-
1.发明申请INTEGRATED THERMAL MANAGEMENT SYSTEM AND ENVIRONMENTAL CONTROL SYSTEM FOR A GAS TURBINE ENGINE 有权综合热管理系统和气体涡轮发动机环境控制系统公开(公告)号：US20130097992A1
公开(公告)日：2013-04-25
申请号：US13278260
申请日：2011-10-21
申请人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Jorn A. Glahn , Christoper M. Dye , Nathan Snape
发明人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Jorn A. Glahn , Christoper M. Dye , Nathan Snape
IPC分类号： F02C7/12
CPC分类号： F02C7/08 , B64D13/06 , F02C3/107 , F02C6/08 , F02C7/14 , F02C7/32 , F02K3/04 , F05D2260/213 , F05D2260/606 , Y02T50/44 , Y02T50/671 , Y02T50/676 , Y10T477/40 , Y10T477/45
摘要： A gas turbine engine includes a first and second pump driven by a spool. An Air-Oil Cooler downstream of the first pump. An air-air precooler is downstream of the second pump, the air-air precooler downstream of the Air-Oil Cooler.
摘要翻译： 燃气涡轮发动机包括由阀芯驱动的第一和第二泵。 第一台泵下游的空气 - 油冷却器。 空气预冷器在空气 - 油冷却器下游的第二个泵，空气预冷器的下游。
-
2.发明授权公开(公告)号：US08978351B2
公开(公告)日：2015-03-17
申请号：US13278260
申请日：2011-10-21
申请人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Jorn A. Glahn , Christoper M. Dye , Nathan Snape
发明人： Gabriel L. Suciu , Allan R. Penda , Brian D. Merry , Jorn A. Glahn , Christoper M. Dye , Nathan Snape
CPC分类号： F02C7/08 , B64D13/06 , F02C3/107 , F02C6/08 , F02C7/14 , F02C7/32 , F02K3/04 , F05D2260/213 , F05D2260/606 , Y02T50/44 , Y02T50/671 , Y02T50/676 , Y10T477/40 , Y10T477/45
摘要： A gas turbine engine includes a first and second pump driven by a spool. An Air-Oil Cooler downstream of the first pump. An air-air precooler is downstream of the second pump, the air-air precooler downstream of the Air-Oil Cooler.
摘要翻译： 燃气涡轮发动机包括由阀芯驱动的第一和第二泵。 第一台泵下游的空气 - 油冷却器。 空气预冷器在空气 - 油冷却器下游的第二个泵，空气预冷器的下游。
-
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。
-
公开(公告)号：US09109464B2
公开(公告)日：2015-08-18
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
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。
-
公开(公告)号：US20130098046A1
公开(公告)日：2013-04-25
申请号：US13278279
申请日：2011-10-21
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。
-
公开(公告)号：US09080511B2
公开(公告)日：2015-07-14
申请号：US13278279
申请日：2011-10-21
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。
-
公开(公告)号：US20140096534A1
公开(公告)日：2014-04-10
申请号：US13645067
申请日：2012-10-04
申请人： Nathan Snape , Gabriel L. Suciu , Simon Pickford , Allan R. Penda
发明人： Nathan Snape , Gabriel L. Suciu , Simon Pickford , Allan R. Penda
CPC分类号： F02C6/08 , F02C7/14 , F05D2260/213 , Y02T50/672 , Y02T50/675
摘要： An air-oil cooler (AOC) for a gas turbine engine is disclosed. The AOC may comprise an oil inlet, an oil outlet, and heat exchange elements between the oil inlet and the oil outlet. The AOC may be longitudinally positioned between a fan and a V-groove of the engine and radially spaced between a low pressure compressor and a low pressure compressor panel. A gas turbine engine comprising an AOC is disclosed. The AOC of the engine may comprise an oil inlet, an oil outlet, and heat exchange elements between the oil inlet and the oil outlet. The AOC of the engine may be longitudinally positioned between a fan and a V-groove of the engine and radially spaced between a low pressure compressor and a low pressure compressor panel. A method of operating an AOC for use on a gas turbine engine is also disclosed.
摘要翻译： 公开了一种用于燃气涡轮发动机的空气 - 油冷却器（AOC）。 AOC可以包括进油口，出油口以及进油口和出油口之间的热交换元件。 AOC可以纵向定位在发动机的风扇和V形槽之间，并且在低压压缩机和低压压缩机面板之间径向间隔开。 公开了一种包括AOC的燃气涡轮发动机。 发动机的AOC可以包括进油口，出油口和进油口和出油口之间的热交换元件。 发动机的AOC可以纵向地定位在发动机的风扇和V形槽之间，并且在低压压缩机和低压压缩机板之间径向间隔开。 还公开了一种操作用于燃气涡轮发动机的AOC的方法。
-
公开(公告)号：US09115593B2
公开(公告)日：2015-08-25
申请号：US13437375
申请日：2012-04-02
CPC分类号： F01D13/02 , F01D15/08 , F01D15/12 , F02C7/047 , F02C7/14 , F02C7/32 , F02K3/06 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump that is selectively driven by a motor or a shaft to communicate air to an interior of the nose cone. The pump shaft is driven by a dedicated geared architecture.
摘要翻译： 示例性的涡轮机组件包括涡轮机的鼻锥体和由马达或轴选择性驱动以将空气传送到鼻锥体的内部的泵。 泵轴由专用的齿轮架构驱动。
-
公开(公告)号：US20130259638A1
公开(公告)日：2013-10-03
申请号：US13437296
申请日：2012-04-02
IPC分类号： F01D1/00
CPC分类号： F01D9/065 , F01D1/02 , F01D5/02 , F01D9/02 , F01D25/12 , F02C7/04 , F02C7/047 , F02C7/18 , F02C7/32 , F05D2220/30 , F05D2260/20 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump at least partially within an interior of the nose cone. The pump is selectively rotated by a motor to communicate air to the interior.
-
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。
-
-
-
-
-
-
-
-
-
搜索结果
24 条记录 (耗时 0.027 秒)
