WO2018203498A1

WO2018203498A1 - Implosion-type engine

Info

Publication number: WO2018203498A1
Application number: PCT/JP2018/016694
Authority: WO
Inventors: 東洋治向山; 義治向山
Original assignee: 東洋治向山
Priority date: 2017-05-03
Filing date: 2018-04-25
Publication date: 2018-11-08
Also published as: JP2018189024A

Abstract

[Problem] A conventional explosion-type engine generates carbon dioxide gas, hazardous gas, and soot, and thereby causes global warming. In addition, fossil fuel has been presently becoming depleted. The present invention uses, as an implosion material that is fuel, hydroxygen gas (2H2+O2), elemental gas of hydrogen (H2), or a gas mixture of these gases with oxygen (O2), air, or the like. The present invention makes use of expansion and condensation reactions that occur as a result of phase change due to combustion of the implosion material, and the only product generated as a result is water. [Solution] In an implosion-type engine according to the present invention, in an intake-and-expansion stage, an implosion material is ignited after being sucked into a cylinder to be sealed therein, and, with the expansion force generated owing to expansion occurring as a result of temperature rise at the time of combustion, a piston is moved to the bottom dead center. In an implosion-and-exhaust stage, the piston is moved to the top dead center by the suction force of the vacuum generated as a result of the implosion reaction after the combustion. Near the top dead center, water and water vapor are exhaust. This engine has a small displacement, can be operated in an anoxic state without relying on carbon, and does not require a compression stage or an explosion stage. The present invention is applicable to a two-cycle or four-cycle implosion-type engine, or an implosion-type rotary engine with three times of ignition per revolution or with six times of ignition per revolution.

Description

Implosion engine

In the present invention, a simple gas such as oxyhydrogen gas (2H2 + O2) or hydrogen (H2) or a mixed gas such as oxygen (O2) or air is used as the implosion material. When ignition is ignited in the sealed container, the implosion material burns, and the implosion material expands due to a temperature rise due to combustion to generate an expansion force, and the inside of the closed container is pressurized. Subsequently, the phase changes after combustion and condenses into water and water vapor. This implosion reaction condenses to about 1200 minutes to form a vacuum state, generating a suction force, and the inside of the sealed container becomes negative pressure. This engine is powered by this expansion force and suction force. It is an implosion type engine that has a small displacement, can be operated in a carbon-free state, and has no compression stroke and no explosion stroke.

Conventionally, there are devices, facilities and equipment that can easily generate oxyhydrogen gas that can be used as implosion material. Oxyhydrogen gas was mixed with the main fuel for engines and burners and used as an auxiliary fuel. However, there is no engine that uses only implosion material as fuel.

Conventional two-cycle, four-cycle engines and rotary engines are explosive engines that use gasoline, light oil, LP gas, etc. as fuel and use the explosive power during combustion. The exhaust gas generated from these engines is carbon monoxide, Carbon dioxide gas, toxic gas, and soot are emitted, causing global warming. Fossil fuels are currently depleted.

Conventional engine operations are an intake stroke, a compression stroke, an ignition stroke, an explosion stroke, and an exhaust stroke, and there is a loss of output in the compression stroke.

The implosion material used in the implosion-type engine of the present invention is carbon-free energy mainly composed of hydrogen. The generated exhaust gas is only moisture, and is composed of carbon monoxide gas, carbon dioxide gas, toxic gas, and soot. There is no occurrence. Oxyhydrogen gas (2H2 + O2) can be easily generated by electrolysis.

The operation of the two-cycle implosion type engine is the intake expansion stroke, ignition timing, and implosion exhaust stroke. The operation of a 4-cycle implosion type engine is an intake expansion stroke, an ignition timing, an implosion stroke, a cooling process, and an exhaust stroke. There is no compression stroke or explosion stroke.

A one-turn, three-ignition rotary implosion type engine has an intake expansion / explosion stroke and a cooling / exhaust stroke. During the intake expansion / explosion stroke, the product of ignition and implosion material is exhausted. The 1-rotation 6-ignition rotary implosion-type engine has a first intake / expansion / explosion stroke and a second intake / expansion / explosion stroke. The first half of each stroke is ignited, and the product of the implosion material is exhausted in the second half. There is no compression stroke or explosion stroke.

JP 2013-144984 A JP 2008-063980 A

The problem to be solved is that when the implosion material is ignited, the implosion material expands due to a temperature rise due to combustion, and at the next moment, the implosion material undergoes a phase change due to the implosion reaction and is reduced to about 1/1200. Condensate to a vacuum. Expansion and implosion occur continuously.

The implosion material is a stable gas with a high ignition temperature, small flammable power, and stable combustion. However, once burned, it burns all at once, and measures such as bubbling tanks and arresters are required.

The implosion reaction generates water or water vapor in the cylinder, and the spark plug electrode gets wet, resulting in poor insulation, resulting in deterioration of engine oil when mixed with engine oil.

This proposal is to adjust the timing chain of 4-cycle engine or diesel engine, belt change, gear change, intake valve, and exhaust bubble operation interval with cam position and cam shape, ignition timing adjustment, fuel Add injection valve, fuel injection pump, pressurization pump, ejector, arrester.

The operation of the 2-cycle and 4-cycle implosion type engine is an implosion type engine by combining the intake expansion stroke, ignition timing, implosion exhaust stroke, implosion stroke, cooling process, and exhaust stroke.

The timing of opening and closing the intake and exhaust valves is synchronized with pistons, connecting rods, crankshafts, camshafts, intake cams, exhaust cams, belts, rods, etc., and the cam shapes of intake cams and exhaust cams are individually adjusted. Do it. The operating range is about 1/2 for the intake cam and about 1/10 for the exhaust cam compared to the conventional engine.

In the case of a two-cycle implosion-type engine, the ignition timing is from the completion of the intake during the intake-expansion stroke until the implosion-exhaust stroke cycle. The implosion material is ignited by an intermittent operation alone, continuously, or at an arbitrary position by the middle of the contraction process cycle.

The rotary implosion type engine has intake and exhaust hole position changes and additions, and an intake valve or rotary valve at the inlet. An exhaust valve or a rotary valve was attached to the outlet of the exhaust hole, and the position of the spark plug was changed.

The operation of the rotary implosion type engine is a rotary implosion type engine that combines an intake expansion / explosion compression stroke, a cooling / exhaust stroke, an ignition timing, a first intake expansion / explosion compression stroke, and a second intake expansion / expansion stroke.

The ignition timing of the rotary implosion-type engine is independent at any position by the spark plug at the position before the front end of the rotor is in front of the exhaust hole and the working chamber is sealed after the intake is completed, and before the space capacity of the working chamber is maximized. The implosion material is ignited by continuous and intermittent operation.

Arresters were installed at the inlet of the implosion engine and the inlet of the rotary implosion engine, and a bubbling tank and check valve were installed at the outlet of the oxyhydrogen gas generator to prevent backfire.

Measures against poor insulation due to electrode wetting caused by water or water vapor generated by the implosion reaction of the spark plug prevent the water droplets by lengthening the spark rod of the spark plug, blow the intake gas to the spark plug, Install in the intake valve pot. To prevent engine oil deterioration, mount the exhaust port in a horizontal plane or mount the engine head downward.

The raw material of the fuel implosion material used in the implosion type engine of the present invention is hydrogen and carbon-free energy. The implosion material can be easily generated by electrolysis, etc., and the moisture consumed by the electrolyte due to the generation of the implosion material Replenish. There is no need for fossil fuels such as gasoline and natural gas.

The operating environment of this implosion type engine can be operated with only implosion material without supplying oxygen when oxyhydrogen gas (2H2 + O2) or mixed gas of hydrogen (2H2) and oxygen (O2) is used. It can be operated indoors, in a vacuum, underwater, and in a bad environment. No vaporizer is required. Exhaust gas generated from implosion material does not generate carbon dioxide, carbon monoxide gas, toxic gas or soot, and is an unburned part of water, water vapor and implosion material. Since it can be used in a carbon-free and oxygen-free state, it can be operated indoors, in a vacuum, underwater, or in a bad environment.

The water and water vapor generated by implosion is pure water, and if this is recovered and reused, it can be operated for a long time without rehydration in a closed state.

The displacement of the exhaust cam is a small amount with the volume ratio of the intake air amount to the exhaust gas amount being about 1/1200, and the operating range of the exhaust cam may be small. Also, no muffler is required at the exhaust port.

If natural power such as solar power generation, wind power generation, and hydropower generation is used, it will save energy and reduce running costs. Energy can be accumulated by storing the implosion material in a tank or accumulator using surplus energy.

The operation of a two-cycle, four-cycle implosion type engine is a combination of an intake expansion stroke, an ignition timing, an implosion exhaust stroke, an implosion stroke, a cooling process, and an exhaust stroke. There is no engine.

The operation of the rotary implosion type engine is a combination of the intake / expansion / explosion stroke, the cooling / exhaust stroke, the ignition timing, the first intake / expansion / explosion stroke, and the compression stroke / explosion stroke, without compression. This is a rotary engine with no output loss due to.

The 2-cycle implosion type engine can obtain twice the output of the 4-cycle implosion type. A one-rotation six-ignition rotary implosion type engine can obtain twice the output of a one-rotation three-ignition rotary implosion type engine.

The basic structure and technology of the conventional 4-cycle engine and rotary engine can be used.

FIG. 1 is an explanatory diagram showing a method for generating oxyhydrogen gas (2H2 + O2) and a method for implementing an operating system of an implosion type engine. Example 1 FIG. 2 is an explanatory view showing a method for carrying out a two-cycle implosion type engine operation. (Example 2) FIG. 3 is an explanatory view showing a method of performing a 4-cycle implosion type engine operation. (Example 3) FIG. 4 is an explanatory view showing a method for carrying out a one-rotation three-ignition rotary implosion type engine operation. Example 4 FIG. 5 is an explanatory diagram showing a method for carrying out a one-rotation six-ignition rotary implosion-type engine operation. (Example 5)

As the implosion material, an oxyhydrogen gas (2H2 + O2) or hydrogen (H2) simple gas, or a mixed gas such as oxygen (O2) or air is used as the implosion material. This implosion material is pressurized and supplied directly from the air inlet of the implosion type engine into the cylinder, or by a fuel injection valve or ejector.

The implosion type engine of the present plan utilizes the form of a conventional four-cycle engine, changes in timing chain or belt, changes in gears, changes in cam position and cam shape, intake valves, and exhaust bubbles. 2 cycle implosion type engine by adding a change in opening and timing, spark plug position, ignition timing change, exhaust port position change, fuel injection valve, fuel injection pump, pressurization pump, ejector, arrester And a 4-cycle implosion type engine.

The operation of the two-cycle implosion type engine is the intake expansion stroke, ignition timing, and implosion exhaust stroke. The operation of the 4-cycle implosion-type engine was an intake expansion stroke, an ignition timing, an implosion stroke, a cooling process, and an exhaust stroke.

In the case of a two-cycle implosion-type engine, the ignition timing is continuous from the completion of intake to the implosion exhaust stroke cycle, and in the case of a four-cycle implosion-type engine, from the completion of intake to the middle of the implosion process cycle, or It was set as the ignition device which ignites the implosion material intermittently by arbitrary positions or by independent operation.

The rotary implosion type engine of this proposal has two places where the space capacity of the working chamber is minimized and maximized by the rotation of the rotary housing and the rotor using the form of the conventional rotary engine. In the case of a one-rotation, three-ignition rotary implosion type engine, the intake hole and the cooling exhaust hole are located at one minimum, the exhaust hole and the cooling intake hole are located at the other, and the working chamber has the largest space capacity between the intake and exhaust holes Install a spark plug near the value. The exhaust holes and the cooling intake holes can be only the cooling intake holes.

In the case of a one-rotation six-ignition rotary implosion-type engine, the first intake hole and the second exhaust hole are provided at one place where the space capacity of the working chamber is minimized, and the first exhaust hole and the second intake hole are provided at the other position. The first spark plug is near the maximum value of the working chamber space capacity between the hole and the first exhaust hole, and the second spark plug is near the maximum value of the space capacity of the working chamber between the second intake hole and the second exhaust hole. Is installed.

A one-turn, three-ignition rotary implosion type engine has an intake / expansion / explosion stroke and a cooling / exhaust stroke, and exhausts products of ignition and implosion material during the intake / expansion stroke. The one-rotation six-ignition rotary implosion-type engine has a first intake / expansion / explosion stroke and a second intake / expansion / expansion stroke, and ignites in the first half of each stroke and exhausts the product of the implosion material in the second half.

The generation method of oxyhydrogen gas (2H2 + O2) necessary for the implosion type engine and the operation system of the implosion type engine will be described with reference to FIG.

The implosion type engine (1) can be operated in an oxygen-free state when oxyhydrogen gas (45) (2H2 + O2) is used as the main fuel, or the oxyhydrogen gas (45), oxygen, and air are used. It can be mixed with an ejector (35) to make an implosion material as a mixed gas.

Electric power supplied to the oxyhydrogen gas generator (2) includes a generator (3) directly connected to the implosion engine (1), solar power generation (4), wind power generation (5), and commercial power supply (6). The battery is selected from the battery (9), the capacitor stack (10), etc. by the power supply selector (7), and the power can be supplied by using one or more.

The power selected by the power supply selector (7) is converted into a DC voltage by the charger (8), and the step-up / step-down DC-DC converter (11) is charged while charging the battery (9) and the capacitor stack (10). ) Is converted into a direct current that is stepped up and down by a step-up / step-down DC-DC converter (11), and this direct current controls and monitors the amount of power by a power detector (12).

The surplus power is charged into the battery (9) and the capacitor stack (10) by the charger (8).

Furthermore, direct current is converted into a pulse by the pulse width converter (13), and electric power is supplied to the electrode (15) immersed in the electrolyte (14) of the oxyhydrogen gas generator (2) for electrolysis.

The oxyhydrogen gas (16) and the electrolyte bubble (17) generated from the oxyhydrogen gas generator (2) by electric power are used as a bubbling tank to separate the oxyhydrogen gas (16) and the electrolyte bubble (17). 1 (19) is passed through the electrolyte to separate the oxyhydrogen gas.

A check valve 1 (18) is arranged in the pipe to prevent backflow of the oxyhydrogen gas (16) and the electrolyte bubbles (17) generated in the oxyhydrogen gas generator (2).

The electrolytic solution (14) in the oxyhydrogen gas generator (2) is electrolyzed into oxyhydrogen gas (16) and electrolytic bubbles (17). The electrolytic solution (14) becomes the foam (17) of the electrolytic solution and flows into the bubbling tank 1 (19) to increase the water level. The electrolytic solution (20) with the increased water level overflows, and the overflowed electrolytic solution (20 ) Returns to the oxyhydrogen gas generator (2) by the bypass pipe (21).

In order to prevent the back flow of the electrolyte (14) from the oxyhydrogen gas generator (2) to the bubbling tank 1 (19), a check valve 2 (22) is installed in the middle of the bypass pipe (21).

The oxyhydrogen gas that has passed through the electrolyte in the bubbling tank 1 (19) and the water vapor generated in the bubbling tank 1 (19), the oxyhydrogen gas and the water vapor (23) are purified water (25) of the bubbling tank 2 (24). The oxyhydrogen gas and the water vapor (23) are separated through the inside to obtain the oxyhydrogen gas (27).

The bubbling tank 1 (19) and the bubbling tank 2 (24) are connected by a communication pipe. When the water level of the bubbling tank 1 (19) becomes low, pure water (25) passes from the bubbling tank 2 (24) through the communication pipe. Replenished and the water level is the same.

A check valve 3 (26) is inserted in the middle of this communication pipe to prevent back flow of the electrolyte in the bubbling tank 1 (19).

When the water level of the bubbling tank 2 (24) becomes low, pure water in the water supply tank (29) is pressurized by the water supply pump (30) according to the set value of the water level detector (28), and the water supply electromagnetic valve (31) is opened to replenish. To do. In order to prevent backflow, a check valve 4 (32) is inserted between the water supply tank (29) and the bubbling tank 2 (24).

Pure water is used as makeup water to the water supply tank (29). Pure water is supplied through the pure water device or the RO pure water device (33).

The oxyhydrogen gas (27) that has passed through the bubbling tank 2 (24) is stored in the accumulator (34).

The accumulator (34) is provided with an accumulator (34) because there is a time lag in the generation amount of the accelerator pedal (36) and the oxyhydrogen gas generator (2). This corresponds to the consumption of (45).

The pressure detector (38) measures the pressure of the oxyhydrogen gas (45), sends a control signal to the pulse width converter (13) according to the pressure setting, and controls the power supplied to the oxyhydrogen gas generator (2). The amount of oxyhydrogen gas (16) generated is monitored and the pressure of the oxyhydrogen gas (37) is controlled.

The pressure of the pressure blower (40) is controlled by the setting of the pressure detector (38) to adjust the pressure of the oxyhydrogen gas (45) supplied to the implosion type engine (1).

The oxyhydrogen gas (45) passes through the check valve 5 (39) and is supplied to the implosion type engine (1).

When the accelerator pedal (36) is depressed, the gas supply valve (41) opens, the gas amount adjustment valve (42) opens in proportion to the accelerator pedal (36), and the supply amount of the oxyhydrogen gas (45) is controlled. The fuel is supplied from the intake port (46) of the implosion type engine (1) through the arrester (43), the fuel injection valve (44), and the ejector (35).

During the intake expansion stroke, the exhaust valve (52) is closed, the intake valve (47) is opened, and the piston (49) is directed from the top dead center to the bottom dead center. The oxyhydrogen gas (45) is proportional to the accelerator pedal (36). ) Is sucked and filled in the cylinder (48) until the middle of the cycle of the intake / expansion / explosion stroke, the intake valve (47) is closed, and the ignition plug (50) is ignited by the spark plug (50) to oxyhydrogen gas in the cylinder (48). When (51) ignites, it generates heat and expands to the bottom dead center. End the intake expansion stroke.

When the oxyhydrogen gas (51) changes phase and implodes at the next moment. The inside of the cylinder (48) is evacuated by this implosion, and the piston (49) is sucked to the top dead center, and the piston (49) goes to the top dead center, and the implosion exhaust stroke is performed.

Each timing of the intake valve (47) and the exhaust valve (52) is performed by individually adjusting the shapes of the intake cam and the exhaust cam.

The exhaust valve (52) opens the piston (49) before top dead center, and exhausts and drains the exhaust water vapor (54), which is water or water vapor that is condensed and generated from the exhaust port (53). The exhaust valve (52) is closed near the top dead center, and the implosion exhaust stroke is completed.

The exhaust water vapor (54) exhausted and discharged from the exhaust port (53) is cooled to become water and returns to the supply tank (29).

Next, the operation returns to the intake / expansion stroke again and shifts to the implosion / exhaust stroke to repeat this operation.

The generator (3) connected to the power shaft of the implosion type engine (1) starts power generation by the rotation of the implosion type engine (1).

All these controls and monitoring controls are performed by the controller (55).

A two-cycle implosion type engine operation will be described with reference to FIG.

The main components of the two-cycle implosion type engine are a camshaft (60), a crankshaft (61), a connecting rod (62), a cylinder (63), a piston (64), a spark plug (65), an intake port (66), An intake valve (67), an intake cam (68), an exhaust port (69), an exhaust valve (70), an exhaust cam (71), and the like are included.

In the intake expansion stroke (56), the exhaust valve (70) is closed. The crankshaft (61) rotates clockwise, the connecting rod (62) is lowered, and the piston (64) is lowered from the top dead center. At the same time, the intake valve (67) is opened by the intake cam (68), and the inside of the cylinder (63) is opened. A negative pressure is applied, and the implosive material is charged into the cylinder (63) through the intake port (66). The intake valve (67) is closed by the intake cam (68) synchronized with the camshaft (60) at the cycle intermediate position of the intake expansion stroke (56), and filling of the implosion material is stopped.

During ignition expansion (57), the implosive material in the cylinder (63) is ignited (76) by the spark plug (65) after the intake valve (75) is closed. The implosion material burns and expands as the temperature rises, and the piston (72) reaches bottom dead center due to the expansion force. The crankshaft (73) rotates to the right, the intake expansion stroke (56) ends, and one cycle ends.

The ignition timing is independent, continuous from the state in which the intake valve (67) and the exhaust valve (70) are closed in the cycle of the intake expansion stroke (56) to the middle position of the cycle of the implosion exhaust stroke (58), or Intermittent ignition (76) ignition (78) may be used at any position.

In the implosion exhaust stroke (58), the implosion material burns, and at the same time the expansion ends, the phase state of the implosion material changes and implosion occurs. Water and water vapor are generated.

The volume ratio of the implosion material at this time is condensed to about 1/1200 or less, and the inside of the cylinder (63) is in a vacuum state, and the piston (77) is sucked in the direction of the top dead center by the suction force. 77) Ascend from bottom dead center.

During the implosion exhaust stroke (59), the crankshaft (79) rotates to the right due to inertia, and the exhaust cam (80) exhausts bubbles from the middle position of the implosion exhaust stroke (58) before the top dead center (80). 81) is opened, and the water and water vapor explosively expelled from the exhaust port (69) are exhausted to just before the top dead center, and the exhaust bubble (81) is closed by the exhaust cam (80) before the top dead center, (58) ends and ends two cycles.

Again, the crankshaft (79) rotates clockwise with inertia and repeats the intake and expansion strokes (56) and the implosion and exhaust stroke (58). In this implosion type engine, when the piston (64) is cycled twice, the crankshaft (61) rotates once and the camshaft (60) rotates once. The ignition (76) by the spark plug (65) is performed once. 2-cycle implosion type engine.

A 4-cycle implosion type engine operation will be described with reference to FIG.

The main components of the 4-cycle implosion type engine are a camshaft (91), a crankshaft (92), a connecting rod (93), a cylinder (94), a piston (95), a spark plug (96), an intake port (97), An intake valve (98), an intake cam (99), an exhaust port (100), an exhaust valve (101), an exhaust cam (102), and the like are included.

In the intake expansion stroke (83), the exhaust valve (101) is closed. The crankshaft (92) rotates clockwise, the connecting rod (93) is lowered, and the piston (95) is lowered from the top dead center. At the same time, the intake valve (98) is opened by the intake cam (99), and the inside of the cylinder (94) is opened. Negative pressure is reached, and the implosive material is sucked into the cylinder (94) through the suction port (97). The intake valve (98) is closed by the intake cam (99) synchronized with the camshaft (91) at the cycle intermediate position of the intake expansion stroke (83), and filling of the implosion material is stopped.

During ignition expansion (84), after closing the intake valve (106), the implosive material in the cylinder (94) is ignited (109) by the spark plug (96). The implosion material burns and expands as the temperature rises, and the expansion force causes the piston (108) to reach bottom dead center. The crankshaft (103) rotates to the right, the expansion stroke (83) ends, and one cycle ends.

The ignition timing is independent, continuous ignition (109) from the state where the intake valve (98) and the exhaust valve (101) are closed in the cycle of the intake expansion stroke (83) to the middle position of the cycle of the implosion exhaust stroke (85). Or intermittent ignition (109) at any position.

In the implosion stroke (85), the implosion material burns, and at the same time the expansion ends, the phase state of the implosion material changes and implosion occurs. Water and water vapor are generated.

The volume ratio of the implosion material at this time is condensed to about 1/1200 or less, and the inside of the cylinder (94) becomes a vacuum state, and the piston (110) is sucked in the direction of the top dead center by the suction force. 110) rise from bottom dead center.

During the implosion stroke (86), the intake valve (106) and the exhaust bubble (101) are closed, and the implosion material in the cylinder (94) is condensed to change its phase state to moisture and water vapor. The inside of (94) is in a vacuum state, the piston (113) is sucked to the top dead center, the connecting rod (111) is also raised, the implosion stroke (85) is finished, and the second cycle is finished.

In the cooling step (87), when the piston (114) reaches the top dead center, the piston (114) again moves to the bottom dead center by the inertial force.

During the cooling process (88), the piston (118) moves from the top dead center to the bottom dead center by the inertial force of the crankshaft (117). At this time, the exhaust bubble (116) is opened by the exhaust cam (115), the outside air is sucked from the exhaust port (100) by the suction force of the piston (118), filled into the cylinder (94), and condensed water or water vapor. To cool the piston (118), cylinder (94), spark plug (96) and engine block. The crankshaft (117) rotates half a round and the piston (118) reaches bottom dead center, the cooling step (87) is completed, and three cycles are completed. At this time, the exhaust bubble (116) is in an open state.

In the exhaust stroke (89), the piston (120) rises from the bottom dead center by the inertial force of the crankshaft (119) while the exhaust bubble (121) continues to open.

During the exhaust stroke (90), the exhaust bubble (124) remains open and the piston (125) moves from bottom dead center to top dead center due to the inertial force of the crankshaft (122). ) Water, water vapor, and cooled outside air are exhausted from the exhaust port (100). The piston (125) reaches top dead center, the crankshaft (122) rotates half a circle, the exhaust bubble (124) is closed by the exhaust cam (123), the exhaust stroke (89) is completed, and the four cycles are completed.

The crankshaft (122) rotates clockwise by the inertial force, reaches the intake expansion stroke (83), and repeats the implosion stroke (85), the cooling step (87), and the exhaust stroke (89). In this implosion type engine, the piston (95) performs four cycles, the crankshaft (92) rotates twice, and the camshaft (91) rotates once. Is a one-time four-cycle implosion-type engine.

The operation of the one-rotation / three-ignition rotary implosion-type engine will be described with reference to FIG.

The main components of the one-rotation / three-ignition rotary implosion type engine are a rotary housing (138), an eccentric shaft (139), a rotor (140), a spark plug (141), an intake hole (142), an exhaust hole (143), and a cooling unit. The intake hole (144), the cooling exhaust hole (145), the first working chamber (146), the second working chamber (147), the third working chamber (148) and the like are formed. Shrink material is supplied.

The space between the rotary housing (138) and the rotor (140) is called a working chamber, and the space capacity changes depending on the rotational position. In this description, the front and rear ends of the rotor (140) in the first working chamber (146) I will explain between.

In the intake expansion / contraction stroke (126), the rotor (140) rotates clockwise, the front end of the rotor (140) of the first working chamber (146) passes through the intake hole (142), and the first working chamber (146) ) From the point when the space volume of the first working chamber increases from the minimum to the intake expansion / expansion stroke (126). Further, when the rotor (140) rotates clockwise, the volume of the first working chamber (146) increases. The inside of the first working chamber (146) becomes negative pressure, and the implosion material is sucked into the first working chamber (146) from the intake hole (142).

During intake (127), the rotor (140) rotates clockwise, the space capacity of the first working chamber (146) increases, and the implosive material is sucked into the first working chamber (146) from the intake hole (142). To charge. The rear end of the first working chamber (146) of the rotor passes through the intake hole (142) just before the space capacity of the first working chamber (146) reaches the maximum value.

During expansion (128), the rotor (140) rotates clockwise and the rear end of the rotor (140) of the first working chamber (146) passes through the intake hole (142) and the first working chamber (146). ) When the front end of the rotor (140) is in front of the exhaust hole (143), that is, when the first working chamber (146) is sealed, the space capacity of the first working chamber (146) is maximized. In front, the implosive material filled in the first working chamber (146) is ignited (149) by the spark plug (141), the implosive material is combusted, and the expansion force due to the expansion accompanying the temperature rise of the implosive material by the combustion Then, it rotates clockwise to increase the space capacity of the first working chamber (146).

During implosion (129), the volume ratio of the implosion material is condensed to about 1/1200 or less due to the phase change after the implosion material is burned, and implosion occurs. As a result of implosion, the first working chamber (146) is in a vacuum state and has a negative pressure. The rotor (140) rotates rightward in the direction of the exhaust hole (143) that reduces the space capacity by the suction force.

The exhaust stroke (130) rotates right by the inertial force of the rotor (140), while the water and water vapor exploded inside the first working chamber (146) is converted into a minimum value in the first working chamber (146) space capacity. The front end of the rotor (140) of the first working chamber (146) passes through the exhaust hole (143) and exhausts from the exhaust hole (143). When the exhaust hole is not attached, the exhaust stroke (130) and the exhaust stroke end (131) are skipped and the cooling intake step (132) is started.

At the end of the exhaust stroke (131), the rotor (140) rotates clockwise, the space capacity of the first working chamber (146) is minimized, and all water and water vapor are exhausted and drained from the exhaust hole (143). The rear end of the rotor (140) of the first working chamber (146) passes through the exhaust hole (143), and the exhaust stroke ends (131).

In the cooling intake process (132), the rotor (140) rotates clockwise due to inertial force, and when the front end of the rotor (140) of the first working chamber (146) passes through the cooling intake hole (144), the cooling intake hole (144) ) Sucks outside air into the first working chamber (146), and cools the rotor (140), the first working chamber (146), and the rotary housing (138). When the exhaust hole (143) is not attached, water and water vapor generated during implosion (129) and the outside air sucked from the cooling intake hole (144) in the cooling intake process (132) are mixed.

During the cooling and intake process (133), the rotor (140) rotates to the right and the space capacity of the first working chamber (146) increases, and the first working chamber (146) becomes negative pressure and cools the outside air as a cooling intake hole. Aspirate from (144). The rotor (140), the first working chamber (146), and the rotary housing (138) are further cooled.

At the end of the cooling intake process (134), the rotor (140) rotates clockwise, the rear end of the rotor (140) passes through the cooling intake hole (144), and the front end of the rotor (140) is the cooling exhaust hole (145). The cooling air intake step (132) is terminated before.

The cooling exhaust stroke (135) becomes the cooling exhaust stroke (135) when the rotor (140) rotates clockwise due to inertial force and the front end of the rotor (140) passes through the cooling exhaust hole (145).

During the cooling and exhaust stroke (136), the rotor (140) rotates clockwise by the inertial force, the space capacity of the first working chamber (146) is reduced, and the first working chamber (146) is pressurized and the first Water, water vapor and cooled outside air in the working chamber (146) are exhausted and discharged from the cooling exhaust hole (145).

At the end of the cooling exhaust stroke (137), the rotor (140) rotates clockwise due to the inertial force, the space capacity of the first working chamber (146) is minimized, and all the water, water vapor, and cooled outside air are cooled by the cooling exhaust hole (145). Drain the exhaust more. The rear end of the rotor (140) of the first working chamber (146) passes through the cooling exhaust hole (145) to complete the cooling exhaust stroke (135).

Further, the rotor (140) rotates to the right due to inertia, and the intake / expansion / expansion stroke (126), the exhaust stroke (130), the cooling / intake step (132), and the cooling / exhaust stroke (135) are repeated. This rotary implosion type engine has a first working chamber (146), a second working chamber (147), a third working chamber (148) and three working chambers, and each working chamber performs the same process. When the rotor (140) rotates once, the spark plug (141) is ignited three times (149). In other words, it is a one-rotation three-ignition rotary implosion type engine that imploses three times in one rotation.

The operation of the 1-rotation 6-ignition rotary implosion type engine will be described with reference to FIG.

The main configuration of the one-rotation six-ignition rotary implosion type engine is as follows: rotary housing (162), eccentric shaft (163), rotor (164), first spark plug (165), second spark plug (166), first intake air Hole (167), first exhaust hole (168), second intake hole (169), second exhaust hole (170), first working chamber (171), second working chamber (172), third working chamber ( 173) and the like, and implosive material is supplied to the first exhaust hole (168) and the second intake hole (169).

The space between the rotary housing (162) and the rotor (164) is called a working chamber, and the space capacity changes depending on the rotational position. In this description, the front and rear ends of the rotor (164) in the first working chamber (171) are arranged. I will explain between.

In the first intake / expansion / expansion stroke (150), the rotor (164) rotates to the right, and the front end of the rotor (164) of the first working chamber (171) passes through the first intake hole (167). From the point of time when the space capacity of the working chamber (171) increases from the minimum, it becomes the first intake / expansion / explosion stroke (150). When the rotor (164) rotates to the right, the space capacity of the first working chamber (171) increases. The inside of the first working chamber (171) becomes negative pressure, and the implosive material is sucked into the first working chamber (171) from the first intake hole (167).

During the first intake (151), the rotor (164) rotates to the right, the space capacity of the first working chamber (171) increases, and the implosion material passes through the first working chamber (171) from the first intake hole (167). ) Will be sucked and filled. The rear end of the rotor (164) of the first working chamber (171) passes through the intake hole (167) just before the space capacity of the first working chamber (171) reaches the maximum value.

During the first expansion (152), the rotor (164) rotates clockwise and the rear end of the rotor (164) of the first working chamber (171) passes through the first intake hole (167), and the first When the front end of the rotor (164) of the working chamber (171) is in front of the first exhaust hole (168), that is, when the first working chamber (171) is in a sealed state, the first working chamber (171) Before the space capacity reaches the maximum, the first spark plug (165) first ignites (174) the implosive material filled in the first working chamber (171). It rotates rightward in the direction of increasing the space capacity of the first working chamber (171) by the expansion force due to the expansion accompanying the temperature rise of the contracted material.

During the first implosion (153), after the implosive material in the first working chamber (171) is combusted, the volume ratio of the implosive material is condensed to about 1/1200 or less due to the phase change. As a result of implosion, the first working chamber (171) becomes a vacuum state and becomes negative pressure, and the rotor (164) rotates rightward in the direction of decreasing the space capacity. Turn right in the direction of the first exhaust hole (168).

The first exhaust stroke (154) rotates clockwise by the inertial force of the rotor (164) while the space capacity of the first working chamber (171) is reduced, and the front end of the rotor (164) of the first working chamber (171). Passes through the first exhaust hole (168), and the water and water vapor exploded inside the first working chamber (171) are exhausted and discharged from the first exhaust hole (168).

At the end of the first exhaust stroke (155), the rotor (164) rotates clockwise while the space capacity of the first working chamber (171) is minimized, and all water and water vapor are exhausted from the first exhaust hole (168). To do. When the rear end of the rotor (164) of the first working chamber (171) passes through the first exhaust hole (168), the first exhaust stroke end (155) ends.

In the second intake / expansion / expansion stroke (156), the rotor (164) rotates clockwise, and the front end of the rotor (164) of the first working chamber (171) passes through the second intake hole (169). From the point when the space capacity of one working chamber (171) increases from the minimum, it becomes the second intake expansion / expansion stroke (156). When the rotor (164) rotates to the right, the space capacity of the first working chamber (171) increases, the inside of the first working chamber (171) becomes negative pressure, and the implosive material is first actuated from the second intake hole (169). Inhaled into chamber (171).

During the second intake (157), the rotor (164) rotates to the right, the space capacity of the first working chamber (171) increases, and the implosion material flows from the second intake hole (169) into the first working chamber (171). ) Will be sucked and filled. Before the space capacity of the first working chamber (171) reaches the maximum value, the rear end of the rotor (164) of the first working chamber (171) passes through the second intake hole (169).

During the second expansion (158), the rotor (164) rotates clockwise and the rear end of the rotor (164) of the first working chamber (171) passes through the second intake hole (169), and the first When the front end of the rotor (164) of the working chamber (171) is in front of the second exhaust hole (170), that is, when the first working chamber (171) is in a sealed state, the first working chamber (171) Before the space capacity reaches the maximum, the second spark plug (166) ignites the implosion material filled in the first working chamber (171) for the second time (175). It rotates rightward in the direction of increasing the space capacity of the first working chamber (171) by the expansion force due to the expansion accompanying the temperature rise of the contracted material.

During the second implosion (159), after the implosive material in the first working chamber (171) is combusted, the volume ratio of the implosive material is condensed to about 1/1200 or less due to the phase change. By the implosion, the first working chamber (171) becomes a vacuum state and becomes negative pressure, and the rotor (164) rotates rightward in the direction of decreasing the space capacity by the suction force. Turn right in the direction of the second exhaust hole (170).

In the second exhaust stroke (160), the space capacity of the first working chamber (171) is reduced while rotating to the right by the inertial force of the rotor (164), and the implosed water inside the first working chamber (171) is reduced. And water vapor are discharged from the second exhaust hole (170).

At the end of the second exhaust stroke (161), the rotor (164) rotates clockwise while the space capacity of the first working chamber (171) is minimized, and all the water and water vapor are exhausted and discharged from the second exhaust hole (170). To do.

Further, the rotor (164) rotates to the right due to inertia, and the first intake expansion / explosion / reduction stroke (150), the first exhaust stroke (154), the second intake expansion / explosion / reduction stroke (156), and the second exhaust stroke (160). )repeat. This rotary implosion type engine has a first working chamber (171), a second working chamber (172), a third working chamber (173) and three working chambers, and each working chamber performs the same process. When the rotor (164) rotates once, the first spark plug (165) ignites three times (174), and the second spark plug (166) also ignites three times (175), that is, six times per revolution. That is, it is a one-rotation six-ignition rotary implosion type engine that imploses six times.

In the rotary implosion-type engine, the first intake hole, the first exhaust hole, the second intake hole, and the second exhaust hole are fitted with intake bubbles, exhaust bubbles, and rotary bubbles synchronized with the rotor, so that the timing of intake and exhaust can be adjusted. Adjust and improve the sealing to prevent backfire.

The main fuel implosion material can be water that will not be depleted. There is no need for fossil fuels such as gasoline and natural gas. Implosion material is carbon-free energy. Operation without oxygen is possible. The explosive engine exhaust does not generate carbon dioxide gas, toxic gas or soot, and only moisture and water vapor. The displacement is very small, and it can be operated indoors, in vacuum, in water, and in bad environments. No vaporizer is required. Exhaust sound is small and no muffler is required.

If natural energy such as solar power generation, wind power generation, and hydroelectric power generation is used, it becomes an energy saving measure and the running cost is reduced. Energy can be accumulated if implosion material is stored in an accumulator.

Water and water vapor generated by the implosion type engine can be used for a long time without hydration if it is recovered and reused with pure water, resulting in a closed cycle engine.

The engine has no compression stroke or explosion stroke, and there is no compression loss. A two-cycle implosion type engine can obtain twice the output of a four-cycle implosion type engine. A 1-rotation 6-ignition rotary implosion type engine can output twice as much as a 1-revolution 3-ignition rotary implosion type engine.

Replacing the conventional engine, diesel engine timing chain, or belt. Gear change. Change cam position. Cam shape change. Add fuel injection valve, fuel injection pump, ejector, arrester. The diversion can be modified by changing the ignition timing.

The position of the intake port of a conventional rotary engine is changed. Change the position of the exhaust hole. Change the spark plug position. Change ignition timing. Conversion can be made by adding intake and exhaust valves.

DESCRIPTION OF SYMBOLS 1 Implosion type engine 2 Oxyhydrogen gas generator 3 Generator 4 Solar power generation 5 Wind power generation 6 Commercial power supply 7 Power supply selector 8 Battery charger 9 Battery 10 Capacitor stack 11 Buck-boost DC-DC converter 12 Power detector 13 Pulse width Converter 14 Electrolyte 15 Electrode 16 Oxyhydrogen Gas 17 Electrolyte Bubble 18 Check Valve 1
19 Bubbling tank 1
20 Electrolyte 21 Bypass piping 22 Check valve 2
23 Oxyhydrogen gas and water vapor 24 Bubbling tank 2
25 Pure water 26 Check valve 3
27 Oxyhydrogen gas 28 Water level detector 29 Supply tank 30 Water supply pump 31 Water supply solenoid valve 32 Check valve 4
33 Pure water device or RO pure water device 34 Accumulator 35 Ejector 36 Accelerator pedal 37 Oxyhydrogen gas 38 Pressure detector 39 Check valve 5
40 Pressurizing blower 41 Gas supply valve 42 Gas amount control valve 43 Arrester
44 Fuel injection valve 45 Oxyhydrogen gas 46 Intake port 47 Intake valve 48 Cylinder 49 Piston 50 Spark plug 51 Oxygen gas 52 Exhaust valve 53 Exhaust port 54 Exhaust steam 55 Controller 56 Intake expansion stroke 57 During ignition expansion 58 Explosion exhaust stroke 59 Camshaft 61 Crankshaft 62 Connecting rod 63 Cylinder 64 Piston 65 Spark plug 66 Intake port 67 Intake valve 68 Intake cam 69 Exhaust port 70 Exhaust valve 71 Exhaust cam 72 Piston 73 Crankshaft 74 Intake cam 75 Intake bubble 76 Ignition 77 Piston 78 Ignition 79 Crankshaft 80 Exhaust cam 81 Exhaust bubble 82 Piston 83 Intake expansion stroke 84 Ignition expansion 85 Explosion stroke 86 Explosion stroke 87 Cooling process 88 Cool During process 89 Exhaust stroke 90 Exhaust stroke 91 Camshaft 92 Crankshaft 93 Connecting rod 94 Cylinder 95 Piston 96 Spark plug 97 Intake port 98 Intake valve 99 Intake cam 100 Exhaust port 101 Exhaust valve 102 Exhaust cam 103 Crankshaft 104 Camshaft 105 Exhaust Valve 106 Intake bubble 107 Intake cam 108 Piston 109 Ignition 110 Piston 111 Connecting rod 112 Crankshaft 113 Piston 114 Piston 115 Exhaust cam 116 Exhaust bubble 117 Crankshaft 118 Piston 119 Crankshaft 120 Piston 121 Exhaust bubble 122 Crankshaft 123 Exhaust cam 124 Exhaust valve 125 Piston 126 Inspiratory expansion / reduction stroke 127 During intake 128 During expansion 129 Explosion 130 Exhaust stroke 131 Exhaust stroke end 132 Cooling intake process 133 During cooling intake process 134 Cooling intake process completed 135 Cooling exhaust stroke 136 Cooling exhaust stroke completed 137 Cooling exhaust stroke end 138 Rotary housing 139 Eccentric shaft 140 Rotor 141 Spark plug 142 Inlet hole 143 Exhaust hole 144 Cooling intake hole 145 Cooling exhaust hole 146 First working chamber 147 Second working chamber 148 Third working chamber 149 Ignition 150 First intake expansion / expansion stroke 151 First intake 152 During first expansion 153 First expansion Medium 154 First exhaust stroke 155 First exhaust stroke end 156 Second intake expansion / expansion stroke 157 Second intake expansion 158 Second expansion 159 Second expansion / expansion 160 Second exhaust stroke 161 Second exhaust stroke end 162 Rotary housing 163 Eccentric shaft 164 Rotor 165 First spark plug 166 Second spark plug 167 First intake hole 168 First exhaust hole 169 Second intake hole 170 Second exhaust hole 171 First working chamber 172 Second working chamber 173 Third working chamber 174 First ignition 175 Second ignition

Claims

An implosion-type engine that uses oxyhydrogen gas (2H2 + O2) or hydrogen (H2) alone, or a mixture of these simple gases and oxygen (O2), air, etc. as the implosion, and this implosion as fuel.
The implosion material characterized in claim 1 filled in a sealed state is ignited, the expansion force due to an expansion reaction in which the implosion material expands as the temperature rises due to this combustion, and the phase change and condensation after combustion In the implosion reaction, the implosion material becomes a vacuum and becomes a negative pressure, which generates suction force. After the implosion material burns, it becomes water or steam. An implosion engine that uses the generated expansion force and suction force as power sources.
The operation of the two-cycle implosion type engine is an intake expansion stroke, ignition, and an implosion exhaust stroke.
The intake expansion stroke of the first cycle is that the intake valve opens and the piston is inertial, and the implosive material supplied to the intake valve is drawn from the top dead center to the bottom dead center. Closes and the intake operation is completed. In the ignition, the implosion material is ignited during the cycle of the implosion exhaust stroke from the completion of the intake operation, and the piston reaches the bottom dead center by the expansion reaction of the implosion material by combustion.
The implosion exhaust stroke of the second cycle is an implosion reaction after the implosion material burns, the inside of the cylinder is in a vacuum state, and the piston moves from bottom dead center to top dead center by suction force. The bubble is opened and water or water vapor generated by the implosion reaction is exhausted and discharged before top dead center. The exhaust bubble is closed near top dead center. The piston reaches top dead center due to inertia. An implosion type engine characterized by having no compression stroke and no explosion stroke.
The operation of the 4-cycle implosion type engine is an intake expansion stroke, ignition, an implosion stroke, a cooling process, and an exhaust stroke.
The intake expansion stroke of the first cycle is that the intake valve opens and the piston is inertial, and the implosive material supplied to the intake valve is drawn from the top dead center to the bottom dead center. Is closed to complete the intake operation. The ignition ignites the implosion material during the cycle of the implosion stroke from the completion of the intake operation, and the piston reaches the bottom dead center due to the expansion reaction of the implosion material by combustion.
In the implosion stroke of the second cycle, after the implosion material burns, the inside of the cylinder is evacuated by the implosion reaction, and the piston reaches from the bottom dead center to the top dead center by the suction force. Water and water vapor generated by the implosion reaction remain in the cylinder.
The cooling process in the third cycle was caused by an implosion reaction by opening the exhaust valve before and after top dead center, and by inertia, Biston headed from top dead center to bottom dead center, sucking outside air from the exhaust port into the cylinder. Mixing with water or steam to cool the engine body, piston and spark plug, the piston reaches the bottom dead center due to inertia.
In the exhaust stroke of the fourth cycle, the exhaust bubble is open and inertia, the piston moves from bottom dead center to top dead center, and the mixture of water and water vapor in the cylinder and cooled outside air is exhausted and drained, and near the top dead center Close the exhaust bubble and reach top dead center. An implosion type engine characterized by having no compression stroke and no explosion stroke.
The operation of the one-rotation / three-ignition rotary implosion type engine has a space capacity of the working chambers of the rotor and the rotary housing, each of which has an intake / expansion / explosion stroke, ignition, exhaust stroke, cooling intake stroke, and cooling exhaust stroke. There are two places where the minimum of the water is the implosive material supplied to the air intake holes in one of the air intake holes by the rotation of the rotor to the working chamber, the cooled outside air in the working chamber, the water or water vapor generated by the implosion reaction A cooling air intake hole that exhausts and discharges water and water vapor generated by the implosion reaction in the working chamber and a cooling air intake hole that sucks cooling air into the working chamber Equipped with. A spark plug is installed in a rotary housing near the maximum space capacity of the working chamber between the intake and exhaust holes. The front and rear ends of the rotor follow the rotation and pass through the intake holes, exhaust holes, cooling intake holes, and cooling exhaust holes.
When the rotor rotates and the front end passes through the intake hole, the intake expansion / reduction stroke takes in the implosion material supplied to the intake hole from the intake hole to the working chamber, and when the rear end of the rotor passes through the intake hole, At the same time, the working chamber is sealed with the front end of the rotor in front of the exhaust hole, and the space capacity of the working chamber is maximized. The implosion material is ignited and combusted before it reaches the maximum, the combustion generates an expansion force and rotates in the direction that maximizes the space capacity. The rotor rotates in the direction that minimizes the space capacity. In the exhaust stroke, water or water vapor generated by the implosion reaction is exhausted and discharged from the exhaust hole before the rotor rotates and the space capacity is minimized. In the cooling intake stroke, when the rotor rotates by inertia and the front end passes through the cooling intake hole, outside air is sucked from the cooling intake hole to cool the rotor, the rotary housing, and the like. In the cooling exhaust stroke, when the rotor rotates by inertia and the front end of the rotor passes through the cooling exhaust hole, the cooled outside air of the working chamber and water or water vapor are cooled and exhausted until the space capacity of the working chamber is reduced to the minimum. Exhaust fluid from the exhaust. An implosion type engine characterized by having no compression stroke and no explosion stroke.
The operation of the one-rotation six-ignition rotary implosion type engine is as follows. For each working chamber, the first intake / expansion / explosion stroke, the first ignition, the first exhaust stroke, the second intake / expansion / explosion stroke, the second ignition, the second There are two places where the space capacity of the working chamber of the rotary housing is minimized, there is an exhaust stroke, one of which is implosion reaction in the working chamber and the first suction hole that sucks the implosive material into the working chamber by the rotation of the rotor The second exhaust hole for exhausting and discharging water and water vapor generated by the above is installed, and the first exhaust hole for exhausting and discharging water and water vapor generated by the implosion reaction in the working chamber and the implosion material are rotors in the working chamber. A second intake hole for intake by rotation of the. A rotary housing in the vicinity of which the space capacity of the working chamber between the first intake hole and the first exhaust hole is maximized is provided with a first spark plug, and the space capacity of the working chamber between the second intake hole and the second exhaust hole is maximized. A rotary housing in the vicinity of the second is provided with a second spark plug, and the front end and the rear end of the rotor follow the rotation and pass through the first intake hole, the first exhaust hole, the second intake hole, and the second exhaust hole.
In the first intake / expansion / expansion stroke, when the rotor rotates and the front end passes through the first intake hole, the implosion material supplied to the intake hole is sucked into the working chamber from the first intake hole. When the air passes through the first air intake hole, the intake air is completed, and at the same time, the working chamber is sealed with the front end of the rotor in front of the first exhaust hole, and the space capacity of the working chamber is maximized. The implosive material is first ignited and burned by the first spark plug before it reaches the maximum, and the rotor rotates in the direction in which expansion force is generated by combustion and the space capacity is maximized. After combustion, the implosion reaction results in a vacuum state. It rotates in the direction where the suction capacity is generated and the space capacity is minimized.
In the first exhaust stroke, when the front end of the rotor passes through the first exhaust hole, water and water vapor generated by the implosion reaction are exhausted and discharged from the first exhaust hole until the space capacity of the working chamber is reduced to the minimum. .
In the second intake expansion / expansion stroke, when the rotor rotates and the front end passes through the second intake hole, the implosion material supplied to the intake hole is sucked into the working chamber from the second intake hole. When the air passes through the second air intake hole, the air intake is completed, and at the same time, the working chamber is sealed with the front end of the rotor in front of the second exhaust hole, and the space capacity of the working chamber is maximized. Before the maximum, the second spark plug ignites the implosion material for the second time and burns. The rotor rotates in the direction in which the expansion force is generated by the combustion and the space capacity is maximized. It rotates in the direction where the suction capacity is generated and the space capacity is minimized.
In the second exhaust stroke, when the front end of the rotor passes through the second exhaust hole, water and water vapor generated by the implosion reaction are exhausted and discharged from the second exhaust hole until the space capacity of the working chamber is reduced to the minimum.
An implosion type engine characterized by having no compression stroke and no explosion stroke.
7. A rotary implosion type engine characterized in that an intake valve and an exhaust valve are attached to an inlet of an intake hole synchronized with the rotation of a rotor and an outlet valve of the exhaust hole, respectively.
An implosion type engine characterized by comprising a generator and an electric motor, and characterized by claim 3, claim 4, claim 5, claim 6 and claim 7.
An implosion type engine characterized in that a safety device such as an ejector or a backfire prevention arrester is provided at an intake port of the implosion type engine, as claimed in claim 3, claim 4, claim 5, claim 6 or claim 7.
A fuel injection valve and a pressurizing device are provided for supplying implosion material to an intake port of an implosion type engine, and characterized by claim 3, claim 4, claim 6, claim 7, and claim 7. Implosion type engine.
An implosion engine characterized by claim 3, claim 4, claim 5, claim 6, and claim 7, comprising natural energy such as solar power generation, wind power generation, and hydropower generation, and an external power source.
An implosion engine characterized by comprising an accumulator or a storage facility for storing implosion material, and claim 4, claim 5, claim 6, claim 7, and claim 7.