会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 7. 发明申请
    • Thermally Enhanced Cascade Cooling System
    • 热增强级联冷却系统
    • US20150052926A1
    • 2015-02-26
    • US13975327
    • 2013-08-24
    • Gerald Allen Alston
    • Gerald Allen Alston
    • F25B27/02
    • F25B27/02B60H1/32F25B1/08F25B7/00Y02A30/274Y02A40/966Y02A40/967
    • A cascade cooling system that uses low-grade thermal and other energy input sources to provide refrigeration and air conditioning in stationary and mobile applications. A two-loop embodiment includes a heat-powered first loop incorporating a vapor-jet compressor and a second loop based on a mechanical compressor powered by an electric motor or other source of rotational torque. The system uses waste heat, solar thermal or a fuel-fired heat source to partially or fully offset mechanical/electrical energy input. The system can also operate entirely on thermal, electrical or mechanical input. The ability to use multiple energy sources in any combination maximizes energy efficiency, performance and reliability. The system is well suited to making beneficial use of waste heat in vehicle applications. In stationary applications, solar thermal and/or waste heat from industrial processes can be used to improve the efficiency of conventional cooling systems.
    • 一种级联冷却系统,其使用低等级的热能和其他能量输入源来在固定和移动应用中提供制冷和空调。 双回路实施例包括结合有蒸气喷射压缩机的热源第一回路和基于由电动机或其它转矩源驱动的机械压缩机的第二回路。 该系统使用废热,太阳能热或燃料热源来部分或全部抵消机械/电能输入。 该系统还可以完全基于热,电或机械输入。 以任何组合使用多种能源的能力最大限度地提高了能源效率,性能和可靠性。 该系统非常适合在车辆应用中有益地利用废热。 在固定应用中,来自工业过程的太阳能热和/或废热可用于提高常规冷却系统的效率。
    • 10. 发明授权
    • Spacecraft radiator system using a heat pump
    • 航天器散热器系统采用热泵
    • US06883588B1
    • 2005-04-26
    • US09624151
    • 2000-07-24
    • Lenny LowRandy Pon
    • Lenny LowRandy Pon
    • B64G1/50F24F5/00F25B9/00F25B27/00F28D15/00F25B13/00
    • F25B27/005B64G1/50B64G1/503B64G1/506F25B9/002Y02A40/966
    • Heat dissipating apparatus or system for dissipating heat generated by a payload on a spacecraft having a plurality of surfaces. The system includes at least one radiator-condenser coupled to one or more of the surfaces of the spacecraft and a heat pump including an evaporator, a compressor, and an expansion valve coupled in a closed-loop manner to the radiator-condenser. The system components are coupled together using small diameter, thin- and smooth-walled tubing. The system enables the radiator-condenser to be elevated above the source or payload temperature, and, along with the use of thin walled tubing, reduces the mass of the spacecraft. Because the radiator-condenser temperatures are elevated, multiple surfaces of the spacecraft (west, east, earth and aft) can be effectively used as radiating surfaces.
    • 用于耗散由具有多个表面的航天器上的有效载荷产生的热的散热装置或系统。 该系统包括耦合到航天器的一个或多个表面的至少一个散热器 - 冷凝器,以及包括蒸发器,压缩机和以闭环方式耦合到散热器 - 冷凝器的膨胀阀的热泵。 系统部件使用小直径,薄壁和平滑的管道连接在一起。 该系统使散热器 - 冷凝器升高到源或有效载荷温度以上,并且与使用薄壁管一起降低了航天器的质量。 由于散热器 - 冷凝器的温度升高,所以航天器的多个表面(西,东,土,船尾)可以有效地用作辐射表面。