CN103075248A

CN103075248A - Turbine rotor energy-saving engine

Info

Publication number: CN103075248A
Application number: CN201310007096XA
Authority: CN
Inventors: 黄荣嵘
Original assignee: Individual
Current assignee: Individual
Priority date: 2013-01-09
Filing date: 2013-01-09
Publication date: 2013-05-01
Anticipated expiration: 2033-01-09
Also published as: CN103075248B

Abstract

The invention discloses a turbine rotor energy-saving engine which comprises a cylindrical engine body, wherein a rotating shaft is arranged on the center of the cylindrical engine body, a rotor is arranged on the rotating shaft, a cylinder housing is sleeved on an outer ring of the rotating shaft, a compression fan is arranged on one end of the rotating shaft, the rotor and an engine body housing corresponding to the rotor are divided into an upper cylinder, a middle cylinder and a lower cylinder, the rotor of the upper cylinder is a three-legged cam, three groups of piston cylinders with longitudinal equal intervals and high-pressure oil pumps of the upper cylinder housing are compressed to reciprocate, three protruding pistons which have the same shaft direction and equal arcs are arranged in the middle section of the rotor and matched with the inner wall of the cylindrical middle cylinder to rotate in a sealing manner, radial sealing grooves are arranged in the inner wall of the middle cylinder at equal arcs, the middle cylinder body is divided into three groups of independent cylinder bodies by sealing members in the radial sealing grooves, each group of cylinder body is provided with an ignition chamber communicated with the middle cylinder, a spark plug and a nozzle are matched with each ignition chamber, two auxiliary cylinders are arranged on the inner layer of the middle cylinder wall to be communicated with the middle cylinder, new energy fuel is combusted in one auxiliary cylinder, cooling water absorbs heat in the other auxiliary cylinder to be vaporized to return the middle cylinder, and discharged waste gas residual pressure is recycled for circulated working by the rotor of the lower cylinder so that the heat efficiency is increased. The turbine rotor energy-saving engine has the advantages of simple structure, small weight and size, energy saving and environment friendliness.

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, human growing to various motor vehicle and various motivation power tool demand thereof, and the different exhaustion of main energy sources day, people have higher requirement to engine performance.Export source engine as machine powers such as vehicle and steamers, that uses at present mainly contains petrol engine, diesel engine, rotary engine and aviation Spray gas motor etc.Petrol engine and diesel engine all are to adopt the cylindrical piston straight reciprocating motion to finish to suck air-fuel mixture gas or pure air, compress again, igniting or spray into the diesel oil compression ignite, work done, exhaust is by the connecting bar and crankshaft outputting power, rotary engine then adopts triangular rotor, gear by rotor center cooperates with the uranium gear, along the casing wall eccentric rotary, finishes air-breathing, compression, the working procedures such as igniting work done, exhaust are come outputting power in the ellipse cylinder body.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 owing to defective on the gas-tight design, so the thermal efficiency is then lower, aeroengine also is very high oil consumption and cost, environmental consciousness is strengthened day by day in the world, and petroleum resources are today of exhaustion day by day, and human have more serious hope to motor raising performance.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 has not satisfied the requirement that society advances.

The content of invention

The object of the invention is to make motor to improve power, reduce oil consumption, toxic emission etc. and significantly reduce, 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 satisfy the social development requirement.

The explanation of turbine rotor energy-saving engine Figure of description

Accompanying drawing 1 is: the overall structure floor map is looked squarely in turbine rotor energy-saving engine front.

Accompanying drawing 2A-A is: turbine rotor energy-saving engine upper cylinder half section's cam rotor and casing wall piston-cylinder, the overall structure generalized sections such as high-pressure service pump.

Accompanying drawing 3B-B is: cylinder section rotary piston and middle cylinder cylinder in the turbine rotor energy-saving engine, the attached cylinder on the casing wall, spark plug, oil nozzle, cooling system, the overall structure generalized sections such as port.

Accompanying drawing 4C-C is: EGR groove work done system of cylinder section under the turbine rotor energy-saving engine, starting electrical machinery system, the overall structure generalized sections such as casing wall exhaust port.

Accompanying drawing 5 is turbine rotor energy-saving engine working stroke figure, Fig. 5-the 1st: upper cylinder half section piston-cylinder suction stroke.Fig. 5-the 2nd: the piston-cylinder pressurized gas enters middle cylinder part guide hole igniting chamber process.Fig. 5-the 3rd: guide hole igniting chamber igniting combustion gas enters the work done cylinder and begins work done.

Accompanying drawing 6 is turbine rotor energy-saving engine expansion space stroke and exhaust process figure, Fig. 6-the 1st: the work done cylinder combustion gas drive rotor piston rotation work done of middle cylinder section, the work done cylinder process is returned in the attached cylinder 1 fuel heat absorption of middle casing wall burning.Fig. 6-the 2nd: the work done cylinder process is returned in 2 li cooling water heat absorptions of the attached cylinder of middle casing wall cooling system vaporization.Fig. 6-the 3rd, middle cylinder section work done cylinder mixed gas turns to lower cylinder section by guide hole.Fig. 6-the 4th, the combination gas that is forwarded to lower cylinder section by middle cylinder section guide hole discharges outside the cylinder 1 through lower rotor part EGR groove by exhaust port, turn uranium 2, centrifugal fan 3, cam rotor section 4, cylinder section 5 in the rotor, cylinder section 6 under the rotor, upper cylinder half 7, middle cylinder 8, lower cylinder 9, compression cylinder 10 compression pistons 11 guide hole igniting chambers 12, work done cylinder 13, air-stopping valve 14, choke valve 15, salient angle piston 16,

Sealing

17a, 17b, 17c, oil nozzle 18, high pressure oil pump 19,

workpiece

20a, 20b, 20c, piston ring 21a, 21b, attached cylinder 22, gas emission conversion mouth 23, spark plug 24, dentation groove 25, guide hole 26, starting electrical machinery rotor 27, relief opening 28, intakeport 29, spring 30, puff prot

The mode of implementing

The present invention adopts novel concentric cam wheel piston compression air; (15) cooperate three groups of cylinder bodies among rotor lobes piston such as Fig. 3; form many group cylinder circulation works done; be equivalent to improve the quantity of cylinder; (21a) penetrated by wooden carbon molecule by Spray mouth (17b) Spray and becomes water gas again to burn with the fuel that water mixes according to C+H2O+ high temperature=CO+H2 principle endothermic decomposition among attached cylinder such as Fig. 3; the cooling of charge mode in the cylinder is sprayed back in the inner water spray heat absorption of attached cylinder (21b) vaporization again; the excellent sealing design; improve compression ratio; the EGR work done; the turbofan supercharging technology; heat energy is reduced the loss; improved the thermal efficiency; greatly reduce the discharging 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; more balance and stability is reliable so that move; the structural design of new reasonable simplification and material application; removed many useless parts such as flywheel and bent axle, so that production technology and workflow require significantly to reduce, be more convenient for popularizing and produce; the part life cycle but improves 2～3 times greatly, has reduced maintenance and cost of production.

Overall structure

The present invention is based on the turn motor of basic innovation of work of rotary engine, but fully different from rotary engine, overall structure arranges as shown in fig. 1 cylinder type loom, be respectively and turn uranium (1), the centrifugal fan of calming the anger (2), cam rotor section (3), cylinder section (4) in the rotor, cylinder section (5) under the rotor, the cylinder shell is divided into upper cylinder half (6), middle cylinder (7), the compositions such as lower cylinder (8), as shown in Fig. 2 A-A, the upper cylinder half rotor is a starlike arc cam that waits, and upper casing wall is the star-shaped three groups of piston-cylinders (9) that arranging of outside equal portions along the axle center, three high pressure oil pumps (18a). (18b). (18c), piston (10) is furnished with workpiece (19) and is located by connecting with wrist pin, and workpiece (19) one ends act on oil pump, makes cam (3) simultaneously compression piston and oil pump synchronous working.Cylinder (9) is provided with intakeport (28), and is provided with spring (29) compression workpiece (19) between the oil pump (18) and drives piston and be the unlatching suction condition.Cylinder section (4) in the rotor) be the concentric right cylindrical, rotor is provided with two ring circumference piston grooves, in piston ring (20a) is arranged (20b), as shown in Fig. 3 B-B, have between the piston ring three with axle in the same way with piston ring (20a) (20b) 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 (20a) and (20b) between fit in an independent annular seal zones work done cylinder (12) with middle cylinder (7) inwall.Compression cylinder (9) has guide hole igniting chamber (11) to connect with middle cylinder work done cylinder (12) at middle casing wall, an one-way movable air-stopping valve (13) is arranged in the hole, the choke valve (14) that compression is carried, igniting chamber between two air valves, oil nozzle (17a) 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), show that along the circumference symmetry radial groove is arranged among middle cylinder such as Fig. 3 B-B, Sealing (16) is arranged in the groove, Sealing and place groove have pressing device to make Sealing and rotor keep cooperating to be closed state makes middle cylinder be divided into three groups of cylinder block that work alone, be disposed with attached cylinder (21a) nozzle (17b) combination between the Sealing on the casing wall, (21b) nozzle (17c) 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.Shown in Fig. 4 C-C, there are several ring reverse dentation grooves of girth (24) in cylinder section (4) under the rotor, piston ring (20c) packing is arranged between groove and the groove, and with guide hole (25) UNICOM, starting electrical machinery stator and rotor (26) are arranged in the rotor, and winding most casing wall has exhaust port (27) under the groove correspondence, with to outlet pipe exhaust such as Fig. 1.

The engine operation operation

Breathing process---drive unlatching cylinder (9) such as Fig. 5-1 piston through spring (29) compression workpiece (19), air enters cylinder through suction port (28).---compression process---starting electrical machinery (26) is such 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 workpiece (19), by workpiece to oil pump (18a) synchronous compression, when piston moves to the cylinder summit, compression work is finished, gas compression is inner at guide hole (11), rotor lobes piston (15) just in time moved puff prot (30) simultaneously, oil nozzle (17a). the same time point fire-fighting of spark plug (23) oil firing, high combustion gas body is with upwards compressing sealing of air-stopping valve (13), choke valve (14) is pressed down unlatching downwards, combustion gas is gone out puff prot and is entered working cylinder (12) promotion salient angle piston (15) motion acting, such as Fig. 5-3.---work done process---as Fig. 6-1 blast combustion gas forward pushing piston (15) cross the aperture that attached cylinder (21a) is communicated with air chamber, attached cylinder (21a) back warp cam pressure oil pump (18b) is mixed to water carbon fuel combination and high-temperature fuel gas that nozzle (17b) sprays, the heat that water carbon fuel has absorbed combustion gas heats up, principle according to C+H2O+ high temperature=CO+H2 generates water gas formation secondary combustion, moved aperture such as Fig. 6-2 of attached cylinder (21b) when piston, the high-temperature gas of twice combustion passes to the attached cylinder (21b) and the water absorption of being sprayed through nozzle (17c) by cam pressure oil pump (18c) of ring cylinder through casing wall, water has absorbed heat and has changed into steam state and regurgitate the return-air chamber again and act on piston, and having reduced temperature namely for cylinder body and rotor has increased again air pressure.---exhaust process---piston (15) had moved Sealing (16) such as Fig. 6-3, Sealing is finished closure at once, piston continues operation and enters next periodic duty, gas by gas emission conversion lead mouthful (22) flow to and the reverse dentation groove of pressure-acting (24) such as the Fig. 1 of Fig. 6-4., flow to guide hole (25) along groove and enter next ring guide groove, the gas energy is fully absorbed, by relief opening (27) exhaust, finish workmanship's stroke at last.

The cooling work principle:

By in the same way cam work done, pressure oil pump is pressed into liquid water and enters the attached cylinder of casing wall (21b), the heat of vaporization gasification that water is drawn casing wall and combustion gas forms steam state, when the pressure of water vapour is higher than cylinder pressure, then air return cylinder (12) swelled mixture cooperation merit is drawn the double action that heat energy transfers mechanical energy increase power to thereby reached middle cylinder body cooling.

1, rotating shaft 2, centrifugal fan 3, cam rotor section 4, cylinder section 5 in the rotor, cylinder section 6 under the rotor, upper cylinder half 7, middle cylinder 8, lower cylinder 9, compression cylinder 10 compression pistons 11 guide hole igniting chambers 12, work done cylinder 13, air-stopping valve 14, choke valve 15, salient angle piston 16,

Sealing

17a, 17b, 17c, oil nozzle 18, high pressure oil pump 19,

workpiece

20a, 20b, 20c, piston ring 21a, 21b, attached cylinder 22, gas emission conversion mouth 23, spark plug 24, dentation groove 25, guide hole 26, starting electrical machinery rotor 27, exhaust 28, air-breathing 29, spring 30, puff prot.

Claims

A kind of turbine rotor energy-saving engine belongs to rotation class power output engine, its feature and claimed scope:

1. rotor cylinder with positive circular inner wall, one is installed in 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, on the cylinder body correspondence also has, in, lower cylinder body, upper rotor part section cooperates with upper cylinder half, upper rotor part is the star-shaped arc cam that waits, outside star-shaped equal portions arrange many group piston-cylinders to upper casing wall along the axle center, three groups of high pressure oil pumps, piston is furnished with workpiece, connects with wrist pin, workpiece one end acts on oil pump, cam can be synchronoused working with oil pump by the while compression piston, and cylinder is provided with suction port, and has spring-compressed workpiece drive piston to be the unlatching suction condition between the oil pump.Piston-cylinder has the guide hole igniting chamber to connect with middle cylinder work done cylinder at middle casing wall, there are breather cheek valve and barrier gas to enter the choke valve of work done cylinder in the hole, cylinder section is the concentric right cylindrical in the rotor, by the circumference equal portions many salient angle pistons that radially rotate with the inside wall of cylinder in high the cooperation with middle cylinder concentric are set, the corresponding side face of piston ring of rotor place has the ring circumferential seal groove, seal ring is installed in the groove, seal ring cooperate up and down cylinder cap with the footpath with the rotor lobes side face of piston ring with the inner region transverse sealing, middle cylinder body and side face of piston ring line are slightly high, the inwall radius of a circle is slightly larger than the rotor lobes piston radius, the middle inside wall of cylinder is equipped with radial seal groove by the circumference equal portions, compression is installed in the groove carries Sealing to fit in many group active chambers 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 nozzle and cooperate 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, the high pressure mixing waste gas of being discharged by middle cylinder is outside dentation EGR guide groove is discharged cylinder, sawtooth in gas and groove concave surfaces such as (or) ladders is the reaction force principle mutually, the driving rotation of turning reaches the manner of execution of EGR work done purpose.
2. cooling system: spray into attached cylinder on the middle casing wall by cooling liquid, the gasification of liquid absorption casing wall heat is with combustion gas mixing, form high-pressure steam, increase again the air pressure work done to reach when cylinder body is lowered the temperature, reached the raising thermal efficiency, increased the manner of execution of output power purpose.
3. in turning inside and turn the startup magneto is housed on the uranium, reduced occupation area.Can also export electric energy during engine operation.