Conical rotary flapping wing aircraft

Abstract

The invention discloses a conical rotary flapping wing aircraft and belongs to the technical field of aircrafts. The conical rotary flapping wing aircraft is composed of an aircraft body, a landing gear, an energy system, a control system, a left conical rotary flapping wing, a right conical rotary flapping wing, a tail rod, a tail wing and a counterweight balancing rod, wherein the energy system comprises a left motor, a left speed reducing gear unit, a right motor, a right speed reducing gear unit, a conveniently charged lithium battery and a motor speed adjusting control device; the parameters of the left motor is the same as those of the right motor; the parameters of the left speed reducing gear unit is also the same as those of the right speed reducing gear unit; the control system comprises a wireless navigation device and a steering engine; the tail wing is used for balancing and controlling pitching flying postures; the structure of the left conical rotary flapping wing is the same as that of the right conical rotary flapping wing; the left and right conical rotary flapping wings are symmetrically arranged at the left and right sides of the aircraft body respectively and are used for providing push forces under the drives of the left and right motors respectively. The aircraft is capable of vertically lifting and hovering and can be applied to various tasks such as aerial photography, geographic survey, traffic duty, military reconnaissance, rescue and relief works when being provided with image shooting devices.

Description

technical field [0001] The utility model relates to a conical rotary flapping-wing aircraft, which belongs to the technical field of aircraft, and in particular relates to an aircraft with wings rotating. Background technique [0002] The traditional flapping wing aircraft relies on the crankshaft linkage mechanism to drive the flapping wings, and the flapping wings flutter up and down to generate thrust. Its efficiency is low, it is inconvenient to adjust the thrust direction, it is difficult to vertically lift, and the fatigue strength of the flapping wing material is relatively high. high. Contents of the invention [0003] The purpose of the present invention is to overcome the above-mentioned defect of traditional flapping-wing aircraft, and invent a conical rotary flapping-wing aircraft with higher efficiency and maneuverability. [0004] The present invention adopts the following technical scheme: a conical rotary flapping wing aircraft includes a fuselage, landing...

AI Technical Summary

Problems solved by technology

[0002] The traditional flapping wing aircraft relies on the crankshaft linkage mechanism to drive the flapping wings, and the flapping wings flutter up and down to generate thrust. Its efficiency is low, it is inconvenient to adjust the thrust direction, it is difficult to vertically lift, and the fatigue strength of the flapping wing material is relatively high. high

Images