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Launch vehicle line type bundling separation device

A separation device and carrier rocket technology, which is applied to the docking device of space navigation aircraft, the propulsion system device of space navigation aircraft, etc., can solve problems such as stress concentration, and achieve the effects of increasing carrying capacity, reducing self-weight and low impact

Inactive Publication Date: 2018-01-16
DALIAN UNIV OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0009] In order to solve the stress concentration problem caused by the point-type connection structure of the bundled rocket, the present invention proposes a wire-type bundled separation device based on the separation plate expansion tube, which can solve the stress concentration caused by the thrust being transmitted from the booster to the core stage through the point connection structure problems, and then significantly reduce the weight of the rocket, increase the rocket's carrying capacity, and at the same time increase the separation reliability and safety

Method used

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  • Launch vehicle line type bundling separation device
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  • Launch vehicle line type bundling separation device

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Embodiment Construction

[0027] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0028] See attached figure 1 , the present invention binds and connects the inter-box section of the core stage with the oblique cone of the booster, forming a plate structure that is placed along the axis of the rocket with an overall approximate "I" cross-section. The present invention includes four groups of structures, and each group of structures is composed of four "I"-shaped square plates. Among them, each group of structures connects the inter-box section 1 of the rocket core stage and the oblique cone section of the booster, and the four groups of structures closely connect the four boosters with the core stage.

[0029] See attached figure 2 And attached Figure 4 , each "I"-shaped square plate includes a first connecting plate 3-1, a second connecting plate 3-2, two separating plates 3-3, a metal flat tube 3-4, a filler 3-5 and a guide Blast 3-6.

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Abstract

A launch vehicle line type bundling separation device belongs to the field of aerospace structure design. The launch vehicle line type bundling separation device is of a plate structure arranged in the axis direction of a vehicle by taking a separation plate type expansion pipe as a separation system, and the entirety of the bundling separation device is similar to an I-shaped section; the bundling separation device comprises four groups of bundling separation structures, inter-tank sections connected to central stages of the vehicle, and oblique nose cones of boosters. Each group of the bundling separation structures are composed of four I-shaped square plates, and each I-shaped square plate comprises two connecting plates, two separating plates, a metal flat pipe, fillers and a detonating fuse; the metal flat pipe is located between the two connecting plates, and the fillers are placed in the metal flat pipe; the detonating fuse is arranged in the fillers, and used for providing energy during separation; and the two separation plates are used for connecting the ends of web plates on both sides of the two connecting plates. The bundling separation device provided by the inventionhas the advantages of uniform force transmission, weight reduction, improvement of carrying capacity of the vehicle, high bearing capacity and separation reliability, no pollution and small impact during separation.

Description

technical field [0001] The invention belongs to the field of aerospace structure design and manufacture, relates to the field of force transmission structure design between a bundled launch vehicle core stage and a booster, and particularly relates to the field of engineering structure optimization. Background technique [0002] In order to meet the requirements of launching different types of satellites, spacecraft, orbiters, interstellar probes and other spacecraft, it is necessary to develop vehicles with different carrying capabilities. In order to shorten the development cycle and reduce the development cost, the vehicle that combines the existing different thrust vehicles according to the requirements becomes the first choice for spacecraft design. At present, the combined connection method between carriers generally adopts "vertical plus level, horizontal bundling". This solution is based on the original carrier, vertically combining two to three-stage carriers into ...

Claims

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Application Information

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IPC IPC(8): B64G1/40B64G1/64
Inventor 王博王立朋陈炳全毕祥军蒋亮亮吴浩刘观日
Owner DALIAN UNIV OF TECH
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