KR20200005833A - The principle and accelerating device of a comprehensive air purifying device utilizing discharge pressure gas of a device that utilizes engines of a spacecraft, a ship, an automobile, an aircraft, a power plant & forward friction resistor - Google Patents

Abstract

Based on a device that utilizes the engine and turbine of a spacecraft, a ship, an automobile, an aircraft, a power plant, and the like, pressure and exhaust gas utilized as thrust and energy is suctioned 100% so that the suctioned pressure helps an explosion process in the compression, explosion, and exhaust of various engine cylinders and that air pollution is reduced 100% (Fig. 50). An intake device is connected to a turbine used as thrust, increases the thrust by injecting pressure into the resistance area of blades, and removes an after-raising back blast by the blades of the turbine and the propellers of a helicopter or the like. Thrust pressure is increased by suctioning the back-blast pressure of the propellers and discharging the suctioned pressured in the direction of the rear of the propellers (Figs. 51, 51-1, and 51-2). Energy efficiency is increased and noise is removed by suctioning the remaining pressure from the suctioned thrust. The principle of a small suction, discharge, and compression tank that can be used in a narrow space when a compression tank is mounted is utilized. The additional principle of additional acceleration due to action and reaction is utilized. The principle of movement of a spacecraft (flying saucer) capable of preventing noise and pollution and moving by mounting the engine inside a moving device is utilized (Fig. 70-1).

Description

Comprehensive device for accelerating air and exhaust devices using engines such as spacecraft, ships, automobiles, aircraft, power plants, etc. {The principle and accelerating device of a comprehensive air purifying device utilizing discharge pressure gas of a device that utilizes engines of a spacecraft, a ship, an automobile, an aircraft, a power plant & forward friction resistor}

The present invention provides a compressor-type pressure gas tank using exhaust gas pressure and general pressure, which are discharged to the outside when all reciprocating engines and rotary turbines, which are used for gasoline, diesel, gas, and pressure gas, operate. A device for maintaining a high pressure by suction; Principle of the device that prevents pollution and improves energy efficiency by injecting pressure into the reciprocating energy of piston and thrust rotational energy of turbine which are used for thrust by inhaled pressure, and also for recycling by polluting highly compressed gas flowing out Wow; It is about the principle of a device that increases the acceleration by mounting a turbine by creating a blocked area inside an airship with limited speed, such as an aircraft and spacecraft.

Energy efficiency is reduced by the use of various pressures as energy and by the outflow pressure of various equipment utilizing engines, turbines and air pressures such as spacecraft, ships, automobiles, aircrafts, power plants, etc., in which pressure or gas is leaked to the outside;

Pollution of pressure and exhaust gas of reciprocating engine and rotary turbine used for thrust;

Additional energy problems to overcome the speed limits of aircraft and spacecraft;

How to use exhaust pressure to solve the above.

Energy efficiency is reduced by the use of various pressures as energy and by the outflow pressure of various equipment utilizing engines, turbines and air pressures such as spacecraft, ships, automobiles, aircrafts, power plants, etc., in which pressure or gas is leaked to the outside;

Pollution of pressure and exhaust gas of reciprocating engine and rotary turbine used for thrust;

Additional acceleration energy problems to overcome the speed limits of aircraft and spacecraft;

The principle and method of applying the discharge pressure to solve the above;

A basic principle of sucking high heat pressure of a turbine for thrust;

A basic principle of recycling the inhaled high temperature pressure;

Solution to the above problems include a method for injecting the pressure gas into the compressor inlet and injecting the inside of the cylinder during the explosion of the reciprocating engine utilizing the sucked pressure for thrust;

Injecting pressure into the thrust zone of the rotary turbine to shorten the distance of the discharge pressure;

As the pressure in the thrust zone becomes higher, it absorbs and utilizes the discharge pressure except for thrust.

As described above, the exhaust gas pressure sucked into the pressure gas tank is equipped with a filter to continuously purify the air pollutant.

If the suction pressure is increased, it reduces the fuel of the existing engine and turbine and increases the injection of suction pressure.

The additional acceleration device for overcoming the limitations of the speed of aircraft and spacecraft is an area where different principles are applied when moving to an external moving speed when used in an isolated space inside. It can be utilized. (Related word): Further research is needed, such as atmospheric pressure, cosmic vacuum, turbine thrust in an insulated space where inertial action stops, reverse braking theory, and additional acceleration.

The device to inhale the high heat pressure of the turbine for thrust requires the study of materials to be utilized by analyzing the turbine dynamically.

Reducing air pollution by 100% by inhaling pressure and exhaust gas utilized as thrust;

A device for removing after-rise storms of propellers such as helicopters;

Energy efficiency increase and noise reduction;

With increasing acceleration at the current highest speed;

Increasing acceleration of the ship's existing velocity;

Can study up to infinite acceleration;

Inhalation of forward friction resistance increases additional acceleration and energy efficiency;

It can prevent air pollution by utilizing external leakage blocking related to pressure.

[FIG. 50] Operating system of entire mobile device and fixed device
51 is a principle view of blade blades 50 and 52 of aircraft, helicopters and drones for propellers.
51-1] Principle drawing of inhalation pressure
51-2] Principle understanding of the area where blade wing suction can be done
70 is an additional acceleration increasing apparatus using an indoor space of a mobile device that operates by using thrust pressure such as an engine / jet engine / turbine of a ship, an automobile, an aircraft, and the like (77)
(Basic Principle / Infinite Acceleration Study in the Universe): See Figure 80-1.
70-1] Principle understanding of additional acceleration increasing device related to spacecraft and aircraft
Fig. 70-2: Principle understanding diagram that allows a single thrust device on a circular rail to move in any direction like a spaceship (flying saucer)
70-3 is an understanding of the principle of the discharge device circular discharge port for increasing the pressure of the thrust pressure sucked into the suction tank of the compressed gas
Fig. 70-4: Understanding the principle of action (58-3) reaction (58-3-1) to obtain additional acceleration in relation to space aircraft
70-5. Understand the principle of action (58-3) reaction (58-3-1) to obtain additional acceleration in relation to space aircraft.
75 is a view of understanding the principle of a compressor-type pressure tank in which a pressure tank may be mounted in a pressure tank to utilize a reduced high pressure;
80 is a reference drawing of a conventional turbojet engine
80-1 Principle diagram of a new technology method 84 of a thrust turbine
82 is a simple diagram of how to use the new technology of the general engine cylinder, such as ships, cars, aircraft, trains, generators
[Relevant Document 1] A drawing of 58 pages of front friction resistance filed by the applicant
[Relevant Document 2] Some pictures of my contact with Creative Economy Town in 1: N file

{Related Words and Partial Contents} Refer to the accompanying full drawings and content

50 FIG.

[Operating System 1]

[Operating System 1-1] Existing Devices that Use Propellers such as Helicopters and Drones from Outside

5. Existing fuel method: Existing fuel tank → Engine where pressure is released / Back of blade blade → Pressure discharge port

[Operating System 1-2]

6. Pressure tank with suctioned pressure → Engine / blade blade discharged pressure → Vent pressure inlet

[Operating System 2]

Engine: Compression → Blasting → Exhaust → Air Compressor Inlet → Compressor Tank → Engine Blasting Inlet → Exhaust After Blasting → Air Compressor Inlet → ∞ = Actual Experiment and Further Research Required

[Operating System 3]

Turbine: Rotating the rotor blades → Inhaling the propulsion resistance air compressor → Discharging to the back of the rotor blades → Using thrust pressure with the discharged pressure → Rotating the rotor blades → ∞ = Experiment and further research required

[Operating System 4]

Propeller: Blade wing thrust propulsion → Resistant air compressor suction → Exhaust to the back of rotating blade → Use thrust pressure with discharged pressure → Rotating blade (blade) → ∞ = Experiment and further research required

[Operating System 5]

When the compressed air of all devices is inhaled, it can absorb the unnecessary resistance of the moving engine to increase energy efficiency, and reduce the carbon emissions of all the devices utilizing energy by the engine by 100%.

[Reference]

Reducing air pollution by 100% by inhaling pressure and exhaust gas utilized as thrust; A device for removing after-rise storms of propellers such as helicopters; Energy efficiency increase and noise reduction; The application of the principle of small suction exhaust compressor tanks that can be used in confined spaces when mounting compression tanks;

51 is a blade wing (50) (52) principle of propeller aircraft, helicopters, drone principle thrust pressure zone pressure absorption zone

51-1] Principle drawing of inhalation pressure

51-1 Direction of pressure relief 50-1 Wing 51-2 52-1 Pressure at the front wing blades Wing back from the rear blade blade 60-1 Direction of blade rotation

51-2] Principle understanding of the area where blade wing suction can be done

62 turn center area

70 is an additional acceleration increasing apparatus using an indoor space of a mobile device that operates by using thrust pressure such as an engine / jet engine / turbine of a ship, an automobile, an aircraft, and the like (77)

(Basic Principle / Infinite Acceleration Study in the Universe): See Figure 80-1.

77 Space to be blocked inside the moving device: noise reduction, pollution prevention, etc. 74 Direction of movement 75 Suction pressure to be sucked into the compression tank 55-2 Pressure suction area excluding thrust 75 Suction pressure discharge direction 53-2 Jet / rocket Pressure relief device for engine Suction pressure to increase thrust 53-3 Pressure relief direction

[Additional Description] The thrust device 59-1 can be installed anywhere in the indoor space.

70-1] Principle understanding of additional acceleration increasing device related to spacecraft and aircraft

58-3 The force at firing the arrow allows for additional acceleration.

58-4 No additional acceleration occurs when the bow is pulled from a fixed outside opposite the direction of travel.

70-2 allows a single thrust device on a circular rail to move in any direction, such as a spaceship (flying saucer).

73-1 General model of spacecraft (flying saucer) 73-2

70-3 is an understanding of the principle of the discharge device circular discharge port for increasing the pressure of the thrust pressure sucked into the suction tank of the compressed gas

53-2 Pressure Relief for Jet and Rocket Engines

53-3 Increase the pressure of the thrust by cutting off the pressure applied to the thrust in the direction of pressure discharge.

[Additional explanation]

53-4 When the thrust outlet is circular in the area where thrust pressure is discharged from the suction pressure tank as above, the pressure relief of the circular outlet acts outside of the moving device, so the principle of action reaction does not apply. Therefore, it can only be used to increase the thrust pressure. After the pressure is increased, the suction device 59-2 of the pressure tank is sucked and used again.

{Reference word} Formation of pressure network (53-1 to 53-4) [Fig. 70-3]

Fig. 70-4: Understanding the principle of action (58-3) reaction (58-3-1) to obtain additional acceleration in relation to space aircraft

58-3 The force at firing the arrow allows for additional acceleration. M ² 58-3-1 Distance traveled by forward reaction

70-5. Understand the principle of action (58-3) reaction (58-3-1) to obtain additional acceleration in relation to space aircraft.

58-4 No additional acceleration occurs when the bow is pulled from a fixed outside opposite the direction of travel.

[Additional explanation]

F = M ² = M = m

F ¹ = M-m = 0

M ² = M = m

F = pull force

M ² = the action when the bow is fired from a moving internal organ and the reaction occurs in the interior space and the force of the moving body forward as a reaction (use the force in the acceleration device);

Action (m) Reaction (M) in Figure 70-5

75 is an additional principle of a compressor pressure tank in which a pressure tank is mounted in a pressure tank to utilize a reduced high pressure.

70 Compressor Engine (see Figures 80-1 and 82) 71 Air Intake Exhaust from Engine 72 Air Purification Filter (Replaceable) 73 Typical Air Intake 58-1 Compressed Air Tank 70-1 General Compression Engine 72-1 Filter connector 58-3 Two compression tanks in the compression tank

71 Pollutant Removal Device (Drain)

[Main Research Projects] General Technology Development Level

A pressure holding and filter removing device of the filter connecting pipe of the air purification filter 72;

A separate suction device separating the air intake port 71 and the general air intake port 73 exhausted from the engine;

[Figure 80] Reference of the existing turbojet engine

80 conventional jet turbines

Description: Different types of engines have different components, but jet engines generally have the following components:

Air Intake

A passage through which air enters a jet engine. In the case of subsonic flight, the air inlet shape does not matter so much, so it is possible to reduce the air resistance. However, when flying at supersonic speed, the air entering the compressor should be less than the speed of sound. In addition, a cone or a ramp is installed to cope with the shock wave caused by the supersonic speed.

Compressor

Compressed air is sent to the combustion chamber. Nearly all jet engines line up fans so that air is gradually compressed as they pass through them. The driving force is obtained by connecting the shaft from the turbine.

Combustor or Combustion Chamber

This is where air from the compressor burns with fuel. At this time, the turbine is turned by the expansion force, and high-speed jet air is blown out through the exhaust port to obtain thrust. It has a flame holder for combustion.

Turbine

Power is obtained by rotating the turbine using the expansion force of the combustion air. This power drives the compressor and, in some cases, connects to the outside to transmit power. Cool the turbine blades with cold (relatively cold) air from the compressor to prevent the turbine blades from melting.

Shaft

Power from the turbine is transmitted to the compressor, and in the case of the turboprop, the torque is transmitted to the outside of the engine.

Afterburner

It is mainly used to gain additional thrust to the fighter. The inflation gas that has combusted and exited the turbine is still at a high temperature so that fuel can be injected into it to burn without additional equipment for additional thrust. However, this method is only used when taking off or requiring a meat building because of poor efficiency.

Exhaust or Nozzle

As the combusted air expands, it exerts a high velocity jet of air through the exhaust and gains thrust. Most have a constant cross-section and retracted in the ejection direction.

[Fig. 80-1] New Technology Approach (84) → Continued Research Needed

80. Conventional turbines (need to reduce the function of compressors and combustion chambers) 84. Enlarged drawing of thrust turbines 85. Thrusters 86. Discharged compressed air discharge areas 87. Absorb and utilize.

80, 80-1 Supplementary Description]

In the existing turbojet engine, the compressor (81) and the combustion chamber (82) will be reduced and added in relation to the turbine (83) and the pressure suction device connected to the turbine (83).

[Figure 82] general engine cylinders, such as ships, cars, aircraft, trains, generators

90. General engine cylinder 92. Blasting pressure outlet to be absorbed 91. Existing fuel injection and absorbed compressed air inlet 93. Piston

[Additional explanation]

In the process of explosion of the cylinder of the engine is sucked into the high vacuum through the air intake port 71 is exhausted from the engine, can increase the efficiency of the engine, 100% rehabilitation of the inhaled pressure in the explosion process, The bearing loss involved and the frictional loss of the piston 93 of the cylinder and the existing exhaust pressure will be nearly proportional. The whole process of;

[Figure 80-1] Position diagram and additional description of the additional compressor to increase the thrust pressure of the compressed air discharge area 86 sucked pressure except the thrust of the thrust turbine 83 by mounting the rotary compressor of the turbine in the thrust region

80. Existing turbine 81-4 Pressure discharge pipe 81-2 .Pressure suction pipe 81-3. Compressor Pressure Tank

[Additional explanation]

The additional compressor 81-1 absorbs the suction pressure 75 to be sucked into the compression tank in the area to be absorbed to maintain the pressure to discharge the thruster secondly through the compressor-type pressure tank 83-1. , Through the pressure discharge pipe (81-4) to increase the resistance of the thruster.

80-2] Content reference

[Additional explanation] (atmospheric pressure 1 atmosphere standard)

The suction pressure of the compressed air discharged area 86 is sucked into the suction compressor because the pressure is rapidly disintegrated at the moment when the thrust-resistant thruster strikes the thrust resistance area of the blade;

Since the travel distance is different according to the firing pressure, the higher the firing pressure is, the less is drawn into the suction compressor due to the influence of the suction compressor to maintain the atmospheric pressure.

Example 1 Principle of maintaining the atmospheric pressure when the pressure of the self-cleaning air cleaner is fired at atmospheric pressure (the suction compression tank only needs to maintain a constant atmospheric pressure).

[Additional description of Figs. 82 and 75]

94. By reusing the pressure absorbed into the outlet, air pollution prevention and energy efficiency can be increased, and a light and high pressure compact compressor can be used as a research project.

95. Air pollution can be prevented 100% by using energy from the compressor type pressure tank of Fig. 75 connected to the cylinder to transfer energy to the cylinder with only exhaust gas and additional pressure.

At this time, by attaching a detachable pollution prevention filter, etc. that can be utilized in the suction of the drain gas (drain) connected to the inside of the compression tank, to keep the inside of the compression tank always in the best state.

[Related Documents 1] Forward Friction Resistance 58 Pages (pending)

Refer to additional cutting section of vessel (primary thrust + secondary thrust = resistance removal + noise reduction)

Propeller Small and fast for thrust (water jet, etc.) Suction discharge pressure Thrust propeller hold empty space Inhaled water

[Related Documents 2] Creative Economy Town (I)

Device used to remove aerodynamic noise by using thrust pressure of engine, jet engine, turbine, etc. of ship, car, aircraft, etc., remove unnecessary thrust pressure, and use anti-pollution pressure tank

Additional efficiency device using thrust pressure of thruster such as engine / jet engine / turbine of automobile, aircraft, etc.

To summarize the above, the first is to increase the pressure of the explosion blade of the cylinder [Fig. 82] and the thrust blade blades of the turbine through the compressor [Fig. 80-1] and the blade blade pressure of the helicopter, etc. Using the same energy as that of raising [Fig. 51, 51-1, 51-2], and the utilization of the suction pressure 75, 76 to be sucked into the compression tank is the same;

70 and the additional principle of acceleration of the reaction reaction of 70-1 ~ 70-7 and;

The principle of a spaceship (flying saucer) (Fig. 70-1);

The principle of adding a small compressor pressure tank that can increase the utilization of the moving space (FIG. 75); Wow

On the basis of this, to prevent pollution by decontaminating outgoing gas; Wow

Energy loss can be expected to achieve additional efficiency of energy by utilizing energy as bearing loss of shaft and friction loss of cylinder to operate each engine. (Needed ongoing research)

[Content of representative]

Based on devices utilizing engines and turbines, such as spacecraft, ships, automobiles, aircraft, power plants, etc., exhaust gas pressure and thrust pressure are sucked into the compression tank (Fig. 75) (52) (59-1, 2) (81-). 1) (92) and the device (51-1,2) (52) (59-1,2) (86, 91) to be utilized for thrust and discharged to the energy;

Apparatus utilizing a high pressure in a compact by mounting a compression tank (Fig. 75) in the compression tank based on the above contents;

An apparatus for inhaling a compression tank (FIG. 75) and utilizing it as a thrust to reduce the front friction resistance (Application No. 10-2013-0102456 and all the applications of the front friction resistance and the applicant (Kim Juhwan));

A device that connects the inhaled compression to an engine and utilizes the additional energy as only the inhaled pressure;

A device for attaching a thrust related device to an isolated indoor space of a mobile device 73 in space and aerospace to utilize as an additional acceleration device 70, 70-1, 2, 3, 4, 5;

Claims (6)

Suction exhaust gas pressure and thrust pressure into the compression tank (FIG. 75) based on the apparatus utilizing engines and turbines of spacecraft, ships, automobiles, aircraft, power plants, etc. and the operating system of FIG. And (2) 81-1 and 92, the apparatus for discharging to the areas (51-1,2) (52) (59-1,2) (86) (91) utilized for the thrust to utilize as energy;
The operating system and process of FIG. 50;
Apparatus utilizing a high pressure in a compact by mounting a compression tank (Fig. 75) in the compression tank based on the above contents; The method of claim 1;
In the process of explosion of the cylinder of all engines, the air inlet 71 exhausted from the engine is sucked into the high vacuum, thereby improving the efficiency of the engine, and the inhaled pressure can be 100% rehabilitation in the explosion process, The bearing loss associated with the friction loss of the piston 93 of the cylinder and the existing exhaust pressure will be approximately proportional. The whole process of; The method of claim 1;
A device for suctioning into the compression tank (FIG. 75) and utilizing thrust to reduce the front friction resistance;
A device that connects the inhaled compression to an engine and utilizes the additional energy as only the inhaled pressure; The method of claim 3;
The suction pressure of the compressed air discharged area 86 is sucked into the suction compressor because the direction and pressure of the thrust-resistant thruster strike the thrust resistance area of the blade rapidly disintegrate;
Since the traveling distance according to the firing pressure is wrong, the device is applied to the principle that the amount of suction to the suction compressor is less the higher the firing pressure under the influence of the suction compressor to maintain the atmospheric pressure; The method of claim 1 and 3;
A device for attaching a thrust related device to an isolated indoor space of a mobile device 73 in space and aerospace to utilize the additional acceleration device 70, 70-1, 2, 3, 4, 5; The turbine apparatus of claim 1;
53-4 When the thrust outlet is circular in the area where thrust pressure is discharged from the suction pressure tank as above, the pressure discharge of the circular outlet acts outside of the moving device, so that the principle of action reaction is not applied; {Reference word} Formation of pressure network (53-1 to 53-4) [Fig. 70-3]

Images