CN102155285A - Novel four-stroke four-cylinder layered dual-vortex combustion energy-saving internal combustion engine with new gas distribution mechanism - Google Patents
Novel four-stroke four-cylinder layered dual-vortex combustion energy-saving internal combustion engine with new gas distribution mechanism Download PDFInfo
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- 230000007246 mechanism Effects 0.000 title abstract description 6
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- 238000010304 firing Methods 0.000 claims description 11
- 230000008859 change Effects 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 10
- 230000000712 assembly Effects 0.000 claims description 8
- 238000000429 assembly Methods 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 8
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- 238000007906 compression Methods 0.000 claims description 7
- 238000005516 engineering process Methods 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 5
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 230000009977 dual effect Effects 0.000 claims description 4
- 239000000945 filler Substances 0.000 claims description 3
- 210000000707 wrist Anatomy 0.000 claims description 3
- 230000007123 defense Effects 0.000 claims description 2
- 230000000977 initiatory effect Effects 0.000 claims description 2
- 238000005461 lubrication Methods 0.000 claims description 2
- 230000008901 benefit Effects 0.000 abstract description 4
- 239000011229 interlayer Substances 0.000 abstract description 4
- 230000001050 lubricating effect Effects 0.000 abstract description 4
- 239000003921 oil Substances 0.000 description 41
- 239000007789 gas Substances 0.000 description 15
- 239000000295 fuel oil Substances 0.000 description 10
- 239000002912 waste gas Substances 0.000 description 6
- 210000001260 vocal cord Anatomy 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000005273 aeration Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000010926 purge Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 235000001674 Agaricus brunnescens Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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Abstract
The invention provides a novel four-stroke four-cylinder layered dual-vortex combustion energy-saving internal combustion engine with a new gas distribution mechanism, which is particularly suitable for various internal combustion engines of sea, land and air. In the internal combustion engine, four cylinder nozzle gaskets (14) and four small cylinder heads (13) with the new gas distribution mechanisms are arranged on four cylinders (28) of the conventional four-stroke vertical four-cylinder double overhead camshaft gasoline engine, and four small cylinders (37) are arranged inversely; two ports (35) are arranged in the front of the wall of each small cylinder (37); gas enters and is exhausted by up and down sliding of a small piston (39); and when big and small pistons (32), (45), (48), (52) and (39) apply work simultaneously, gas exhaust is to push intake and exhaust turbines (66), (69), (73) and (77) to apply secondary work. The internal combustion engine has the advantages of simple structure, good lubricating condition, long service life, stable work, high rotating speed and soundlessness, realizes that fuel vortex performs layered dual-vortex combustion in hot air interlayer, and realizes one combustion four power applications, thereby having larger high-power output, sving fuel by about 50 percent, and reducing emission by 85 percent.
Description
Affiliated technical field
Patent of the present invention relates to the upright four-cylinder gasoline machine of a kind of four-stroke, the two whirlpool combustion energy saving internal-combustion engines that change of the new distribution device four cylinder layerings of especially a kind of novel four-stroke.
Background technique
The structure of present known four-stroke four-cylinder gasoline machine is by compositions such as, bent axle, crankcase, gearbox, gear, four chain bar assemblies, four piston assemblies, four cylinders, four cylinder heads, distribution devices.The distribution device of at present domestic four-stroke four-cylinder internal combustion engine all adopts compositions such as camshaft, rocking arm, pitman arm shaft, intake valve, exhaust valve, air valve seat ring, valve spring.These parts are the indispensable moving parts of present four stroke engine, it is again the distribution device of four stroke engine maturation, over more than 100 year, the size internal-combustion engine is all using, but its deficiency, and this distribution device still has its shortcoming, during as engine operation, the inlet and outlet door is subjected to the trouble that the dry vocal cords of high temperature vibration deformation come, and to the oil consumption aspect, it is not enough to save fuel oil.Domestic in addition internal-combustion engine, fuel oil " filler opening " and " jet " traditional set-up mode have two kinds, and a kind of is at the motor rear mixed gas inlet to be set, and when air inlet, fuel oil and air are mixed together to be opened by " intake valve " and enter combusted cylinder.Another kind is diesel engine and a kind of two-stroke gasoline engine, and " top of combustion chamber is provided with oil sprayer ", oil spout and air mixing are burnt together in cylinder.Pressurized machine on the domestic in addition motor car engine mainly is divided into two classes according to the difference of structure---engine driven supercharging and turbosupercharging.Early stage pressurized machine all belongs to engine driven supercharging, is known as " super pressurized machine " Supercharger when just coming out, and just prolongs afterwards and has used this title.Just be called as Turbocharger after the turbosupercharger invention.It is a kind of that the bent axle of four cylinder engine is provided with employing substantially at present, a kind of is to have arranged four pairs of cranks and four crank pins on the bent axle, one, four pairs of cranks and two crank pins, two crank pins are arranged on 360 ° of top dead centers synchronously, in addition two, Third Mate's crank and two crank pins, two crank pins are arranged on 360 ° of lower dead center synchronously.When engine operation, require circulation behind 180 ° of the piston intakes one time of every cylinder, one to three cylinder, four to two cylinders, 720 ° of four air inlets, motor is finished a work cycle.
Summary of the invention
In order to overcome the parts of domestic existing four-stroke four-cylinder internal combustion engine distribution device, in the next trouble of the dry vocal cords of high temperature vibration deformation, to saving the technical problem of Low oil Fuel, patent of the present invention provides the new distribution device four cylinder layerings of a kind of novel four-stroke two whirlpool combustion energy saving internal-combustion engines that change, the two whirlpool combustion energy saving internal-combustion engines that change of the new distribution device four cylinder layerings of this a kind of novel four-stroke, not only every little cylinder wall the place ahead of new distribution device is provided with two mouths, two mouths have slided up and down air inlet by small piston, exhaust, and the residual gas of each firing chamber can purge out outside the machine, very unimpeded at intake duct and air outlet flue, can reduce the loss of suction of big small piston, and push away the resistance of waste gas, the wind that supercharging comes can cool off into row's turbine, and the hot air that two mouths enter is to rotate to enter cylinder, fuel oil enters in the cylinder being to rotate to enter through the platform jet, and the supercharged engine fuel oil changes the whirlpool two commentaries on classics of layering whirlpool burning in the middle of hot air changes the whirlpool interlayer, burning promotes the acting of big small piston simultaneously and advances to arrange turbine and do the secondary merit, stroke four actings of primary combustion.This machine is simple in structure, lubricating condition is good, the life-span is long, engine mildness, rotating speed height, not only safe but also noiseless, hot air change the whirlpool, and to change whirlpool heat atomizing with fuel oil more abundant, further improve the thermal efficiency, improve aeration quantity again, make motor have bigger high power and the output of high moment of torsion, fuel consume is minimum, the advantage of exhaust emission minimum.
Patent of the present invention solves the technological scheme that its technical problem adopts: the structure of the upright four cylinder Dual Over Head Camshaft petrol engine of existing four-stroke is by compositions such as, bent axle, crankcase, gearbox, gear, four chain bar assemblies, four piston assemblies, four cylinders, four cylinder heads, distribution devices.It is characterized in that: on the crankcase of the upright four cylinder Dual Over Head Camshaft petrol engine of existing four-stroke, load onto that newly-designed four cylinder jet pads, four little cylinder heads, four little cylinder heads are established new distribution device, four little cylinders adopt to stand upside down and are provided with.1, four little cylinder heads are established the structure of new distribution device; 2, the working procedure of patent of the present invention and energy-saving effect.
1, the structure that four little cylinder heads are established new distribution device is by, small crankshaft case, small crankshaft, the small crankshaft flywheel, four little cylinders, four chainlet bar assemblies, four small piston assemblies, one one. two advance to arrange the turbine urceolus, one three. four advance to arrange the turbine urceolus, two turbine left and right side caps, one one. two advance to arrange turbine, one three. four advance to arrange turbine, seat about two turbines, seat in two turbines, two turbine head flaps, eight little oil rings of turbine shaft, two turbine timing minor sprockets, two turbine timing gimmals, two turbines connect tooth sprocket, two turbine driven gears, compositions such as four little cylinder-head covers.Four little cylinders, small crankshaft case, two advance to arrange the turbine urceolus, are the whole structures of stopping.Four little cylinders, every little cylinder wall the place ahead is provided with two mouths, is synchronous air inlets during two mouth air inlets, is synchronous exhaust during exhaust.A firing chamber is respectively established at each four big or small cylinder top, respectively establish a rear combustion chamber and establish the platform jet, above the platform jet is located at behind the plane, four firing chambers, the one side of platform jet is respectively established at four cylinder rears, it is exactly four integral platform jets that eight plane jets lump together, an oil sprayer is respectively established in each platform jet back upper place, and four oil sprayer sides are respectively established a spark plug.Two are advanced to arrange the turbine urceolus, respectively establish two air inlets on two urceolus faces, and two relief openings are respectively established in two urceolus the place aheads, and four air inlets, four relief openings, two advance to arrange the turbine urceolus, are overall structures.One one. two advance to arrange two turbines of turbine, and axis hole is established at the center of two turbines, axis hole with one one. it is drive fit that two two shaft heads that advance to arrange turbine are connected.One three. four advance to arrange three turbines of turbine, and axis hole is established at three turbine centers, axis hole with one three. it is drive fit that four three shaft heads that advance to arrange turbine are connected.Four are entered to arrange every axle center of turbine and are provided with oilhole, establish four little oil rings of turbine on every axle.Two are advanced to arrange to establish in the turbine urceolus four and advance to arrange seat, two turbine head flaps, two turbine timing minor sprockets, two turbine timing gimmals, two turbine left and right side caps about seat in turbine, two turbines, two turbines.Each nozzle limit, a urceolus left and right sides respectively is provided with bolt connecting hole.Four advance to arrange in the turbine about, establish a round block plate Yi Bian whenever have only, another side is established half of circle block plate, also has one side of something to establish the whirlpool blade, a round block plate and half of round block plate, it is hollow that there is one side of something the centre, is intake duct.In addition one side of something is established the whirlpool blade, and the intermediate space of whirlpool blade is an air outlet flue, has a slice tip to establish two little votex sheets of branch in the blade of whirlpool, is the timing dotted line of into arranging turbine, and being the wind that comes of supercharging can purge waste gas in the big or small cylinder through two little votex sheets.Round block plate, an one side of something are justified block plate, half of whirlpool blade, are overall structures.Steel ball and oilhole are established in each axle afterbody center.Seat in two turbines, second air outlet flue is established in every below, is after waste gas promotes whirlpool blade acting, and waste gas enters second air outlet flue outlet through the intermediate space of whirlpool blade and does the secondary merit promoting the whirlpool blade.Four small pistons, every is same with the existing piston structure, only respectively sets up one one word oil ring about piston the place ahead, is provided with six oil gas rings in every small piston, is respectively: two compression rings, an oil gas ring, two word oil rings, an oil ring.Have two compression rings to be located at the small piston top, an oil gas ring is established in two compression ring belows, respectively establishes one one word oil ring about an oil gas ring, respectively establish one one word oil ring below and establish an oil ring, several oil gas ring designs are chomas, are to aim at two mouth sides, mainly play the sealing oil effect during work.The structure of an oil gas ring is, aiming at two mouths is compression rings, and other partly is an oil ring, and oil ring and compression ring are overall structures.15 millimeters stroke is arranged at two mouth tops of every little cylinder, is the stroke of small piston top and piston ring, and 15 millimeters strokes are that engine rotation has that air inlet is closed, compressed, burning, EXO are used.Four are advanced to arrange turbine and small crankshaft is a synchronous speed, and large crankshaft changes two circles, and small crankshaft turns around, and acting once.Each turbine left and right side cap, the adjustment bolt is established at every lid center, and bolt head is established steel ball, is to adjust four to advance to arrange the use of turbine shaft running clearance, these four cylinders and crankcase are overall structures, set up an electronic wind eddies fan in the air-strainer in the wings in addition.The structure of small crankshaft, the structure of small crankshaft are same with available engine bent axle and crank, and only the structure of small crankshaft is more a little bit smaller than this machine large crankshaft, and the axle center of small crankshaft is provided with oilhole.
2, the working procedure and the energy-saving effect of patent of the present invention are: when engine operation, timing minor sprocket on the bent axle, drive timing hinge wheel on the small crankshaft and four with the big chain of timing and advance to arrange the turbine rotation, after a piston and small piston waste discharge gas promote into row's turbine, close air outlet flue, " three pistons are in compressive state simultaneously ", advance to arrange turbine and forward intake duct to, two mouths of one little cylinder are being opened already, at this moment a piston enters air and moves to lower dead center from top dead center, a small piston moves to two mouths of top dead center in lower dead center simultaneously, when a piston enters air to the lower dead center timing, the motion of one small piston will have been closed two mouths, when a piston in lower dead center when top dead center motion will arrive closed line, small piston just begins to have closed two mouths, at this moment rotate to cylinder platform jet ejection rich mixture by oil sprayer and enter the middle layering rotation of hot air interlayer compression, in the movement process of this piston and a little piston, one piston and small piston while are to the air and the fuel oil of firing chamber distilled edition cylinder, until a piston and small piston are will be near top dead center the time, plug ignition, one piston and a small piston absorb firing pressure simultaneously, expansion stroke begins, " three pistons are in exhaust condition " simultaneously, in the time will beginning waste discharge gas after a piston and the small piston acting, open two mouths by a small piston, at this moment waste gas one bravely goes out to advance moving row's turbine to do the secondary merit.In this motion, two are advanced to arrange turbine, and two small pistons are that one, three piston goes to air inlet work cycle next time.Institute is above-mentioned to be two and to advance to arrange turbine, two small pistons and. three pistons and work method.Also have two to advance to arrange turbine, two small pistons and four, two piston work methods are same with the work method of one, three pistons.
According to above-mentioned newly-designed internal-combustion engine as can be known, its structure of this motor is above four-stroke four little cylinders are upside down in, be four cylinders of four-stroke below, every in four little cylinder walls of top four-stroke the place ahead is provided with two mouths, two mouths have air inlet, exhaust, when four small pistons slide up and down, can open or close its door, this machine provides pure air by the wind eddies fan, advancing air and be heat along every heat that advances to arrange turbine inlet and every big or small cylinder wall rotates and enters, the supply rich mixture is provided by every oil sprayer, " internal combustion ", mixed gas enters the air blanketing centre to rotate through excessive cylinder platform jet during oil spout, when the compressed in layers stroke, above two mouths of every small piston sealing, make every big small piston absorb firing pressure simultaneously, every of the promotion of exhaust is simultaneously advanced to arrange turbine and is done the secondary merit, thereby bigger high power and high moment of torsion have been increased, clearly, the benefit of this new technology maximum of this machine is to have given up existing traditional mushroom valve, thereby saved the trouble that valve mechanism comes at the dry vocal cords of high temperature vibration deformation, and the waste gas in the big or small cylinder is purged thoroughly, obviously improved the combustion thermal efficiency height, power is big.Four are advanced to arrange turbine inlet and two mouths, and air intake-exhaust is very unimpeded, and resistance is little, supercharging charging efficiency height, mixed gas heat atomizing quality better helps smooth combustion, the pressure hot air that the wind eddies fan provides to big or small cylinder play pressurization, can further improve aeration quantity, mixed gas platform jet is arranged on each only big cylinder top plan rear, near spark plug, denseer mixed gas is arranged, other is rare mixed gas from spark plug place far away, and some places are air.This machine is simple in structure, lubricating condition good, the life-span is long, engine mildness, rotating speed height, not only safe but also noiseless, realized that the supercharged engine fuel oil changes the whirlpool and enters in the middle of the hot air interlayer that layering is two changes the whirlpools burning, stroke four actings of every big cylinder primary combustion, it is the new work engine that the internal-combustion engine process is pursued, it has brought new development prospect with four stroke engine, save fuel oil about 50%, reduce to discharge 85%.
The beneficial effect of patent of the present invention is, the new technology of patent of the present invention is compared with the technology of available engine, the energy-conservation advantage and the effect that are had, it is directly brought by technical characteristics, and it is to have changed the trouble that existing valve mechanism comes at the dry vocal cords of high temperature vibration deformation, and the lubricating condition of this machine is good, powerful, the life-span of new distribution device is the twice of available engine, and it can also save fuel oil over half.
Description of drawings
Below in conjunction with drawings and Examples patent of the present invention is further specified.
1, the Front Frame figure of patent of the present invention.
2, a structural drawing of four cylinder platform jets.
3, four little cylinder head bottom surface platform jet plan structure figure.
4, four little cylinder head plane structure charts.
5, motor right side reef knot composition.
6, motor rear mechanism structure figure.
7, the new air distribution structure figure in motor left side side.
In Fig. 1,1. four cylinder-head covers, 2. small crankshaft, 3. five small crankshaft under tiles cover, 4. four chainlet bar bottoms, 5. turbine driven gears, 6. timing hinge wheel seat, 7. timing hinge wheel, 8. nut 9. oil sealings, 10 small crankshaft flywheels, 11. the flywheel lid, the big chain of 12.. timing, 13. 4 little cylinder heads, 14. four cylinder jet pads, 15. the motor left cap, 16. 4 cylinders and crankcase, 17. motors, 18. bent axle timing minor sprocket, 19. large crankshaft, 20. big chain bar under tile seats, 21. oil pump, 22. water outlet, 23. bent axle under tile lid, 24. bent axle left and right sides oil sealings, 25. electronic induction heads, 26. crankshaft-flywheel, 27. the bent axle afterbody connects gearbox, 28. starter motors, 29. 4 cylinders, 30. big chain bar, 31. wrist pin, 32. 4 pistons, 33. 1 pairs of piston rings, 34 4 firing chambers, 35. two mouths of four little cylinders, 36. 4 relief openings, 37. 4 little cylinders, 38. four pairs of small piston rings, 39. four small pistons, each four one word oil ring about 40. 4 small pistons, 41 4 small piston pins, 42. four chainlet bars, 43. distributors.
In Fig. 2,44. 1 cylinders, 46 1 pairs of piston rings of 45 1 pistons, 47. two cylinders, 48. 2 pistons, 49. 1 pairs of piston rings, 50. oilhole, 51. 3 cylinders, 52. 3 pistons, 53 1 pairs of piston rings, 54. cylinder screw rods, the one side of 55. Siping City's platform jets, 56. the one side of three platform jets, 57. oilholes, the one side of 58. 2 platform jets, 59. the water hole, the one side of 60. 1 platform jets, 61. bolt connecting holes.
In Fig. 3,62. turbine right cap, 63. 1 three. four advance to arrange the turbine urceolus, 64. oil outlet, 65, the right seat of turbine, 66. four advance to arrange turbine, seat in 67. turbines, 68. 4 little oil rings of turbine shaft, 69. three advance to arrange turbine, 70. turbine head flaps, 71. oilholes, 72. turbine head flap, 73. two enter to arrange turbine, 74. 1, two advance to arrange the turbine urceolus, 75. 4 little oil rings of turbine shaft, 76. seat in the turbine, 77. one advances to arrange turbine, 78. turbines left side seat, 79. oil outlets, 80. turbine left cap, 81. turbine timing minor sprocket, 82. turbine timing gimmals, 83. 1 platform jets, 84. oil sprayer, 85. spark plug, 86. 1 firing chambers, two mouths of 87. 1 little cylinders, 88. two platform jets, 89. oil sprayer, 90. spark plugs, 91. 2 firing chambers, 92. two mouths of two little cylinders, 93. oilhole, 94. 3 platform jets, 95. oil sprayers, 96. spark plug, 97. three firing chambers, two mouths of 98. 3 little cylinders, 99. Siping City's platform jets, 100. oil sprayer, 101. spark plug, 102. turbine timing gimmals, 103. turbine timing minor sprockets.
In Fig. 4,104. an air inlet seat, 105. two air inlet seats, 106. three air inlet seats, 107. four air inlet seats, 108. five small crankshaft seats, 109. three little cylinders, 110. four little cylinder head gaskets, 111. oilhole, 112. two little cylinders, 113. one little cylinder 114. chain catheter blocks, 115. chain conduits.
In Fig. 5,116. five small crankshaft lids, 117. turbine driven gears, 118. turbine connects tooth sprocket, 119. tooth sprocket pins, 120. four unification air bend pipes, 121. small screw, 122. the tooth sprocket port lid, 123. three. four advance to arrange turbine timing dotted line 124. water channels, 125 gearbox bolt connecting holes, 126. electronic wind eddies fan, 127. air-strainer, 128. two jump rings, 129. air throttle valves.
In Fig. 6,130. tooth sprocket port lids, 131. water intakes, 132. turbine timing minor sprockets.
In Fig. 7,133 timing hinge wheel timing dotted lines, 134. chain regulators, 135 generators, 136. generator driving belt, 137. the generator main Moving plate, 138. crankshaft nuts, 139. one, two advance to arrange turbine timing dotted line, .140. turbine connects tooth sprocket, 141. the tooth sprocket pin, 142. tooth sprocket port lids, 143. small crankshaft casees.
Specific embodiments
The facility scheme of patent of the present invention is in Fig. 3: take earlier eight little oil rings of turbine shaft (68) (75) to distribute to be contained on four axle collar positions of advancing to arrange turbine (66) (69) (73) (77), on axle collar position, load onto seat (67) (76) in each turbine, load onto seat about each turbine again, load onto each turbine timing minor sprocket (81) (103) again and fix, load onto each turbine timing gimmal (82) (102) again with nut.The opposing party respectively loads onto two at two two shaft heads that advance to arrange turbine and advances to arrange turbine (66) (69) and be tightly fixed, advancing to arrange each one of turbine (66) (69) (73) (77) distribution threading to four again subsequently advances to arrange in the turbine urceolus (63) (74), after load onto each turbine head flap (72) (70) at every shaft head again and respectively have screw rod to fix, load onto each turbine left and right side cap (62) (80) and each is fixed with screw rod at each left and right sides nozzle that only advances to arrange turbine urceolus (63) (74) again, each is with (78) (65) about seat (76) (67) and turbine in the screw rod fixed turbine on each urceolus face.
The facility scheme of patent of the present invention is loaded onto each turbine driven gear (5) (117) at the shaft head and the axle afterbody of small crankshaft (2) earlier, and is respectively fixed with nut in Fig. 4, and it is fixing to load onto timing hinge wheel seat (6) at small crankshaft (2) head again.The opposing party take four pairs of small piston rings (38) and small piston (39) about four one word oil rings (40) respectively, distribution is contained in drips several drop lubrications in the ring position of four small pistons (39), again four small pistons (39) are distributed and be contained in the wrist pin place of four chainlet bars (42), and each penetrates with chainlet bar (42) with a small piston pin (40) and to be connected, and each fixes each small piston pin (40) with two round jump rings, take the axial region distribution of four chainlet bars (42) to be connected subsequently again with four crank pins of small crankshaft (2), and cover each chainlet bar under tile lid (3), and each is fixed with two screw rods.After again four small pistons (39) on the small crankshaft (2) distribute are put in the four little cylinders (37), and on the axle of small crankshaft (2), respectively cover a small crankshaft lid (116), and each is fixed with two cylinder screw rods.
The facility scheme of patent of the present invention is in Fig. 5, take one four unification air bend pipe (120) and four four air inlet seats (104) that advance to arrange on the turbine urceolus (74) (63), (105), (106), (107) connect, and at each air inlet seat (104), (105), (106), (107) fix four unification air bend pipes (120) with two screw rods, four unification air bend pipe (120) the other ends are connected with an end of an air throttle valve (129), air throttle valve (129) the other end is connected with air-strainer (127), and each is fixed with a round jump ring.
The facility scheme of patent of the present invention is in Fig. 6, at four cylinders (29) rear, locate to load onto each oil sprayer (84), (89), (95), (100) in every cylinder (44) (47) (51) (29) platform jet (83), (88), (94), (99), it is fixing simultaneously that side is loaded onto each spark (85), (90), (96), (101) plug again.
The facility scheme of patent of the present invention is in Fig. 7, below load onto timing minor sprocket (18) and the big chain of timing (12) on the bent axle, again the big chain of timing (12) is contained on the timing hinge wheel (7), aim at timing hinge wheel (7) timing dotted line (133), and fix with four screw rods, each chain conduit (114), (115) are loaded onto in the back before and after timing hinge wheel (7).Motor (17) left side side, below loads onto chain regulator (134), fixes with two screw rods.After again large crankshaft (19) head load onto motor left cap (15) and fix with screw rod, load onto generator main Moving plate (137) and fix with screw rod, the back generator main Moving plate (137) go up and dynamic panel on load onto rotating band (136), adjust with nut simultaneously and fix.
Institute is above-mentioned to be the two whirlpool burning structure new technologies of changeing of patent layering of the present invention; being domestic initiation, because this machine structure and design method have a variety of patterns, is again the achievement in research that I have studied the more than ten years; in order to guard against other people's air defenses to make the new technology of this motor, following 2 points are protected in request again.
Claims (4)
1. two whirlpool combustion energy saving internal-combustion engines that change of new distribution device four cylinder layerings of novel four-stroke, it is on the crankcase of the upright four cylinder Dual Over Head Camshaft petrol engine of existing four-stroke, load onto newly-designed four cylinder jet pads, four little cylinder heads, four little cylinder heads are established new distribution device, four little cylinders adopt to stand upside down and are provided with, the structure of the upright four cylinder Dual Over Head Camshaft petrol engine of existing four-stroke by, bent axle, crankcase, gearbox, gear, four chain bar assemblies, four piston assemblies, four cylinders, four cylinder heads, compositions such as distribution device, in Fig. 3: take earlier eight little oil rings of turbine shaft (68) (75) to distribute to be contained on four axle collar positions of advancing to arrange turbine (66) (69) (73) (77), on axle collar position, load onto seat (67) (76) in each turbine, load onto seat about each turbine again, loading onto each turbine timing minor sprocket (81) (103) again fixes with nut, load onto each turbine timing gimmal (82) (102) again, the opposing party respectively loads onto two at two two shaft heads that advance to arrange turbine and advances to arrange turbine (66) (69) and be tightly fixed, advancing to arrange each one of turbine (66) (69) (73) (77) distribution threading to four again subsequently advances to arrange in the turbine urceolus (63) (74), after load onto each turbine head flap (72) (70) at every shaft head again and respectively have screw rod to fix, load onto each turbine left and right side cap (62) (80) and each is fixed with screw rod at each left and right sides nozzle that only advances to arrange turbine urceolus (63) (74) again, each is with (78) (65) about seat (76) (67) and turbine in screw rod fixed turbine on each urceolus face, in Fig. 4, load onto each turbine driven gear (5) (117) at the shaft head and the axle afterbody of small crankshaft (2) earlier, and respectively fix with nut, it is fixing to load onto timing hinge wheel seat (6) at small crankshaft (2) head again.The opposing party take four pairs of small piston rings (38) and small piston (39) about four one word oil rings (40) respectively; distribution is contained in drips several drop lubrications in the ring position of four small pistons (39); again four small pistons (39) are distributed and be contained in the wrist pin place of four chainlet bars (42); and each penetrates with chainlet bar (42) with a small piston pin (40) and to be connected; and each fixes each small piston pin (40) with two round jump rings; take the axial region distribution of four chainlet bars (42) to be connected subsequently again with four crank pins of small crankshaft (2); and cover each chainlet bar under tile lid (3); and each is fixed with two screw rods; after again four small pistons (39) on the small crankshaft (2) distribute are put in the four little cylinders (37); and on the axle of small crankshaft (2), respectively cover a small crankshaft lid (116); and each is fixed with two cylinder screw rods; in Fig. 5; take one four unification air bend pipe (120) and four four air inlet seats (104) that advance to arrange on the turbine urceolus (74) (63); (105); (106); (107) connect; and at each air inlet seat (104); (105); (106); (107) fix four unification air bend pipes (120) with two screw rods; four unification air bend pipe (120) the other ends are connected with an end of an air throttle valve (129); air throttle valve (129) the other end is connected with air-strainer (127); and each is fixed with a round jump ring; in Fig. 6; at four cylinders (29) rear; at every cylinder (44) (47) (51) (29) platform jet (83); (88); (94); (99) locate to load onto each oil sprayer (84); (89); (95); (100); side is loaded onto each spark (85) again; (90); (96); (101) plug is fixing simultaneously; in Fig. 7; below load onto timing minor sprocket (18) and the big chain of timing (12) on the bent axle; again the big chain of timing (12) is contained on the timing hinge wheel (7); aim at timing hinge wheel (7) timing dotted line (133); and fix with four screw rods; each chain conduit (114) is loaded onto in the back before and after timing hinge wheel (7); (115); motor (17) left side side, below loads onto chain regulator (134); fix with two screw rods; after again large crankshaft (19) head load onto motor left cap (15) and fix with screw rod; loading onto generator main Moving plate (137) fixes with screw rod; rotating band (136) upward and on the dynamic panel is loaded onto at generator main Moving plate (137) in the back; adjust with nut simultaneously and fix; institute is above-mentioned to be the two whirlpool burning structure new technologies of changeing of patent layering of the present invention; it is domestic initiation; because this machine structure and design method have a variety of patterns; it is again the achievement in research that I have studied the more than ten years; in order to guard against other people's air defenses to make the new technology of this motor, below request is protected again
At internal-combustion engine filler opening is set, single-cylinder, perhaps many cylinders, 360 ° of cylinder top plan circumference, 360 ° of firing chamber cylindrical planar circumferential, 360 ° of cylinder gasket cylinder limit circumference, jet is set, or filler opening etc., in cylinder, enter the fuel layering burning, all disapprove, 360 ° of the outside pistons of internal-combustion engine, with compression ring and oil ring a choma is set, perhaps a plurality of chomas, cylinder wall use air inlet, exhaust, all disapprove.
2. the two whirlpool combustion energy saving internal-combustion engines that change of the new distribution device layering of novel four-stroke according to claim 1 is characterized in that: advance to arrange and be provided with intake duct and air outlet flue in the turbine, air outlet flue is that whirlpool blade intermediate space is an air outlet flue.
3. the two whirlpool combustion energy saving internal-combustion engines that change of the new distribution device layering of novel four-stroke according to claim 1, it is characterized in that: above the big cylinder a little cylinder is set, a little cylinder adopts to stand upside down and is provided with, a little cylinder wall the place ahead is provided with two mouths, during two mouth air inlets are synchronous air inlets, are synchronous exhaust during exhaust.
4. the two whirlpool combustion energy saving internal-combustion engines that change of the new distribution device layering of novel four-stroke according to claim 1, it is characterized in that: one one word oil ring respectively is set about small piston the place ahead, an oil ring respectively is set, add that the oil gas ring on the small piston ring has formed a rectangular choma, a rectangular choma has been the sealing oil effect when being work.
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| Application Number | Priority Date | Filing Date | Title |
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| CN2011100280155A CN102155285B (en) | 2011-01-26 | 2011-01-26 | Novel four-stroke four-cylinder layered dual-vortex combustion energy-saving internal combustion engine with new gas distribution mechanism |
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| CN2011100280155A CN102155285B (en) | 2011-01-26 | 2011-01-26 | Novel four-stroke four-cylinder layered dual-vortex combustion energy-saving internal combustion engine with new gas distribution mechanism |
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| CN102155285B CN102155285B (en) | 2013-05-22 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103511586A (en) * | 2013-05-22 | 2014-01-15 | 喻名伟 | Mechanical energy engine |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86106958A (en) * | 1986-09-25 | 1988-04-06 | 加尔布拉斯工程控股有限公司 | Reciprocating engine |
| CN2339759Y (en) * | 1996-07-24 | 1999-09-22 | 董振宝 | Single-cylinder double-piston-opposite type engine |
| CN1793626A (en) * | 2005-12-19 | 2006-06-28 | 张永志 | One-cylinder two-piston opposed internal combustion engine |
| WO2007010186A1 (en) * | 2005-07-15 | 2007-01-25 | Lotus Cars Limited | Opposed piston engine with variable timing |
| GB2431695A (en) * | 2005-10-28 | 2007-05-02 | Gregory Lawrence Leonard | Internal combustion five-stroke engine with opposed pistons and eccentric gearing |
-
2011
- 2011-01-26 CN CN2011100280155A patent/CN102155285B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86106958A (en) * | 1986-09-25 | 1988-04-06 | 加尔布拉斯工程控股有限公司 | Reciprocating engine |
| CN2339759Y (en) * | 1996-07-24 | 1999-09-22 | 董振宝 | Single-cylinder double-piston-opposite type engine |
| WO2007010186A1 (en) * | 2005-07-15 | 2007-01-25 | Lotus Cars Limited | Opposed piston engine with variable timing |
| GB2431695A (en) * | 2005-10-28 | 2007-05-02 | Gregory Lawrence Leonard | Internal combustion five-stroke engine with opposed pistons and eccentric gearing |
| CN1793626A (en) * | 2005-12-19 | 2006-06-28 | 张永志 | One-cylinder two-piston opposed internal combustion engine |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103511586A (en) * | 2013-05-22 | 2014-01-15 | 喻名伟 | Mechanical energy engine |
| WO2014187145A1 (en) * | 2013-05-22 | 2014-11-27 | Yu Mingwei | Mechanical energy engine |
| CN103511586B (en) * | 2013-05-22 | 2018-05-15 | 喻名伟 | Mechanical energy engine |
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| Publication number | Publication date |
|---|---|
| CN102155285B (en) | 2013-05-22 |
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Effective date of registration: 20201120 Address after: No. 58, Tonggang Road, Nantong City, Jiangsu Province, 226000 Patentee after: NANTONG YATAI ENGINEERING TECHNOLOGY Co.,Ltd. Address before: 565400 Guizhou city in Renhuai Province, central town of Fu Le more supermarket floor seven Patentee before: Yang Chengyuan |