Flapping-wing air vehicle with auxiliary lifting force device
A flapping-wing aircraft and lift technology, applied in the field of flapping-wing aircraft, can solve problems such as limited maneuverability, inability to control the left and right wings independently, and complex flight movements of birds, so as to achieve the effect of improving flight ability
Inactive Publication Date: 2021-01-29
GUANGDONG GUOSHIJIAN TECH DEV CO LTD
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- Application Information
AI Technical Summary
Problems solved by technology
[0003] However, due to the complex flight movements of birds
There are many existing technologies, most of which simply imitate the up and down swing of bird wings, without the expansion and contraction of wings like birds, and cannot independently control the left and right wings, so the flight efficiency is low and the maneuverability is quite limited.
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[0041] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0042] In describing the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or impl...
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The invention discloses a flapping-wing air vehicle with an auxiliary lifting force device. The flapping-wing air vehicle comprises a vehicle body, wing devices, a run-up device, a motor and a battery, an empennage is mounted at the tail of the fuselage; the run-up device is mounted on the lower side of the machine body; the two sets of wing devices are installed on the two sides of the fuselage,the wing devices and the run-up device are driven by motors, the multiple motors are powered by batteries, and an auxiliary lift device is arranged above the top of the fuselage. A fixed wing, A hydrogen balloon, A multi-axis aircraft and other devices capable of improving the lifting force of the aircraft are additionally arranged on the basis of the flapping-wing aircraft, stable lifting force is provided for the aircraft, and flying is better facilitated.
Description
technical field [0001] The invention relates to the technical field of aircraft, and more specifically relates to a flapping-wing aircraft equipped with an auxiliary lift device. Background technique [0002] At present, insects, birds, and bats that can fly in nature all use flapping wings to fly, which has the characteristics of high maneuverability and low energy consumption. The flapping-wing aircraft is different from the fixed-wing aircraft and the rotary-wing aircraft. It is an aircraft that adopts the flying mode of insects, birds, and bats. [0003] However, due to the more complicated flight movements of birds. There are many in the prior art, most of which simply imitate the up and down swing of the wings of birds without the expansion and contraction of wings like birds, and can not independently control the left and right wings, so the flight efficiency is low and the maneuverability is quite limited. Therefore, it is necessary to provide a flapping wing aircr...
Claims
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Patent Timeline
Login to View More IPC IPC(8): B64C27/22B64C27/32B64C33/02
CPCB64C27/22B64C27/32B64C33/02
Inventor 王志成
Owner GUANGDONG GUOSHIJIAN TECH DEV CO LTD