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Unmanned flying object pushing assisting structure and unmanned flying object launcher

A flying object and boosting technology, which is applied in the direction of launching/dragging transmissions, etc., can solve the problems of uncertain flight of flying objects, adverse effects of flying objects, instability, etc.

Active Publication Date: 2021-05-14
成都云鼎智控科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] After the rocket is boosted to take off, the rocket will still boost the flying object for a period of time, but in the traditional boosting method, when the fuel of the rocket is exhausted, the rocket and the parts supporting the flying object will not be separated from the flying object immediately, but It will fly with the flying object for a period of time, but because the rocket and the parts supporting the flying object are not designed for flight, the state of the rocket and the flying object will cause uncertain and unstable factors to the flight of the flying object , adversely affect the flying state of the flying object

Method used

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Embodiment Construction

[0028] The present invention will be clearly and completely described below in conjunction with the accompanying drawings. Those skilled in the art will be able to implement the present invention based on these descriptions. Before the present invention is described in conjunction with the accompanying drawings, it should be pointed out that:

[0029] The technical solutions and technical features provided in each part of the present invention, including the following description, can be combined with each other under the condition of no conflict.

[0030] In addition, the embodiments of the present invention referred to in the following description are generally only a part of the embodiments of the present invention, rather than all the embodiments. Therefore, based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

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Abstract

The invention relates to flying object launching, in particular to an unmanned flying object pushing assisting structure and an unmanned flying object launcher, and the unmanned flying object pushing assisting structure comprises a pushing assisting rod, one end of the pushing assisting rod is used for being connected with the front end of a rocket for assisting pushing of an unmanned flying object, and the other end of the pushing assisting rod is used for abutting against the unmanned flying object; the pushing assisting rod is of a hollow tubular structure, an elastic mechanism is arranged in an inner cavity of the boosting rod, and the elastic mechanism is used for being in a compressed state before the rocket boosts the unmanned flying object to take off, when the rocket takes off or in the flying process and starts to recover in the flying process of the unmanned flying object. After the elastic mechanism recovers or in the recovery process, the boosting rod is pushed away from the unmanned flying object and separated from the unmanned flying object. By adopting the unmanned flying object pushing assisting structure, the separation of the rocket and the flyer is easily, ingeniously and quickly realized, the unmanned flying object is prevented from flying together with the rocket, and the interference of the rocket and the boosting rod on the overlong-time flying of the unmanned flying object is prevented.

Description

technical field [0001] The invention relates to the launching of flying objects, in particular to an unmanned flying object booster structure and an unmanned flying object launching stand. Background technique [0002] At present, the launch methods of flying objects mainly include: hand-throwing launch, rocket-assisted launch, catapult take-off launch, airborne launch, vehicle launch, etc. [0003] The rocket-assisted launch method is widely used in the take-off and launch of small and medium-sized flying objects. It is a common method of flying object launch. Complete the flight mission under the action of the engine. The thrust range of the rocket-assisted take-off and launching method is relatively large, which can meet the requirements of flying objects. This launching method is not restricted by the take-off site, has strong maneuverability, and expands the use range of flying objects. Moreover, its cost is relatively low, and it has better advantages economy. [00...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04
CPCB64F1/04
Inventor 唐冰徐文秀姚若麟刘以建
Owner 成都云鼎智控科技有限公司