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Protective cover mechanism of separation socket

A technology of shedding sockets and protective covers, which is applied in the structural field of aviation missile systems, can solve problems such as limited installation space, complicated implementation methods, and inapplicable structural forms, and achieve the effect of avoiding excessive friction

Active Publication Date: 2016-01-13
BEIJING AUTOMATION CONTROL EQUIP INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

And for the miniature guided missile that the body is a square, because the upper surface of the body is a plane, the installation space is limited, the existing structural form cannot be applied, and the opening angle of 180° is to be achieved in a way that is better than that on a cylindrical body. complex

Method used

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  • Protective cover mechanism of separation socket
  • Protective cover mechanism of separation socket
  • Protective cover mechanism of separation socket

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Embodiment Construction

[0035] The technical solutions of the present invention will be further described in detail below through specific examples.

[0036] In this embodiment, the cross-section of a missile projectile body is a square of 230 mm × 190 mm, a shedding socket protective cover mechanism, after the missile is launched and separated, the shedding plug on the launch carrier is separated from the shedding socket on the projectile body, and the The fall-off socket protection cover mechanism automatically rebounds to protect the fall-off socket; the fall-off socket protection cover mechanism is fixed on the body through two mounting holes with a diameter of 2.8 mm on the bracket 8; it also includes a first-stage torsion spring group 100 And the second stage torsion spring group 200; specifically as figure 1 and figure 2 shown;

[0037] 1. The first stage torsion spring group 100

[0038] The first-stage torsion spring group 100 consists of the socket cover 1, the first-stage torsion sprin...

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Abstract

The invention, which belongs to the field of the cruise missile system structure, relates to a protective cover mechanism of a separation socket, wherein the protective cover mechanism is suitable for protecting a separation socket on a cruise missile with a small size and a planar upper surface of the cruise missile body. After emission and separation of a missile, a separation plug arranged on an emission carrier is separated from a separation socket of a missile body; and automatic springback of the protective cover mechanism is carried out and thus the separation socket is protected. The protective cover mechanism is fixed on the missile body by mounting holes of a support (8). Besides, the protective cover mechanism includes a first-level torsional spring set (100) and a second-level torsional spring set (200). According to the technical scheme, the single-fan-shaped protective cover mechanism with the largest starting angle of 170 degrees is provided and is applied to a cruise missile with a small size and a planar upper surface of the cruise missile body to protec the separation socket.

Description

technical field [0001] The invention belongs to the field of aerial missile system structure, and relates to a shedding socket protective cover mechanism, which is suitable for protecting the shedding socket on the airborne missile whose upper surface of the projectile body is flat and has a small volume. Background technique [0002] Before the launch of the flying missile, the shedding plug on the launch carrier and the shedding socket on the projectile body need to maintain an electrical connection state, maintain the launch carrier to supply power to the missile, and maintain signal transmission between the two. At the moment of missile launch, the launcher ejection mechanism separates the missile body from the launch carrier, and simultaneously separates the shedding socket from the plug. After the missile is separated, there is a need for a shedding socket protective cover mechanism that can realize the automatic rebound function and play the role of protecting the she...

Claims

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Application Information

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IPC IPC(8): H01R13/508
Inventor 晏升辉程鹏
Owner BEIJING AUTOMATION CONTROL EQUIP INST
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