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Guided missile and engine cabin segment missile body thereof

A technology for engine compartments and projectiles, which is applied to projectiles, self-propelled projectiles, offensive equipment, etc., can solve problems such as insufficient cable installation space, and achieve the effect of reducing production requirements

Active Publication Date: 2015-03-11
CHINA AIR TO AIR MISSILE INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The object of the present invention is to provide a kind of engine compartment projectile, to solve the problem in the prior art that the cable installation space is insufficient due to the space occupied by the fixed plate; the purpose of the present invention is also to provide a body missile

Method used

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  • Guided missile and engine cabin segment missile body thereof
  • Guided missile and engine cabin segment missile body thereof

Examples

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Embodiment Construction

[0015] An example of a missile figure 2 Shown: including the cable fairing and the guidance and fuze cabin section missile body, the engine cabin section missile body 10 and the steering gear intersection missile body arranged in front and rear order, the cable fairing is arranged on the periphery of the engine cabin section missile body, and the engine cabin section missile body The body includes an engine compartment section body extending axially along the front-to-back direction and a fixed piece fixed on its outer peripheral surface. The fixed piece includes a left fixed piece 9 and a right fixed piece 5 which are arranged separately and arranged at intervals from left to right. The left and right fixed pieces The outer peripheral surface of the engine compartment section body between the opposite sides of the engine compartment and the left and right fixed pieces surrounds a wiring groove 11 for the corresponding cables to be laid along the front and rear directions. Th...

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Abstract

The invention relates to a guided missile and an engine cabin segment missile body thereof. The engine cabin segment missile body comprises an engine cabin segment body which extends axially along a frontward / backward direction, and fixing sheets which are fixedly arranged on the peripheral face of the engine cabin segment body, wherein the fixing sheets comprise a left fixing sheet and a right fixing sheet which are arranged separately at a certain interval on left and right sides; the opposite side faces of the left fixing sheet and the right fixing sheet and the peripheral face of the engine cabin segment body between the left fixing sheet and the right fixing sheet define a wiring groove for distributing a corresponding cable along the frontward / backward direction. By adopting the guided missile and the engine cabin segment missile body thereof, the problem of insufficient cable installation space since a certain space is occupied by the fixing sheets in the prior art is solved.

Description

technical field [0001] The invention relates to a guided missile and an engine compartment missile body thereof. Background technique [0002] Existing air-to-air missiles such as figure 1 Shown: including the cable fairing and the missile body of the guidance and fuze compartment, the missile body of the engine compartment 4 and the missile body of the steering gear section arranged in front and rear order, and there is no structure between the missile body of the steering gear interval section and the missile body of the guidance fuse cabin section Connection, between the missile body of the steering gear and the missile body of the guidance and fuze cabin, it is necessary to realize the electrical connection through cables. In order to realize the installation of the cable fairing, the outer wall of the engine compartment projectile is fixed with a left hanging piece 1 and a right hanging piece, and a cable is formed between the left and right hanging piece and the engin...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/00
Inventor 翟磊董景渲张菁牛绿伟张鹏
Owner CHINA AIR TO AIR MISSILE INST
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