A Miniature Flapping Rotor Aircraft with Differential Flapping of Two Wings

Abstract

The invention discloses a micro-flapping rotor aircraft with differential flapping of two wings, and relates to the field of micro-aircraft. The aircraft includes a wing, a transmission mechanism, a power unit and a base; the power unit and the transmission mechanism are fixed on the base, and a wing is respectively fixed at both ends of the transmission mechanism; during work, the micro-motor in the power unit provides power to drive the transmission mechanism The inner rod of the wing lifts up and down, causing the two wing connecting rods to move in opposite directions at the same time, driving a pair of symmetrically arranged wings to move down and up alternately to achieve differential flapping. The present invention ensures that the average lift remains unchanged during the flapping of the wings at the same frequency, the transient lift fluctuations of the wings are significantly reduced, the lift is more uniform throughout the flapping cycle, and the requirements for the output power of the motor are effectively reduced, significantly Improve energy efficiency.

Description

technical field [0001] The invention relates to the field of micro-aircraft, in particular to a micro-flapping-rotor aircraft with differential flapping of two wings. Background technique [0002] Since the 1990s, with the continuous improvement of traditional aircraft design technology, people have been exploring the mechanism of animal flight and swimming more and more deeply, and the rapid development of microelectronics technology has led to the rapid development of the field of micro air vehicle design. , has broad application prospects in national security and national economic construction, and is applied to tasks such as reconnaissance, communication, exploration and assistance in rescue under complex environmental conditions. [0003] The patent application whose publication number is CN 101492093: "Design Method of Flapping Rotor and Miniature Flapping Rotor Aircraft Designed by Using the Method" discloses a miniature flapping rotor aircraft. supply. MAVs are lig...

AI Technical Summary

Problems solved by technology

[0005] The present invention aims at flapping both wings in the same direction for the existing miniature flapping rotor aircraft, resulting in extremely large wing lift and transient energy consumption during down-shooting, and very little lift and transient energy consumption during up-shooting. Due to the huge difference in transient energy consumption, large fluctuations in system lift, and low overall energy utilization, a miniature flapping rotor aircraft with differential flapping wings was proposed.

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