发明名称 |
SYSTEME DE COMMANDE ELECTRIQUE POUR UNE GOUVERNE DE DIRECTION D'UN AVION |
摘要 |
<p>The system (1) has a rudder bar (5) activated by a pilot of an aircraft and associated to a transducer (6), which provides a flight order representing the action of the pilot on the bar. A calculation unit (7) determines a deflection command permitting to bring a rudder (2) to a position located between two displacement limits. An actuator (9) displaces the rudder based on the deflection command. An information source assembly (11) generates current values of flight parameters. A varying unit (12) varies the limits based on the current values before transmitting the limits to the unit (7).</p> |
申请公布号 |
CA2640521(A1) |
申请公布日期 |
2007.08.30 |
申请号 |
CA20072640521 |
申请日期 |
2007.02.19 |
申请人 |
AIRBUS FRANCE;AIRBUS |
发明人 |
ROUGELOT, CHRISTOPHE;RONCERAY, DIDIER |
分类号 |
B64C13/50 |
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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