Symmetric hexrcopter

A six-axis aircraft, symmetrical technology, applied in the field of aircraft, can solve the problems of the aircraft not being able to vertically lift and hover, high energy consumption, poor stability and safety, etc.

Active Publication Date: 2016-01-06
BEIJING INST OF REMOTE SENSING EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional hexacopters consume a lot of energy when cruising, have poor stability and safety, and are basically unable to save themselves when they lose part or all of their power
Traditional aircraft cannot lift vertically and hover
Traditional helicopters have high energy consumption, low efficiency, and low safety and stability

Method used

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Embodiment Construction

[0009] Now in conjunction with accompanying drawing the present invention is described in detail: a kind of symmetrical type hexacopter, comprises fuselage 1, left composite wing 2, right composite wing 3, support 4, front rotor 5, rear rotor 6 and landing gear 7. The fuselage 1 is equipped with a control system and airborne equipment. The left compound wing 2 and the right compound wing 3 have the same structure, and they are symmetrically installed on the left and right sides of the fuselage 1. The front rotor 5 and the rear rotor 6 have the same structure, and they are respectively installed at the front and rear ends of the fuselage 1 through brackets 8 . The front rotor 5 and the rear rotor 6 are respectively driven by two motors. The front rotor 5 and the rear rotor 6 turn in opposite directions, and the rotation speed is convenient to adjust. The plane of rotation of the front rotor 5 and the plane of rotation of the rear rotor 6 are in the same horizontal plane. The...

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PUM

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Abstract

The invention relates to a symmetric hexrcopter, which belongs to the technical field of aircrafts and comprises an airframe, a left composite wing, a right composite wing, a support, front rotor wings, rear rotor wings and an undercarriage. A control system and an airborne device are arranged in the airframe. The left composite wing and the right composite wing have the same structure and are symmetrically arranged on the left side and the right side of the airframe. The front rotor wings and the rear rotor wings have the same structure and are respectively arranged on the front end and the rear end of the airframe through the support. The undercarriage adopts a jumper and wheel type composite structure. The left composite wing and the right composite wing have the same structure and are symmetrically arranged on the left side and the right side of the airframe. The left composite wing and the right composite wing are respectively provided with two rotor wings internally, and each rotor wing is driven by an engine. Vanes of the left composite wing comprises front vanes and rear vanes capable of deflecting around a wing axis. The symmetric hexrcopter can be lifted vertically by only a small take-off and land zone. The symmetric hexrcopter generates larger lifting force, and is safe, stable and flexible.

Description

technical field [0001] A symmetrical hexacopter belongs to the technical field of aircraft, in particular to a hexacopter. Background technique [0002] Traditional hexacopters consume a lot of energy while cruising, have poor stability and safety, and are basically unable to save themselves when they lose part or all of their power. Conventional aircraft cannot vertically lift and hover. Traditional helicopters have high energy consumption, low efficiency, and low safety and stability. SUMMARY OF THE INVENTION [0003] The purpose of the present invention is to overcome the above-mentioned shortcomings of traditional hexacopters, airplanes and helicopters, and to invent a highly efficient and safe symmetrical hexacopter capable of vertical take-off and landing. [0004] A symmetrical hexacopter comprises a fuselage, a left composite wing, a right composite wing, a bracket, a front rotor, a rear rotor and a landing gear. The fuselage is equipped with a control system an...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/82
Inventor 王志成
Owner BEIJING INST OF REMOTE SENSING EQUIP
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