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Air-ground amphibious manned carrier aircraft

An aircraft, ground and air technology, applied in the field of manned aircraft, can solve the problems of large rotor size and inconvenient driving, and achieve the effects of high safety, ease of congestion, and high practicability

Inactive Publication Date: 2017-06-06
李春石
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention aims to solve the problem that the rotor on the existing ducted rotor flying vehicle is too large and inconvenient to drive on the road, and further provides a ground-air amphibious manned and loaded aircraft

Method used

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  • Air-ground amphibious manned carrier aircraft
  • Air-ground amphibious manned carrier aircraft
  • Air-ground amphibious manned carrier aircraft

Examples

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specific Embodiment approach 1

[0019] Specific implementation mode one: combine Figure 1 to Figure 6 Illustrate the present embodiment, a kind of land-air amphibious manned and loaded aircraft, it comprises vehicle body 1, control box 2 and some ducted rotors 3, control box 2 is arranged on the top of vehicle body 1, and each ducted rotor 3 all comprises Guard ring and several evenly distributed propeller blades, it also includes vertically arranged rotor shaft 4, one or more horizontally arranged rotor brackets 5, each of the two ends of each rotor bracket 5 is horizontally fixed to a ducted rotor 3 , each rotor bracket 5 includes a fixed rod 51 and two telescopic rods 52, the two telescopic rods 52 are respectively slidably connected to the two ends of the fixed rod 51 along the length direction of the fixed rod 51, and the middle part of each rotor bracket 5 is respectively The rotor shaft 4 is rotatably fixed on the top of the control box 2. When the aircraft is running on the ground, several rotor bra...

specific Embodiment approach 2

[0028] Specific implementation mode two: combination Figure 1 to Figure 6 Illustrate the present embodiment, a kind of land-air amphibious manned and loaded aircraft, it comprises vehicle body 1, control box 2 and two ducted rotors 3, control box 2 is arranged on the top of vehicle body 1, each ducted rotor 3 It includes a retaining ring and several evenly distributed propeller blades, and it also includes a vertically arranged rotor shaft 4, two horizontally arranged rotor supports 5 arranged parallel to each other, and each rotor support 5 includes a fixed rod 51 and a telescopic rod 52 One end of the fixed rod 51 is rotatably fixed on the top of the control box 2 through the rotor shaft 4, the ducted rotor 3 is fixed on one end of the telescopic rod 52, and the other end of the telescopic rod 52 is slidably connected along the length direction of the fixed rod 51. At the other end of the fixed rod 51, when the aircraft is flying, the two ducted rotors 3 are symmetrically a...

specific Embodiment approach 3

[0034] Specific implementation mode three: combination Figure 1~6To illustrate this embodiment, the rotor shaft 4 includes a plurality of coaxial and rotatably fixed tube shafts 41, the rotor shaft 4 is rotatably fixed above the control box 2, and each tube shaft 41 is provided with an internal The number of the ring gear 42 and the tube shaft 41 is consistent with the number of the rotor bracket 5, and one rotor bracket 5 is fixedly connected with a tube shaft 41. The control box 2 is provided with a motor 21, and several tube shafts 41 pass through the gear pair 43 in turn. Connect with motor 21. Designed in this way, the gear pair includes some gears and some internal gear rings that mesh with each other. For example, when the aircraft is provided with two rotor brackets 5, the motor drives the bottom internal gear ring to rotate through a gear, thereby driving the bottom tube. The shaft rotates, and the uppermost tube shaft is rotated by meshing with the uppermost intern...

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Abstract

The invention provides an air-ground amphibious manned carrier aircraft, and belongs to the technical field of means of transportation. The invention solves the problem that a rotor on an existing ducted rotor flying vehicle is too large and is inconvenient for the existing ducted rotor flying vehicle to travel on a road. Each of two ends of each rotor bracket is horizontally and fixedly connected with a ducted rotor, each rotor bracket comprises a fixed rod and two telescopic rods, the two telescopic rods are in slip connection with two ends of the fixed rod respectively in the length direction of the fixed rod, and the middle of each rotor bracket is rotationally and fixedly connected above a control box through a rotor shaft respectively; when the aircraft runs on the ground, a plurality of rotor brackets are arranged up and down directly facing one another and are in a contraction state; and when the aircraft is in a flight state, a plurality of ducted rotors are arranged in uniform distribution around the axis of the rotor shaft, and the rotor brackets are in an extension state. The air-ground amphibious manned carrier aircraft provided by the invention is used for road running and low-altitude flying.

Description

technical field [0001] The invention relates to a manned aircraft, in particular to a ground-air amphibious manned and loaded aircraft. Background technique [0002] An aircraft is a flying object that can fly off the ground, fly in space and be controlled by humans. With the development of science, various aircrafts have gradually appeared, such as a ducted rotor-mounted vehicle that appeared in order to relieve road traffic pressure. The human flying vehicle can not only realize vertical take-off and landing and hovering flight like a helicopter, but also can drive on ordinary roads. It is a three-dimensional transportation tool that is convenient for travel and has a wide range of uses. [0003] Most of the existing ducted rotor flying vehicles cannot meet the respective industry regulations for flying and road driving, so in practice the following problems occur: 1, the ducted rotor size is too large and the installation position does not meet the country's road driving ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B60F5/02B64C27/08
CPCB64C27/08B60F5/02
Inventor 李春石
Owner 李春石