CN117287299A - Ma Daxi Qifeng conch PD-X95 closed cycle engine and method - Google Patents

Abstract

The invention relates to the technical field of engines, in particular to a motor Sichuan North wind-blown conch PD-X95 closed-cycle engine and a method. The engine is started to ignite, the wood durian is ignited, a proper amount of high-temperature flame excites the oxyhydrogen generator to discharge combustible gas, the combustible gas is transmitted to a fourth area, and finally the combustible gas is transmitted to the engine to support combustion, the second turbocharger collects heat output by the tail of the engine and is led back to the first air inlet of the first turbocharger, closed circulation is realized, the heat of the tail nozzle is utilized to carry out turbocharging again, the heat is led back to the first air inlet, circulation of heat energy is realized without loss, and energy loss is reduced.

Description

Ma Daxi Qifeng conch PD-X95 closed cycle engine and method

Technical Field

The invention relates to the technical field of engines, in particular to a motor Sichuan northern wind-blown conch PD-X95 closed cycle engine and a method.

Background

Conventional engines consume large amounts of fuel during afterburning, and the oil that drives their operation is limited, so there is a great need for new energy sources to replace the diminishing oil.

The prior publication No. CN201884129U discloses a nuclear engine, which consists of a shell, an air inlet, a power supply, an accelerator, a nuclear reaction cavity, an air compressor, a worm wheel and a tail nozzle, wherein one end of the power supply is connected with the air inlet, the other end of the power supply is connected with the accelerator, the other end of the accelerator is connected with the inlet of the nuclear reaction cavity, the outlet of the nuclear reaction cavity is connected with the turbine, and the turbine is communicated with the tail nozzle. The accelerator is composed of more than 10 segmented coils. The charged particle beam formed by hydrogen atoms in the air ionized by high voltage is utilized to strike hydrogen elements in water molecules, so that nuclear fusion reaction is generated, and a large amount of energy generated by the nuclear fusion reaction is supplied to an engine to enable the engine to operate. Can completely replace fuel oil, and effectively solves the increasingly shortage of petroleum resources.

However, the engine is capable of carrying out air inlet once and air outlet once, and heat loss of an air outlet is caused, so that energy loss is caused.

Disclosure of Invention

The invention aims to provide a motor Sichuan northern wind-blown conch PD-X95 closed cycle engine and a method thereof, which solve the problems of energy loss caused by heat loss of an air outlet and air inlet of the engine.

In order to achieve the above purpose, the invention provides a motor Sichuan North wind-blown conch PD-X95 closed cycle engine, which comprises a first turbocharger, a second turbocharger and a combustion assembly, wherein the first turbocharger is provided with a first air inlet and a tail nozzle, the second turbocharger is provided with a second air inlet and an air outlet, the tail nozzle is communicated with the second air inlet, the air outlet is communicated with the first air inlet, and the combustion assembly is connected with the first turbocharger.

The combustion assembly comprises a grenade, a hydrogen-oxygen generator and a fourth zone, wherein the grenade is connected with the first turbocharger, the hydrogen-oxygen generator is connected with the grenade, and the fourth zone is connected with the hydrogen-oxygen generator.

Wherein, ZVS electronic components are arranged in the fourth area, and the ZVS generator converts the electric energy converted by the heat energy into plasma.

Wherein the second turbocharger is provided with a filler port and a fuel ash collecting port.

Ma Daxi Qifeng conch PD-X95 closed cycle starting method comprises the following steps:

the engine is started to ignite, so that the first turbocharging is realized. The wooden garnet device is ignited, a proper amount of high-temperature flame excites the oxyhydrogen generator to discharge combustible gas, and the combustible gas is transmitted to a fourth area and finally transmitted to a main engine for supporting combustion. (the wooden durian, the oxyhydrogen generator and the fourth zone are equivalent to a set of externally-hung cylindrical engines, and are communicated with the main engine through a series of pipelines to form a local closed loop).

The fourth region has ZVS electronic components, and the ZVS generator converts the electric energy converted by the heat energy into plasma;

the second turbocharging collects heat output by the tail of the engine and is led back to the air inlet of the first turbocharging to realize closed cycle.

Wherein the fourth region has ZVS electronics, the ZVS generator converting the previously thermally converted electrical energy into a plasma, the steps further comprising:

there are three places for plasma, the first, for ionizing air to create a loss of gravity suspension; second, for collection and storage; and thirdly, mixing and reacting with atoms emitted by an atomic gun installed in the fourth area and solid fuel fixedly sprayed outside the engine to jointly generate high-temperature heat energy.

According to the motor Sichuan northern wind-blown conch PD-X95 closed-cycle engine and the method, the engine is started to be ignited, the wooden durian is ignited, a proper amount of high-temperature flame excites the oxyhydrogen generator to discharge combustible gas, the combustible gas is transmitted to the fourth area and finally transmitted to the engine to support combustion, the second turbocharger collects heat output by the tail of the engine and returns to the first air inlet of the first turbocharger, closed cycle is realized, the heat of the tail nozzle is utilized to carry out turbocharging again, the heat is returned to the first air inlet, circulation of heat energy is realized without loss, and energy loss is reduced.

Drawings

In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below.

Fig. 1 is a schematic diagram of a motor north-west whelk PD-X95 closed cycle engine according to a first embodiment of the present invention.

Fig. 2 is a step diagram of a motor-northwest conch PD-X95 closed cycle starting method according to a second embodiment of the present invention.

In the figure: 101-first turbocharger, 102-second turbocharger, 103-first air inlet, 104-tail nozzle, 105-second air inlet, 106-air outlet, 107-wooden durian, 108-oxyhydrogen generator, 109-fourth zone, 110-filler mouth, 111-collecting fuel ash mouth.

Detailed Description

The following detailed description of embodiments of the invention, examples of which are illustrated in the accompanying drawings and, by way of example, are intended to be illustrative, and not to be construed as limiting, of the invention.

The first embodiment of the application is as follows:

referring to fig. 1, fig. 1 is a schematic diagram of a motor sirocco conch PD-X95 closed cycle engine according to a first embodiment of the present invention. The invention provides a motor Sichuan northern wind-blown conch PD-X95 closed cycle engine which comprises the following components: comprising a first turbocharger 101, a second turbocharger 102, the first turbocharger 101 having a first air inlet 103 and a tail nozzle 104, the second turbocharger 102 having a second air inlet 105 and an air outlet 106, and a combustion assembly comprising a garnet 107, an oxyhydrogen generator 108 and a fourth zone 109. The second turbocharger 102 is provided with a filler port 110 and a collected fuel ash port 111.

For the present embodiment, the tail nozzle 104 is in communication with the second air inlet 105, the air outlet 106 is in communication with the first air inlet 103, and the combustion assembly is connected to the first turbocharger 101. The second turbocharger 102 collects heat output from the tail of the engine and guides the heat back to the first air inlet 103 of the first turbocharger 101 to realize a closed cycle, wherein the size of the first air inlet 103 is adjustable.

Wherein the grenade 107 is connected to the first turbocharger 101, the oxyhydrogen generator 108 is connected to the grenade 107, and the fourth zone 109 is connected to the oxyhydrogen generator 108. The first turbocharger 101 is sleeved with the grenade 107, the grenade 107 is of a three-layer structure, an air inlet end of the grenade 107 is communicated with a main combustion chamber of the first turbocharger 101, a tail end of the grenade is communicated with the oxyhydrogen generator 108, a needle capable of being used for ignition is arranged in the grenade, fuel in the grenade 107 is ignited, the fuel in the grenade 107 is yak manure powder, the oxyhydrogen generator 108 is of a three-layer structure, the outermost layer is formed by communicating high-temperature flame with the outermost layer of the grenade 107, the innermost layer is filled with the oxyhydrogen generator 108, the slow-release fuel is provided with a heat energy conversion device, the middle layer is converted into electric energy, the oxyhydrogen generator 108 is arranged in the middle, the tail ends of the oxyhydrogen generator 108 are respectively provided with a conduit opening, and the conduit opening is respectively connected with the main combustion chamber of the first turbocharger 101, and the tail nozzle 104 of the first turbocharger 101 is provided. In the grenade 107, the dry yak manure powder is ignited by a lighting device with a lightning rod, the fuel smolders to generate carbon monoxide, also called grenade gas, after the grenade 107 is heated and boosted, the air inlet end is opened, the air inlet end is used for sucking the air of the first turbocharger 101 after ignition, the air inlet end is mixed with the grenade 107, the air outlet end of the grenade 107 is used for entering the hydrogen-oxygen generator 108, the thermal energy of the yak manure is limited, the thermal mass is exhausted slowly, at this time, the hydrogen-oxygen generator 108 is reached, the solid fuel of the hydrogen-oxygen generator 108 needs to be activated, the solid fuel (silicon material powder and sodium hydroxide powder) is filled in the hydrogen-oxygen generator 108, the combustible gas hydrogen and oxygen are released, and the continuous supply of the grenade gas fuel is kept, wherein the hydrogen and the oxygen of the hydrogen-oxygen generator 108 are combustion-supporting agents. The oxyhydrogen generator 108 has a thermoelectric conversion device for converting electrical energy, which is directly fed into the ZVS generator to power the ZVS electronic components, and after being energized, passes through a series of structure generating devices therein, and finally generates plasma.

Next, ZVS electronics are located in the fourth region 109, and a ZVS generator converts the thermal energy converted electrical energy into a plasma. The fourth zone 109 has ZVS electronics, and the ZVS generator converts the electrical energy from the previous thermal energy conversion to a plasma, wherein the plasma has three locations, the first, for ionizing air to create a loss of weight suspension, facilitating flight. The second is used for collecting and storing. The third type of the fuel gas is mixed with the fuel gas (the fuel gas) emitted from the atomic gun mounted in the fourth area 109 and the solid fuel (the fuel gas) fixed outside the engine to generate combustion, and the combustion is performed together with the fuel gas generated in the previous step to generate high-temperature heat energy.

Meanwhile, the second turbocharger 102 is provided with a filler port 110 and a collected fuel ash port 111. The method can be used for adding silicon dioxide as fuel and collecting ashes of metal silicon, and can be used for supplementing fuel for combustion, and can also be used as a smelting furnace for collecting combustion products.

Using a motor of this embodiment a north-wind-blown conch PD-X95 closed cycle engine,

igniting, namely igniting the wood durian 107, enabling a proper amount of high-temperature flame to excite the oxyhydrogen generator 108 to discharge combustible gas, transmitting the combustible gas to the fourth area 109, and finally transmitting the combustible gas to an engine to support combustion; the fourth zone 109 has ZVS electronics, and the ZVS generator converts the electrical energy from the previous thermal energy conversion to a plasma, wherein the plasma has three locations, the first, for ionizing air to create a loss of weight suspension, facilitating flight. Second, for collection and storage. Thirdly, the fuel is used for generating high-temperature heat together with atoms emitted by an atomic gun installed in the fourth zone 109, solid fuel fixed outside the engine (sprayed out) and mixed reaction (the combustible gas generated in the previous step is mixed together to generate combustion at this time); the second air inlet 105 of the second turbocharger 102 collects heat output from the tail nozzle 104 and guides the heat back to the first air inlet 103 of the first turbocharger through the air outlet 106, thereby realizing a closed cycle. The circulation of heat energy is realized without loss, and the energy loss is reduced.

The second embodiment of the present application is:

on the basis of the first embodiment, please refer to fig. 2, wherein fig. 2 is a step diagram of a motor-west north-wind-blown conch PD-X95 closed-cycle starting method according to a second embodiment of the present invention. The Ma Daxi Qifeng conch PD-X95 closed cycle starting method of the embodiment comprises the following steps of:

201: the engine is started to ignite, so that the first turbocharging is realized. The wood durian 107 is ignited, and a proper amount of high temperature flame excites the oxyhydrogen generator 108 to discharge combustible gas, and the combustible gas is transmitted to the fourth area 109 and finally transmitted to the main engine to support combustion. (the wooden durian, the oxyhydrogen generator and the fourth zone are equivalent to a set of externally-hung cylindrical engines, and are communicated with the main engine through a series of pipelines to form a local closed loop).

202: the fourth zone 109 has ZVS electronics, the ZVS generator converting the electrical energy of the previous thermal energy conversion into plasma;

203: the second turbocharging collects heat output by the tail of the engine and is led back to the air inlet of the first turbocharging to realize closed cycle.

Specifically, the engine is started to ignite, the wood durian 107 is ignited, a proper amount of high-temperature flame excites the oxyhydrogen generator 108 to discharge combustible gas, and the combustible gas is transmitted to the fourth area 109 and finally transmitted to the engine to support combustion; the fourth area 109 has ZVS electronic components, and the ZVS generator converts the electric energy converted from the heat energy into plasma, wherein the plasma has three places, the first place is used for ionizing air to generate heavy suspension, which is beneficial to flying, the second place is used for collecting and storing atoms emitted by an atomic gun installed in the fourth area 109, and the third place is used for mixing and reacting with solid fuel (sprayed) fixed outside an engine (the combustible gas generated before is mixed together to generate combustion) to jointly generate high-temperature heat energy; the second turbocharging device is provided with the filler port 110 and the fuel ash collecting port 111, and can be used for throwing silicon dioxide as fuel and collecting ash metallic silicon. The heat from the air outlet 106 is used to re-turbo the engine and the heat is directed back to the air inlet. The circulation of heat energy is realized without loss.

The foregoing disclosure is only illustrative of one or more preferred embodiments of the present application and is not intended to limit the scope of the claims hereof, as it is to be understood by those skilled in the art that all or part of the process of implementing the described embodiment may be practiced otherwise than as specifically described and illustrated by the appended claims.

Claims (6)

1. Ma Daxi is Qifeng blows conch PD-X95 closed cycle engine, its characterized in that includes first turbo charger, second turbo charger and combustion subassembly, first turbo charger has first air inlet and tail spout, second turbo charger has second air inlet and gas outlet, the tail spout with the second air inlet intercommunication, the gas outlet with first air inlet intercommunication, combustion subassembly with first turbo charger is connected.

2. The Ma Daxi Qifeng conch PD-X95 closed cycle engine of claim 1,

the combustion assembly comprises a grenade, a oxyhydrogen generator and a fourth zone, wherein the grenade is connected with the first turbocharger, the oxyhydrogen generator is connected with the grenade, and the fourth zone is connected with the oxyhydrogen generator.

3. The Ma Daxi Qifeng conch PD-X95 closed cycle engine of claim 1,

and the ZVS electronic components are arranged in the fourth region, and the ZVS generator converts the electric energy converted by the heat energy into plasma.

4. The Ma Daxi Qifeng conch PD-X95 closed cycle engine of claim 1,

the second turbocharger is provided with a filler port and a fuel ash collecting port.

5. Ma Daxi the method for starting the closed cycle of the conch PD-X95 blown by northern wind is suitable for the Ma Daxi conch PD-X95 closed cycle engine blown by northern wind according to claim 1, and is characterized by comprising the following steps:

the engine is started to ignite, so that the first turbocharging is realized. The wooden garnet device is ignited, a proper amount of high-temperature flame excites the oxyhydrogen generator to discharge combustible gas, and the combustible gas is transmitted to a fourth area and finally transmitted to a main engine for supporting combustion. (the wooden durian, the oxyhydrogen generator and the fourth zone are equivalent to a set of externally-hung cylindrical engines, and are communicated with the main engine through a series of pipelines to form a local closed loop).

The fourth region has ZVS electronic components, and the ZVS generator converts the electric energy converted by the heat energy into plasma;

the second turbocharging collects heat output by the tail of the engine and is led back to the air inlet of the first turbocharging to realize closed cycle.

6. The Ma Daxi conch PD-X95 closed cycle starting method of claim 5, wherein said fourth zone has ZVS electronics, the ZVS generator converting the electrical energy from the previous thermal energy conversion to a plasma, said steps further comprising:

there are three places for plasma, the first, for ionizing air to create a loss of gravity suspension; second, for collection and storage; and thirdly, mixing and reacting with atoms emitted by an atomic gun installed in the fourth area and solid fuel fixedly sprayed outside the engine to jointly generate high-temperature heat energy.