Turbojet type multiple-spindle aircraft and control method thereof

A technology of multi-axis aircraft and turbojet, which is applied in the direction of aircraft, jet power plant, rotorcraft, etc., can solve the problems of inability to complete ultra-high load and ultra-long range, easily damaged propellers or rotors, and low reliability, and achieve Conducive to application and development, long cruising distance, noise reduction effect

Inactive Publication Date: 2016-06-01
杨海涛
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • Turbojet type multiple-spindle aircraft and control method thereof
  • Turbojet type multiple-spindle aircraft and control method thereof
  • Turbojet type multiple-spindle aircraft and control method thereof

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Embodiment Construction

[0023] Embodiments of the present invention will be further described below in conjunction with the accompanying drawings.

[0024] Please see attached figure 1 to attach image 3 Shown, a kind of turbojet type multi-rotor aircraft, comprises multi-rotor aircraft frame platform 202, many support arms 208, a plurality of multi-rotor aircraft power units 206 and control platform 207; Described control platform 207 is arranged on described On the upper surface of the multi-axis aircraft frame platform 202, the control platform 207 is equipped with a control system and a battery used by the electric turbojet or the fuel used by the fuel jet turbine; one end of the plurality of support arms 208 is respectively Connected with the multi-axis aircraft rack platform 202, the plurality of support arms 208 are singular or even, and distributed around the multi-axis aircraft rack platform 202; The quadrocopter power units 206 are respectively arranged on the other ends of the plurality ...

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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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/12B64D27/18
CPCB64C27/12B64D27/18
Inventor 杨海涛
Owner 杨海涛
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