发明名称 |
AIRCRAFT LANDING GEAR MECHANICAL POSITION INDICATOR |
摘要 |
A mechanical position indicator for providing a visual indication that a first part of an aircraft landing gear has assumed a predetermined position relative to a second part, the position indicator being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element in a deployed position, the position indicator being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator from the first state to a second state in which the indicator element is displaced from the deployed position, the position indicator being arranged to inhibit the indicator element thereafter returning to the deployed position. |
申请公布号 |
EP2643214(A1) |
申请公布日期 |
2013.10.02 |
申请号 |
EP20110785062 |
申请日期 |
2011.11.09 |
申请人 |
MESSIER-DOWTY LIMITED |
发明人 |
HODGKINSON, BEN;LACY, STUART;WEBB, CHRIS;ANSON, GARRY |
分类号 |
B64D45/00;B64C25/00 |
主分类号 |
B64D45/00 |
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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