Feather cracking simulation lift enhancement mechanism of micro flapping aircraft

Abstract

The invention discloses a feather cracking simulation lift enhancement mechanism of a micro flapping aircraft. The feather cracking simulation lift enhancement mechanism comprises an aircraft body frame, wing rear-end pieces, a secondary flight feather II, a secondary flight feather I, a primary flight feather II, a primary flight feather I, four flexible feather hinges, a flexible wing hinge and wing front-end pieces, wherein all the parts of the flapping aircraft are arranged in an axial eudipleural manner; the wing front-end pieces are respectively mounted on two sides of the aircraft body frame and can do up-and-down flapping around the aircraft body frame under the traction of a flapping driving device; the wing front-end pieces are connected with the wing rear-end pieces through the flexible wing hinge; the secondary flight feather II, the secondary flight feather I, the primary flight feather II and the primary flight feather I are respectively connected with the wing rear-end pieces through the four flexible feather hinges. The sum of total rising forces of an upper flapping section and a lower flapping section is higher than that of a conventional flapping aircraft which does not simulate cracking; the feather cracking simulation lift enhancement mechanism has the advantages of high pneumatic efficiency, simple structure, high reliability and the like.

Description

technical field [0001] The invention belongs to the technical field of micro-flapping-wing aircraft, and in particular relates to a high-efficiency micro-flapping-wing aircraft imitating feather cracking and increasing lift mechanism. Background technique [0002] Micro flapping wing aircraft is a kind of bionic aircraft, theoretically beyond the scope of traditional aircraft design and aerodynamic research. Compared with traditional fixed-wing and rotary-wing micro-aircraft, the main feature of micro-orthopting-wing aircraft is that it can generate lift and thrust at the same time, and it also has the characteristics of high efficiency, high maneuverability, low noise, and no need for special take-off and landing sites. In nature, almost without exception, all flying creatures use flapping wings to fly. Therefore, so far the researches of various countries on the micro-aircraft have been gradually focused on the micro-flapping-wing aircraft. [0003] From the perspective ...

AI Technical Summary

Problems solved by technology

[0007] The purpose of the present invention is to solve the current situation that the existing bird-like miniature flapping-wing aircraft only has bionic wings but no feather bionics, and the aerodynamic efficiency of the whole machine is low, and improve the flight performance of the miniature flapping-wing aircraft. Simple structure and strong reliability micro-flapping-wing aircraft imitating feather cracking and increasing lift mechanism

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