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Ejection type unmanned aerial vehicle

An unmanned aerial vehicle and ejection technology, applied in the field of unmanned aerial vehicles, can solve the problems of being unable to apply to uneven ground, manual pulling by catapult, and occupying a large space, so as to reduce occupied space, facilitate transportation, and improve use effect of effect

Pending Publication Date: 2021-07-23
南京联汇智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the process of realizing the present invention, the inventor found that at least the following problems in the prior art have not been solved: At present, in order to realize the take-off of some unmanned aerial vehicles in specific occasions, usually a catapult is used to provide the unmanned aerial vehicle Take-off power, but the existing catapults usually need to be manually pulled, which is laborious and laborious, and also needs to occupy a large space, and cannot be applied to uneven ground

Method used

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  • Ejection type unmanned aerial vehicle
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  • Ejection type unmanned aerial vehicle

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Embodiment Construction

[0022] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments.

[0023] In describing the present invention, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", " The orientation or positional relationship indicated by "outside", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, so as to Specific orientation configurations and operations, therefore, are not to be construed as limitations on the invention.

[0024] In the description of the present invention, it should be noted that, unless otherwise specified and...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, and discloses an ejection type unmanned aerial vehicle. The ejection type unmanned aerial vehicle comprises a bottom plate, supports are fixedly mounted at the four corners of the top end of the bottom plate correspondingly, an unmanned aerial vehicle body is movably arranged among the four supports, and suction blocks are fixedly mounted at the four ends of the bottom side of a support of the unmanned aerial vehicle body correspondingly; and grooves a are formed in the sides, close to the unmanned aerial vehicle body, of the four supports. Through the arranged grooves a and grooves b, when the unmanned aerial vehicle is used, the four suction blocks on the bottom side of the unmanned aerial vehicle body can be arranged on springs of the four grooves a correspondingly, an electromagnetic block is pushed through a push rod motor a, the suction blocks are sucked, so that when the push rod motor a retracts a motor shaft, the springs can be compressed, and when the springs are compressed to a certain degree, the electromagnetic block is powered off, and ejection of the unmanned aerial vehicle body is completed. Compared with the prior art, ejection in the vertical direction can be achieved, the occupied space in the prior art is effectively reduced, use is convenient, and the use effect is extremely good.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a catapult unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as unmanned aerial vehicle, is an unmanned aircraft controlled by radio remote control equipment and its own program control device. Because of its small size, low cost, easy to use, low requirements on the combat environment, and strong battlefield survivability, it is favored by armies all over the world and is widely used in the military field. In addition, countries around the world are actively expanding the application scope of civilian drones, and the technical and economic effects of using drones in fields such as electric power, communications, meteorology, agriculture, forestry, ocean, and exploration are promising. [0003] In the process of realizing the present invention, the inventor found that at least the following problems in the prior art have not b...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06B64F1/22B62B3/04B62B5/00
CPCB64F1/06B64F1/22B62B3/04B62B5/00B64U70/70B64U10/10
Inventor 戴鹏
Owner 南京联汇智能科技有限公司
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