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Rocket launching platform applicable to rockets with different models and attitudes

A rocket launch platform and an adjustable technology, which is applied in the direction of rocket launchers, weapon types, offensive equipment, etc., can solve the problem of single function of the launcher, and achieve the effect of simple switching, flexible attitude adjustment, and compact structure

Active Publication Date: 2016-12-07
TSINGHUA UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] At present, in the field of weather modification engineering, most launchers have a single function, that is, they can only adjust the launch pitch angle
In model spacecraft sports, most launchers only achieve the effect of vertically positioned launches

Method used

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  • Rocket launching platform applicable to rockets with different models and attitudes
  • Rocket launching platform applicable to rockets with different models and attitudes
  • Rocket launching platform applicable to rockets with different models and attitudes

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0017] The overall structure of a rocket model and attitude-adjustable rocket launch platform in this implementation case is as follows: figure 1 Shown, comprise launching frame 5, moving platform 27, support platform 28, fixed platform 21, support leg 20, first branch chain, second branch chain, the 3rd branch chain, the 4th branch chain, the 5th branch chain, the 5th branch chain Six branched chains, the seventh branched chain, the eighth branched chain and the ninth branched chain (the first to ninth branched chains are figure 1 I to IX in); the connection relationship of each part is: the circumference of the first branch chain I, the second branch chain II, and the third branch chain III are evenly distributed and fastened on the launch frame 5; the fourth branch chain IV, the fifth branch chain The branch chain V is respectively connected between the launch frame 5 and the support platform 28, and forms a space closed-loop mechanism with the launch frame 5 and the suppor...

Embodiment 2

[0037] The overall structure of this embodiment is as Figure 4 As shown, the difference from Example 1 lies in the structures of the first branch I, the second branch II and the third branch III.

[0038] The first branch chain I, the second branch chain II, and the third branch chain III have the same structure, such as Figure 5 As shown, all include: upper rocker 1, guide rail 02, support shaft 03, lower rocker 7, lower motor 8 and kinematic pair; the assembly relationship of the various components is: support shaft 03 and upper rocker 1 are connected by bearings Form a revolving pair, the upper end rocker 1 and the guide rail 02 and the guide rail 02 and the lower end rocker 7 are connected by pivot pins, the lower end rocker 7 and the output shaft of the lower end motor 8 are connected by a key, and the lower end motor 8 is fastened to the launch frame 5 by bolts In the motor slot above; there are 4 kinematic pairs, one is the rotating pair located between the support s...

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Abstract

The invention provides a rocket launching platform applicable to rockets with different models and attitudes, and belongs to the technical field of rocket launching devices. The rocket launching platform applicable to rockets with different models and attitudes comprises a launching framework, a movable platform, a supporting platform, a fixed platform, supporting legs, and a first branch chain to a ninth branch chain, wherein the first branch chain, the second branch chain and the third branch chain are evenly distributed on the launching framework and fastened to the launching framework in a circumferential manner, the fourth branch chain and the fifth branch chain are connected between the launching framework and the supporting platform respectively, a space closed-loop mechanism is formed by the fourth branch chain, the fifth branch chain, the launching framework and the supporting platform, the sixth branch chain is connected between the supporting platform and the movable platform, the seventh branch chain, the eighth branch chain and the ninth branch chain are connected between the movable platform and the fixed platform respectively, a space closed-loop mechanism is formed by the seventh branch chain, the eighth branch chain, the ninth branch chain, the movable platform and the fixed platform, the three supporting legs are located at the bottom of the fixed platform and are distributed circumferentially, one end of each supporting leg is fastened to the fixed platform through a bolt, and the other end of each supporting leg is fastened to the launching ground through a ground nail. The rocket launching platform applicable to rockets with different models and attitudes has the advantages of being compact in structure, high in adaptability to different working conditions, flexible in attitude adjustment, relatively easier to control and the like, and rockets of different models can be launched.

Description

technical field [0001] The invention belongs to the technical field of rocket launching devices, in particular to a rocket launching platform with adjustable rocket model and attitude. Background technique [0002] With the development of weather modification engineering and model spacecraft sports, rocket launch is no longer far away from us. Rocket launch device and launch technology have become important technologies to improve launch efficiency and affect launch effects. [0003] Artificial weather modification refers to artificially affecting the physical and chemical processes of the local atmosphere through scientific and technological means under appropriate conditions in order to avoid or mitigate meteorological disasters, rationally use climate resources, and achieve rain and snow enhancement, hail prevention, rain elimination, and fog elimination. , anti-frost and other activities. Specific to the implementation process, people load chemical reagents that affect ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 刘辛军孟齐志谢福贵罗璇
Owner TSINGHUA UNIV
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