Flapping-wing air vehicle driving device and flapping-wing air vehicle

A technology for a flapping aircraft and a driving device, applied in the field of aircraft, can solve the problem of single driving mode of the flapping aircraft, and achieve the effects of solving the single driving mode, enriching the driving mode and improving the load capacity.

Pending Publication Date: 2022-03-01
BEIJING INST OF NANOENERGY & NANOSYST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The embodiment of the present application provides a flapping-wing aircraft drive device and the flapping-wing aircraft to solve the problem of a single drive mode of the flapping-wing aircraft

Method used

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  • Flapping-wing air vehicle driving device and flapping-wing air vehicle
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  • Flapping-wing air vehicle driving device and flapping-wing air vehicle

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Embodiment Construction

[0027] The implementation manner of the present application will be further described in detail below with reference to the drawings and embodiments. The detailed description and drawings of the following embodiments are used to illustrate the principles of the application, but not to limit the scope of the application, that is, the application is not limited to the described embodiments.

[0028] In the description of the present application, it should be noted that, unless otherwise stated, the terms "first" and "second" are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance; The meaning is two or more; the orientation or positional relationship indicated by the terms "inner", "outer", "top", "bottom" etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing this The application and simplified description do not indicate or imply that the device or e...

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Abstract

The invention discloses an ornithopter driving device and an ornithopter. The flapping wing aircraft driving device comprises a driving bracket and a flapping wing structure, wherein the flapping wing structure is arranged on the driving bracket through a rotating shaft. The driving support is provided with an iron core, and the iron core is sleeved with a coil. The flapping wing structure is located above the iron core, a permanent magnet is arranged on the side, facing the iron core, of the flapping wing structure, when the coil is powered on, the coil and the iron core generate a magnetic field, and the magnetic field attracts or repels the permanent magnet, so that the flapping wing structure rotates close to or away from the iron core. According to the flapping-wing air vehicle driving device, current and reverse current are alternately supplied to the coil, vertical flapping of the flapping-wing structure can be achieved, power can be provided for the flapping-wing air vehicle, the flapping force degree, amplitude and frequency of the flapping-wing structure can be adjusted by adjusting the magnitude and turning frequency of the supplied current, and the flapping effect of the flapping-wing air vehicle is improved. Different lift forces and speeds are provided for the ornithopter, the driving modes of the ornithopter can be enriched, and the loading capacity of the ornithopter is improved.

Description

technical field [0001] The present application relates to the technical field of aircraft, and in particular to a driving device of an orchid-wing aircraft and an ortho-wing aircraft. Background technique [0002] The flapping-wing aircraft has a history of hundreds of years. In recent years, researchers have made great progress in the research and manufacture of the flapping-wing aircraft, especially the miniature flapping-wing aircraft. However, due to technical difficulties such as single drive mode and low load capacity of the micro flapping-wing aircraft, the development of the micro flapping-wing drive is limited, and the commercialization, civilianization, and militarization of the miniature flapping-wing aircraft are all difficult. Contents of the invention [0003] The embodiments of the present application provide a driving device for a flapping-wing aircraft and the flapping-wing aircraft to solve the problem of a single driving method for the flapping-wing airc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 吴治峄胡双婷王中林
Owner BEIJING INST OF NANOENERGY & NANOSYST
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