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A Flapping Wing Mechanism Combining Electromagnetic Drive and Rope Drive

An electromagnetic drive, rope drive technology, applied in the field of flapping wing mechanism, can solve the problems of limited carrying power energy, easy structure breakage, large friction resistance, etc., to avoid motion instability and asymmetry, avoid mechanical vibration and other problems. The effect of energy loss, vibration reduction and energy consumption

Active Publication Date: 2021-07-16
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

In this scheme, the frictional resistance between the gears in the gear reduction group is large, and the energy loss is high. At the same time, due to the light weight and small size of the MAV, the energy of the carried power supply is limited, and the energy density of the current battery is limited. High energy loss is obviously not good for improving the endurance performance of the aircraft
In order to solve the above problems, someone proposed the design scheme of "electromagnetic drive connecting rod" and "motor driven rope transmission". In the scheme of "electromagnetic drive connecting rod", the rod structure is often in the harsh working state of friction and high-speed rotation The structure is prone to breakage, and the reliability is poor; in the "motor-driven rope transmission" scheme, although the high-speed rotating gear reduction group is removed, there are eccentric gears

Method used

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  • A Flapping Wing Mechanism Combining Electromagnetic Drive and Rope Drive
  • A Flapping Wing Mechanism Combining Electromagnetic Drive and Rope Drive
  • A Flapping Wing Mechanism Combining Electromagnetic Drive and Rope Drive

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Embodiment Construction

[0026] In order to understand the above-mentioned purpose, features and advantages of the present invention more clearly, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that, in the case of no conflict, the embodiments of the present application and the features in the embodiments can be combined with each other.

[0027] In the following description, many specific details are set forth in order to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described here. Therefore, the protection scope of the present invention is not limited by the specific details disclosed below. EXAMPLE LIMITATIONS. The present invention will be further described in detail with reference to the accompanying drawings and embodiments.

[0028] figure 1 It is an overall schematic diagram of a flapping wing mechanis...

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Abstract

The application discloses a flapping wing mechanism combining electromagnetic drive and rope transmission, which includes a rope drive mechanism, an electromagnetic drive mechanism and a pair of flapping wings. Through the technical solution of the present invention, energy absorption and energy storage can be buffered during the flapping wing movement, so as to achieve the effects of vibration reduction and energy consumption reduction, and at the same time can realize precise control of movement, avoiding the vibration caused by eccentric gear shaking in the traditional design. motion instability and asymmetry.

Description

technical field [0001] The invention relates to the field of micro-aircraft, specifically but not exclusively, to a flapping wing mechanism combining electromagnetic drive and rope drive. Background technique [0002] Since the 1990s, with the continuous maturity of traditional aircraft design technology and the great progress of microelectronics technology, the concept of micro air vehicle has been proposed and its rapid development has been promoted. Micro air vehicles are small in size, light in weight and strong in maneuverability. They have broad application prospects in national security and national economic construction, and can be used for investigation, exploration, and rescue assistance in complex environments. At the same time, as people continue to explore the flight principles of natural organisms (such as insects), bionic design is more and more applied to the field of micro-aircraft, and various bionic flapping-wing micro-aircraft that imitate the flight of i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 吴江浩贾媛李港张梓箫张艳来
Owner BEIHANG UNIV