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Multi-impeller remotely-controlled aircraft

A technology of remote-controlled aircraft and fuselage, which is applied in the field of remote-controlled aircraft, and can solve the problems that the aircraft is not easy to fly stably, and the power of a single propeller is limited.

Pending Publication Date: 2017-06-13
王长民
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Remote-controlled aircraft often use propellers as power sources, but usually the power of a single propeller is limited, and large-volume aircraft are not easy to fly stably

Method used

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  • Multi-impeller remotely-controlled aircraft
  • Multi-impeller remotely-controlled aircraft
  • Multi-impeller remotely-controlled aircraft

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Embodiment Construction

[0023] Remote control aircraft, including fuselage.

[0024] The fuselage includes a fuselage transverse plate 1 . An upper vertical board 3 is fixed above the head of the horizontal board 1 of the fuselage, and a lower vertical board 4 is fixed below the head of the horizontal board 1 of the fuselage.

[0025] Fuselage rear top fixes two vertical empennages 5.

[0026] In this embodiment, two vertical empennages 5 are fixed above the tail of the fuselage transverse plate 1 .

[0027] The middle parts of both sides of the fuselage are respectively provided with wings 2 .

[0028] In this embodiment, wings 2 are respectively provided at the middle of both sides of the fuselage transverse plate 1 , and the wings 2 include a front fixed wing 21 and a front movable wing 22 .

[0029] The two front fixed wings 21 are fixedly connected with the fuselage. In this embodiment, the front fixed wings 21 and the fuselage transverse plate 1 are integrally structured.

[0030] The rear ...

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Abstract

A multi-impeller remotely-controlled aircraft has vertical tail fins and a horizontal tail; a steering engine is arranged below a front fixed wing of each wing, each steering engine is connected to a front engine corner below a front moving wing of the corresponding wing, and the front engine corner is connected with a horizontal tail moving fin of the horizontal tail through a rear link; a protective cabin is fixed below a transverse plate of a fuselage; at least two propeller channels are arranged above the protective cabin on the transverse plate; a motor and a propeller are arranged in each propeller channel; each propeller shaft is arranged in the corresponding propeller channel axially along the fuselage, and a motor is fixed to the edge of each propeller channel; a shell of each motor is supported on the edge of the corresponding propeller channel through a corresponding cross support, and the shell of the motor is foxed to a cross support face of one side of the cross support; the other side of each cross support is fixed to the edge of the corresponding propeller channel. The multi-impeller remotely-controlled aircraft has more than two propellers and has higher power.

Description

technical field [0001] The invention belongs to the field of remote-controlled airplanes, in particular to remote-controlled airplanes. Background technique [0002] Remote-controlled aircraft often use propellers as power sources, but usually the power of a single propeller is limited, and large-volume aircraft are not easy to fly stably. Contents of the invention [0003] The purpose of the present invention is to provide a multi-blade remote-controlled aircraft. The aircraft has at least two propellers, which can provide greater power to the aircraft. [0004] The technical solutions adopted are: [0005] Multi-propeller remote control aircraft, including fuselage. Two vertical tail fins are fixed on the upper part of the rear of the fuselage. The middle part of both sides of the fuselage is respectively provided with wings. There is a horizontal stabilizer on the fuselage behind each wing. [0006] The bottom of the front fixed wing of each wing is equipped with a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/18A63H29/00
CPCA63H27/02A63H29/22
Inventor 王长民
Owner 王长民
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