阅读说明：本技术 一种飞行器 (Aircraft ) 是由 薛礼强 薛童 于 2021-01-29 设计创作，主要内容包括：本发明公开一种飞行器,包括飞行器本体；飞行器本体包括碟型的壳体,壳体的最大直径外缘处设有多个用于水平移动的喷气孔,其上下两面均设有出气窗和用于上下移动的通气管；壳体的上下两面分别设有上叶轮和下叶轮,上叶轮和下叶轮的叶片端部均设有电刷,其边缘处设有与出气窗连通的储气室；上叶轮与下叶轮外缘中间环绕固设有多个锥齿；壳体的顶部和底部中心分别设有第一进气窗和第二进气窗；第一进气窗和第二进气窗内设有连通的仓门。本发明的有益效果：本发明为一个稳固的整体,上下对称,流线型设计,空气阻力小,恶劣的天气也不会影响正常飞行,设计新颖,结构合理,作为一种新兴的交通工具,极大的方便了人们的出行,可大面积推广应用。(The invention discloses an aircraft, which comprises an aircraft body; the aircraft body comprises a dish-shaped shell, a plurality of air injection holes for horizontal movement are arranged at the outer edge of the maximum diameter of the shell, and an air outlet window and an air pipe for up-and-down movement are arranged on the upper surface and the lower surface of the shell; the upper surface and the lower surface of the shell are respectively provided with an upper impeller and a lower impeller, the blade ends of the upper impeller and the lower impeller are respectively provided with an electric brush, and the edge of the upper impeller and the lower impeller is provided with an air storage chamber communicated with the air outlet window; a plurality of bevel teeth are fixedly arranged around the middle of the outer edges of the upper impeller and the lower impeller; the center of the top and the bottom of the shell is respectively provided with a first air inlet window and a second air inlet window; and bin doors communicated with each other are arranged in the first air inlet window and the second air inlet window. The invention has the beneficial effects that: the invention is a stable whole, is symmetrical up and down, has streamlined design, small air resistance, novel design and reasonable structure, does not influence normal flight in severe weather, is a novel traffic tool, greatly facilitates the travel of people, and can be popularized and applied in a large area.)

1. An aircraft, comprising an aircraft body, characterized in that:

the aircraft body comprises a dish-shaped shell; a plurality of air injection holes for horizontal movement are formed in the outer edge of the maximum diameter of the shell; the air injection hole windowing is controlled by a control rod; the upper surface and the lower surface of the shell are both provided with an air outlet window and an air pipe used for moving up and down; the upper surface and the lower surface of the shell are respectively provided with an upper impeller and a lower impeller; the blades of the upper impeller and the lower impeller rotate in opposite directions and synchronously; the blade ends of the upper impeller and the lower impeller are respectively provided with an electric brush; the edges of the upper impeller and the lower impeller are provided with air storage chambers communicated with the air outlet window; a plurality of bevel teeth are fixedly arranged around the middle of the outer edges of the upper impeller and the lower impeller; the center of the top and the bottom of the shell is respectively provided with a first air inlet window and a second air inlet window; bin doors communicated with each other are arranged in the first air inlet window and the second air inlet window;

the control vision of the aircraft body is provided by an external camera.

2. The aircraft of claim 1, wherein: the gas injection holes are cylindrical gas injection holes; the vent pipe is of a cylindrical structure; the number of the vent pipes is four.

3. The aircraft of claim 1, wherein: the number of the bevel teeth is six.

4. The aircraft of claim 1, wherein: the blades of the aircraft body are in an involute shape, the position close to the center of a circle in the aircraft body is of a fish scale-shaped structure, and the position close to the outer edge of the tail part is 40% of the fish tail-shaped structure and is provided with barbs; the blades of the aircraft body are concave near the center of a circle, the outer edges of the blades are straight near the outer edges, and the blades are clamped by plane plates arranged up and down.

Technical Field

The invention relates to the technical field of vehicles, in particular to an aircraft.

Background

Vehicles in the narrow sense refer to all man-made devices for human mobility or transportation.

At present, vehicles are an indispensable part of modern life. With the change of times and the progress of science and technology, more and more vehicles around people bring great convenience to the life of each person. The distance of people to meet is greatly shortened by using the land automobile, the ship in the sea and the airplane in the sky; the invention of rocket and spacecraft makes the human ideal for exploring another planet. In perhaps the near future, people may travel to space to visit, and each person may go to another planet to investigate learning.

Disclosure of Invention

To solve the above existing problems, the present invention provides an aircraft. The invention is realized by the following technical scheme.

An aircraft comprising an aircraft body;

the aircraft body comprises a dish-shaped shell; a plurality of air injection holes for horizontal movement are formed in the outer edge of the maximum diameter of the shell; the air injection hole windowing is controlled by a control rod; the upper surface and the lower surface of the shell are both provided with an air outlet window and an air pipe used for moving up and down; the upper surface and the lower surface of the shell are respectively provided with an upper impeller and a lower impeller; the blades of the upper impeller and the lower impeller rotate in opposite directions and synchronously; the blade ends of the upper impeller and the lower impeller are respectively provided with an electric brush; the edges of the upper impeller and the lower impeller are provided with air storage chambers communicated with the air outlet window; a plurality of bevel teeth are fixedly arranged around the middle of the outer edges of the upper impeller and the lower impeller; the center of the top and the bottom of the shell is respectively provided with a first air inlet window and a second air inlet window; bin doors communicated with each other are arranged in the first air inlet window and the second air inlet window;

the control vision of the aircraft body is provided by an external camera.

Preferably, the gas injection holes are cylindrical gas injection holes; the vent pipe is of a cylindrical structure; the number of the vent pipes is four.

Preferably, the number of the bevel teeth is six.

Preferably, the blades of the aircraft body are involute, the position close to the center of a circle in the aircraft body is of a fish scale structure, and the position close to the outer edge of the tail part is 40% similar to the fish tail structure and is provided with barbs; the blades of the aircraft body are concave near the center of a circle, the outer edges of the blades are straight near the outer edges, and the blades are clamped by plane plates arranged up and down.

The invention has the beneficial effects that: the invention is a stable whole, is symmetrical up and down, has a streamlined design, has small air resistance, cannot influence normal flight in severe weather, and cannot break blades by strong wind; the helicopter can take off and land as well as the airplane can propel; the novel design, it is rational in infrastructure, as a new emerging vehicle, very big the trip of having made things convenient for people, can popularize and apply by a large scale.

Drawings

FIG. 1 is a schematic view of the overall structure of an aircraft of the present invention;

FIG. 2 is a block diagram of the upper impeller of the present invention;

fig. 3 is a structural view of a lower impeller in the present invention.

Detailed Description

The technical scheme of the invention is more fully explained in detail by combining the attached drawings.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be considered as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.

Detailed description of the preferred embodimentsfor embodiment 1, an aircraft comprises an aircraft body;

the aircraft body comprises a dish-shaped shell 1, a plurality of air injection holes 2 for horizontal movement are arranged at the maximum diameter outer edge of the shell 1, the air injection holes 2 are cylindrical air injection holes, the windows of the air injection holes 2 are controlled by a control rod, air outlet windows 3 and air pipes 4 for up-and-down movement are arranged on the upper surface and the lower surface of the shell 1, the air pipes 4 are cylindrical structures, the number of the air pipes is four, and the four air pipes in the middle are switched to use in the air inlet windows at the edges of the upper cabin door and the lower cabin door (on a water stop surface, people enter from the upper surface, and people enter; the upper and lower two sides of the shell 1 are respectively provided with an upper impeller 5 and a lower impeller 6, the rotation directions of the blades of the upper impeller 5 and the lower impeller 6 are opposite and synchronously rotate, the end parts of the blades of the upper impeller 5 and the lower impeller 6 are respectively provided with an electric brush 7, the edges of the upper impeller 5 and the lower impeller 6 are provided with an air storage chamber 8 communicated with the air outlet window 3, wherein the middle of the outer edges of the upper impeller 5 and the lower impeller 6 is surrounded by six conical teeth 9 to prevent unstable current control, the rotating speeds of the upper impeller 5 and the lower impeller 6 are opposite and synchronous, the upper impeller and the lower impeller use centrifugal force to carry air and hydraulic pressure to the edges and stabilize the action of the machine body (gyroscope principle), the top and the bottom center of the shell 1 are respectively provided with a first air inlet window 10 and a second air inlet window 11, and a cabin door 12 communicated with each other is arranged in the first air inlet window.

The blade of the aircraft body is in an involute shape, the inner part of the aircraft body is approximately 60% of the center of a circle and is in a fish scale-shaped structure (the blade is slightly like a ratchet wheel after being provided with a radian), the tail part of the aircraft body is approximately 40% like a fishtail and is provided with barbs (the blade is smooth from the center to the outer edge, otherwise, the blade is similar to the barbs), the blade is approximately recessed in the center of the circle, the edge part of the aircraft body (the fishtail) is.

The power of aircraft body is pure electronic, leans on blade edge charcoal brush to rotate at a high speed under the lorentz effect, and similar electromagnetic guide rail big gun principle, each fumarole windowing is controlled by a control lever (all around about from top to bottom), is equipped with the barb on the blade in order to prevent that air chamber pressure is big, the backward flow.

The control vision of the aircraft body is provided by the outer camera.

The invention is a stable whole, is symmetrical up and down, has a streamlined design, has small air resistance, cannot influence normal flight in severe weather, and cannot break blades by strong wind; the helicopter can take off and land as well as the airplane can propel; the novel design, it is rational in infrastructure, as a new emerging vehicle, very big the trip of having made things convenient for people, can popularize and apply by a large scale.

In the present invention, unless otherwise specifically stated or limited, the terms "mounted," "connected," "fixed," and the like are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly above and obliquely above the second feature, or simply meaning that the first feature is at a lesser level than the second feature.

In the description herein, reference to the terms "one embodiment," "some embodiments," "an example," "a specific example," or "some examples" or the like means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the present invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention should be included in the scope of the present invention.