发明名称 |
Aircraft engine thrust demand unit controller |
摘要 |
<p>The control has a fixed support for a movable lever which is coupled to an output for transmitting signals proportional to displacement of the lever w.r.t. the support. A recirculating ball-screw drive includes a lead-screw (3) and a ball nut (4) engaged on the screw. - One of the screw and nut is coupled to the lever, and linearly movable with it w.r.t. the other of the screw and nut. An output stepping motor (10) is coupled to the ball-screw assembly for relative rotation of the stator (6) and rotor (5) accompanied by relative rotation of the nut and screw.</p> |
申请公布号 |
ES8604460(A1) |
申请公布日期 |
1986.07.01 |
申请号 |
ES19650005349 |
申请日期 |
1984.08.08 |
申请人 |
BRITISH AEROSPACE PUBLIC LIMITED COMPANY |
发明人 |
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分类号 |
F02D11/10;B64C13/46;B64D31/04;F02D9/02;F16H25/22;G05G7/02;(IPC1-7):B64D31/04 |
主分类号 |
F02D11/10 |
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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