发明名称 TWO-PHASE TYPE HEAT TRANSFER DEVICE FOR HEAT SOURCES OPERATING AT A WIDE TEMPERATURE RANGE
摘要 A two-phase type heat transfer device (10) for heat sources operating at a wide temperature range. The heat transfer device (10) includes an evaporator (21) collecting heat from a heat source, a condenser (21) providing heat to a cold sink by a first working fluid passing through liquid and vapor transport lines (25, 27) that connect the evaporator (21) and the condenser (23). The evaporator (21) is arranged inside a saddle (31) configured for avoiding that the temperature of the first working fluid in the evaporator (21) is greater than its critical point. The invention also refers to aircraft ice protection systems using the heat transfer device (10).
申请公布号 US2017113804(A1) 申请公布日期 2017.04.27
申请号 US201615331232 申请日期 2016.10.21
申请人 Airbus Defence and Space S.A. 发明人 BLANCO MAROTO Ana;REDONDO CARRACEDO Francisco Jose;TORRES SEPULVEDA Alejandro;MISHKINIS Donatas;MARTINEZ MARTIN Juan
分类号 B64D15/02;B64C3/00;B64D29/00;F28D15/02 主分类号 B64D15/02
代理机构 代理人
主权项 1. A two-phase type heat transfer device comprising: an evaporator configured to collect heat from a heat source; a condenser configured to provide heat to a cold sink, and liquid and vapor transport lines connected to the evaporator and the condenser, wherein a first working fluid circulates through the liquid and vapor transport lines, the evaporator and the condenser, wherein an operating temperature of the heat source is in a range between temperatures T1 and T2, wherein T1 is at least 75° C.; wherein the first working fluid has a critical point temperature Tc1 higher than T1 and lower than T2, and a freezing point temperature Tf of the first working fluid is lower than a certain minimum environmental external temperature T3 for the liquid transport line; and wherein the evaporator is arranged in a saddle configured to avoid having the temperature of the first working fluid in the evaporator exceed the critical point temperature Tc1.
地址 Madrid ES