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Aircraft black box recovery method and device

A recovery method and black box technology, which is applied in the direction of aircraft black boxes, aircraft indicating devices, aircraft parts, etc., can solve the problems of limited black box recovery methods and poor recovery effects, and achieve easy separation, avoid electronic circuits or mechanical structures, detonation The effect of simple conditions

Active Publication Date: 2019-07-16
ZHONGBEI UNIV
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the deficiencies in the prior art, the present invention provides a recovery method of the aircraft black box and an aircraft black box recovery device, which adopts the method of timing blasting and exploding bolts to separate from the mother body and the airbag landing method, which can solve the problem of limited black box recovery methods in the current aircraft development process. Problems such as poor recycling effect

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  • Aircraft black box recovery method and device

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Embodiment Construction

[0023] The present invention will be further described below in conjunction with drawings and embodiments.

[0024] The invention provides a method for reclaiming an aircraft black box, comprising the following steps:

[0025] (1) Use explosive bolts to install the black box protective shell on the aircraft, and the black box is located inside the black box protective shell;

[0026] (2) The aircraft takes off after receiving the ignition command, the black box is powered on and starts to record data, and the timer in the protective shell of the black box starts timing;

[0027] (3) The aircraft transfers from the level flight stage to the re-entry stage. Before the final stage of re-entry begins to land, the black box completes the data recording, and the timer outputs the timing detonation signal to the tiny explosive device next to the explosion bolt, and the tiny explosive device receives the timing detonation signal. After the explosion, the explosion bolt is opened, and...

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PUM

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Abstract

The invention provides an aircraft black box recovery method. A black box is mounted and fixed on an aircraft by explosive bolts, an ignition command of the aircraft is used as the starting timing condition, a timer outputs an explosion signal when the preset time is reached to make a tiny explosive device to explode the explosive bolts, the black box is disengaged from the aircraft, at the same time the timer restarts, and after reaching the preset time, airbags open to decelerate. The invention simultaneously provides an aircraft black box recovery device, which comprises a black box protective shell, the main air bag, the small air bag, an air bag box, the explosive bolts, the timer, a control chip, an igniter, nitrogen solid ions, and the like. The mode that the black box is disengagedfrom a mother body by timing explosion of the explosive bolts and lands through the air bags is adopted, and the problems of limited recovery method and poor recovery effect of the black box in the current aircraft development process can be solved.

Description

technical field [0001] The invention relates to a recovery method of an aircraft black box and an aircraft black box recovery device, which belong to the technical field of aircraft testing of aerospace, aviation and weapons. Background technique [0002] In the process of aircraft development, the records of its own dynamic information and environmental information during its launch and flight are indispensable. The black box that realizes this function must be installed on the aircraft, and the test data of the aircraft is stored in real time during the flight test until the aircraft falls. Since the falling speed of the aircraft is extremely fast and can even reach the supersonic speed of several Machs, a huge impact force will be generated during the collision with the ground. For this reason, a special protection design must be carried out on the black box to ensure reliable recovery of recorded data. [0003] The current protection design mainly focuses on the vibrat...

Claims

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Application Information

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IPC IPC(8): B64D45/00B64F5/60
CPCB64D45/00B64F5/60B64D2045/0065Y02P70/50
Inventor 张彦军陈良昌
Owner ZHONGBEI UNIV
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