发明名称 RADOME FOR AIRFRAME
摘要 PROBLEM TO BE SOLVED: To contrive to restrain temperature rise of a bonding part of a ceramic radome and a radome ring and protect falling off of the ceramic radome by prohibiting heat conduction from the ceramic radome through aerodynamic heating. SOLUTION: The radom 4 for an airframe 1 flying toward a dedicated target comprises an abrasion material 14 that is provided on the surface of the radom 4 and out a range of radio wave beams that an antenna 2 of the airframe 1 transmits and receives, restraining temperature rise of the radome 4 by thermal decomposition of itself to form a protection boundary layer 13 during flying of the airframe 1.
申请公布号 JP2000213899(A) 申请公布日期 2000.08.02
申请号 JP19990017148 申请日期 1999.01.26
申请人 MITSUBISHI ELECTRIC CORP 发明人 YAMAGUCHI SHUJI;TSUKIDATE RIYUUJI
分类号 F42B15/34;H01Q1/42;(IPC1-7):F42B15/34 主分类号 F42B15/34
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