公开(公告)号：US20170167442A1

公开(公告)日：2017-06-15

申请号：US15322294

申请日：2014-09-25

申请人： PATCHED CONICS, LLC.

发明人： Junichiro KAWAGUCHI

IPC分类号： F02K9/46 ,  F17C7/04 ,  F04B39/06 ,  F04B27/00 ,  F04B39/00

CPC分类号： F02K9/46 ,  B64G1/26 ,  B64G1/402 ,  F02K9/50 ,  F04B27/00 ,  F04B39/0005 ,  F04B39/0027 ,  F04B39/06 ,  F04F13/00 ,  F05D2220/80 ,  F17C7/04 ,  F17C2201/018 ,  F17C2201/054 ,  F17C2221/011 ,  F17C2221/012 ,  F17C2221/013 ,  F17C2221/014 ,  F17C2221/033 ,  F17C2221/035 ,  F17C2221/08 ,  F17C2223/013 ,  F17C2223/0153 ,  F17C2223/0161 ,  F17C2223/035 ,  F17C2225/0123 ,  F17C2227/0142 ,  F17C2227/0302 ,  F17C2227/0309 ,  F17C2227/0376 ,  F17C2260/02 ,  F17C2270/0197

摘要： A heat exchanger generally employs a method for supplying liquid having critical pressure or higher or high pressure in order to suppress boiling. However, gas obtained by a evaporator behind the heat exchanger has relatively low pressure, and therefore supplying the liquid to the heat exchanger requires a system for converting an energy form of the obtained gas into kinetic energy or electrical energy, and increasing the pressure by a mechanical pump. Thus, the complicated system involving an efficiency loss is only solution, and it is difficult to achieve simplification of a system or reduction in the weight of a propellant supply device in a moving body, specifically, a flying object.