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Amphibious multifunctional vertical take-off and landing aircraft

A vertical take-off and landing, aircraft technology, applied in the direction of vertical take-off and landing aircraft, aircraft, convertible aircraft, etc., can solve the problems of high cost, aircraft relying on manual handling, falling into water, etc., to ensure flexibility, reduce costs, The effect of simplifying the structure

Active Publication Date: 2016-10-12
SHENYANG AEROSPACE UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, whether it is a helicopter in the traditional sense or a multi-rotor that is popular now, without adding additional power devices, they all lack the ability to move on land and water.
In special areas where flying is restricted or the space is low, the aircraft can only be carried manually, and there is a danger of falling into the water when flying above the water in case of an emergency and an emergency landing
All of the above seriously limit the function of vertical take-off and landing aircraft
If an additional power unit is added to achieve land and water navigation capabilities, it will not only make the aircraft structure more complex and cost higher, but also increase the weight of the aircraft itself

Method used

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  • Amphibious multifunctional vertical take-off and landing aircraft
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  • Amphibious multifunctional vertical take-off and landing aircraft

Examples

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Embodiment Construction

[0030] The structural composition of the amphibious multifunctional vertical take-off and landing aircraft includes: a propeller 1, a DC brushless motor 2, a steering gear 3, a stepping motor 4 and a support base 8; the DC brushless motor 2 is connected to the propeller 1, and the DC brushless motor 2 is the main power output unit, which provides power for the aircraft by driving the propeller 1 to rotate; the steering gear 3 is connected with the DC brushless motor 2 and the propeller 1 through the steering gear control arm 6 to control the horizontal deflection angle of the rotating surface of the propeller 1 , to realize the vertical climbing and forward flight of the aircraft; the stepper motor 4 is arranged on the support base 8, and controls the propeller 1 by being connected with the steering gear control arm; the support base 8 is a four-leg support base, and the support base 8 can be disassembled and replaced with a pulley base 9 or a boat-shaped base 10.

[0031] The...

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PUM

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Abstract

The invention mainly provides a vertical take-off and landing aircraft with a novel framework. The vertical take-off and landing aircraft comprises a propeller, a brushless direct current motor, a steering engine, a stepping motor and a supporting base. The brushless direct current motor is connected with the propeller. The brushless direct current motor is a main power output unit and drives the propeller to rotate to provide power for the aircraft. The steering engine is connected with the brushless direct current motor and the propeller through a steering engine operating arm and controls the horizontal deflection angle of a rotation face of the propeller, and vertical climbing and forward flight of the aircraft are achieved. The stepping motor is arranged on the base and connected with the steering engine operating arm. The supporting base is a four-leg supporting base and can be dismounted and replaced with a pulley base or a ship-shaped base. The aircraft is stable and reliable in structure, an aerial navigation mode, a land navigation mode and a water navigation mode are switched conveniently, and the aircraft can be much developed on manned aircrafts for civil use, investigation aircrafts for military use, water search-and-rescue aircrafts and other.

Description

technical field [0001] The invention belongs to the field of aircraft manufacturing, and in particular relates to a novel aircraft structure, which can simultaneously satisfy various navigation modes such as air flight, land navigation and water surface navigation under the condition of using a single power system. Background technique [0002] Compared with fixed-wing aircraft, vertical take-off and landing aircraft are favored by many people because of their smaller take-off site restrictions and stronger air retention capabilities in small areas. However, whether it is a helicopter in the traditional sense or a multi-rotor that is popular now, without adding additional power devices, they all lack the ability to move on land and water. In special areas where flight is restricted or the space is low, the aircraft can only be transported manually, and there is a danger of falling into the water when an emergency landing is required when flying above the water. Above all, h...

Claims

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Application Information

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IPC IPC(8): B60F5/02B64C37/00B64C27/52B64C29/00
CPCB64C27/52B64C29/00B64C37/00B60F5/02B64U10/10
Inventor 孟光磊潘海兵梁宵田丰薛继佳朱琳琳喻勇涛
Owner SHENYANG AEROSPACE UNIVERSITY
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