Turbojet type multiple-spindle aircraft and control method thereof

Abstract

The invention discloses a turbojet type multiple-spindle aircraft and a control method thereof. The multiple-spindle aircraft comprises a multiple-spindle aircraft machine frame platform, a plurality of support arms, a plurality of multiple-spindle aircraft power devices and a control platform, wherein the control platform is arranged on the upper end surface of the multiple-spindle aircraft machine frame platform; a control system, and a battery for electric turbojet or fuel used for a fuel oil jet turbine are mounted on the control platform; one ends of the support arms are respectively connected with the multiple-spindle aircraft machine frame platform, and the support arms are distributed around the multiple-spindle aircraft machine frame platform; the multiple-spindle aircraft power devices are correspondingly arranged at the other ends of the support arms and are connected with the control system on the control platform; an electric turbojet or a fuel oil turbine jet engine is arranged in each of the multiple-spindle aircraft power devices. The turbine type multiple-spindle aircraft disclosed by the invention is a multiple-spindle aircraft with large power, high load, long range and high safety.

Description

technical field [0001] The invention relates to a multi-axis aircraft, in particular to a turbojet type multi-axis aircraft and a control method thereof. Background technique [0002] Existing multi-axis UAVs powered by rotor propellers have a short battery life and cannot complete ultra-long-range missions. Because the thrust provided by the rotor propellers is limited, they cannot carry more batteries and extended application equipment, and cannot mount heavy items. Affect the promotion and application range of drones. [0003] Existing multi-axis UAVs powered by rotor propellers are extremely vulnerable to damage. When the rotor propeller encounters debris, birds hit or hit tree trunks and other obstacles during flight, the exposed rotor propeller blades will be damaged or even scrapped, threatening the aircraft. The safety of itself and attached equipment. [0004] Power propulsion devices with rotors generate thrust through high-speed rotating propellers or rotors t...

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a turbojet multi-axis aircraft and its control method, which uses an electric turbojet or a fuel turbojet engine as power, and solves the problem that the existing multi-axis aircraft using propellers or rotor power devices cannot operate due to limited rotor power. Complete tasks of ultra-high load and ultra-long range, low reliability, easy damage to propellers or rotors, easy threat to personal safety, and a lot of noise during use

Images