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    • 1. 发明授权
    • Method and apparatus for manufacturing superfluidity helium
    • 制造超滤氦的方法和装置
    • US5347819A
    • 1994-09-20
    • US141742
    • 1993-10-27
    • Nobuyoshi SajiHiroshi OhyaHiroshi AsakuraShunji Nagai
    • Nobuyoshi SajiHiroshi OhyaHiroshi AsakuraShunji Nagai
    • F17C13/00F25B9/10F25J1/00F25B19/00
    • F25B9/10
    • Method and apparatus for manufacturing superfluidity helium (He II). The method includes the steps of (a) providing .sup.3 He gas (b) providing liquid .sup.4 He, (c) compressing the .sup.3 He gas to produce compressed .sup.3 He gas, (d) indirectly cooling the compressed .sup.3 He gas with liquid .sup.4 He to produce cryogenic .sup.3 He gas (e) adiabatically expanding the cryogenic .sup.3 He gas to produce cryogenic .sup.3 He gas having a temperature of less than about 1.18.degree. K., preferably less than 1.8.degree. K., and (f) indirectly cooling the liquid .sup.4 He with the cryogenic .sup.3 He gas produced in step (e) to produce superfluidity helium. The apparatus includes a first container for liquid helium and a second container for containing superfluidity helium, and a first line for connecting the first and second containers. A .sup.3 He refrigeration circuit is provided to cool the .sup.4 He in directly with cryogenic .sup.3 He to produce superfluidity helium. The method and apparatus enables superfluidity helium to be produced without the use of a large vacuum pump whose lubricants might contaminate the superfluidity helium. The method and apparatus also allow superfluidity helium at or near standard pressure to be easily produced and maintained.
    • 制造超流氦的方法和装置(氦II)。 该方法包括以下步骤:(a)提供提供液体4He的3He气体(b),(c)压缩3He气体以产生压缩的3He气体,(d)用液体4He间接冷却压缩的3He气体以产生低温3He气体 e)绝热膨胀低温3He气体以产生温度低于约1.18°K,优选小于1.8°K的低温3He气体,和(f)间接地用步骤中产生的低温3He气体冷却液体4He (e)产生超流氦。 该装置包括用于液氦的第一容器和用于容纳超流氦的第二容器和用于连接第一和第二容器的第一管线。 提供3He制冷回路以直接用低温3He冷却4He以产生超流氦。 该方法和装置使得能够生产超流氦,而不需要使用其润滑剂可能污染超流氦的大型真空泵。 该方法和装置还允许容易地产生和维持在标准压力附近或接近标准压力的超流氦。
    • 3. 发明授权
    • Turbine expansion machine with variable nozzle mechanism
    • 涡轮膨胀机具有可变喷嘴机构
    • US06382910B1
    • 2002-05-07
    • US09695905
    • 2000-10-26
    • Takashi KatoKatsumi KawanoToru ShimbaTadao HiyamaHiroshi TsujiSeiichiro YoshinagaHiroshi AsakuraNobuyoshi SajiTakehiko Ishizawa
    • Takashi KatoKatsumi KawanoToru ShimbaTadao HiyamaHiroshi TsujiSeiichiro YoshinagaHiroshi AsakuraNobuyoshi SajiTakehiko Ishizawa
    • F01D1712
    • F01D17/165Y10S62/91
    • An adiabatic expansion apparatus 22 with a built-in turbine impeller 12 adiabatically expands gas at a cryogenic temperature when the impeller rotates. A control device 24 is connected coaxially with the turbine impeller to control the impeller. A variable nozzle mechanism 30 is provided for varying the throat area for the gas at a cryogenic temperature to be introduced into the turbine impeller. The adiabatic expansion apparatus is installed in a vacuum vessel 14, and a control device is disposed outside the vacuum vessel. The variable nozzle mechanism comprises a nozzle component 32 built into the adiabatic expansion apparatus, and a driving component 34 installed outside the vacuum vessel. The nozzle component and the driving component are connected to the turbine impeller with a coaxial, thin cylindrical component 36, and drive the nozzle component when the cylindrical component rotates about the axis Z of the turbine impeller. The actuator and most of components of the nozzle driving mechanism can be installed at normal temperature under atmospheric pressure, the heat input can be suppressed to an extremely minimal level, and the variable nozzle of the expansion turbine can be driven. Thus, according to the invention, helium gas at a cryogenic temperature can be expanded adiabatically at a high adiabatic efficiency.
    • 具有内置涡轮叶轮12的绝热膨胀装置22在叶轮旋转时在低温下绝热膨胀气体。 控制装置24与涡轮机叶轮同轴地连接以控制叶轮。 提供可变喷嘴机构30,用于改变在低温下气体的喉部区域,以引入涡轮叶轮。 绝热膨胀装置安装在真空容器14中,控制装置设置在真空容器的外部。 可变喷嘴机构包括内置于绝热膨胀装置中的喷嘴部件32和安装在真空容器外部的驱动部件34。 喷嘴部件和驱动部件通过同轴的薄的圆柱形部件36连接到涡轮机叶轮,并且当圆柱形部件围绕涡轮叶轮的轴线Z旋转时驱动喷嘴部件。 致动器和喷嘴驱动机构的大部分部件可以在大气压下的常温下进行安装,能够将热输入抑制到极小的水平,并且可以驱动膨胀涡轮机的可变喷嘴。 因此,根据本发明,在低温下的氦气可以以绝热的高效绝热膨胀。