发明名称 Aircraft e.g. tilt rotor aircraft, has position light that is provided on wing tip along with pivoting reflector
摘要 Each position light (18a) provided on the wing tip of the aircraft (11), has its base connected to the wing tip. A pivoting reflector connected to the base reflects light from a light source of the position light, in selected directions and at selected non-oscillating light intensities regardless of the orientation of the wing tip. Independent claims are also included for the following: (a) Position light for aircraft; (b) Method of modifying an aircraft to tilt rotor aircraft
申请公布号 DE10046247(A1) 申请公布日期 2002.03.28
申请号 DE20001046247 申请日期 2000.09.19
申请人 BELL HELICOPTER TEXTRON, INC. 发明人 DOYEN, FRED W.
分类号 B64C27/52;B64C29/00;B64D47/06;(IPC1-7):B64D47/06 主分类号 B64C27/52
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