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    • 10. 发明授权
    • Capillary two-phase thermodynamic power conversion cycle system
    • 毛细管两相热力转换循环系统
    • US06857269B2
    • 2005-02-22
    • US10431826
    • 2003-05-08
    • Karl William Baker
    • Karl William Baker
    • B64G1/50F01K15/02F25B41/06F01K7/34
    • F25B41/067B64G1/506F01K15/02F25B2500/18
    • A two-phase thermodynamic power system includes a capillary device, an inline turbine, and a condenser for generating output power as a generator or receiving input power as a refrigerator. The capillary device, such as a heat loop pipe or a capillary pumped loop, is coupled to the inline turbine for generating output power for power generation or for receiving input power for powered refrigeration. The capillary device receives input heat that is used to change phase of liquid received from the condenser into vapor for driving the turbine. The power system is well suited for space applications using a radioisotope heat source, using waste heat from a radioisotope power system as a heat source, waste heat from spacecraft components such as electronics as a heat source or solar energy as a heat source. The heat source is useful for driving the capillary wick as well as a superheater for increased power efficiency and lifetime operation. The power system is well suited for space receiving heat from a heat source to produce useful mechanical energy. The refrigeration system is well suited for receiving input mechanical power to the turbine for removing waste heat from a spacecraft at a low temperature and rejecting that heat into space at a higher temperature.
    • 两相热力动力系统包括毛细管装置,内联涡轮机和用于产生输出功率作为发电机或接收作为冰箱的输入功率的电容器。 毛细管装置,例如热回路管或毛细管抽吸回路,联接到在线涡轮机,用于产生用于发电的输出功率或用于接收用于动力制冷的输入功率。 毛细管装置接收用于将从冷凝器接收的液体的相位改变成蒸汽以用于驱动涡轮机的输入热量。 电力系统非常适合使用放射性同位素热源的空间应用,使用来自放射性同位素电力系统的废热作为热源,将来自诸如电子设备的航天器组件作为热源或作为热源的太阳能的余热。 热源可用于驱动毛细管芯以及过热器,以提高功率效率和寿命运行。 电力系统非常适合于从热源接收热量以产生有用的机械能的空间。 制冷系统非常适合于接收到涡轮机的输入机械动力,以在低温下从宇宙飞船去除废热,并将该热量排斥到较高温度的空间。