发明名称 SELF-CENTERING STEERING MODULE AND METHOD
摘要 <p>An apparatus for steering a nosewheel on an aircraft, or the like, while the aircraft is on the ground. The apparatus includes a steering shaft that engages a cluster of gears and transfers torque from a steering command to the gears. The steering shaft is rotatable from a centered position in response to steering torque. A centering mechanism imparts a counter-torque on the cluster of gears to restore the steering shaft to the centered position when steering torque is released. The gear cluster comprises two drive gears that accurately guide the steering shaft to the centered position under the influence of the centering mechanism. The gear cluster is configured to minimize and compensate for gear wear, permitting accurate and consistent centering of the main shaft each time a steering torque is released.</p>
申请公布号 EP1545971(B1) 申请公布日期 2007.12.12
申请号 EP20020776181 申请日期 2002.10.08
申请人 TRIUMPH BRANDS INC. 发明人 DELEA, JAMES, F.;LONDON, LARRY, R.;HARTMAN, HARRY, W.
分类号 B64C25/50;B64C13/04;G05G1/08;G05G5/05 主分类号 B64C25/50
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