件系统包括限定附件齿轮箱轴的附件齿轮箱。大体上沿着附件齿轮箱轴的交叉齿轮组将第一齿轮组和第二齿轮组互相连接。

7. 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。

8. 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。

9. 发明申请

US20130047624A1 DISTRIBUTED LUBRICATION SYSTEM 有权
标题翻译：分布式润滑系统
公开(公告)号：US20130047624A1
公开(公告)日：2013-02-28
申请号：US13222183
申请日：2011-08-31
申请人： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye , Nathan Snape , Matthew J. Howlett , Matthew G. Dixon
发明人： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye , Nathan Snape , Matthew J. Howlett , Matthew G. Dixon
IPC分类号： F02C7/06
CPC分类号： F01D25/20 , F01D15/08 , F01D25/125 , F01D25/18 , F02C7/06 , F02C7/14 , F05D2260/98 , Y02T50/675
摘要： A gas turbine engine includes a spool, a gearbox having gearing driven by the spool, and a lubrication system. The lubrication system includes a first heat exchanger positioned in a first air flow path, a second heat exchanger positioned in a second air flow path, and a lubrication pump fluidically connected to both the first heat exchanger and the second heat exchanger. A first air fan is driven by the gearbox for inducing air flow through the first air flow path. A second air fan is driven by an electric motor for inducing air flow through the second air flow path.
摘要翻译：燃气涡轮发动机包括阀芯，具有由阀芯驱动的齿轮传动装置的齿轮箱和润滑系统。润滑系统包括位于第一空气流路中的第一热交换器，位于第二空气流路中的第二热交换器和与第一热交换器和第二热交换器流体连接的润滑泵。第一空气风扇由齿轮箱驱动，用于引导空气流过第一空气流动路径。第二空气风扇由用于引导空气流过第二空气流路的电动机驱动。

10. 发明授权

US09194294B2 Gas turbine engine oil tank 有权
标题翻译：燃气轮机油箱
公开(公告)号：US09194294B2
公开(公告)日：2015-11-24
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： F01D25/18 , F02C7/06 , F02C7/32
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。

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