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
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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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