发明名称 RECOGNITION/ANTI-COLLISION LIGHT FOR AIRCRAFT
摘要 A recognition light includes a reflector having an axis and first and second annular semi-parabolic reflective surfaces (40, 42) which have respective focal points axially spaced apart from one another, and first and second annular lamps (34, 36) respectively disposed at the focal points. A cover (14) surrounds the reflector and lamps and includes a lens (20) for focusing the light along a plane perpendicular to the axis of the reflector, the lens including first and second Fresnel lens portions each including a convex lens and a prism lens, the convex lenses being disposed adjacent one another and transaxially aligned with the first and second lamps, respectively. A light detector detects light emitted from at least one of the lamps, a monitor circuit provides a fail signal when a characteristic of the light output of at least one of the lamps does not satisfy a specified criteria, and a control circuit first activates the first lamp and then the second lamp in response to receipt of the fail signal of the monitor circuit.
申请公布号 CA2349601(C) 申请公布日期 2008.03.18
申请号 CA19992349601 申请日期 1999.11.05
申请人 GODFREY ENGINEERING, INC. 发明人 DRAVES, RAYMOND HENRY;DEMARCO, RALPH ANTHONY;KNIGHT, TODD CHRISTOPHER;KIELBON, TIMOTHY SCOTT;PATEL, ANISH VIKRAM;STEPHENS, MERLE KEITH
分类号 B64D47/06;B60Q1/26;F21V7/00;F21V13/04 主分类号 B64D47/06
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