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公开(公告)号：US09016041B2
公开(公告)日：2015-04-28
申请号：US12956674
申请日：2010-11-30
摘要： A gas turbine engine includes: a front fan having at least one rotor carrying fan blades disposed within a fan duct, and drivingly connected to a low pressure turbine, the front fan including at least one row of outer fan blades disposed outwardly of and connected to the fan blades, the outer fan blades extending across an outer bypass duct which circumscribes the fan duct; a core engine located between the front fan and the low pressure turbine; an aft fan disposed downstream of the low pressure turbine, having at least one rotor carrying aft turbine blades disposed within an aft turbine duct, the aft turbine further including at least one row of aft fan blades disposed outwardly of and connected to the aft turbine blades, and extending across an aft fan duct that surrounds the core engine; and apparatus operable to selectively throttle flow through the outer bypass duct.
摘要翻译： 燃气涡轮发动机包括：前风扇，其具有至少一个承载风扇叶片的转子，风扇叶片设置在风扇管道内，并且驱动地连接到低压涡轮机，所述前风扇包括至少一排外风扇叶片，所述外风扇叶片设置在外部并连接到 风扇叶片，外风扇叶片延伸穿过外部旁路管道，外部旁路管道外围风扇管道; 位于前风扇和低压汽轮机之间的核心发动机; 设置在所述低压涡轮机下游的后风扇，具有至少一个转子，所述至少一个转子承载设置在后涡轮机管道内的后涡轮机叶片，所述后涡轮机还包括设置在所述后涡轮机叶片外侧并连接到所述后涡轮叶片的至少一排后翼扇叶片 并且延伸穿过围绕所述核心发动机的后部风扇管道; 以及可操作以选择性地调节通过外部旁路管道的流动的装置。
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公开(公告)号：US20120131902A1
公开(公告)日：2012-05-31
申请号：US12956674
申请日：2010-11-30
摘要： A gas turbine engine includes: a front fan having at least one rotor carrying fan blades disposed within a fan duct, and drivingly connected to a low pressure turbine, the front fan including at least one row of outer fan blades disposed outwardly of and connected to the fan blades, the outer fan blades extending across an outer bypass duct which circumscribes the fan duct; a core engine located between the front fan and the low pressure turbine; an aft fan disposed downstream of the low pressure turbine, having at least one rotor carrying aft turbine blades disposed within an aft turbine duct, the aft turbine further including at least one row of aft fan blades disposed outwardly of and connected to the aft turbine blades, and extending across an aft fan duct that surrounds the core engine; and apparatus operable to selectively throttle flow through the outer bypass duct.
摘要翻译： 燃气涡轮发动机包括：前风扇，其具有至少一个承载风扇叶片的转子，风扇叶片设置在风扇管道内，并且驱动地连接到低压涡轮机，所述前风扇包括至少一排外风扇叶片，所述外风扇叶片设置在外部并连接到 风扇叶片，外风扇叶片延伸穿过外部旁路管道，外部旁路管道外围风扇管道; 位于前风扇和低压汽轮机之间的核心发动机; 设置在所述低压涡轮机下游的后风扇，具有至少一个转子，所述至少一个转子承载设置在后涡轮机管道内的后涡轮机叶片，所述后涡轮机还包括设置在所述后涡轮机叶片外侧并连接到所述后涡轮叶片的至少一排后翼扇叶片 并且延伸穿过围绕所述核心发动机的后部风扇管道; 以及可操作以选择性地调节通过外部旁路管道的流动的装置。
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3.发明授权Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans 有权飞机燃气涡轮发动机具有可变转矩分流反转旋转低压涡轮机和增压器逆向旋转风扇公开(公告)号：US06763654B2
公开(公告)日：2004-07-20
申请号：US10260480
申请日：2002-09-30
IPC分类号： F02K3072
CPC分类号： F01D1/24 , F02C3/067 , F02K3/072 , Y02T50/671
摘要： A gas turbine engine turbine assembly includes a high pressure spool having a high pressure turbine drivingly connected to a high pressure compressor by a high pressure shaft which is rotatable about an engine centerline. A low pressure turbine has counter rotatable low pressure inner and outer shaft turbines with a row of low pressure variable vanes disposed therebetween and drivingly connected to coaxial low pressure inner and outer shafts respectively which are located radially inwardly of the high pressure spool. The low pressure inner and outer shaft turbines are drivingly connected to a forward and aft fan blade rows by the low pressure inner and outer shafts. A single direction of rotation booster is drivenly connected to the low pressure outer shaft and axially located aft and downstream of the aft fan blade row.
摘要翻译： 一种燃气涡轮发动机涡轮组件包括具有高压涡轮机的高压阀芯，所述高压涡轮机通过可围绕发动机中心线旋转的高压轴驱动地连接到高压压缩机。 低压涡轮机具有反转的低压内外涡轮机，其一排低压可变叶片设置在它们之间并分别驱动地连接到位于高压线轴的径向内侧的同轴低压内外轴和外轴。 低压内外涡轮机通过低压内外轴驱动连接到前风扇叶片和后风扇叶片排。 单向旋转助力器驱动地连接到低压外轴并且轴向位于后风扇叶片排的后部和下游。
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4.发明授权Variable torque split aircraft gas turbine engine counter rotating low pressure turbines 有权可变扭矩分裂飞机燃气涡轮发动机反转低压涡轮机公开(公告)号：US06763652B2
公开(公告)日：2004-07-20
申请号：US10253236
申请日：2002-09-24
IPC分类号： F02G106
CPC分类号： F02C3/067 , Y02T50/671
摘要： An aircraft gas turbine engine includes a low pressure turbine having a low pressure turbine flowpath and low pressure inner and outer shaft turbines with counter rotatable low pressure inner and outer shaft turbine rotors, respectively. The low pressure inner and outer shaft turbine rotors include low pressure first and second turbine blade rows disposed across the turbine flowpath which are drivingly connected to first and second fan blade rows by low pressure inner and outer shafts, respectively. At least one row of low pressure variable vanes is operably disposed across the low pressure turbine flowpath between the low pressure inner and outer shaft turbines. The low pressure first turbine blade rows of the low pressure inner shaft turbine may be in tandem with or interdigitated with the second turbine blade rows of the low pressure outer shaft turbines.
摘要翻译： 飞机燃气涡轮发动机包括分别具有低压涡轮流动路径的低压涡轮机和具有反向可旋转的低压内外涡轮转子的低压内外涡轮机。 低压内外涡轮转子包括横跨涡轮流路设置的低压第一和第二涡轮叶片排，它们分别通过低压内轴和外轴驱动地连接到第一和第二风扇叶片排。 至少一排低压可变叶片可操作地设置在低压内外涡轮机之间的低压涡轮流动路径上。 低压内轴涡轮机的低压第一涡轮机叶片排可以与低压外轴涡轮机的第二涡轮叶片排串联或互相指向。
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公开(公告)号：US07784266B2
公开(公告)日：2010-08-31
申请号：US11612247
申请日：2006-12-18
IPC分类号： B63H11/00
CPC分类号： F01D17/105 , F01D17/162 , F02C6/06 , F02C9/18 , F02K3/02 , F02K3/06 , F02K3/075
摘要： A method of supplying air to a vehicle is provided, wherein the method includes modulating a flow of air from between a fan assembly of a turbofan engine and a high pressure compressor of the turbofan engine with a core driven fan stage coupled in parallel to the high pressure compressor. The method also includes channeling the air from the core driven fan stage to the vehicle.
摘要翻译： 提供了向车辆供应空气的方法，其中所述方法包括调节来自涡扇发动机的风扇组件和涡扇风扇发动机的高压压缩机之间的空气流，其中核心驱动扇形平台并联连接到高压 压缩机。 该方法还包括将空气从核心驱动风扇级引导到车辆。
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公开(公告)号：US07134271B2
公开(公告)日：2006-11-14
申请号：US10982477
申请日：2004-11-05
摘要： An aft FLADE gas turbine engine including a fan section drivenly connected to a low pressure turbine section followed by an aft FLADE turbine having at least one row of aft FLADE fan blades radially extending across a FLADE duct circumscribing the aft FLADE turbine, and at least one thrust vectoring nozzle in pressurized fluid flow receiving communication with the FLADE duct. One embodiment of the engine includes spaced apart right and left hand FLADE exhaust nozzles in pressurized fluid flow receiving communication with the FLADE duct and offset from a main engine exhaust nozzle located downstream of the aft FLADE turbine. Right and left hand valves disposed in right and left hand ducts extending between a FLADE airflow manifold in pressurized fluid flow receiving communication with the FLADE duct may be used to vector thrust. The right and left hand FLADE exhaust nozzle may be fixed or thrust vectoring nozzles.
摘要翻译： 一种后FLADE燃气涡轮发动机，其包括驱动地连接到低压涡轮机部分和后FLADE涡轮机的风扇部分，所述后部FLADE涡轮机具有径向延伸穿过外部FLADE涡轮机的FLADE管道的至少一排后FLADE风扇叶片，以及至少一个 加压流体流中的推力矢量喷嘴与FLADE管道相通。 发动机的一个实施例包括间隔开的左右FLADE排气喷嘴，其与FLADE管道的加压流体流动接收连通并且与位于后FLADE涡轮机下游的主发动机排气喷嘴偏移。 设置在与FLADE管道的加压流体流动接收连通的FLADE气流歧管之间延伸的右侧和左侧管道中的右侧和左侧阀可用于向量推力。 右侧和左侧FLADE排气喷嘴可以是固定的或推力矢量喷嘴。
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公开(公告)号：US08777554B2
公开(公告)日：2014-07-15
申请号：US12870423
申请日：2010-08-27
申请人： John Lewis Baughman
发明人： John Lewis Baughman
IPC分类号： F04D27/02 , F04D29/18 , F01D5/22 , F01D17/00 , F03B15/02 , F01D1/24 , F01D13/00 , F04D1/08 , F02K3/02
摘要： A fan system is disclosed having a forward fan stage configured to pressurize an airflow and an aft fan stage having a tip-fan configured to pressurize a first portion of a pressurized air flow from the forward fan stage wherein the aft fan stage is driven by a second portion of the pressurized airflow.
摘要翻译： 公开了一种风扇系统，其具有被配置为对气流进行加压的前风扇级和具有尖端风扇的后风扇级，该风扇级配置成对来自前风扇级的加压空气流的第一部分进行加压，其中后风扇级由 加压气流的第二部分。
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公开(公告)号：US20080141654A1
公开(公告)日：2008-06-19
申请号：US11612247
申请日：2006-12-18
IPC分类号： F02K3/02
CPC分类号： F01D17/105 , F01D17/162 , F02C6/06 , F02C9/18 , F02K3/02 , F02K3/06 , F02K3/075
摘要： A method of supplying air to a vehicle is provided, wherein the method includes modulating a flow of air from between a fan assembly of a turbofan engine and a high pressure compressor of the turbofan engine with a core driven fan stage coupled in parallel to the high pressure compressor. The method also includes channeling the air from the core driven fan stage to the vehicle.
摘要翻译： 提供了向车辆供应空气的方法，其中所述方法包括调节来自涡扇发动机的风扇组件和涡扇风扇发动机的高压压缩机之间的空气流，其中核心驱动扇形平台并联连接到高压 压缩机。 该方法还包括将空气从核心驱动风扇级引导到车辆。
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