Air-ground amphibious mini unmanned aerial vehicle

An unmanned aerial vehicle (UAV) and miniature technology, applied in the field of UAV, can solve the problems of complex structure, difficult to maneuver, slow development of large-scale quadrotor UAV, etc. Effect

Pending Publication Date: 2017-08-18
江苏守卫者航天科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional large UAVs mainly use four-rotors, six-rotors or multi-rotors to perform tasks such as shooting, monitoring and reconnaissance in the near-groun

Method used

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  • Air-ground amphibious mini unmanned aerial vehicle
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Examples

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Embodiment Construction

[0016] combine figure 1 , a new type of land-air amphibious micro UAV, including upper rotor assembly 1, frame 2, motor 3-1 (with self-locking function), motor 3-2 (with self-locking function), connecting rod 4 and lower rotor Component 5. The upper rotor assembly 1 is fixedly connected to the frame 2 by bolts, the motor 3-1 is fixed to the upper rotor assembly 1 by bolts, the output shaft of the motor 3-1 is connected to the connecting rod 4 through a key, and the motor 3-2 is connected by The bolt is fixedly connected on the lower rotor assembly 4, and the output shaft of the motor 3-2 is rotatably connected with the connecting rod 4 through the key.

[0017] combine figure 2 , there are four upper rotor assemblies 1, and the distribution of the upper rotor assemblies 1 is carried out in the following manner: the lines connecting the centers of the two upper rotor assemblies are perpendicular to each other. Each upper rotor assembly 1 includes a blade 6 , a motor 7 and a...

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Abstract

The invention provides an air-ground amphibious mini unmanned aerial vehicle which comprises a rack, an upper rotor wing component, four lower rotor wing components and a connecting rod. The upper rotor wing component comprises an upper paddle and an upper motor arranged on the rack, the upper paddle is connected with a rotating shaft of the upper motor, and the upper end of the connecting rod is rotatably connected with the rack through an upper steering motor with a self-locking function; center connecting lines of the two lower rotor wing components which are arranged oppositely are perpendicular to each other, each lower rotor wing component comprises a base, an annular hub, a plurality of rollers, a lower paddle and a lower motor, each base is rotatably connected with the lower end of the connecting rod through a lower steering motor with a self-locking function, the center of each annular hub is connected with a base bearing, the rollers are arranged along the periphery of the corresponding annular hub and rotate around a rotating shaft in the tangential direction of the corresponding annular hub, each lower motor is arranged on the corresponding base, and each lower paddle is connected with a rotating shaft of the corresponding lower motor. Lower rotor wings of the unmanned aerial vehicle can realize air-ground amphibious switching by swinging the connecting rod.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle technology, and Terne is a ground-air amphibious miniature unmanned aerial vehicle. Background technique [0002] Traditional large-scale UAVs mainly use four-rotor, six-rotor or multi-rotor to perform tasks such as shooting, monitoring and reconnaissance in the near-ground environment. However, due to reasons such as complex structure and difficult manipulation, the development of large-scale quadrotor UAVs has been relatively slow. . In recent years, with the advancement of new materials, micro-electro-mechanical (MEMS), micro-inertial navigation (MIMU) and flight control technologies, micro-UAVs have developed rapidly and have gradually become the focus of attention. [0003] Micro drones are especially suitable for monitoring, reconnaissance and other tasks in near-ground environments (such as indoors, urban areas and jungles, etc.), and have broad military and civilian prospects; at the same tim...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C37/00B64C27/32
CPCB64C27/08B64C27/32B64C37/00B64U50/14B64U10/10
Inventor 张志安张广麟谢磊梅新虎
Owner 江苏守卫者航天科技有限公司
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