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公开(公告)号：US08695324B2
公开(公告)日：2014-04-15
申请号：US12796353
申请日：2010-06-08
IPC分类号： F02K3/02
CPC分类号： F02C3/064 , F01D5/022 , F02K3/077 , Y02T50/672
摘要： A fan assembly having an outer fan system is disclosed, the fan assembly comprising an outer fan first stage and an outer fan second stage both extending radially outward from an arcuate platform.
摘要翻译： 公开了一种具有外部风扇系统的风扇组件，风扇组件包括从弧形平台径向向外延伸的外部风扇第一级和外部风扇第二级。
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公开(公告)号：US20110167792A1
公开(公告)日：2011-07-14
申请号：US12642967
申请日：2009-12-21
IPC分类号： F02K3/02
CPC分类号： F02K3/075 , F01D17/162 , F02C7/042 , F02K3/077
摘要： An adaptive gas turbine engine is disclosed having a convertible fan system adapted to have a variable fan pressure ratio while the air flow into the convertible fan system remains substantially constant and an adaptive core having a compressor capable of maintaining a substantially constant core pressure ratio while a core airflow flow rate is varied.
摘要翻译： 公开了一种自适应燃气涡轮发动机，其具有适于具有可变风扇压力比的可变风扇系统，同时进入可转换风扇系统的空气流保持基本恒定，并且具有压缩机的自适应型芯能够保持基本上恒定的芯压比，而 核心气流流量变化。
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公开(公告)号：US20110120082A1
公开(公告)日：2011-05-26
申请号：US12796353
申请日：2010-06-08
IPC分类号： F02K3/02
CPC分类号： F02C3/064 , F01D5/022 , F02K3/077 , Y02T50/672
摘要： A fan assembly having an outer fan system is disclosed, the fan assembly comprising an outer fan first stage and an outer fan second stage both extending radially outward from an arcuate platform.
摘要翻译： 公开了一种具有外部风扇系统的风扇组件，风扇组件包括从弧形平台径向向外延伸的外部风扇第一级和外部风扇第二级。
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公开(公告)号：US07509797B2
公开(公告)日：2009-03-31
申请号：US11118171
申请日：2005-04-29
申请人： James Edward Johnson
发明人： James Edward Johnson
IPC分类号： F02K1/00
摘要： A turbojet engine includes a core engine, an afterburner, and a converging-diverging exhaust nozzle in serial flow communication. A thrust vectoring system is joined between a compressor and the nozzle. A controller is operatively joined to the thrust vectoring system for selectively varying distribution of air bled from the compressor into the exhaust nozzle for vectoring propulsion thrust.
摘要翻译： 涡轮喷气发动机包括核心发动机，加力燃烧器和串联流动通信中的会聚发散排气喷嘴。 推力矢量系统连接在压缩机和喷嘴之间。 控制器可操作地连接到推力矢量系统，用于选择性地改变从压缩机排放到排气喷嘴中的空气分配，用于矢量推进推力。
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公开(公告)号：US20110171007A1
公开(公告)日：2011-07-14
申请号：US12642943
申请日：2009-12-21
IPC分类号： F01D17/00
CPC分类号： F02K3/075 , F01D17/162 , F02C7/042 , F02C9/18 , F02C9/20 , F02K3/077 , F05D2220/327
摘要： A convertible fan system is disclosed having a fan rotor with a plurality of fan blades having an arcuate splitter that forms a portion of an inner flow passage and an outer flow passage wherein an inner portion of the fan blade pressurizes an inner flow in the inner flow passage and an outer portion of the fan blade pressurizes an outer flow in the outer flow passage and a vane system having an outer vane that is adapted to be able to vary the flow in the outer flow passage such that pressure ratio of the fan system can be varied.
摘要翻译： 一种敞篷式风扇系统，其具有风扇转子，该风扇转子具有多个风扇叶片，所述风扇叶片具有形成内部流动通道的一部分的弧形分离器和外部流动通道，其中风扇叶片的内部部分对内部流动中的内部流动进行加压 通道和风扇叶片的外部部分对外部流动通道中的外部流动进行加压，以及具有外部叶片的叶片系统，其适于能够改变外部流动通道中的流动，使得风扇系统的压力比可以 变化多变
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公开(公告)号：US20110120083A1
公开(公告)日：2011-05-26
申请号：US12796372
申请日：2010-06-08
IPC分类号： F02K3/02
CPC分类号： F02C3/064 , F01D5/022 , F02K3/077 , Y02T50/672
摘要： A gas turbine engine comprising an outer fan system is disclosed, having an outer fan first stage having a circumferential row of outer fan first blades, an outer fan second stage having a circumferential row of outer fan second blades located axially aft from the outer fan first stage wherein the outer fan first stage and the outer fan second stage are adapted to rotate with the fan rotor.
摘要翻译： 公开了一种包括外风扇系统的燃气涡轮发动机，其具有外风扇第一级，其具有圆周排的外风扇第一叶片;外风扇第二级，其具有周向列的外风扇第二叶片，所述外风扇第二叶片从外风扇第一 其中外风扇第一级和外风扇第二级适于与风扇转子一起旋转。
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公开(公告)号：US07631484B2
公开(公告)日：2009-12-15
申请号：US11308219
申请日：2006-03-13
IPC分类号： F02K3/02
CPC分类号： F02K3/062 , F02C3/073 , F02C7/042 , F05D2240/80 , Y02T50/672
摘要： A fan assembly for a gas turbine engine includes a turbine rotor adapted to be disposed aft of a core of the gas turbine engine; a row of turbine blades carried by the rotor, each turbine blade extending from the rotor to a tip, the turbine blades adapted to extract energy from a stream of pressurized combustion gases generated by the core; and at least two rows of axially-spaced apart, radially-extending fan blades carried by the row of turbine blades for rotation therewith.
摘要翻译： 一种用于燃气涡轮发动机的风扇组件，包括适于设置在燃气涡轮发动机的核心的后方的涡轮转子; 由转子承载的一排涡轮叶片，每个涡轮叶片从转子延伸到尖端，涡轮机叶片适于从由芯产生的加压燃烧气体流中提取能量; 以及至少两排轴向间隔开的径向延伸的风扇叶片，所述风扇叶片由所述一排涡轮机叶片承载以与其一起旋转。
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公开(公告)号：US20080155961A1
公开(公告)日：2008-07-03
申请号：US11617371
申请日：2006-12-28
申请人： James Edward Johnson
发明人： James Edward Johnson
IPC分类号： F02K3/02
摘要： A gas turbine engine includes a turbomachinery core operable to generate a flow of pressurized combustion gases at a variable flow rate, while maintaining a substantially constant core pressure ratio; a rotating fan disposed upstream of the core, the fan adapted to extract energy from the core and generate a first flow of air which is compressed at a first pressure ratio; and at least a first bypass duct surrounding the core downstream of the fan adapted to selectively receive at least a first selected portion of the first flow which is compressed at a second pressure ratio lower than the first pressure ratio, and to bypass the first selected portion around the core, thereby varying a bypass ratio of the engine. The fan is adapted to maintain a flow rate of the first flow substantially constant, independent of the bypass ratio.
摘要翻译： 燃气涡轮发动机包括涡轮机芯，其可操作以产生可变流量的加压燃烧气体流，同时保持基本上恒定的芯压比; 设置在所述芯的上游的旋转风扇，所述风扇适于从所述芯提取能量并产生以第一压力比压缩的第一空气流; 以及至少第一旁路管道，围绕所述风扇下游的所述核心，适于选择性地接收所述第一流动的第一选定部分，所述第一流量以比所述第一压力比低的第二压力比被压缩，并绕过所述第一选定部分 围绕芯部，从而改变发动机的旁路比。 风扇适于保持第一流量的流量基本上恒定，而与旁路比无关。
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公开(公告)号：US06666018B2
公开(公告)日：2003-12-23
申请号：US10328679
申请日：2002-12-23
IPC分类号： F02K306
摘要： A pulse detonation system for a turbofan engine including a fan assembly and a turbine sub-system, which includes at least one turbine, is configured to create a temperature rise and a pressure rise within the turbofan engine and to generate thrust for the turbofan engine. The pulse detonation system includes a pulse detonation core assembly comprising at least one detonation chamber configured to detonate a fuel mixture. The pulse detonation core assembly is positioned between the fan assembly and the turbine sub-system.
摘要翻译： 包括风扇组件和包括至少一个涡轮机的涡轮机子系统的涡轮风扇发动机的脉冲爆震系统构造成在涡轮风扇发动机内产生温度升高和压力上升，并产生用于涡轮风扇发动机的推力。 脉冲爆震系统包括脉冲爆震核心组件，其包括至少一个被配置为引爆燃料混合物的爆震室。 脉冲爆震芯组件位于风扇组件和涡轮机子系统之间。
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公开(公告)号：US5694768A
公开(公告)日：1997-12-09
申请号：US484083
申请日：1990-02-23
摘要： An improved variable cycle turbofan-ramjet engine is disclosed. The engine includes a split fan assembly, a bypass channel surrounding a core engine and a mode selector valve for selectively bypassing air around an aft fan and the core engine. In a first, single bypass mode of operation, the mode selector valve allows air to flow through both a forward fan and the aft fan, and a portion of which bypasses the core engine. In a second, double bypass mode of operation, the mode selector valve allows air from the forward fan to bypass the aft fan and a portion of the air from the forward fan to bypass the core engine. In a third, ramjet mode of operation, the mode selector vane bypasses air around the aft fan and the core engine and the core engine is shut down for ramjet operation. In the preferred embodiment, the forward fan is allowed to windmill and powers a fuel pump connected thereto for providing fuel to a ram burner of the engine for ramjet operation.
摘要翻译： 公开了一种改进的可变循环涡扇喷气发动机。 发动机包括分体风扇组件，围绕核心发动机的旁通通道和用于选择性地绕过尾风扇和核心发动机的空气的模式选择阀。 在第一个单旁路操作模式中，模式选择阀允许空气流过前风扇和后风扇，其一部分绕过核心发动机。 在第二个双旁路操作模式中，模式选择阀允许来自前风扇的空气绕过后风扇和来自前风扇的一部分空气绕过核心发动机。 在第三种冲压式操作模式中，模式选择器叶片绕过后风扇绕过空气，并且核心发动机和核心发动机关闭以进行冲压喷射操作。 在优选实施例中，允许前风扇对与其连接的燃油泵进行风力发电，为燃料喷射操作的发动机的冲压燃烧器提供燃料。
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