发明名称 Helicopter cargo hook.
摘要 <p>A releasable self-resetting cargo hook for helicopters and other aircraft for supporting suspended loads. The cargo hook apparatus includes a pivotally supported load arm (78) maintained in its load supporting condition by a pivotally mounted latch arm (100) whose position, in turn, is controlled by a pivotally mounted latch (120). The position of the latch (120) is determined by a pivotally mounted lock arm lever (142) whose normal position is determined by a stop pin (156) and which is operated by a release mechanism (146). The interconnection between the latch (120) and lock arm lever (142) is through a cam slot (132) defined on the latch (120) receiving a lock arm lever follower (150), and the cam slot-follower relationship prevents impact forces imposed on the cargo hook structure from inadvertently producing lock arm lever rotation and latch movement.</p>
申请公布号 EP0245927(A2) 申请公布日期 1987.11.19
申请号 EP19870302178 申请日期 1987.03.13
申请人 AEROQUIP AG 发明人 SMITH, DONALD E.;HAUNHORST, GREG A.
分类号 B64D1/04;B64D1/22;B64D9/00;B66C1/34;F16B45/02;(IPC1-7):B66C1/34 主分类号 B64D1/04
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