发明名称 HELICOPTER GEARBOX AUXILIARY COOLING SYSTEM
摘要 <p>A cooling system using one or more heat pipes rotating about a central axis to transfer heat energy from one medium to another. The heat pipes are oriented within a rotating member such that the axis of the heat pipe is non-coaxial with that of a central axis of the rotating member. Centrifugal forces are used to assist the movement of the working fluid within the heat pipe. The cooling system also includes heat pipes associated with a planetary carrier assembly and supplemental heat exchangers for use in aircraft and other machinery.</p>
申请公布号 CA2828643(A1) 申请公布日期 2014.04.26
申请号 CA20132828643 申请日期 2013.09.26
申请人 BELL HELICOPTER TEXTRON INC. 发明人 MCGLAUN, MONTE A.;JACKSON, K. MYRON
分类号 B64D33/08;B64C27/12;B64D35/00;F16H57/04;F16N39/02;F28D15/02 主分类号 B64D33/08
代理机构 代理人
主权项
地址