发明名称 Aircraft tow connector
摘要 A tow connector engageable with a nose strut of an aircraft for towing the aircraft. The connector has an arm and a base extending therefrom with spaced fingers extending from the base parallel to the arm. Each finger has an upper portion which houses a slideable shaft and a notch located at the forward end of each finger for engaging lateral studs on a nose strut of an aircraft. The shafts are slideable between the notches in the fingers and a pair of stops mounted on the base. The tow connector includes an adjustment mechanism having a pin with a head biased upwardly by a spring to protrude above the top surface of each finger adjacent to the rear end of each shaft to maintain the shafts in the forward lock position. A moveable handle is connected to a compression plate to move the heads downwardly to provide clearance to move the shafts.
申请公布号 US5129667(A) 申请公布日期 1992.07.14
申请号 US19900601457 申请日期 1990.10.22
申请人 GRATTON, RICHARD 发明人 GRATTON, RICHARD
分类号 B60D1/07;B64F1/22 主分类号 B60D1/07
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