System integrating rocket with unmanned aerial vehicle and using method thereof

A technology for drones and rockets, applied in the field of aircraft, can solve problems such as the adverse effects of the normal launch and flight process of rockets, the large acceleration of the drone, and the change of force, so as to eliminate adverse effects, shorten time, and have high reliability. Effect

Inactive Publication Date: 2019-04-02
朱潇潇
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In view of the fact that the UAV and booster rocket combination in the prior art causes the center of gravity of the UAV to move and the force changes, which in turn leads to a decrease in its static stability; the acceleration of the UAV is large and the speed changes drastically. The launch process has a strong nonlinearity, coupled with the existing installation errors and disturbances, which will adversely affect the normal launch and flight process of the rocket, which in turn leads to the problem of great uncertainty in the entire system. The present invention Provide a kind of integrated system of rocket and UAV and its use method, it does not change the structure of UAV itself, and also eliminates the influence of UAV on the normal launch and flight process of model rockets; in addition, It also has the advantages of simple operation and high reliability

Method used

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  • System integrating rocket with unmanned aerial vehicle and using method thereof
  • System integrating rocket with unmanned aerial vehicle and using method thereof
  • System integrating rocket with unmanned aerial vehicle and using method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0046] Such as figure 1 , image 3 with Figure 4 As shown, a rocket-drone integrated system includes a rocket body 1, a linkage ejection device 3 and a UAV 5. Inside the rocket body 1, a nose cone cabin 105, a loading cabin 106, and an engine are sequentially arranged from top to bottom. The cabin 107, the UAV 5 is a multi-rotor UAV, such as a coreless flying machine, the UAV 5 is fixed in the cargo compartment 106 through the linkage ejection device 3, and the nose cone cabin 105 is opened after reaching a certain height and distance. To form an ejection channel, the linkage ejection device 3 is used to eject the UAV 5 from the cargo compartment 106; the rocket-UAV integrated system in this embodiment can quickly reach a certain height and distance The unmanned aerial vehicle 5 pops up to realize tasks such as reconnaissance, exploration, and monitoring, and greatly shortens the time from taking off and flying to the desired location, that is, to quickly reach the destinat...

Embodiment 2

[0050] With embodiment 1, difference is: as Image 6 with Figure 7 As shown, the linkage ejection device 3 includes a support base 301, an ejection spring 302 and a locking mechanism 303. The support base 301 is a circular platform and is horizontally fixed in the load compartment 106. There are multiple ejection springs 302 and are evenly arranged on the support base. 301, the locking mechanism 303 is located at the center of the support seat 301, and the locking mechanism 303 is used to lock the UAV 5. The opening of the nose cone cabin 105 will cause the locking mechanism 303 to fail, and then the UAV 5 will be ejected by the ejection spring 302. ejected.

[0051] Specifically the above structure, such as Figure 8 As shown, the UAV 5 is composed of a frame, a drive motor, a propeller, an image transmission system, and a power supply. The bottom center of the UAV 5 frame is provided with a locking bracket 501 and a plurality of ejectors are arranged around the locking br...

Embodiment 3

[0055] A method for using the rocket-drone integrated system adopts the rocket-drone integrated system described in Embodiment 2, which is described in detail below.

[0056] A method for using a rocket-drone integrated system, the steps of which are:

[0057] a. The rocket body 1 is ignited and lifted into the air, and under the action of the engine arranged inside the engine compartment 107, it flies to a predetermined position, and the flight attitude of the rocket body 1 is adjusted so that the direction of flight is vertically upward;

[0058] b. UAV 5 unlocks the driving motor, so that the driving motor is in an idle state;

[0059] c. Before the flight speed decreases to zero, the steering gear 2 controls the separation of the left nose cone section 102 and the right nose cone section 103, pulls the rope 307, and drives the latch 304 to leave the jack;

[0060] d. When the left nose cone section 102 or the right nose cone section 103 rotates to the outside at an angle ...

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Abstract

The invention discloses a system integrating a rocket with an unmanned aerial vehicle (UAV) and a using method thereof, and belongs to the technical field of aircraft. The system comprises a rocket body, a linkage ejection device and the UAV, wherein the interior of the rocket body is sequentially provided with a nose cone compartment, a cargo carrying compartment and an engine compartment from top to bottom; the UAV is a multi-rotor UAV; the UAV is fixed in the cargo carrying compartment through the linkage ejection device; the nose cone compartment can be opened to form an ejection passage;and the linkage ejection device is used for ejecting the UAV from the cargo carrying compartment. The system integrating the rocket with the UAV breaks the traditional idea that the rocket can only combined with a fixed-wing UAV, and eliminates the adverse effect of the rocket on the static stability of the UAV without changing the self structure of the UAV. The system integrating the rocket withthe UAV also eliminates the adverse effect of the UAV on the normal launch and flight process of the rocket, so that the system integrating the rocket with the UAV can be higher in overall efficiencyand more stable. In addition, the system has the advantages of simple operation, high reliability and the like.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and more specifically relates to a rocket-drone integrated system and a method for using the same. Background technique [0002] In recent years, with the rapid development of aerospace technology, model rockets and multi-rotor UAVs have developed rapidly in their respective fields, and UAV aerial photography has even gradually become a part of everyone's life. [0003] At present, the combination of rockets and UAVs is mainly for military rockets to boost fixed-wing UAVs. In the launch stage, due to the addition of booster rockets, the center of gravity of the combination of UAVs and booster rockets will move, and the UAV will be stressed. change, leading to a decrease in its static stability. At the same time, the acceleration of the UAV is large and the speed changes drastically. The UAV has a strong nonlinearity during the launch process, and there may be installation errors and disturbance...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08F42B15/00F42B15/01F42B15/36
CPCF42B15/00F42B15/01F42B15/36B64C27/08B64U50/15B64U70/80B64U30/20B64U10/10
Inventor 朱潇潇徐浩
Owner 朱潇潇
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