发明名称 Improved thermal beacon assembly.
摘要 <p>An improved beacon assembly 30 for use with a beacon 34 for providing radiant energy. The invention 30 includes a single plate 32 having an open interior to provide a frame through which the radiant energy from said beacon 34 may pass and apparatus 36 for mounting the plate 32 and the beacon 34 to the missile 10. In a more specific embodiment, the plate 32 is constructed of aluminum and has arcuate inner 42 and outer 44 peripheries connected by substantially straight sections 46 and 48 to provide a pie shape with a pie shaped piece removed from the small end thereof to provide a frame through which the radiant energy from the beacon 34 may pass. The imp roved beacon assembly of the present invention 30 affords a low cost lightweight retrofit of existing missiles with a thermal beacon 34.</p>
申请公布号 EP0418034(A2) 申请公布日期 1991.03.20
申请号 EP19900309940 申请日期 1990.09.11
申请人 HUGHES AIRCRAFT COMPANY 发明人 GREENE, SIDNEY R.
分类号 F41F3/04;F41G7/30;F41G7/32;F42B15/04;G01S1/70;G01S17/66;G02B5/00 主分类号 F41F3/04
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