阅读说明：本技术 一种飞行器 (Aircraft ) 是由 李亚虾 于 2021-09-22 设计创作，主要内容包括：本发明公开了一种飞行器,包括依次连接的前端部件、中端部件和末端部件,还包括导体金属,所述末端部件均与所述的前端部件、中端部件的电流方向相反；所述前端部件、中端部件和末端部件之间通过导体相连接,所述中端部件的左右两侧均设置有磁吸滑动变阻器,所述前端部件、末端部件靠近所述中端部件的端部均设置有磁吸滑动变阻器。本发明具有如下优点：结构设计合理,速度快,且节能环保,可用于载人载货,具有很好的推广前景。(The invention discloses an aircraft, which comprises a front end component, a middle end component, a tail end component and conductor metal, wherein the front end component, the middle end component and the tail end component are sequentially connected; the front end part, the middle end part and the tail end part are connected through conductors, magnetic attraction sliding rheostats are arranged on the left side and the right side of the middle end part, and the magnetic attraction sliding rheostats are arranged at the end parts of the front end part and the tail end part close to the middle end part. The invention has the following advantages: the structure design is reasonable, the speed is high, the energy is saved, the environment is protected, the device can be used for carrying people and goods, and the popularization prospect is good.)

1. An aircraft, characterized in that: the current direction of the tail end part is opposite to that of the front end part and the middle end part; the front end part, the middle end part and the tail end part are connected through conductors, magnetic attraction sliding rheostats are arranged on the left side and the right side of the middle end part, and the magnetic attraction sliding rheostats are arranged at the end parts of the front end part and the tail end part close to the middle end part.

2. The aircraft of claim 1, wherein: the conductor is an arc-shaped wire.

3. The aircraft of claim 1, wherein: the conductor is a straight wire.

Technical Field

The invention relates to the technical field of underground tunnel type flight, in particular to an aircraft.

Background

Aircraft (flight vehicle) is an apparatus that flies in the atmosphere or in an extra-atmospheric space (space). Aircraft fall into 3 categories: aircraft, spacecraft, rockets, and missiles. Flying in the atmosphere is referred to as an aircraft, such as a balloon, airship, airplane, etc. They fly by the static buoyancy of air or the aerodynamic force generated by the relative movement of air. Flying in space is called a spacecraft, such as an artificial earth satellite, a manned spacecraft, a space probe, a space shuttle and the like. They are propelled by a launch vehicle to obtain the necessary velocity to enter space and then rely on inertia to make orbital motion similar to celestial bodies. The flying vehicle must fly underground and then fly in the atmosphere, and starts at the side of a tunnel, namely a switch, and the height of a conductor metal (namely an airship) can quickly rise.

The existing aircraft is not energy-saving and environment-friendly enough, and how to provide the aircraft which is reasonable in design, high in speed, energy-saving and environment-friendly becomes a research direction.

Disclosure of Invention

The invention aims to solve the problems in the background art and provide an aircraft.

In order to solve the technical problems, the technical scheme provided by the invention is as follows: an aircraft comprises a front end component, a middle end component and a tail end component which are connected in sequence, and further comprises conductor metal, wherein the current directions of the tail end component, the front end component and the middle end component are opposite; the front end part, the middle end part and the tail end part are connected through conductors, magnetic attraction sliding rheostats are arranged on the left side and the right side of the middle end part, and the magnetic attraction sliding rheostats are arranged at the end parts of the front end part and the tail end part close to the middle end part.

Preferably, the conductor is an arc-shaped wire.

Preferably, the conductor is a straight wire.

The invention has the following advantages: the structure has reasonable design, high speed, controllable speed, energy conservation and environmental protection, can be used for carrying people and goods, and has good popularization prospect.

Drawings

Fig. 1 is a schematic structural view of embodiment 1 of the present invention.

Fig. 2 is a schematic structural diagram of embodiment 2 of the present invention.

As shown in the figure: 1. front end component, 2, middle end component, 3, end component, 4, conductor, 5, magnetic slide rheostat, 6,

A conductive metal.

Detailed Description

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.

To facilitate an understanding of the invention, the invention will now be described more fully with reference to the accompanying drawings.

Preferred embodiments of the present invention are shown in the drawings. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

With reference to fig. 1, an aircraft comprises a front end component 1, a middle end component 2, a tail end component 3 and a conductor metal 6 (i.e. airship), wherein the current directions of the tail end component 3 and the front end component 1 and the middle end component 2 are opposite; the front end part 1, the middle end part 2 and the tail end part 3 are connected through a conductor 4, magnetic attraction sliding rheostat 5 are arranged on the left side and the right side of the middle end part 2, and the magnetic attraction sliding rheostat 5 are arranged at the end parts, close to the middle end part 2, of the front end part 1 and the tail end part 3.

As a preferred embodiment of this embodiment, the conductor 4 is an arc-shaped wire.

With reference to fig. 2, an aircraft comprises a front end component 1, a middle end component 2 and a tail end component 3 which are connected in sequence, and further comprises a conductor metal 6 (i.e. an airship), wherein the current directions of the tail end component 3 and the front end component 1 and the middle end component 2 are opposite; the front end part 1, the middle end part 2 and the tail end part 3 are connected through a conductor 4, magnetic attraction sliding rheostat 5 are arranged on the left side and the right side of the middle end part 2, and the magnetic attraction sliding rheostat 5 are arranged at the end parts, close to the middle end part 2, of the front end part 1 and the tail end part 3.

As a preferred embodiment of this embodiment, the conductor 4 is a straight wire. Can be used for space flight to reach light speed.

When the invention is implemented, two or more groups of equal power supplies are found, the power supplies are quickly and continuously converted on the same straight line, so that the current continuously runs forward, the invention is similar to a relay race mode, the two groups of power supplies are synthesized by connecting hundreds of small power supplies in parallel, and the power supplies are required to be added when the light speed is required to be reached. And (3) constructing a pipeline or a tunnel, wherein a right lower left groove is arranged in the tunnel, namely the concave aircraft, and a right lower left groove is formed into a convex aircraft, and the right lower left groove and the convex aircraft are matched. Hundreds or thousands of wires (red and blue) are found to be respectively disconnected with two different colors and straight lines to fill the pipeline in a circular mode, so that the magnetic wave is absorbed in the middle of the wave collection, and the magnetic wave collection can simultaneously wrap conductor metal (namely an aircraft) and run together, and the current can absorb all metal conductors, so that the conductor metal can both build the aircraft, carry people and goods, and do not need fuel (except space).

The principle of the invention is as follows: front-end component: when the switch is just started, the magnetic slide rheostat turns on the switch from small to large, so that the current moves forward all the time, and the metal moves forward; a middle-end component: namely, the power supply is continuously and discontinuously converted, so that the power supply always runs forward, and the metal conductor then runs forward; end: namely, the current direction is changed, and the magnetic switch is used to make the metal conductor fly.

The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features. The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the present invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.