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Vehicle-umbrella separating mechanism for initiating explosive release

A separation mechanism and pyrotechnic technology, applied in the directions of parachutes, aircraft parts, transportation and packaging, etc., can solve the problems of difficult direction control and damage, and achieve the effects of high reliability, safe and reliable structure, and small size.

Pending Publication Date: 2017-10-10
NO 60 RES INST OF GENERAL STAFF DEPT PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The parachute recovery system has been used on target drones and some UAVs for a long time. The disadvantage of the general parachute recovery is that it is difficult to control the direction after the parachute is opened.
Where a drone lands with a parachute, variable surface winds or high terrain can drag the aircraft along the ground, causing damage

Method used

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  • Vehicle-umbrella separating mechanism for initiating explosive release

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Embodiment Construction

[0010] This embodiment provides an aircraft umbrella separation mechanism for pyrotechnic release, the structure of which is as follows: figure 1 As shown, it includes a first dropout joint 1, a second dropout joint 5, a piston 3, an ignition head 4, a steel ball 6, a limit wire 7 and a compression spring 8, the first dropout joint is connected with the main umbrella belt through a dropout pin 2, and the second The second dropout joint is connected with the fuselage through the dropout pin; the lower end of the first dropout joint is provided with a protruding end, and a cavity for installing the piston is arranged in the protruding end, and a penetrating steel ball receiving hole is provided on the inner wall of the cavity, and the bottom of the piston There is an ignition head, and a limit wire is set on the top of the piston. The limit wire is an aluminum wire, and the diameter of the limit aluminum wire is not less than 2.5mm. The knot 5 is provided with a groove for inser...

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Abstract

The invention discloses a vehicle-umbrella separating mechanism for initiating explosive release. The mechanism is mainly applied to vehicle-umbrella separating in the recovery process of a fixed-wing unmanned aerial vehicle. A piston in a cavity can be pushed to act through the chemical energy produced by explosion of an initiating explosive device, a limiting aluminum wire is cut off, a steel ball is released, and disengagement and separation of two connectors are achieved. The vehicle-umbrella separating mechanism of the unmanned aerial vehicle has the advantages of being small in size, simple in control mode and high in reliability.

Description

technical field [0001] The present invention relates to an executive mechanism of an unmanned aerial vehicle, specifically an umbrella separation mechanism released by pyrotechnics, which mainly applies the separation of the umbrella during the recovery process of the fixed-wing unmanned aerial vehicle, and controls the unmanned aerial vehicle manually or by sensors The parachute is separated. Background technique [0002] The parachute recovery system has been used on target drones and some UAVs for a long time. The general disadvantage of parachute recovery is that it is difficult to control the direction after the parachute is opened. Where a drone lands with a parachute, variable surface winds or high terrain can drag the aircraft along the ground, causing damage. Therefore, the current method is to separate the parachute once the plane lands to ensure the safety of the plane after landing, so a parachute separation mechanism is very necessary for the parachute recovery...

Claims

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Application Information

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IPC IPC(8): B64D17/80
CPCB64D17/80
Inventor 戴勇夏杨陈刚廖武华蔡勘勘
Owner NO 60 RES INST OF GENERAL STAFF DEPT PLA
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