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Efficient aircraft

An aircraft and high-efficiency technology, applied in the field of aircraft, can solve the problems of long take-off time and inconvenient change of direction in the air, etc., and achieve the effect of not being easily damaged

Inactive Publication Date: 2018-04-27
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the advancement of science and technology, aircraft has gradually entered people's sight, and has been widely used in surveying, agriculture, military, mail, emergency rescue, and places where people need to work in the air in daily life, but the take-off time of traditional aircraft is time-consuming. Long, inconvenient to change direction in the air

Method used

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Embodiment Construction

[0010] Now in conjunction with accompanying drawing the present invention is described in detail, a kind of high-efficiency aircraft, comprises fuselage 1, rotor 2, strut rod 3, motor 4, annular protection shell 5, electromagnet 6 and landing wheel 7.

[0011] The fuselage 1 is equipped with a control system and airborne equipment. The blades of the rotor 2 are symmetrical and can adjust the windward angle of the blades between 0-30 degrees. The support rods 3 are hollow structures distributed on both sides of the fuselage 1 . The motor placement device is located at the outer end of each support rod 3 and fitted. The motor placement device can rotate horizontally on the support rod 3 . The motor 4 is placed on the motor placement device 6 . The middle part of the edge of the ring-shaped protective shell 5 has a ring-shaped smooth concave structure in which the tip of the rotor 2 can be placed. The take-off and landing wheels 7 are retractable into the fuselage.

[0012] ...

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Abstract

The invention belongs to the technical field of aircrafts, and particularly relates to the efficient aircraft. The efficient aircraft comprises a fuselage, a rotor wing, supporting rods, motors, an annular protection shell and motor storing devices and taking-off and landing wheels. The fuselage is internally provided with a control system and airborne equipment. Wing blades of the rotor wing aresymmetrical, and the windward angles of the wing blades can be adjusted within 0-30 degrees. The supporting rods are each of a hollow structure and distributed on both sides of the fuselage. The motorstoring devices are located at the outer ends of the supporting rods and matched with the outer ends of the supporting rods. The motor storing devices can rotate horizontally on the supporting rods.The motors are stored on the motor storing devices. The middle of the edge of the annular protection shell is of an annular inner smooth concave structure, and wing tips of the rotor wing can be stored in the annular inner smooth concave structure. The taking-off and landing wheels can be retracted into the fuselage. The efficient aircraft is safe and stable, and is not prone to being destroyed.

Description

technical field [0001] A high-efficiency aircraft belongs to the technical field of aircraft, and in particular relates to an efficient aircraft. Background technique [0002] With the advancement of science and technology, aircraft has gradually come into people's sight, and has been widely used in surveying, agriculture, military, mail, emergency rescue, and places where people need to work in the air in daily life, but the take-off time of traditional aircraft is time-consuming. It is too long, and it is inconvenient to change direction in the air. Contents of the invention [0003] The purpose of the present invention is to overcome the above-mentioned deficiency of traditional aircraft, and invent a high-efficiency aircraft with simple structure and high efficiency that is convenient to control. [0004] A high-efficiency aircraft includes a fuselage, a rotor, a support pole, a motor, an annular protective case, a motor placement device and landing wheels. [0005] ...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/00B64C25/10B64C25/36B64D27/24B64D27/26
CPCB64C25/10B64C25/36B64C27/006B64C27/08B64D27/24B64D27/40
Inventor 王志成王鹏飞
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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