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A hovercraft and its control method

A control method and technology for hovercraft, which are applied in the directions of air cushion, vehicle parts, transportation and packaging, etc., can solve the problems of easy wear and complex structure of hovercraft, and achieve the effect of reducing wear and friction.

Active Publication Date: 2021-09-07
昆山合朗航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the problems of the existing hovercraft such as easy wear and tear and complex structure, the present invention provides a hovercraft, comprising:

Method used

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  • A hovercraft and its control method
  • A hovercraft and its control method
  • A hovercraft and its control method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0061] refer to Figure 1-9 , the present invention provides a hovercraft, including a hull 1, two first propeller modules 4, two second propeller modules 5 and a control circuit board module; including a hull 1, at least one first propeller module 4, at least one second The propeller module 5 and the control circuit board module; the hull is provided with a plurality of exhaust holes 105; the first propeller module 4 is connected to the hull 1, and the first propeller module 4 can generate the first power, and the first power can pass through the exhaust holes 105; the second propeller module 5 is connected to the hull 1, and the second propeller module 5 can generate a second power, and the second power can push the hull 1 to run; the control circuit board module is installed on the hull, and the control circuit board The module can control the first propeller module and the second propeller module so that the first propeller module and the second propeller module control th...

Embodiment 2

[0095] refer to Figure 11-12 , this embodiment is a modification carried out on the basis of Embodiment 1. This embodiment extracts the control circuit board module 2, two first propeller modules 4, and two second propeller modules 5 removed from the hovercraft provided in Embodiment 1. And the battery modules are directly assembled to form an aircraft.

[0096] Specifically, the front left and right sides of the control circuit board module 2 and the rear left and right sides are respectively provided with a first slot structure, and the sides of the first propeller module 4 and the second propeller module 5 are provided with a first plug-in structure. The first propeller module 4 is directly horizontally installed into the first slot structure on the left and right sides of the front end of the control circuit board module 2 through the first plug-in structure, and the two second propeller modules are directly horizontally installed on the back of the control circuit board ...

Embodiment 3

[0099] This embodiment provides a method for controlling a hovercraft, wherein the hovercraft is the hovercraft in Embodiment 1. The control methods of the hovercraft mainly include:

[0100] The control circuit board module first controls the first propeller module to change the state of the hull; the control circuit board module then controls the second propeller module to change the state of the hull;

[0101] Or, the control circuit board module first controls the second propeller module to change the state of the hull; the control circuit board module then controls the first propeller module to change the state of the hull;

[0102] Or, the circuit board module simultaneously controls the first propeller module and the second propeller module to change the state of the hull.

[0103] In this embodiment, controlling the first propeller module by the control circuit board module to change the state of the hull specifically includes: controlling the intelligent main control...

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Abstract

The invention discloses a hovercraft and a control method thereof. The hovercraft comprises: a hull, the hull is provided with a plurality of exhaust holes; at least one first propeller module is connected with the hull, and the first propeller module can generate First power, the first power can pass through the exhaust hole; at least one second propeller module, the second propeller module is connected with the hull, and the second propeller module can generate second power, and the second power can push the hull run. The control circuit board module is installed on the hull; the control circuit board module is provided with an intelligent main control module, and the intelligent main control module is used to control the speed and steering of the first propeller module and the second propeller module, so as to realize the control of the hovercraft route. The control method of the hovercraft provided by the present invention can realize the control of the forward, reverse and steering of the hovercraft directly through the control of the propeller rotation speed and steering on the two second propeller modules respectively, and the structure is simple and the operation is convenient.

Description

technical field [0001] The invention relates to the technical field of ship design, in particular to a hovercraft and a control method thereof. Background technique [0002] Hovercraft is a ship that uses high-pressure air to form an air cushion between the bottom of the ship and the water surface or the ground to lift all or part of the hull, thereby greatly reducing the resistance of the hull during navigation and realizing high-speed navigation. [0003] The bottom of the existing hovercraft is usually provided with a flexible air-sealing device, which usually requires a blower to press air to the bottom flexible air-sealing device to make it bulge to form an air cushion. [0004] After the above-mentioned existing hovercraft is used for a long time, it is easy to cause wear and tear of the flexible air-sealing device, and it is not suitable for land driving; moreover, the existing hovercraft has a complicated structure, and screws or other auxiliary materials are needed ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B60V1/00B60V1/14B60V1/18
CPCB60V1/00B60V1/14B60V1/18
Inventor 袁舟
Owner 昆山合朗航空科技有限公司
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