发明名称 |
EXHAUST HEAT SYSTEM FOR AIRCRAFT AND EXHAUST HEAT METHOD FOR AIRCRAFT |
摘要 |
<P>PROBLEM TO BE SOLVED: To provide an exhaust heat system for aircraft that can effectively exhaust heat generated in an actuator without deteriorating the performance of the actuator for steering in an aircraft. <P>SOLUTION: The exhaust heat system for aircraft is mounted on the aircraft which has at least one of an auxiliary power generator and an engine. The exhaust heat system for aircraft includes a radiator and a heat transmission part. The radiator is disposed on a channel of air flowing into at least one of the auxiliary power generator and the engine or on a branched path from the channel. The heat transmission part transmits the heat generated on the actuator for steering of the aircraft to the radiator. <P>COPYRIGHT: (C)2013,JPO&INPIT |
申请公布号 |
JP2013103698(A) |
申请公布日期 |
2013.05.30 |
申请号 |
JP20110251013 |
申请日期 |
2011.11.16 |
申请人 |
FUJI HEAVY IND LTD |
发明人 |
HITOMI ATSUSHI;SASAKI TORU;MURATA IWAO |
分类号 |
B64D47/00;B64C13/38;B64D33/02;F28F27/00 |
主分类号 |
B64D47/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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