发明名称 |
Actuator for aircraft stabilizers with a failure responsive lock control mechanism |
摘要 |
A horizontal stabilizer actuator 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.
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申请公布号 |
US6672540(B1) |
申请公布日期 |
2004.01.06 |
申请号 |
US20020308527 |
申请日期 |
2002.12.03 |
申请人 |
ROCKWELL COLLINS, INC. |
发明人 |
SHAHEEN MILAD A.;DREHER ROBERT V. |
分类号 |
B64C13/28;F16H25/22;F16H25/24;F16H61/12;(IPC1-7):B64D13/38 |
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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