专利检索 ap:("MITSUBISHI HEAVY IND LTD") AND inv:"MIHARA YORICHIKA" 第 1 页

1.

发明公开
AIRCRAFT/SPACECRAFT FLUID COOLING SYSTEM AND AIRCRAFT/SPACECRAFT FLUID COOLING DEVICE 审中-公开
标题翻译：液体冷却系统，用于飞机/飞行器飞机/太空飞行器和油冷却器

公开(公告)号：EP2693033A4

公开(公告)日：2015-01-14

申请号：EP12762853

申请日：2012-03-21

申请人： MITSUBISHI HEAVY IND LTD

发明人： KITAYAMA OSAMU , ISHIKAWA KEITARO , MIHARA YORICHIKA , AOYAMA TAICHI , NISHIMURA SHINJI

IPC分类号： F02K9/40 , B64G1/00 , B64G1/40 , F02K9/32 , F02K9/60 , F02K9/64 , F28D7/10

CPC分类号： F28F1/00 , B64G1/402 , F02C1/08 , F02C7/16 , F02C7/18 , F02C7/185 , F02C7/224 , F02K9/34 , F02K9/40 , F02K9/46 , F02K9/48 , F02K9/60 , F02K9/64 , F02K9/972 , F05D2260/20 , F28D7/106 , F28F2265/26

摘要： Provided are an aircraft/spacecraft fluid cooling system and an aircraft/spacecraft fluid cooling method in which a fluid in a pipe installed in aircraft or spacecraft can be cooled efficiently so that the amount of fluid required for cooling the fluid can be reduced. A fluid cooling system (1) includes a feed line (6) that feeds a fluid from a storage tank (4) to a pump (8), and a cooling section (26) that expands a propellant having traveled through the pump (8), feeds the propellant to the outer periphery of the feed line (6) so as to cool the propellant in the feed line (6), and discharges the expanded propellant outside.