阅读说明：本技术 阶梯电极环形大气动力机 (Step electrode annular big air power machine ) 是由 张玉福 于 2019-01-10 设计创作，主要内容包括：本发明阶梯电极环形大气动力机,为一种大气压差产生动力的动力机。环形底板上由外环板和内环板围成气流环道,由离子发生器产生的离子气流由高电压阶梯电极板以同性相斥加速,高速离子流减小环形内底板大气压与底板下面外部天然大气压形成压差动力,作为动力机。有环形密封上盖使环道内不受外界影响,环道内上部有离子气输入管进入离子,有带空气过滤器和空气孔的大气平衡管与外界大气相通。有高电压盒输出连线连到所有高电压阶梯电极板上,高电压盒上有控制动力大小旋钮。没有运动、传动、转动等机械部件,仅用电池供电子电路,极节能环保。可做出环形大小不同底面积变化动力大小,并可多个动力机串并联增加动力。用于航空低空飞行器上和飞行汽车上,作升力器和推力器,用于地面汽车和江河湖海船上作推力器,可直接带动发电机发电。本动力机广泛用于民用,工农业生产,国民经济和其他许多方面。(The invention relates to a step electrode annular atmospheric power machine, which is a power machine for generating power by atmospheric pressure difference. The annular bottom plate is surrounded by the outer ring plate and the inner ring plate to form an airflow loop, the ion airflow generated by the ion generator is accelerated by the high-voltage stepped electrode plates in a mode that like poles repel each other, and the high-speed ion flow reduces the pressure difference force formed by the atmospheric pressure of the annular inner bottom plate and the external natural atmospheric pressure below the bottom plate to serve as a power machine. The upper ring channel is provided with an annular sealing cover to prevent the interior of the ring channel from being influenced by the outside, the upper part in the ring channel is provided with an ion gas input pipe for entering ions, and an atmosphere balance pipe with an air filter and an air hole is communicated with the outside atmosphere. The output connecting wire of the high voltage box is connected to all the high voltage step electrode plates, and the high voltage box is provided with a knob for controlling the power. No mechanical parts such as movement, transmission, rotation and the like exist, and only a battery is used for supplying an electronic circuit, so that the energy is saved, and the environment is protected. The power size can be changed by changing the bottom area of the ring with different sizes, and a plurality of power machines can be connected in series and in parallel to increase the power. The high-speed propeller is used on an aviation low-altitude aircraft and a flying automobile as a booster and a thruster, is used on a ground automobile and a ship in rivers, lakes and seas as thrusters, and can directly drive a generator to generate electricity. The power machine is widely used in civil use, industrial and agricultural production, national economy and other aspects.)

1. The utility model provides an annular atmospheric power machine, includes the air current circuit, produces high-speed air current component, and the air current circuit is enclosed by annular bottom plate (1), outer annular plate (2), inner annular plate (3) that high-speed ion flow reduces the atmospheric pressure on the bottom plate and the natural atmospheric pressure outside the bottom plate produces the atmospheric pressure differential power: produce high-speed air current component by connect high-pressure ladder electrode board (6), control power size knob (15) in ladder electrode seal box (5) of the homopolar repulsion acceleration high-speed ion current on outer ring plate (2) constitute, its characterized in that: the bottom of an air flow loop formed by surrounding an annular bottom plate (1), an outer ring plate (2) and an inner ring plate (3) is input with ion current (A) through an ion gas inlet groove (11) by an ion gas input tube (10), the ion current enters the bottom of an ion generator box (16) through a gas inlet (21) to be ionized by the gas (Q) to be ionized, the ion current flows through round holes (22) around a discharge needle by a discharge needle (18) on a discharge needle voltage plate (19) added with high voltage (e) to generate, the ion current (A) is connected to the ion gas inlet (12) through an ion gas outlet (20), the high voltage generated by a high voltage box (14) is connected to all high voltage stepped electrode plates (6) through a high voltage connecting wire (F) to accelerate the ion current (A), the polarity on the high voltage stepped electrode plates (6) is the same as that of the accelerated ion current (A), the annular top of the air flow loop is provided with an annular sealing upper cover (, an atmosphere balance pipe (7) with an air filter (8) and an air hole (9) inside is communicated with the outside atmosphere.

The technical field is as follows:

the invention relates to an engine, in particular to a power machine which generates power by atmospheric pressure difference.

Background art:

the power machines are of various types and are widely applied. The atmospheric pressure difference is utilized to generate power, and the power is applied to human beings for a long time. Particularly, on an aviation aircraft, the aircraft wings generate lift force by utilizing the fact that the atmospheric pressure on the upper surface is smaller than the atmospheric pressure on the lower surface, and a helicopter rotor wing generates the lift force and also has thrust. According to a fifth new principle of high lift, atmospheric pressure is reduced only above an object, and natural atmospheric pressure is arranged below the object. The principle is to ionize working medium into ions, accelerate the ions by an electric field to generate high-speed ion flow, and calculate the reduced atmospheric pressure by the Bernoulli principle and a formula. On the aerospace, the ion thruster made by Newton's third law is applied to space satellites. The use of electric fields to accelerate ions to produce high velocity ion streams was proposed by Gordard, the father of the United states rocket in 1906, and space satellite high velocity ion streams have now reached thousands to tens of thousands of meters per second. When the device is used on the ground, the speed of the theoretical calculation airflow per second is more than 400 meters, and the reduced atmospheric pressure above an object is almost zero.

The Chinese patent of invention CN1264790A, applied by the inventor in 2000, reflects that the atmospheric power machine is invented by utilizing the mature technologies. The 'annular atmospheric power machine' declared in 03 and 12 months in 2010 and the 'simplified annular atmospheric power machine' declared in 03 and 25 months in 2010 respectively obtain the patent rights of Chinese inventions in 11 and 13 days in 2013 and 09 days in 01 and 09 months in 2013.

The invention content is as follows:

the invention is based on 'annular atmospheric power machine' and 'simplified annular atmospheric power machine', and is improved and perfected, so that the annular atmospheric power machine becomes a product which can be widely applied.

The invention solves the technical problems and adopts the following specific technical measures.

The annular bottom plate is surrounded by the outer ring plate and the inner ring plate to form an airflow loop, the ion flow at the bottom of the airflow loop is provided by the ion generator, and the ion flow is input to the annular bottom plate through the open slot with a certain angle by the ion gas pipe. A high-voltage polar plate for accelerating ions adopts a step polar plate. The upper sealing cover is arranged on the ring and is communicated with the outside atmosphere by an atmosphere balance pipe with an air filter and an air hole.

The beneficial effect of this way, has solved the shortcoming of prior art, makes it accomplish the product that can extensively safe application in a large number. The ion generator provides ions, and extremely abundant gas working medium raw materials are arranged on the earth. The high-voltage stepped electrode plate not only makes the electric field uniform, but also reduces the volume, material and cost of the shell. The upper surface of the ring is covered with a cover, so that the interior of the ring channel is not influenced by the outside, and the application is safe. The atmospheric balance pipe can make the atmospheric power machine work, the air filter arranged on the atmospheric balance pipe ensures that the gas in the loop is clean, ions are not influenced by external dust, water vapor and the like to be reduced, and the air holes ensure that the pressure of the air layer on the upper surface in the loop is balanced with the outside atmospheric pressure.

Description of the drawings:

FIG. 1 is a top view of an annular power ring of the present invention

FIG. 2 is a side view of an annular power ring of the present invention

FIG. 3 is a side view of an ionizer

FIG. 4 is a top view of an ionizer

FIG. 5 is a circuit diagram of an ionizer

In the figure, 1, an annular bottom plate, 2, an outer annular plate, 3, an inner annular plate, 4, an annular sealing upper cover, 5, a stepped electrode sealing box, 6, a high-voltage stepped electrode plate, 7, an atmospheric balance tube, 8, an air filter, 9, an air hole, 10, an ionic gas input tube, 11, an ionic gas outlet groove, 12, an ionic gas inlet, 13, an atmospheric inlet and outlet, 14, a high-voltage box, 15, a control power size knob, 16, an ion generator box, 17, an insulating partition plate, 18, a discharge needle, 19, a discharge needle electric pressure plate, 20, an ionic gas outlet, 21, a gas inlet to be ionized, 22, a circular hole around the discharge needle, A, an ion current, D, atmosphere, e, high voltage, F, a high-voltage connecting wire, Q gas to be ionized, L, high-speed airflow at the bottom in the ring, a section of an I, an electrode part, an I-I electrode part amplification part, a K, a switch, an E, a battery, an R, a resistor, BG., a triode, L1, a 1L 2, a primary coil, L3, a secondary coil, a transformer, a.

Detailed description of the preferred embodimentsthe invention will now be described in further detail with reference to the accompanying drawings in which:

referring to fig. 1, fig. 2, an air flow loop is enclosed by an outer ring plate (2) and an inner ring plate (3) on an annular base plate (1), an annular sealing upper cover (4) is arranged on the loop to protect the interior of the loop from being influenced by the outside, an ion air input pipe (10) at the upper part in the loop forms an inner bottom ion high-speed air flow (L) under the action of the same polarity repulsive force of an ion air outlet groove (11) in the loop, an ion flow (a) is sprayed to the annular base plate (1) and enters from an ion air inlet (12), an air filter (8) is arranged in an atmosphere balance pipe (7) at the upper part in the loop to prevent external dust, water and the like from entering the loop to influence the ion electrode plate, the ion flow (a) is communicated to an air hole (9) through the air filter (8) by an atmosphere inlet (13), when the pressure in the loop is lower than the outside atmospheric pressure, the atmospheric pressure is higher than the outside, the atmospheric pressure is higher than the atmospheric pressure, the ion flow (a) is communicated to the air hole (9) through an air outlet (I-outlet groove (6), and the high ion air outlet groove (6) is connected with a high ion power knob (14).

Referring to fig. 3, 4 and 5, ion current (a) is generated by introducing a working medium gas (Q) to be ionized into the bottom of an ion generator box (16) from a gas inlet (21) to be ionized, an array of discharge needles (18) are welded on a discharge needle pressure plate (19) at the bottom, the gas (Q) to be ionized passes through a circular hole (22) around the discharge needle on an insulating partition plate (17), the discharge needles (18) transform the gas (Q) to be ionized into the ion current (a) with the same polarity as the discharge needle (18) and the discharge needle pressure plate (19) thereof through physical and electrochemical actions, the ion current (a) is connected to an ion inlet (12) through an ion gas outlet (20), and enters the annular bottom plate (1) through an ion gas outlet groove (11) to form a thin-layer ring inner bottom ion high-speed gas flow (L), the atmospheric pressure on the annular bottom plate (1) is reduced, the ion current (a) forms a pressure difference with the natural atmospheric pressure outside the annular bottom plate, the annular bottom ion voltage (19) forms a high-voltage difference voltage with the discharge needle pressure plate (19), a high-voltage transformer (19) and a high-polarity voltage transformer (366) or a high-voltage transformer (366) which is connected with a high-polarity triode.

Application example:

the power machine of the invention has no mechanical movement, rotation and other parts. Fuel oil is not used, and only a battery is used for supplying the fuel oil to the electronic circuit, so that the energy is saved and the environment is protected. The thrust booster can be widely used on aviation aircrafts, particularly low-altitude aircrafts and flying automobiles below 3000 meters as a booster and a thruster. The power machine is used as a thruster on ground automobiles and ships in rivers, lakes and seas, can directly drive a generator to generate electricity, and converts atmospheric static pressure energy into electric energy.

The power machine of the invention can be used for manufacturing various power machines with different power of different sizes of the base plate area, and a plurality of power machines can be connected in series and in parallel to increase the power.

The power machine of the present invention may be used widely in civil use, industrial and agricultural production, national economy and other fields.