发明名称 |
ELECTRONICALLY CONTROLLED AIRCRAFT RETRACTABLE LANDING LIGHT WITH MANUAL REFRACTION CAPABILITY |
摘要 |
An electronically controlled retractable landing light (100) for use with aircraft. A controller (106) compares the commanded position of a lighthead (108) by means of a contactless absolute position sensor (212).Operation of a brake (111), motor (110), and lamp (112) is controlled by a control unit (210). Electrical power to the brake (111), motor (110), and lamp (112) is slowly applied and removed to reduce electromagnetic emissions and extend the service life of a power stage (208), brake (111), motor (110), and lamp (112). The lighthead (108) may be manually stowed in the event of a fault.
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申请公布号 |
WO03050002(A1) |
申请公布日期 |
2003.06.19 |
申请号 |
WO2002US37472 |
申请日期 |
2002.11.21 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
BARNHART, BRIAN, J.;MUBASLAT, SAED, M.;HAMILTON, SCOTT, E.;GIFFEN, CRAIG, E. |
分类号 |
B60Q11/00;B64D47/04;(IPC1-7):B64D47/04 |
主分类号 |
B60Q11/00 |
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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