CN203335230U - Turbine rotor energy-saving engine - Google Patents

Turbine rotor energy-saving engine Download PDF

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Publication number
CN203335230U
CN203335230U CN2013200097309U CN201320009730U CN203335230U CN 203335230 U CN203335230 U CN 203335230U CN 2013200097309 U CN2013200097309 U CN 2013200097309U CN 201320009730 U CN201320009730 U CN 201320009730U CN 203335230 U CN203335230 U CN 203335230U
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China
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cylinder
rotor
piston
energy
middle cylinder
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Expired - Lifetime
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CN2013200097309U
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Chinese (zh)
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黄荣嵘
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Priority to CN2013200097309U priority Critical patent/CN203335230U/en
Priority to PCT/CN2013/087798 priority patent/WO2014107996A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/40Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
    • F01C1/46Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the outer member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/356Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
    • F01C1/3566Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along more than one line or surface
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/14Adaptations of engines for driving, or engine combinations with, other devices

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

The utility model discloses a turbine rotor energy-saving engine which is a cylindrical machine body. A rotating shaft is arranged in the center of the cylindrical machine body, a rotor is arranged on the shaft, the rotor is sleeved with a cylinder shell, an air pressing fan is arranged at one end of the rotating shaft, the rotor is divided into an upper cylinder rotor, a middle cylinder rotor and a lower cylinder rotor, the corresponding machine body shell is divided into an upper cylinder, a middle cylinder and a lower cylinder, the upper cylinder rotor is a star-shaped equal-arc cam, three sets of piston air cylinders and three sets of high-pressure oil pumps of the body shell of the upper cylinder are correspondingly and longitudinally equal in distance and are compressed to carry out reciprocating motion, three protruding pistons in the middle section of the rotor are matched with the inner wall of the cylindrical middle cylinder to be in sealing rotation, the protruding pistons and the shaft are identical in direction and equal in arc length, radial sealing grooves are formed in the inner wall of the middle cylinder in an equal-arc mode, groove sealing pieces divide the body of the middle cylinder into three sets of independent cylinder bodies, each set of cylinder body is provided with an ignition chamber to be communicated with the middle cylinder and is provided with a sparking plug and an oil nozzle, two auxiliary cylinders are arranged on the inner layer of the wall of the middle cylinder to be communicated with the middle cylinder, new energy fuel is combusted in one auxiliary cylinder, cooling water absorbs heat and is gasified in the other auxiliary cylinder and returns to the middle cylinder, and the excess pressure of discharged waste gas is reused by the lower cylinder rotor to carry out circulating acting to improve heat efficiency. The turbine rotor energy-saving engine is simple in structure and small in size, saves energy and is environmentally friendly.

Description

The turbine rotor energy-saving engine
Technical field
The motor that belongs to power car, steamer, aircraft, generator set and all kinds of movable machinery power output source.
Background technique
Current social science and technology and rapid economic development, the mankind are growing to various motor vehicle and various motivation power tool demand thereof, and the different exhaustion of main energy sources day, and people have higher requirement to engine performance.Export source engine as machine powers such as vehicle and steamers, at present application mainly contain petrol engine, diesel engine, rotary engine and aviation Spray gas motor etc.Petrol engine and diesel engine are all to adopt the cylindrical piston straight reciprocating motion to complete to suck air-fuel mixture gas or pure air, compressed again, light a fire or spray into the diesel oil compression ignite, acting, exhaust, by the connecting bar and crankshaft outputting power, rotary engine adopts triangular rotor, gear by rotor center coordinates with the uranium gear, in the ellipse cylinder body, along the casing wall eccentric rotary, completes the working procedures such as air-breathing, compression, ignition-powering, exhaust and carrys out outputting power.The type of cooling that petrol engine and diesel engine adopt and exhaust mode, make a large amount of heat-energy losses, thermal efficiency ratio is lower, cause huge energy waste, the petrol engine thermal efficiency preferably can only reach 30%, the diesel engine thermal efficiency also is no more than 45%, rotary engine is due to defect on gas-tight design, so the thermal efficiency is lower, aeroengine is also very high oil consumption and cost, in the world, environmental consciousness is strengthened day by day, and petroleum resources are today of exhaustion day by day, and the mankind improve performance to motor more serious hope.Petrol engine and rotary engine have higher rotating speed, but torsion is smaller, and the torsion of diesel engine is larger, but rotating speed is but not high, and heavy, and the mutual shortcoming, can not meet the requirement that society advances.
The model utility content
The purpose of this utility model is to make motor to improve power, reduces oil consumption, toxic emission etc. and significantly reduces, and to reach the purpose of energy-saving and emission-reduction, weight and volume reduce, and output power increases, and service behaviour is more reliable and more stable, to meet the social development requirement.
A kind of turbine rotor energy-saving engine, comprise: a rotor cylinder with positive circular inner wall, one is arranged on the rotor with centrifugal pressure fan of cylinder body rotatably with the cylinder body concentric, described rotor is divided into three parts by two rotor piston rings, cylinder body is to there being upper cylinder half, middle cylinder, lower cylinder, upper rotor part section coordinates with upper cylinder half, upper rotor part is the star-shaped arc cam that waits, along axle center, outside star-shaped decile arranges many group piston-cylinders to upper casing wall, three groups of high pressure high pressure high pressure oil pumps, piston is furnished with connecting rod, with wrist pin, connect, connecting rod one end acts on the high pressure high pressure oil pump, cam can be synchronoused working with the high pressure high pressure oil pump by the while compression piston, cylinder is provided with suction port, and between the high pressure high pressure oil pump, there is the spring-compressed connecting rod to drive piston and be the unlatching suction condition, piston-cylinder has the guide hole igniting chamber to connect with middle cylinder acting cylinder at middle casing wall, in hole, there are one-way movable air-stopping valve and barrier gas to enter the choke valve of acting cylinder, in rotor, cylinder section is the concentric right cylindrical, by circumference equal dividing, many salient angle pistons that radially rotate with the inside wall of cylinder in middle cylinder concentric high cooperation the together are set, the corresponding side face of piston ring of rotor place has the ring circumferential seal groove, seal ring is installed in groove, seal ring coordinate cylinder cap up and down with footpath by the rotor lobes side face of piston ring with the inner region transverse sealing, upper thread specific activity plug two ends, the two ends upper thread that middle cylinder matches with piston is high, middle inside wall of cylinder radius of a circle is greater than the rotor lobes piston radius, the middle inside wall of cylinder is equipped with radial seal groove by circumference equal dividing, compression is installed in groove carries Sealing to fit in many group active chambers together with rotor, every group of active chamber arranges a plurality of attached cylinders along casing wall, attached cylinder is porose to be connected with air chamber, be provided with oil nozzle and coordinate cam burner oil or cooling liquid, the cylinder group end has gas emission conversion guide hole to connect with lower cylinder group, the lower cylinder section that turns arranges dentation EGR guide groove, by in the cylinder high pressure mixing waste gas of discharging outside dentation EGR guide groove is discharged cylinder, the mutual reaction force principle of sawtooth in gas and groove, the driving rotation of turning, reach the manner of execution of EGR acting purpose.
Preferably, described turbine rotor energy-saving engine also comprises cooling system: attached cylinder on casing wall in cooling liquid sprays into, the gasification of liquid absorption casing wall heat, with combustion gas mixing, form high-pressure steam, increase again the air pressure acting to reach when cylinder body is lowered the temperature, reached the raising thermal efficiency, increased the manner of execution of output power purpose.
Preferably, described turbine rotor energy-saving engine is equipped with the startup magneto in turn inside and rotating shaft, has reduced occupation area, during engine operation, can also export electric energy.
The beneficial effects of the utility model:
The utility model adopts novel concentric cam wheel piston compression air, the rotor lobes piston coordinates three groups of cylinder bodies, form many group cylinder circular work, be equivalent to improve the quantity of cylinder, attached cylinder is sprayed by wooden carbon molecule and according to C+H2O+ high temperature=CO+H2 principle endothermic decomposition, is become water gas again to burn with the fuel that water mixes by oil nozzle, in attached cylinder, the cooling of charge mode in cylinder is sprayed back in water spray heat absorption vaporization again, the excellent sealing design, improve compression ratio, the EGR acting, the turbofan supercharging technology, heat energy is reduced the loss, improved the thermal efficiency, greatly reduce the discharge of oil consumption and waste gas, improved output power simultaneously, weight and volume have also been reduced, economic development and environment protection to human society has played positive effect, so with conventional diesel engine equal volume and weight under, can improve the output power of several times, and can reach the high rotating speed of rotary engine, the high torsion that has possessed again diesel engine, the working method of turning of the many piston cycle of multi-cylinder, make and move that more balance and stability is reliable, the structural design of new reasonable simplification and material application, many useless parts such as flywheel and Qu You have been removed, make production technology and workflow require significantly to reduce, be more convenient for universal production, the part life cycle but improves 2~3 times greatly, maintenance and cost of production have been reduced.
The accompanying drawing explanation
Accompanying drawing 1 is: the overall structure floor map is looked squarely in turbine rotor energy-saving engine front;
Accompanying drawing 2 is: turbine rotor energy-saving engine upper cylinder half cam rotor and casing wall piston-cylinder, the overall structure cross section A-A schematic diagram such as high-pressure service pump;
Accompanying drawing 3 is: cylinder section rotary piston and middle cylinder cylinder in the turbine rotor energy-saving engine, the attached cylinder on casing wall, spark plug, oil nozzle, cooling system, the overall structure section B-B schematic diagram such as port;
Accompanying drawing 4 is: cylinder section EGR groove working system under the turbine rotor energy-saving engine, starting electrical machinery system, the overall structure section C-C schematic diagram such as casing wall exhaust port;
Accompanying drawing 5 is turbine rotor energy-saving engine working stroke figure, Fig. 5-1st: upper cylinder half section piston-cylinder suction stroke; Fig. 5-2nd: the piston-cylinder pressurized gas enters middle cylinder part guide hole igniting chamber process; Fig. 5-3rd: guide hole igniting chamber igniting combustion gas enters the acting cylinder and starts acting;
Accompanying drawing 6 is turbine rotor energy-saving engine working stroke and exhaust process figure, Fig. 6-1st: the acting cylinder combustion gas drive rotor piston rotation acting of middle cylinder section, the acting cylinder process is returned in the attached cylinder 1 fuel heat absorption burning of middle casing wall; Fig. 6-2nd: in the attached cylinder of middle casing wall cooling system, the acting cylinder process is returned in cooling water heat absorption vaporization; Fig. 6-3rd, middle cylinder section acting cylinder mixed gas turns to lower cylinder section by guide hole; Fig. 6-4th, by the combination gas that forwards lower cylinder section to of cylinder section guide hole through lower rotor part EGR groove, by exhaust port, discharged outside cylinder.
Wherein: 1, rotating shaft; 2, centrifugal fan; 3, cam rotor section; 4, cylinder section in rotor; 5, cylinder section under rotor; 6, upper cylinder half; 7, middle cylinder; 8, lower cylinder; 9, compression cylinder; 10 compression pistons; 11 guide hole igniting chambers; 12, acting cylinder; 13, air-stopping valve 14, choke valve; 15, salient angle piston; 16, Sealing; 17, oil nozzle: comprise oil nozzle a, oil nozzle b, oil nozzle c; 18, high pressure oil pump: comprise high pressure oil pump d, high pressure oil pump e, high pressure oil pump f; 19, connecting rod; 20, piston ring: comprise piston ring g, piston ring h, piston ring i; 21, attached cylinder: comprise attached cylinder j, attached cylinder k; 22, gas emission conversion mouthful; 23, spark plug; 24, dentation groove 25, guide hole; 26, starting electrical machinery rotor; 27, relief opening; 28, intakeport; 29, spring; 30, puff prot.
Embodiment
The utility model is based on the turn motor of basic innovation of work of rotary engine, but fully different from rotary engine, overall structure arranges cylinder type loom as shown in fig. 1, be respectively and turn uranium (1), the centrifugal fan of calming the anger (2), cam rotor section (3), cylinder section (4) in rotor, cylinder section (5) under rotor, the cylinder shell is divided into upper cylinder half (6), middle cylinder (7), the compositions such as lower cylinder (8), as shown in Figure 2, the upper cylinder half rotor is a starlike arc cam that waits, upper casing wall is the star-shaped three groups of piston-cylinders (9) that arranging of outside equal portions along axle center, three high pressure oil pumps (d), (e), (f), piston (10) is furnished with connecting rod (19) and is located by connecting with wrist pin, connecting rod (19) one ends act on high pressure oil pump, make cam (3) compression piston and high pressure oil pump synchronous working simultaneously.Cylinder (9) is provided with intakeport (28), and is provided with spring (29) compression connecting rod (19) between high pressure oil pump (18) and drives piston and be the unlatching suction condition.In rotor, cylinder section (4) is the concentric right cylindrical, rotor is provided with two ring circumference piston grooves, piston ring (g) is inside arranged (h), as shown in Figure 3, between piston ring, have three with axle in the same way with piston ring (g) (h) within lateral extent isometric, same radius, salient angle piston (15) with arc length such as circumference, piston ring is opened and upper cylinder half (6) outward, the interior casing wall of lower cylinder (8) closely cooperates, make piston ring (g) and (h) between fit in an independent annular seal zones acting cylinder (12) with middle cylinder (7) inwall.Compression cylinder (9) has guide hole igniting chamber (11) to connect with middle cylinder acting cylinder (12) at middle casing wall, an one-way movable air-stopping valve (13) is arranged in hole, a choke valve (14) that compression is carried, between two air valves, it is igniting chamber, oil nozzle (a) radially is housed side by side, spark plug (23), guide hole and working cylinder are by puff prot (30) UNICOM.With salient angle side face of piston ring parallel ring be enclosed within rotor outer be middle cylinder (7), middle cylinder has radial groove as shown in Fig. 3 along the circumference symmetry, Sealing (16) is arranged in groove, Sealing and place groove have pressing device to make Sealing and rotor keep coordinating to be closed state makes middle cylinder be divided into three groups of cylinder block that work alone, be disposed with attached cylinder (j) oil nozzle (b) combination between Sealing on casing wall, (k) oil nozzle (c) combination of attached cylinder (cooling waster vat), attached cylinder has aperture and cylinder (12) UNICOM, and mouthful (22) are led in the gas emission conversion.As shown in Figure 4, under rotor, there are several ring reverse dentation grooves of girth (24) in cylinder section (4), piston ring (i) packing is arranged between groove and groove, and with guide hole (25) UNICOM, starting electrical machinery stator and rotor (26) are arranged in rotor, and have exhaust port (27) going up most casing wall under bar groove correspondence, with to the outlet pipe exhaust as Fig. 1.
The engine operation operation
Breathing process: as Fig. 5-1 piston drives and opens cylinder (9) through spring (29) compression connecting rod (19), air enters cylinder through suction port (28).
Compression process: starting electrical machinery (26) is as Fig. 5-2, rotating cam (3) compression piston (10) advances guide hole igniting chamber (11) at the inner motion compresses air of cylinder (9), choke valve (14) seals guide hole under spring pressure, cam rotates to connecting rod (19), by connecting rod to high pressure oil pump (d) synchronous compression, when piston moves to the cylinder summit, compression work completes, gas compression is inner at guide hole (11), rotor lobes piston (15) just in time moved puff prot (30) simultaneously, oil nozzle (a), the same time point fire-fighting of spark plug (23) oil firing, high combustion gas body is by upwards compressing sealing of air-stopping valve (13), choke valve (14) is pressed down to unlatching downwards, combustion gas is gone out puff prot and is entered acting cylinder (12) promotion salient angle piston (15) motion acting, as Fig. 5-3.
Acting process: as Fig. 6-1 blast combustion gas promotes forward piston (15), cross the aperture that attached cylinder (j) is communicated with air chamber, the water carbon fuel combination that attached cylinder (j) back warp cam compression high pressure oil pump (e) sprays to oil nozzle (b) and high-temperature fuel gas are mixed, the heat that water carbon fuel has absorbed combustion gas heats up, generate water gas formation secondary combustion according to the principle of C+H2O+ high temperature=CO+H2, when piston moved the aperture of attached cylinder (k) as Fig. 6-2, the high-temperature gas of twice combustion passes to the ring cylinder attached cylinder (k) through casing wall absorbs with the water sprayed through oil nozzle (c) by cam compression high pressure oil pump (f), water has absorbed heat and has changed into steam state and regurgitate the return-air chamber again and act on piston, reduce temperature to cylinder body and rotor and increased again air pressure.
Exhaust process: piston (15) had moved Sealing (16) as Fig. 6-3, Sealing completes closure at once, piston continues operation and enters next periodic duty, gas by the gas emission conversion lead mouthful (22) flow to and the reverse dentation groove of pressure-acting (24) as Fig. 6-4.As shown in Figure 1, flow to guide hole (25) along groove and enter next ring guide groove, the gas energy is fully absorbed, finally, by relief opening (27) exhaust, complete workmanship's stroke.
The cooling work principle:
By cam acting in the same way, the compression high pressure oil pump is pressed into liquid water and enters the attached cylinder of casing wall (k), the heat of vaporization gasification that water is drawn casing wall and combustion gas forms steam state, when the pressure of water vapour during higher than cylinder pressure, return acting cylinder (12) expansion and mix acting, thereby reached middle cylinder body cooling, draw the double action that heat energy transfers mechanical energy increase power to.

Claims (3)

1. a turbine rotor energy-saving engine, it is characterized in that: a rotor cylinder with positive circular inner wall, one is arranged on the rotor with centrifugal pressure fan of cylinder body rotatably with the cylinder body concentric, described rotor is divided into three parts by two rotor piston rings, cylinder body is to there being upper cylinder half, middle cylinder, lower cylinder, upper rotor part section coordinates with upper cylinder half, upper rotor part is the star-shaped arc cam that waits, along axle center, outside star-shaped decile arranges many group piston-cylinders to upper casing wall, three groups of high pressure oil pumps, piston is furnished with connecting rod, with wrist pin, connect, connecting rod one end acts on high pressure oil pump, cam can be synchronoused working with high pressure oil pump by the while compression piston, cylinder is provided with suction port, and between high pressure oil pump, there is the spring-compressed connecting rod to drive piston and be the unlatching suction condition, piston-cylinder has the guide hole igniting chamber to connect with middle cylinder acting cylinder at middle casing wall, in hole, there are one-way movable air-stopping valve and barrier gas to enter the choke valve of acting cylinder, in rotor, cylinder section is the concentric right cylindrical, by circumference equal dividing, many salient angle pistons that radially rotate with the inside wall of cylinder in middle cylinder concentric high cooperation the together are set, the corresponding side face of piston ring of rotor place has the ring circumferential seal groove, seal ring is installed in groove, seal ring coordinate cylinder cap up and down with footpath by the rotor lobes side face of piston ring with the inner region transverse sealing, upper thread specific activity plug two ends, the two ends upper thread that middle cylinder matches with piston is high, middle inside wall of cylinder radius of a circle is greater than the rotor lobes piston radius, the middle inside wall of cylinder is equipped with radial seal groove by circumference equal dividing, compression is installed in groove carries Sealing to fit in many group active chambers together with rotor, every group of active chamber arranges a plurality of attached cylinders along casing wall, attached cylinder is porose to be connected with air chamber, be provided with oil nozzle and coordinate cam burner oil or cooling liquid, the cylinder group end has gas emission conversion guide hole to connect with lower cylinder group, the lower cylinder section that turns arranges dentation EGR guide groove, by in the cylinder high pressure mixing waste gas of discharging outside dentation EGR guide groove is discharged cylinder, the mutual reaction force principle of sawtooth in gas and groove, the driving rotation of turning, reach the manner of execution of EGR acting purpose.
2. turbine rotor energy-saving engine according to claim 1, it is characterized in that: also comprise cooling system: attached cylinder on casing wall in cooling liquid sprays into, the gasification of liquid absorption casing wall heat, with combustion gas mixing, form high-pressure steam, increase again the air pressure acting to reach when cylinder body is lowered the temperature, reached the raising thermal efficiency, increased the manner of execution of output power purpose.
3. turbine rotor energy-saving engine according to claim 1, is characterized in that: in turn inside and rotating shaft, the startup magneto is housed, has reduced occupation area, during engine operation, can also export electric energy.
CN2013200097309U 2013-01-09 2013-01-09 Turbine rotor energy-saving engine Expired - Lifetime CN203335230U (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN2013200097309U CN203335230U (en) 2013-01-09 2013-01-09 Turbine rotor energy-saving engine
PCT/CN2013/087798 WO2014107996A1 (en) 2013-01-09 2013-11-25 Turbine rotor energy-saving engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013200097309U CN203335230U (en) 2013-01-09 2013-01-09 Turbine rotor energy-saving engine

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Publication Number Publication Date
CN203335230U true CN203335230U (en) 2013-12-11

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WO (1) WO2014107996A1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103075248A (en) * 2013-01-09 2013-05-01 黄荣嵘 Turbine rotor energy-saving engine
CN108661785A (en) * 2018-07-26 2018-10-16 谭建文 Without the rotary Atkinson cycle engine of bent axle
CN111075564A (en) * 2019-12-27 2020-04-28 孙金良 Turbine rotor engine
CN113374571A (en) * 2021-06-15 2021-09-10 刘兴和 External pressure type rotor engine
CN114856724A (en) * 2022-04-29 2022-08-05 重庆江增船舶重工有限公司 Double-valve control system and method applied to supercritical carbon dioxide turbine
CN116677493A (en) * 2023-08-02 2023-09-01 成都工业学院 Circumferential rotor engine

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GR1010404B (en) * 2021-07-15 2023-02-10 Αντωνιος Κωνσταντινου Μαστροκαλος Hydrostatic rotary motor

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Publication number Priority date Publication date Assignee Title
JPS63179133A (en) * 1986-10-29 1988-07-23 Mazda Motor Corp 3-cylinder rotary piston engine with pumping loss reducing device
CN1022772C (en) * 1992-05-16 1993-11-17 丑毅 Combined blade rotary engine
CN1094477A (en) * 1994-03-25 1994-11-02 张真 Curred rotor engine
CN100501140C (en) * 2006-06-09 2009-06-17 王福山 Environment-friendly energy-saving type rotary piston engine
CN103075248B (en) * 2013-01-09 2015-04-08 黄荣嵘 Turbine rotor energy-saving engine

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103075248A (en) * 2013-01-09 2013-05-01 黄荣嵘 Turbine rotor energy-saving engine
CN103075248B (en) * 2013-01-09 2015-04-08 黄荣嵘 Turbine rotor energy-saving engine
CN108661785A (en) * 2018-07-26 2018-10-16 谭建文 Without the rotary Atkinson cycle engine of bent axle
CN108661785B (en) * 2018-07-26 2024-01-23 谭建文 Crankless rotary Atkinson cycle engine
CN111075564A (en) * 2019-12-27 2020-04-28 孙金良 Turbine rotor engine
CN111075564B (en) * 2019-12-27 2022-10-28 孙金良 Turbine rotor engine
CN113374571A (en) * 2021-06-15 2021-09-10 刘兴和 External pressure type rotor engine
WO2022262700A1 (en) * 2021-06-15 2022-12-22 刘兴和 External-pressure-type rotor engine
CN114856724A (en) * 2022-04-29 2022-08-05 重庆江增船舶重工有限公司 Double-valve control system and method applied to supercritical carbon dioxide turbine
CN114856724B (en) * 2022-04-29 2023-10-24 重庆江增船舶重工有限公司 Double-valve control system and method applied to supercritical carbon dioxide turbine
CN116677493A (en) * 2023-08-02 2023-09-01 成都工业学院 Circumferential rotor engine
CN116677493B (en) * 2023-08-02 2023-09-26 成都工业学院 Circumferential rotor engine

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