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Multi-axis aircraft

An aircraft and aviation technology, applied in the field of aircraft, can solve the problems that aircraft are easily affected by air pressure and air flow, the aircraft structure is simple, and the functionality is low, so as to achieve the effect of stabilizing wind pressure and air flow, preventing crashes, and reducing volume

Inactive Publication Date: 2019-06-18
郭屹
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The object of the present invention is to provide a multi-axis aircraft in order to solve the problem that the aircraft is easily affected by the air pressure and air flow and often crashes during the use of the aircraft, and the existing aircraft has a simple structure and low functionality. aviation vehicle

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0035] A multi-axis aviation aircraft, comprising an aircraft main body, a power chamber is arranged at the bottom of the aircraft main body, a spiral disk is rotatably connected to the top of the aircraft main body through a connecting seat, and ground supports are fixedly connected to both sides of the aircraft main body, The floor support includes an arc support, a load-bearing rod and a landing rod, the load-bearing rod is fixed on one side of the arc-shaped support, the landing rod is fixed on the other side of the load-bearing rod, and the bottom of the landing rod is fixed A spacer is connected, the surface of the arc-shaped bracket is embedded with reinforcing ribs, a support arm is fixedly connected around the spiral disk, one side of the support arm is fixedly connected with an embedding block, and the other side of the support arm One end of one side is rotatably connected with a positive rotor, the other end of the other side of the support arm is rotatably connecte...

Embodiment 2

[0037] A multi-axis aviation aircraft, comprising an aircraft main body, a power chamber is arranged at the bottom of the aircraft main body, a spiral disk is rotatably connected to the top of the aircraft main body through a connecting seat, and ground supports are fixedly connected to both sides of the aircraft main body, The floor support includes an arc support, a load-bearing rod and a landing rod, the load-bearing rod is fixed on one side of the arc-shaped support, the landing rod is fixed on the other side of the load-bearing rod, and the bottom of the landing rod is fixed A spacer is connected, the surface of the arc-shaped bracket is embedded with reinforcing ribs, a support arm is fixedly connected around the spiral disk, one side of the support arm is fixedly connected with an embedding block, and the other side of the support arm One end of one side is rotatably connected with a positive rotor, the other end of the other side of the support arm is rotatably connecte...

Embodiment 3

[0039] A multi-axis aviation aircraft, comprising an aircraft main body, a power chamber is arranged at the bottom of the aircraft main body, a spiral disk is rotatably connected to the top of the aircraft main body through a connecting seat, and ground supports are fixedly connected to both sides of the aircraft main body, The floor support includes an arc support, a load-bearing rod and a landing rod, the load-bearing rod is fixed on one side of the arc-shaped support, the landing rod is fixed on the other side of the load-bearing rod, and the bottom of the landing rod is fixed A spacer is connected, the surface of the arc-shaped bracket is embedded with reinforcing ribs, a support arm is fixedly connected around the spiral disk, one side of the support arm is fixedly connected with an embedding block, and the other side of the support arm One end of one side is rotatably connected with a positive rotor, the other end of the other side of the support arm is rotatably connecte...

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Abstract

The invention discloses a multi-axis aircraft. The multi-axis aircraft comprises an aircraft body. A power chamber is formed in the bottom of the aircraft body, a spiral disc is rotatably connected tothe top end of the aircraft body through a connecting base, and landing supports are fixedly connected to two sides of the aircraft body. Each landing support comprises an arc-shaped support, a loadbearing rod and a landing rod. The load bearing rods are fixed to one sides of the arc-shaped supports, and the landing rods are fixed to the other sides of the load bearing rods. Cushion blocks are fixedly connected to the bottoms of the landing rods. By setting the included angles between forward rotors and reverse rotors as 0 degree, 45 degrees and 180 degrees, the forward rotors and the reverse rotors coincide when the aircraft stops running, and accordingly, the aircraft is downsized. When the aircraft operates, the wind pressure and the air flow are stabilized through the rotation anglesof the forward rotors and the reverse rotors, the forward rotors and the reverse rotors can be effectively placed in symmetry, and accordingly, the wind pressure and the air flow are stabilized through the forward rotors and the reverse rotors.

Description

technical field [0001] The invention belongs to the technical field of aircraft, in particular to a multi-axis aviation aircraft. Background technique [0002] An aircraft is a device that flies in the atmosphere or in extraatmospheric space (space). Aircraft are divided into 3 categories: aircraft, spacecraft, rockets and missiles. Those flying in the atmosphere are called aircraft, such as balloons, airships, airplanes, etc. They rely on the static buoyancy of the air or the aerodynamic force generated by the relative motion of the air to lift into the air. Those flying in space are called spacecraft, such as artificial earth satellites, manned spacecraft, space probes, and space shuttles. Propelled by the launch vehicle, they gain the necessary speed to enter space, and then rely on inertia to do orbital motions similar to celestial bodies. They are manufactured by humans, can fly off the ground, fly in space and are controlled by humans in the atmosphere or outside th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C27/32B64C25/32
Inventor 不公告发明人
Owner 郭屹
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