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An aircraft with rotatable electric motors

An aircraft and wing technology, applied in the field of aircraft, can solve problems such as being unable to fly for a long time, and achieve the effects of saving take-off and landing time, improving flight safety factor, and improving efficiency

Inactive Publication Date: 2019-01-25
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the constraints of battery technology, multi-rotor drones cannot fly for a long time, and the horizontal flight speed teaches fixed-wing aircraft to be slower.

Method used

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  • An aircraft with rotatable electric motors

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Embodiment Construction

[0014] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0015] The embodiment of the present invention discloses an aircraft with a rotatable motor, which can not only improve the flight safety factor but also maintain the flying state for a long time, and can also perform vertical take-off and landing in any open field, because the aircraft with a rotatable motor does not A runway is needed so the take-off and landing time is saved, and the efficiency can be improved to the greatest extent when dealing with any tas...

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Abstract

The invention relates to an aircraft with rotatable electric motors, belonging to the technical field of aircraft, in particular to an aircraft with rotatable electric motors, comprising a fuselage, awing, a tail wing, an electric motor, a propeller, a bearing rod, a fixed rod and a landing gear; wherein the fuselage is internally provided with an engine. The wing is divided into two fins with the same size and the same function, and the two fins are symmetrically distributed on the fuselage. The tail fin is at the tail part of the fuselage; Four electric motors are symmetrically distributedon the wings, and the propellers are composed of the same-sized airfoils and are respectively distributed on the electric motors. The bearing rod is divided into four wings and a motor. The fixed rodis connected with the fixed wing. The landing gear is mounted on the lower part of the wing. The invention not only can improve the flight safety coefficient but also can maintain the flight state fora long time, and can carry out vertical take-off and landing in any open field.

Description

technical field [0001] The invention relates to the technical field of aircraft, and more specifically relates to an aircraft with a rotatable motor. Background technique [0002] Traditional aircraft can be divided into fixed-wing aircraft, helicopters and multi-rotor aircraft. Among them, the fixed-wing aircraft has fast flight speed, high maneuverability, large flight radius, and high safety performance factor. However, due to its own limitations, the conditions for take-off are harsh, and the take-off of the fixed-wing aircraft must have a long enough runway. Helicopters can take off and land vertically, but their structures are complicated, and it takes a lot of money to train helicopter pilots. It requires high driving skills and cannot be widely promoted. In recent years, the development of multi-rotor drones has given aviation vehicles another development direction. It does not need a runway and can directly lift vertically. However, due to the constraints of batte...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/28B64C27/52
CPCB64C27/28B64C27/52
Inventor 王鹏飞王志成
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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