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

Inactive Publication Date: 2009-07-22
ENG COLLEGE OF ENG CORPS PLA UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In addition, it is required that during the blasting process, the personnel on board should not be harmed, the structure of other parts of the aircraft and equipment on board should not be damaged, and the flight attitude of the aircraft should not be unacceptably affected.

Method used

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  • Cutting method for emergency opening lock catch of passenger plane test flight service cabin door
  • Cutting method for emergency opening lock catch of passenger plane test flight service cabin door
  • Cutting method for emergency opening lock catch of passenger plane test flight service cabin door

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Embodiment Construction

[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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Abstract

The invention discloses a cutting method for a lock catch when a service door is emergently opened during test flight of passenger plane. The method includes the followings: (1) choice of cutting position: the cutting position is chosen to be at the inner side of the lock catch close to the edge of the service door; (2) determination of incision parameters: the incision is U-shaped, and the length and the width are respectively equal to the width and depth of a U-shaped groove of the lock catch; (3) choice of cutter: a flexible cutter is used, and the cutting ability is 1.25-1.35 times of the maximum thickness among three sections of the lock catch; (4) installation of cutter: the cutter is configured to be U-shaped and tightly stuck with the surface of the inner side of the lock catch; (5) initiation of cutter: after an insensitive electric detonator receives signals of explosion initiation, a silver micro-primacord fuse is initiated, and the primacord fuse is connected with the cutter through an energy amplifier; the energy amplifier carries out initiation on the cutter and cuts off the lock catch. The cutting method of the lock catch in the invention is fast and high-efficient, thereby avoiding the defect of connection of a plurality of cutters and having the benefit for the safety of test flight staff.

Description

technical field [0001] The invention relates to a method for cutting locks when a flight test service cabin door of an airliner is opened in an emergency. Background technique [0002] According to Article 15 (4) of CCAR-21R2 "Regulations on Certification of Civil Aviation Products and Parts", "except for glider or manned balloon, the applicant shall prove that sufficient measures have been taken for each flight test so that Members of the flight test team were able to disembark and use parachutes in an emergency;  …” In order to ensure the safety of the flight test team members during the flight test of the large passenger aircraft, it is necessary to equip the flight test aircraft with an in-flight emergency opening system for the service hatch. The "system" adopts precise blasting technology, and must be able to release the emergency pressure in the cabin of the aircraft in accordance with the captain's instructions and actions when necessary, release the restraint betwe...

Claims

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Application Information

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IPC IPC(8): F42D3/00B64D25/00
Inventor 王耀华龙源刘影金广谦陆明顾月兵尤峻马海洋王兵
Owner ENG COLLEGE OF ENG CORPS PLA UNIV OF SCI & TECH
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