Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

An air-to-air missile recovery hatch cover

A technology of air-to-air missiles and recovery cabins, which is applied in the direction of self-propelled missiles, jet propulsion devices, rocket engine devices, etc., to achieve the effect of saving recovery and reliable connection

Active Publication Date: 2014-11-12
CHINA AIR TO AIR MISSILE INST
View PDF0 Cites 8 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The collection system must be small and efficient

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • An air-to-air missile recovery hatch cover
  • An air-to-air missile recovery hatch cover
  • An air-to-air missile recovery hatch cover

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0018] Below in conjunction with the accompanying drawings the present invention will be described in detail, please refer to the accompanying drawings 1 to 3.

[0023] During implementation, the inner and outer surfaces of the hatch cover substrate 1 are arc surfaces of 80° to 90°, preferably 87°.

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention belongs to air-to-air missile recovery technology, and relates to a hatch cover of an air-to-air missile recovery compartment, which includes a hatch cover substrate [1], a B-type hook [2], an explosion bolt connection seat [4], a hatch cover substrate [1] and a missile bomb The body has the same arc surface, the explosive bolt connection seat [4] is located on the inner arc surface of the hatch cover base plate [1] near the end of the missile head, and the Type B hook [2] is located on the inner arc surface of the hatch cover base plate [1]. Near one end of the missile tail, a drogue parachute suspension point [3] is arranged between the Type B grab [2] and the explosion bolt connection seat [4]. The invention realizes the reliable connection between the hatch cover and the projectile body with a simple hatch cover form, saves the space of the recovery cabin, and provides a larger installation space for the recovery umbrella system; the hatch cover forms an effective windward section, so that the hatch cover can Under the joint action of the power and the thrust of the explosive bolt, the guiding parachute is quickly taken away from the missile body, avoiding the structure of the airfoil and rudder surface of the missile body, and an effective parachute opening channel is formed.

Description

A kind of air-to-air missile recovery compartment hatch technical field [0001] The invention belongs to air-to-air missile recovery technology, relating to a kind of air-to-air missile recovery compartment hatch. Background technique The air-to-air missile that breaks down in the test or the air-to-air missile that has completed the air flight test task has extremely high The value of scientific research, which can be obtained through recycling technology can provide physical evidence and a fault reproduction platform for technical research, shortening the research and development time. production cycle and reduce development costs. Recovery technology has been widely used in fields such as spacecraft recovery, intercontinental ballistic missile development and aircraft recovery. There are cases of successful application inside and outside. The recovery systems equipped with these products mostly use compound deceleration methods to complete the recovery tasks. Such...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): F02K9/34F42B15/00
Inventor 张磊鸣高先锋
Owner CHINA AIR TO AIR MISSILE INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products