公开(公告)号：US11528829B2

公开(公告)日：2022-12-13

申请号：US17624139

申请日：2020-06-30

申请人： BEIHANG UNIVERSITY ,  Weixing Yuan ,  Tongzhi Yang ,  Kexian Ren ,  Bo Yang ,  Ze Miao

发明人： Weixing Yuan ,  Tongzhi Yang ,  Kexian Ren ,  Bo Yang ,  Ze Miao

IPC分类号： H05K7/20

摘要： An overall efficient heat dissipation system for a high power density cabinet comprises a pump-driven two-phase circulation loop high-power-chip direct heat dissipation system and a cabinet air-cooling system. The cabinet air-cooling system comprises a refrigerant circulation loop and a cabinet internal air circulation loop. The refrigerant circulation loop includes a pump-driven two-phase circulation loop and a vapor compression circulation loop. The pump-driven two-phase circulation loop high-power-chip direct heat dissipation system performs fixed-point heat dissipation for main heating elements, such as CPU and GPU, in a server, and the cabinet air-cooling system performs air-cooling heat dissipation for other heating elements in the server.

公开(公告)号：US10974191B2

公开(公告)日：2021-04-13

申请号：US16624751

申请日：2018-06-22

申请人： BEIHANG UNIVERSITY ,  Weixing Yuan ,  Yan Zheng ,  Bin Yu

发明人： Weixing Yuan ,  Yan Zheng ,  Bin Yu

IPC分类号： B01D53/22 ,  B01D53/26 ,  B64D13/06 ,  B64D37/32

摘要： Disclosed is an aircraft environmental control and fuel tank inerting coupling system based on a membrane separation method. The dehumidification of gas in an aircraft environmental control system and the separation of oxygen and nitrogen in a fuel tank inerting system are realized respectively, based on the selective permeability of a membrane to water vapour/air and oxygen/nitrogen. In the coupling system, part of drying gas passing through a membrane dehumidification heat exchanger (5) enters a membrane air separator (9), and the other part thereof is cooled through a large expansion turbine (8) and then directed into a cockpit for refrigeration; and nitrogen-rich gas generated by the membrane air separator (9) is directed into a fuel tank for inerting. Oxygen-rich gas is mixed with gas supplied by the environmental control system, thus increasing the oxygen content of gas supplied by the aircraft cockpit.

公开(公告)号：US20110296865A1

公开(公告)日：2011-12-08

申请号：US13142452

申请日：2010-01-15

申请人： Weixing Yuan ,  Yufei Yang ,  Xiugan Yuan

发明人： Weixing Yuan ,  Yufei Yang ,  Xiugan Yuan

IPC分类号： F25D11/00

CPC分类号： F25B27/005 ,  F25B29/003 ,  F25B2400/075 ,  F25B2400/24 ,  F25B2700/1931 ,  F25B2700/1933 ,  F25B2700/2111

摘要： A hybrid-driven cold/heat storage type heat pump unit utilizing a solar photovoltaic power and a commercial power, which has a DC compressor (2) and an AC compressor (8), is a dual supply heat pump system driven by a solar photovoltaic DC power and a common commercial AC power in combination. When there is sunshine, the DC generated by a solar cell panel (60) is used for driving the DC compressor (2) directly to produce cold and heat capacity, and the produced cold and heat capacity could be stored respectively in a phase-change cold storage medium (39) and a phase-change heat storage medium (20). When the DC power is insufficient, the AC power from power network is used for power supply.

摘要翻译： 利用具有DC压缩机（2）和AC压缩机（8）的太阳能光伏发电和商用电力的混合动力式冷热蓄热机组是由太阳能光伏驱动的双电源热泵系统 直流电源和共同商用交流电源组合使用。 当有阳光时，由太阳能电池板（60）产生的直流用于直接驱动直流压缩机（2）以产生冷热容量，所产生的冷热容量可以分别存储在相变 冷藏介质（39）和相变储热介质（20）。 当直流电不足时，电力网的交流电用于供电。