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公开(公告)号：US2675A
公开(公告)日：1842-06-18
申请号：US2675D
CPC分类号： F03D3/00 , F01D1/28 , Y02E10/74 , Y10T137/785 , Y10T137/7908
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公开(公告)号：US20150044025A1
公开(公告)日：2015-02-12
申请号：US14390253
申请日：2013-04-02
申请人： EQUITHERM S.A.R.L.
发明人： Luc Maîtrejean
IPC分类号： F01D5/04
摘要： A multi-stage turbine (16) is designed as an induction turbine with vapour induction in at least one intermediary stage. It is more particularly conceived as a radial-outward-flow type multi-stage turbine, with an axial main vapour inlet port (82) and an annular secondary vapour inlet port (84), which is arranged in the turbine (16) so as to annularly induce, in an intermediary stage of said turbine, a secondary vapour stream into an already partially expanded radial main vapour stream. The annular secondary vapour inlet port (84) comprises as a ring-zone (92) with through holes (94), which radially surrounds said axial main vapour inlet port (82) in a first turbine housing part (80). The axial vapour inlet port comprises a first tubular vapour inlet connection (82). The annular vapour inlet port comprises a second tubular vapour inlet connection (84) surrounding the first tubular vapour inlet connection (82), so as to define with the latter an annular space (86), wherein the ring-zone (92) with through holes (94) is arranged in this annular space (86).
摘要翻译： 多级涡轮机（16）被设计为在至少一个中间级中具有蒸汽感应的感应涡轮机。 更特别地被认为是具有轴向主蒸汽入口（82）和环形二次蒸气入口（84）的径向向外流动型多级涡轮机，其被布置在涡轮机（16）中，以便 在所述涡轮机的中间阶段环形地将次级蒸气流引入已经部分膨胀的径向主蒸气流中。 环形二次蒸汽入口（84）包括具有通孔（94）的环带（92），其在第一涡轮机壳体部分（80）中径向地围绕所述轴向主蒸汽入口（82）。 轴向蒸汽入口包括第一管状蒸汽入口连接（82）。 环形蒸汽入口包括围绕第一管状蒸汽入口连接（82）的第二管状蒸汽入口连接（84），以便与后者形成环形空间（86），其中环带（92）具有通孔 孔（94）布置在该环形空间（86）中。
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公开(公告)号：US08839599B1
公开(公告)日：2014-09-23
申请号：US14047693
申请日：2013-10-07
申请人： Juan Pedro Mesa, Jr.
发明人： Juan Pedro Mesa, Jr.
IPC分类号： F02C3/14 , F02C5/12 , F02C3/04 , F02K7/00 , F01D1/28 , F01D1/32 , F02C3/16 , F01D5/04 , F01D5/06
摘要： An axially aligned combustion engine with a rotationally fixed housing and rotationally disposed rotor is presented. Particularly, the rotor includes an engine assembly and one or more air compressor assemblies axially aligned about an axis within the housing. The engine assembly includes a plurality of radially disposed combustion chambers extending from a closed interior edge outward toward an at least partially open access port disposed at an outer peripheral edge of the engine assembly. As the engine assembly rotates within the housing, the radially disposed combustion chambers are successively aligned with or communicatively disposed with an air manifold to receive compressed air, actuator(s) to receive fuel and ignite the fuel, and an exhaust manifold to expel the combusted gases.
摘要翻译： 提出了具有旋转固定壳体和旋转地设置的转子的轴向对准的内燃机。 特别地，转子包括发动机组件和围绕壳体内的轴线轴向对齐的一个或多个空气压缩机组件。 发动机组件包括从封闭的内部边缘向外延伸到设置在发动机组件的外周边缘处的至少部分开放的进入端口的多个径向设置的燃烧室。 当发动机组件在壳体内旋转时，径向设置的燃烧室依次与空气歧管对准或通信地设置以接收压缩空气，致动器以接收燃料并点燃燃料，以及排气歧管以排出燃烧的 气体。
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公开(公告)号：US20130004321A1
公开(公告)日：2013-01-03
申请号：US13264610
申请日：2010-07-28
IPC分类号： F01D5/14
CPC分类号： F01D5/048 , F01D1/28 , F05D2220/40 , F05D2240/307 , F05D2250/70 , F05D2260/20
摘要： A turbine wheel includes a plurality of blades having a scallop cut-out profile. The scallop cut-out profile is formed by cutting-out a back side wall part of the blade between the suction surface side of a blade part and the pressure surface side of the adjacent blade.
摘要翻译： 涡轮机叶轮包括具有扇形切口轮廓的多个叶片。 扇形切割轮廓通过在叶片部分的吸力表面侧和相邻叶片的压力表面侧之间切割叶片的后侧壁部而形成。
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公开(公告)号：US4136896A
公开(公告)日：1979-01-30
申请号：US852673
申请日：1977-11-18
申请人： Michael R. Rodman , Paul M. Holmes , Joseph Habib
发明人： Michael R. Rodman , Paul M. Holmes , Joseph Habib
摘要： A fitting for connecting a metal conduit to a conventional 37.degree. flared adapter which does not require flaring of the conduit, and constitutes a compression type fitting utilizing a radially contractable ferrule and compression nut. Metal-to-metal sealing contact is achieved, and no modification of the conduit is required.
摘要翻译： 用于将金属导管连接到常规的37°喇叭形适配器的装置，其不需要对管道进行扩口，并且构成利用可径向收缩的套圈和压缩螺母的压缩型配件。 实现金属对金属的密封接触，并且不需要对管道进行改造。
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公开(公告)号：US3930744A
公开(公告)日：1976-01-06
申请号：US405092
申请日：1973-10-10
申请人： James V. Theis, Jr.
发明人： James V. Theis, Jr.
摘要： A pressure gas engine having an inner first member of circular cross section with a periphery containing first energy conversion means for converting gas pressure to power and an outer second member extending around the first member and with a generally circular inner surface facing the outer surface of the first member and having second energy conversion means in the inner surface facing the first member and for converting gas velocity to power. In certain embodiments the inner and outer arrangements of the first and second members will be reversed. At least one of these first and second members is rotatable about an axis of rotation by the force exerted thereon due to the gas acting on its energy conversion means with one of the energy conversion means in either the first member or the second member comprising at least one and preferably a plurality of spaced converging-diverging nozzles each lying on a chord of its member that is less than the diameter and exhausting toward the other energy conversion means with the other energy conversion means comprising a series of impulse turbine buckets facing the nozzles. Each bucket is inclined with respect to its member and is adapted to be aligned with the nozzle exhaust on relative movement of the first and second members with respect to each other.
摘要翻译： 一种压力气体发动机，其具有圆形横截面的内部第一构件，其周边包含用于将气体压力转换成动力的第一能量转换装置和围绕第一构件延伸的外部第二构件和面向外部表面的大致圆形的内表面 第一构件并且在面向第一构件的内表面中具有第二能量转换装置，并且用于将气体速度转换成功率。 在某些实施例中，第一和第二构件的内部和外部布置将被反转。 这些第一和第二构件中的至少一个可以通过施加在其上的力而围绕旋转轴线旋转，因为气体作用在其能量转换装置上，其中第一构件或第二构件中的一个能量转换装置至少包括 一个并且优选地多个间隔开的会聚发散喷嘴，每个位于其构件的弦上，其小于直径并朝向另一个能量转换装置排出，而另一个能量转换装置包括面向喷嘴的一系列脉冲涡轮机叶片。 每个桶相对于其构件倾斜，并且适于与第一和第二构件相对于彼此的相对运动与喷嘴排气对准。
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110.发明授权
公开(公告)号：US3656300A
公开(公告)日：1972-04-18
申请号：US3656300D
申请日：1968-10-11
CPC分类号： F01D1/28 , F01D5/041 , F02C1/05 , G21D5/02 , Y10S376/91
摘要： A method and an installation for converting nuclear energy to mechanical energy by incorporating fissionable material in at least some of the vanes defining a continuous tortuous duct in a turbine, directing a compressed fluid flow through said duct, extending this fluid flow in at least part of the duct to effect transfer of released nuclear energy to the fluid flow and directing the fluid flow upon the driving vanes of the turbine to effect rotation thereof thereby converting the released nuclear energy to mechanical energy.
摘要翻译： 一种用于将核能转换为机械能的方法和装置，其中将至少一些叶片中的至少一些叶片中的可裂变材料结合到涡轮中，所述至少一些叶片限定了涡轮机中的连续曲折的管道，将压缩的流体流引导通过所述管道， 所述管道用于将释放的核能转移到流体流动并且将流体流引导到涡轮的驱动叶片上以实现其旋转，从而将释放的核能转换为机械能。
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