Cutting method for emergency opening lock catch of passenger plane test flight service cabin door
A cutting method and emergency opening technology, which is applied in the field of cutting locks during the emergency opening of passenger aircraft flight test service doors, can solve the problems of not being able to injure people on board, not being affected by the flight attitude of the aircraft, and not being able to damage the aircraft structure and on-board equipment, etc., to achieve The effect of reducing the amount of explosives
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[0025] The present invention will be further explained below in conjunction with the accompanying drawings.
[0026] The cutting location was chosen to be on the inside of the latch close to the edge of the service door. The groove depth of the locking U-shaped groove at this place is 19.2mm, and the groove width is 26.1mm; the thicknesses of the lower wing plate, web plate and upper wing plate of the U-shaped groove are 6mm, 4.75mm, and 2.5mm respectively.
[0027] Cutting parameters: such as figure 1 and figure 2 As shown, the length a and width b of the slit are equal to the width and depth of the locking groove respectively; the depths of the slits c1, c2 and c3 are respectively equal to the three wall thicknesses of the U-shaped groove; d is the width of the slit, which is determined by appropriate The selected cutter is determined, where d is 1mm.
[0028] The cutter adopts a flexible energy-concentrating cutter with lead-antimony alloy as the drug-type cover and she...
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