发明名称 |
Stabilization system for aircraft subjected to gust loading has yaw sensor in cockpit connected to regulator and frequency measurement circuits with connections to ailerons and spoilers on wing |
摘要 |
<p>A sensor (27) in the cockpit measures the yawing motion produced by sideways gusts of wind (29) hitting the fin and rudder (38) of the aircraft (22). The yaw signals (31) are transmitted directly to a regulator circuit (33) and a frequency measurement circuit (34). The frequency measurement circuit is connected to the regulator circuit. The regulator circuit in turn sends a feedback control signal (36) to aerodynamic control surfaces (40) especially ailerons (39) and spoilers (37) on the wings (26).</p> |
申请公布号 |
DE102004029194(A1) |
申请公布日期 |
2006.01.26 |
申请号 |
DE20041029194 |
申请日期 |
2004.06.16 |
申请人 |
AIRBUS DEUTSCHLAND GMBH |
发明人 |
ENZINGER, MICHAEL;KORDT, MICHAEL |
分类号 |
B64C13/16 |
主分类号 |
B64C13/16 |
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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