发明名称 |
Actuator for aircraft stabilizers with a failure responsive lock control mechanism |
摘要 |
<p>A horizontal stabilizer actuator (10) for a winged aircraft which is selectively pivotally controlled by a pilot or operator at a remote location in the aircraft and which has a primary load path responsive to the selective control by the pilot or operator for setting the pivoted position of the stabilizer and which has a secondary load path which is responsive to a failure in the primary load path to be automatically actuated to a condition locking the stabilizer in a fixed position. <IMAGE></p> |
申请公布号 |
EP1426290(B1) |
申请公布日期 |
2007.05.23 |
申请号 |
EP20030257589 |
申请日期 |
2003.12.02 |
申请人 |
ROCKWELL COLLINS, INC. |
发明人 |
SHAHEEN, MILAD A.;DREHER, ROBERT V. |
分类号 |
B64C13/28;F16H25/00;F16H25/22;F16H25/24;F16H61/12 |
主分类号 |
B64C13/28 |
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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