发明名称 LEVERAGE ACTIVATED AIRCRAFT TOW BAR
摘要 <p>This invention relates to aircraft tow bars. Previously, no tow bar enabled a user to transfer one's weight into lateral motion of the tow bar in order to tow the aircraft. Embodiments of the present invention use an arm member (12) having a handle (22) on a first end and a yoke (24) on a second end. The yoke is configured to detachably couple to an aircraft nose gear. A leg member (16) has a first end pivotably mounted to the arm member. A base unit (14) is mounted to a second end of the leg member. The leg member is pivotably adjusted to two positions for allowing a downward force applied to the handle to translate to a corresponding force exerted on the nose gear sufficient to either pull or push the aircraft.</p>
申请公布号 WO2015058217(A1) 申请公布日期 2015.04.23
申请号 WO2014US69917 申请日期 2014.12.12
申请人 GUIDA, NICHOLAS 发明人 GUIDA, NICHOLAS
分类号 B64F1/22 主分类号 B64F1/22
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