发明名称 |
INTERNALLY LOCKING ACTUATOR WITH DIRECT ACTING INTEGRAL LOCKSENSOR |
摘要 |
<p>The present invention provides a lock sensor for use in an actuator such as is used in aircraft landing gear systems. The lock sensor comprises at least one field emitting device (46) mounted on a locking actuator pressure vessel where the field emitting device (46) monitors the position of at least one target (48). The field emitting device (46) emits a field that when breached by the target sends a signal to indicate that the actuator is in a locked state.</p> |
申请公布号 |
CA2479454(A1) |
申请公布日期 |
2006.02.28 |
申请号 |
CA20042479454 |
申请日期 |
2004.08.30 |
申请人 |
ATAMAN, GARY STEPHEN;COFFIN, MARK |
发明人 |
ATAMAN, GARY STEPHEN;COFFIN, MARK |
分类号 |
F15B15/26;B64C25/00;F15B21/08;F16F9/56;G01N7/00 |
主分类号 |
F15B15/26 |
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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