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A symmetrical hexacopter

A six-axis aircraft, symmetrical technology, applied in the field of aircraft, can solve problems such as low safety and stability, low efficiency, and inability to self-rescue

Active Publication Date: 2017-10-10
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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  • A symmetrical hexacopter
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Embodiment Construction

[0009] The present invention will now be described in detail with reference to the drawings: a symmetrical six-axis aircraft, comprising a fuselage 1, a left composite wing 2, a right composite wing 3, a bracket 4, a front rotor 5, a rear rotor 6 and a landing gear 7. The fuselage 1 is equipped with a control system and airborne equipment. The left composite wing 2 and the right composite wing 3 have the same structure, and they are installed symmetrically 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 mounted on the front and rear ends of the fuselage 1 through brackets 4. The front rotor 5 and the rear rotor 6 are driven by two motors respectively. The front rotor 5 and the rear rotor 6 rotate in opposite directions, and the speed is convenient to adjust. The rotation plane of the front rotor 5 and the rotation plane of the rear rotor 6 are in the same horizontal plane. The front roto...

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Abstract

A symmetrical hexacopter belongs to the field of aircraft technology, comprising 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 and airborne equipment. The left composite wing and the right composite wing have the same structure, and they are symmetrically installed on the left and right sides of the fuselage. The front rotor and the rear rotor have the same structure, and they are respectively installed at the front and rear ends of the fuselage through brackets. The landing gear adopts skid and wheel combination structure. The left composite wing and the right composite wing have the same structure, and they are symmetrically installed on the left and right sides of the fuselage. There are two rotors inside each of the left and right composite wings, each powered by an engine. The vanes of the left compound wing include a front vane and a rear vane that can deflect around the wing axis. The symmetrical hexacopter has a small take-off and landing site and can vertically ascend and descend. The generated lift is large, safe, stable and flexible.

Description

Technical field [0001] A symmetrical six-axis aircraft belongs to the technical field of aircraft, and particularly relates to a six-axis aircraft. Background technique [0002] The traditional six-axis aircraft consumes a lot of energy when cruising, has poor stability and safety, and basically cannot save itself when it loses part or all of its power. Traditional airplanes cannot lift and hover vertically. 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 six-axis aircraft, airplanes and helicopters, and to invent an efficient and safe symmetrical six-axis aircraft that can take off and land vertically. [0004] A symmetrical six-axis aircraft includes 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...

Claims

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Application Information

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