Retractable unmanned aerial vehicle

An unmanned aerial vehicle and telescopic technology, applied in the field of unmanned aerial vehicles, can solve the problems of inability to achieve all-round protection of propeller blades, inconvenient storage and transportation, and potential safety hazards, and achieve convenient storage and transportation, convenient operation, and structure. Simple and compact effect

Pending Publication Date: 2017-08-18
PRODRONE TECH (SHENZHEN) CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Nowadays, UAV technology is constantly improving and its applications are becoming more and more extensive. However, because the arms and blades need to be stretched in one direction, it takes up too much space and is not convenient for storage and transportation.
In order to solve this problem, the current solution is to reduce the volume of the UAV in the non-working state by folding, but this cannot achieve all-round protection of the blades, so there are potential safety hazards

Method used

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Embodiment Construction

[0047] The present invention will be described below according to the embodiments shown in the accompanying drawings. It can be thought that embodiment disclosed this time is an illustration in every point, and is not restrictive. The scope of the present invention is not limited by the description of the following embodiments but only by the scope of the claims, and includes the same meaning as the scope of the claims and all modifications within the scope of the claims.

[0048] like figure 1 The shown embodiment of the retractable UAV of the present invention is a schematic diagram of a three-dimensional decomposition structure, including a main cabin 1 of the unmanned aerial vehicle. The guard cover 2 is a net cover provided with a plurality of mesh holes 3 on the surface, and the side of the guard cover 2 facing the main compartment 1 is designed to be open. Each shield 2 is slidably connected with a motor paddle mechanism through a telescopic first slide rail mechanism...

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Abstract

The invention provides a retractable unmanned aerial vehicle which comprises a main chamber, wherein the left and right sides of the main chamber are respectively provided with a shield; a motor blade mechanism is in sliding connection in each shield respectively through a retractable first slide rail mechanism; each motor blade mechanism is in sliding connection with the main chamber through a retractable second slide rail mechanism; each motor blade mechanism is contained in the space composed of the shields and the main chamber when the first slide rail mechanism and the second slide rail mechanism are in a contraction state; and the main chamber is arranged in two shields. The retractable unmanned aerial vehicle provided by the invention can realize maximum volume reduction and comprehensive protection of blades within the non-working time of the unmanned aerial vehicle, so as to facilitate storage and transport and provide higher safety.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a retractable unmanned aerial vehicle. Background technique [0002] UAV is an unmanned aerial vehicle controlled by radio remote control equipment and self-contained program control device. At present, it is mostly used in combination with shooting equipment for inspection and aerial photography. Nowadays, UAV technology is constantly improving and its application is becoming more and more extensive. However, because the arms and blades need to be stretched in one direction, it takes up too much space and is not convenient for storage and transportation. In order to solve this problem, the current solution is to reduce the volume of the UAV in the non-working state by folding, but this cannot achieve all-round protection of the blades, so there are potential safety hazards. Contents of the invention [0003] The purpose of the present invention is to provide ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30B64D45/00
CPCB64C1/30B64D45/00B64U10/10
Inventor 黄立吴晗付文王效杰顾兴刘华斌
Owner PRODRONE TECH (SHENZHEN) CO LTD
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