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    • 3. 发明授权
    • Multistage two-phase turbine
    • 多级两相涡轮机
    • US6122915A
    • 2000-09-26
    • US303631
    • 1999-05-03
    • Lance G. Hays
    • Lance G. Hays
    • F03G4/00B01D17/00B01D19/00F01D1/00F01D1/32F01D15/00F01D25/32F01K21/00F01K25/04F03G7/04F03G7/00
    • F03G7/04B01D17/00B01D19/0052F01D1/00F01D1/32F01D15/00F01D25/32F01K21/005F05D2210/13F05D2240/36
    • A multistage two-phase turbine having multiple stages to receive fluid, each stage having an inlet and outlet comprising nozzles at the inlet to each stage to accelerate the fluid that consists of a mixture of gas and liquid, to form two-phase jets; a rotating separator structure to receive and separate the two-phase jets into gas streams and liquid stream in each stage; the turbine having a rotating output shaft, and there being structure to convert the kinetic energy of the liquid streams into shaft power; structure to remove the separated liquid from at least one stage and transfer it to nozzles at the next stage; structure to remove the separated liquid from the last stage and transfer it to primary outlet structure; and structure to remove the separated gas from at least one stage and transfer it to a secondary outlet structure.
    • 具有多级以接收流体的多级两相涡轮机,每级具有入口和出口,该入口和出口在每个级的入口处包括喷嘴,以加速由气体和液体的混合物组成的流体,以形成两相射流; 旋转分离器结构,用于在两个阶段中接收和分离两相流入气流和液体流; 涡轮机具有旋转的输出轴,并且存在将液体流的动能转换成轴功率的结构; 结构,以从至少一个阶段除去分离的液体并将其在下一阶段转移到喷嘴; 结构,以从最后阶段除去分离的液体并将其转移到主出口结构; 以及从至少一个阶段除去分离的气体并将其转移到次级出口结构的结构。
    • 9. 发明申请
    • Variable phase turbine apparatus
    • 可变相涡轮机
    • US20100111669A1
    • 2010-05-06
    • US12290627
    • 2008-11-03
    • Lance G. HaysPhillip R. Welch
    • Lance G. HaysPhillip R. Welch
    • F01D17/16
    • F02C1/00F01D15/00
    • Variable phase turbine apparatus comprising, in combination a rotatably driven load structure, defining an axis, confinement means forming a fluid flow passage extending generally axially and adjacent said load structure, a turbine operatively connected to said load structure, to transmit rotary drive thereto, two-phase flow nozzle means receiving pressurized flow via said passage, and directing flow of fluid from said passage, expanded in the nozzle means, at the turbine to rotate the turbine, the nozzle means configured to expand flow consisting of two or more of the following phases: v) gas vi) liquid vii) gas and liquid mixture viii) supercritical gas and liquid mixture, and with efficient conversion of enthalpy.
    • 可变相涡轮机装置包括组合有可旋转驱动的负载结构,限定轴线,限制装置,形成大致轴向延伸并且邻近所述负载结构的流体流动通道,可操作地连接到所述负载结构的涡轮,以将旋转驱动器传送到其上, 相流流动喷嘴意味着经由所述通道接收加压流动,并且引导流体从所述通道流出,在喷嘴装置中膨胀在涡轮机处以使涡轮旋转,喷嘴装置构造成扩展由以下两个或更多个组成的流动 相:v)气体vi)液体vii)气体和液体混合物viii)超临界气体和液体混合物,并有效转化焓。
    • 10. 发明授权
    • Heat recovery system
    • 热回收系统
    • US06668537B1
    • 2003-12-30
    • US09966206
    • 2001-09-26
    • Lance G. Hays
    • Lance G. Hays
    • F02C618
    • F01K23/106F02C6/18
    • A hot exhaust heat recovery system comprising, in combination a chamber having inlet and outlet porting for flow through of hot exhaust gas, in the chamber interior, separate heat exchanger structures in separate sequential segments said chamber interior, to receive heat transferred from said exhaust gas, said structures receiving pressurized liquid for flow in different paths there-through, to develop vapor streams at different pressures and temperatures without use of boiler drums, the structures having outlets to communicate with a vapor driven turbine or turbines having inlet ports at different inlet fluid pressure zones.
    • 一种热废热回收系统,其特征在于包括具有用于流过热废气的入口和出口的腔室,在腔室内部,分离的热交换器结构,在单独的顺序区段中,所述室内部,以接收从所述废气传递的热量 所述结构接收用于在不同路径中流动的加压液体,以在不使用锅炉鼓的情况下在不同的压力和温度下形成蒸汽流,所述结构具有与蒸汽驱动的涡轮机或具有不同入口流体的入口端口的涡轮机连通的出口 压力区。