发明名称 Active cable-cutting assembly for aircraft
摘要 An active, automatic-firing, impact responsive cable-cutting apparatus for use on conventional aircraft such as helicopters for virtually instantaneously forcibly severing obstructive cables. A lightweight, non-corrosive frame comprising a mounting base portion and an integral, outwardly extending, angular deflection arm is adapted to be selectively mounted on an aircraft or on an extension pole which extends downwardly toward the ground or forward of the nose of the aircraft. Mechanical firing components of the assembly are housed within a cylindrical sleeve adapted to be accessed for maintenance through a removable butt. Sharpened, serrated guide blades extending along outwardly angled forward edges of the frame are adapted to strain the outer periphery of a cable as it is forcibly deflected and guided into a central mouth. A removable cutting block is provided at the interior of the apparatus adjacent the cutting assembly mouth in operative association with a rigid, angular, cutter knife. The pivotally mounted cutter knife may be selectively tensioned and operationally defines a cutting angle suitable to engage cables of a wide range of thicknesses. Impacted cables are forcibly severed when the cutter knife is lowered adjacent to the surface of the cutting block in response to activation of an associated firing mechanism, which virtually instantaneously detonates the cutting jaws to sever the offensive cable in a scissors-like motion. Alternative embodiments include a semi-automatic self loading version having an operative cartridge magazine, and a winged version adapted to be mounted upon a rigid extension pole or cable for offensive cable removal.
申请公布号 US4826103(A) 申请公布日期 1989.05.02
申请号 US19870043683 申请日期 1987.04.28
申请人 CUSTOM AIR, INC. 发明人 MCKOWN, JAMES M.
分类号 B60R19/54;B64C27/00;B64D45/00;(IPC1-7):B64D45/00 主分类号 B60R19/54
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