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
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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 |
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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