发明名称 |
ADAPTIVE TRAILING EDGE ACTUATOR SYSTEM AND METHOD |
摘要 |
<p>An adaptive trailing edge system for an aircraft may include an adaptive trailing edge element mounted to a trailing edge. An electric motor actuator having an electric motor may be configured to actuate the adaptive trailing edge element. A linkage system may couple the electric motor actuator to the adaptive trailing edge element for actuation thereof.</p> |
申请公布号 |
CA2857892(A1) |
申请公布日期 |
2015.03.24 |
申请号 |
CA20142857892 |
申请日期 |
2014.07.28 |
申请人 |
THE BOEING COMPANY |
发明人 |
MOSER, MATTHEW A.;FINN, MICHAEL R. |
分类号 |
B64C13/50;B64C3/50;B64C13/30 |
主分类号 |
B64C13/50 |
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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