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Power assembly for bionic flapping-wing flying robot

A technology for flying robots and power components, applied in the field of bionic aircraft, can solve the problems of large windward area of ​​the fuselage, reduce wind resistance, disadvantage, etc., and achieve the effect of slender overall shape, reducing wind resistance, and reducing windward area

Pending Publication Date: 2022-06-03
HARBIN INST OF TECH SHENZHEN GRADUATE SCHOOL
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the existing flapping-wing aircraft, the rocker arm of its wing partly extends to the inside of the fuselage, and the drive device inside the fuselage drives the rocker arm to swing up and down, that is, the drive device and the wings are respectively located on the inside and outside of the fuselage. Space needs to be opened inside the fuselage to accommodate the driving device, resulting in a large windward area of ​​the fuselage, which is not conducive to reducing wind resistance

Method used

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  • Power assembly for bionic flapping-wing flying robot
  • Power assembly for bionic flapping-wing flying robot
  • Power assembly for bionic flapping-wing flying robot

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Embodiment Construction

[0027] Embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0028] In the description of the present invention, it should be understood that the orientation descriptions, such as up, down, front, back, left, right, etc. indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, and are only In order to facilitate the description of the present invention and simplify the description, it does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in ...

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Abstract

The invention discloses a power assembly for a bionic flapping-wing flying robot. The power assembly comprises a fuselage, the two swing rods are connected to the left side and the right side of the fuselage correspondingly, can swing up and down relative to the fuselage, extend from the fuselage to the left side and the right side of the fuselage correspondingly and are used for installing wings; the two connecting rods are connected to the positions, away from the machine body, of the two swing rods correspondingly and used for driving the swing rods to swing up and down. The driving device is arranged on the machine body and used for enabling the connecting rod to move up and down; by applying the components, the component compactness of the whole robot can be improved, and the wind resistance of the robot body can be reduced.

Description

technical field [0001] The invention relates to the technical field of bionic aircraft, in particular to a power assembly for a bionic flapping-wing flying robot. Background technique [0002] Flapping flight is an efficient way of flying. In nature, birds and insects complete various flight actions by flapping their wings. Humans have invented a variety of bionic flapping-wing flying robots by imitating the flapping wings of animals. In the flapping-wing flying robots, the power component is the core component that drives the flapping wings, mainly used to drive the flapping of the wings. [0003] In the existing flapping-wing aircraft, the rocker arm of its wing partly extends to the inside of the fuselage, and the drive device inside the fuselage drives the rocker arm to swing up and down, that is, the drive device and the wings are respectively located on the inside and outside of the fuselage. The interior of the fuselage needs to open up a space to accommodate the dri...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02
CPCB64C33/02Y02T50/60
Inventor 徐文福潘尔振胡晓坤徐晖袁晗
Owner HARBIN INST OF TECH SHENZHEN GRADUATE SCHOOL