Two stroke internal combustion engine

Information

  • Patent Grant
  • 6467440
  • Patent Number
    6,467,440
  • Date Filed
    Wednesday, June 23, 1999
    25 years ago
  • Date Issued
    Tuesday, October 22, 2002
    22 years ago
Abstract
A two stroke internal combustion engine, comprising one or more power cylinders with intake and exhaust ports and a source of scavenging of the power cylinders, with improvements, including use of double-sided cylinders with upper and lower cavities used as power or pumping cavities connected to each other in different combinations.
Description




CROSS-REFERENCE TO RELATED PATENTS AND APPLICATIONS




Two Stroke Internal Combustion Engine. Patent of Russian Federation No. 2143077, Int. Cl. F02 B 33/00, registered Dec. 20, 1999, published in 1999, Bul. No 35, priority date Jun. 22, 1998, application No 98111885/06.




REFERENCES CITED




1. Two Stroke Internal Combustion Engine. RU Patent No. 2063524, Int. Cl. F02 B 33/22, published in 1996, Bul. No. 19.




2. Two Stroke Internal Combustion Engine. U.S. Pat. No. 2,522,649, US Cl. 123-70, 1950.




3. Radial Two Stroke Internal Combustion Engine with Piston Scavenging Pumps. SU Patent No. 54112, Int. Cl. F02 B 33/22, 75-22, 1939.




INFORMATION SOURCES, TAKEN INTO CONSIDERATION




1. RU Patent No. 2063524 Cl, Jul. 10, 1996




2. U.S. Pat. No. 2,522,649 A, Sep. 19, 1950




3. SU Patent No. 54112 A, Feb. 28, 1939




4. SU Patent No. 2472 A, Mar. 31, 1927




5. U.S. Pat. No. 3,880,126 A, Apr. 29, 1975




6. U.S. Pat. No. 5,265,564 A, Nov. 30, 1993




7. GB Patent No. 994371 A, Nov. 7, 1961




BACKGROUND OF THE INVENTION




This invention relates to further development of two stroke internal combustion engines (from hereinafter referred to as ‘TSICE’), which have one or more power cylinders with intake and exhaust ports, and a source of scavenging of the power cylinders.




Some terms and abbreviations used in the following description of previous art and present invention are defined below.




Pistons of TSICE move reciprocally within two limits, conventionally named as ‘top dead center’ and ‘bottom dead center’. From hereinafter top dead center is referred to as ‘TDC’ and bottom dead center as ‘BDC’.




Cavity of a cylinder, which is a space within the walls of the cylinder limited by a face of a piston, from hereinafter is referred to as ‘cavity’.




In a double-sided cylinder, a piston has two faces, front and rear, which form two cavities within the walls of the cylinder on the opposite sides of the piston. In further description, due to the upright position of the cylinders on the drawings, the said cavities are referred to as ‘upper cavity’ and ‘lower cavity’.




The main problems, known as deficiencies of TSICE, are the partial mixing of burned gases with the fresh air-fuel mixture, and the loss of some fresh air-fuel mixture through the exhaust ports at the time of scavenging.




As long as improvements can be achieved, reducing these problems, there is a chance to increase power per liter of displacement.




The so-called direct-flow scavenging/charging of the power cylinders has to be organized, when fresh air-fuel mixture fills up the cavity of the power cylinder starting from the intake port towards the exhaust port, so that burned gases always remain in the way of the air-fuel mixture to the exhaust port with minimum mixing.




One of the ways to achieve direct-flow scavenging/charging is to have two power cylinders, connected to each other with a common combustion chamber, where one of the cylinders has an intake port, and another has the exhaust port, as it is in RU Patent No. 2,063,524. Scavenging/charging starts in one cylinder and ends in the other, most importantly, cleaning the area of combustion chamber of burned gases and providing unidirectional displacement of burned gases with fresh air-fuel mixture.




TSICE, according to RU Patent No. 2,063,524, uses a pumping cylinder as a source of scavenging/charging of power cylinders. It comprises the first power cylinder with an intake port, connected to a pumping cylinder, and the second power cylinder with an exhaust port, said cylinders having a common combustion chamber and pistons connected each to its own crank, with the crank of the second piston having advanced crank angle against the crank of the first piston, enabling advanced opening and closing of the exhaust port in relation to the intake port.




Use of an additional cylinder, piston and crank solely for the purpose of scavenging/charging of another cylinder, increases the size and weight of the engine and reduces power per liter of displacement, and should be considered a drawback of the above named patent.




According to the totality of distinctive characteristics, the engine construction of RU Patent No. 2,063,524 is considered the closest prototype of present invention.




BRIEF SUMMARY OF THE INVENTION




Presented is TSICE, which has double-sided cylinders with upper and lower cavities used as power or pumping cavities, connected to each other in different combinations, which reduces the number of cranks and pistons and size and weight of the engine and increases power per liter of displacement.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

shows one-cylinder TSICE at the end of the power stroke during scavenging/charging with piston having a baffle.





FIG. 2

shows cross section with a top view of the piston illustrating construction of the baffle, forming the gas flow.





FIG. 3

shows position of a piston at the moment of exhaust of burned gases from power cylinder before the beginning of scavenging, when the intake port is still closed.





FIG. 4

shows TSICE with pumping cylinder used for scavenging/charging of the power cylinder, with piston of the power cylinder having a baffle.





FIGS. 5 .

. .


10


illustrate preferred embodiments of the present invention and their crank diagrams.





FIGS. 5A .

. .


5


D show the crank angle diagrams of TSICE with the crank of the first cylinder advanced by α°=180°+β° in relation to the crank of the second cylinder.





FIGS. 7A .

. .


7


D show the crank angle diagrams of TSICE with the crank of the first cylinder advanced by α°=β° in relation to the crank of the second cylinder.





FIG. 6

shows TSICE comprising two double-sided cylinders with two pumping and two power cavities and piston cranks having angular deviation β° against each other.





FIG. 8

shows TSICE comprising two double-sided cylinders, with four power cavities, connected to external supercharger, and piston cranks having angular deviation β° against each other.





FIGS. 9A .

. .


9


D show TSICE comprising two double-sided cylinders with two pumping and two power cavities and piston cranks having angular deviation 180°+β° against each other.





FIG. 9E

shows four-cylinder TSICE, which is a combination of two engines, presented on

FIGS. 9A .

. .


9


D.





FIGS. 10A .

. .


10


D show TSICE comprising two double-sided cylinders, with four power cavities, connected to external supercharger, and piston cranks having angular deviation 180°+β° against each other.





FIG. 11

shows TSICE comprising one power cylinder and one dual action cylinder, connected to a supercharger through a distribution valve.





FIG. 12

shows TSICE comprising two power cylinders and two dual action cylinders, connected to a supercharger through a distribution valve.





FIG. 13

shows single-row double-bank TSICE comprising power cylinder in the first bank and double-sided cylinder in the second bank with pumping cavity, connected to a supercharger.





FIG. 14

shows double-row double-bank TSICE comprising two power cylinders in the first bank and two double-sided cylinders in the second bank with pumping cavities, connected to a supercharger, and piston cranks having angular deviation β° against each other.





FIGS. 15A

,


15


B show double-row double-bank TSICE comprising two power cylinders in the first bank and two double-sided cylinders in the second bank with pumping cavities, connected to a supercharger, and piston cranks having angular deviation 180°+β° against each other.





FIGS. 16A

,


16


B show double-row double-bank TSICE comprising two pumping cylinders in the first bank, connected to a supercharger, and two double-sided cylinders in the second bank with piston cranks having angular deviation 180°+β° against each other.





FIG. 17

shows four-row double-bank TSICE comprising four power cylinders in the first bank and four double-sided cylinders in the second bank, whose all cavities are power cavities, connected to external supercharger.





FIG. 18

shows double-row double-bank TSICE comprising two power cylinders in the first bank and two double-sided cylinders in the second bank, whose upper cavities are dual action cavities.





FIG. 19

shows TSICE comprising two power cylinders connected by a common combustion chamber and charged by two external superchargers.





FIG. 20

shows TSICE comprising two pairs of power cylinders, each pair having a common combustion chamber, and charged by two external superchargers.











REFERENCE NUMERALS IN DRAWINGS


















1




First cylinder of the first bank






2




Second cylinder of the first bank






3




Third cylinder of the first bank






4




Fourth cylinder of the first bank






5




First cylinder of the second bank






6




Second cylinder of the second bank






7




Third cylinder of the second bank






8




Forth cylinder of the second bank






9




Piston of cylinder 1






10




Piston of cylinder 2






11




Piston of cylinder 3






12




Piston of cylinder 4






13




Piston of cylinder 5






14




Piston of cylinder 6






15




Piston of cylinder 7






16




Piston of cylinder 8






17




Upper cavity of cylinder 1






18




Lower cavity of cylinder 1






19




Upper cavity of cylinder 2






20




Lower cavity ot cylinder 2






21




Upper cavity of cylinder 3






22




Lower cavity of cylinder 3






23




Upper cavity of cylinder 4






24




Lower cavity of cylinder 4






25




Upper cavity of cylinder 5






26




Lower cavity of cylinder 5






27




Upper cavity of cylinder 6






28




Lower cavity of cylinder 6






29




Upper cavity of cylinder 7






30




Lower cavity of cylinder 7






31




Upper cavity of cylinder 8






32




Lower cavity of cylinder 8






33




Intake port of cavity 17






34




Intake port of cavity 18






35




Intake port of cavity 19






36




Intake port of cavity 20






37




Intake port of cavity 21






38




Intake port of cavity 22






39




Intake port of cavity 23






40




Intake port of cavity 24






41




Intake port of cavity 25






42




Intake port of cavity 26






43




Intake port of cavity 27






44




Intake port of cavity 28






45




Intake port of cavity 29






46




Intake port of cavity 30






47




Intake port of cavity 31






48




Intake port of cavity 32






49




Exhaust port of cavity 17






50




Exhaust port of cavity 18






51




Exhaust port of cavity 19






52




Exhaust port of cavity 20






53




Exhaust port of cavity 21






54




Exhaust port of cavity 22






55




Exhaust port of cavity 23






56




Exhaust port of cavity 24






57




Exhaust port of cavity 25






58




Exhaust port of cavity 26






59




Exhaust port of cavity 27






60




Exhaust port of cavity 28






61




Exhaust port of cavity 29






62




Exhaust port of cavity 30






63




Exhaust port of cavity 31






64




Exhaust port of cavity 32






65




Dual purpose port (intake - for pumping cylinder and exhaust -







for power cylinder)






6




Common combustion chamber






67




Common compression chamber






68




Longitudinal partition






69




Transverse partition






70




Crank of piston 9






71




Crank of piston 10






72




Crank o fpiston 11






73




Crank of piston 12






74




Piston rod






75




Crosshead






76




Connecting rod






77




Crank-and connecting rod assembly






78




Oil-filled crankcase






79




Spark plug






80




High pressure direct fuel injector






81




Arc groove in cylindrical surface of piston 9, facing the intake







port 33






82




Bottom side wall of groove 81






83




Top side wall of groove 81






84




Top face of piston 9






85




Top edge of intake port






86




External cylindrical edge of top side wall 83 of groove 81






87




Diffuser in form of a gap between edge 86 of top side wall







83 of groove 81 and wall of cylinder 1






88




Recess in the face of power piston, open towards exhaust port






89




Top edge of exhaust port






90




Starting supercharger






91




Supercharger






92




Engine intake manifold






93




Damping chamber






94




Distribution valve






95




Cut-off valve






96




Self-acting delivery valve






97




Check valve






98




Self-acting suction valve






99




Low pressure direct fuel injector






100




Fuel pipeline






101




Low pressure external fuel injector






102




Channel, connecting cavities 17 and 19






103




Channel, connecting cavities 17 and 25






104




Channel, connecting cavities 17 and 26






105




Channel, connecting cavities 17 and 28






106




Channel, connecting cavities 18 and 19






107




Channel, connecting cavities 19 and 20






108




Channel, connecting cavities 17 and 20






109




Channel, connecting cavities 19 and 26






110




Channel, connecting cavities 19 and 27






111




Channel, connecting cavities 19 and 28






112




Channel, connecting cavities 21 and 23






113




Channel, connecting cavities 25 and 28






114




Channel, connecting cavities 25 and 26






115




Channel, connecting cavities 26 and 27






116




Channel, connecting cavities 27 and 28






117




Channel, connecting cavities 25 and 27 to cavities 17 and 26






118




Channel, connecting cavity 17 to cavity 19 or to the engine







intake manifold






119




Channel, connecting cavity 19 to cavity 21 or to the engine







intake manifold






120




Channel, connecting cavities 19, 21, 27, 28, 29 and 30 to the







engine intake manifold














DETAILED DESCRIPTION OF THE INVENTION




Present invention is applicable to the following three types of TSICE:




1) spark ignited (e.g. gasoline, propane) engine with an external mixing of air and fuel in the intake manifold and use of air-fuel mixture for scavenging of power cylinders;




2) spark ignited (e.g. gasoline) engine with scavenging of power cylinders with pure air and direct fuel injection into the power cylinders at the beginning of compression stroke after their ports are already closed;




3) self-ignited (diesel) engine with scavenging of power cylinders with pure air and direct fuel injection into the power cylinders at the end of compression stroke.




All three types of engines have an oil-filled crankcase. TSICE charged with air-fuel-oil mixture through a dry crankcase are not considered, since they are pollutive and have other known disadvantages.




If exhaust ports of the power cylinders close before their intake ports, charging of power cylinders can continue after the exhaust ports are closed, making coefficient of admission possibly more than 1.0.




In TSICE of second and third types cylinders are scavenged/charged with pure air, having fuel injected directly into the cavity of power cylinder. In these engines low pressure fuel injector


101


in the engine intake manifold is not present. Instead, in the second type of spark-ignited engine low pressure direct fuel injector


99


installed in the power cylinder is used together with a spark plug


79


. In self-ignited TSICE of the third type spark plug


79


is replaced with a high pressure direct fuel injector


80


. The direct injection of fuel into the power cylinders after scavenging is complete and ports of the power cylinders are closed, eliminates fuel loss and mixing of a fresh charge with burned gases.




Drawings and descriptions are made as for the first type of TSICE.




One of the embodiments of the present invention, shown on

FIG. 6

, has two double-sided cylinders


1


and


2


, whose upper cavities


17


and


19


are power cavities, and lower cavities


18


and


20


are pumping cavities. Cavities


17


and


19


have common combustion chamber


66


. Cavities


18


and


20


have common compression chamber


67


. Power cavity


17


has the exhaust port


49


, and power cavity


19


has the intake port


35


. Pumping cavity


18


has the intake port


34


, and pumping cavity


20


has the exhaust port


52


, which is connected to the intake port


35


by the channel


107


. Crank


70


of the piston


9


has an advanced by β° crank angle against crank


71


of the piston


10


, as shown in

FIGS. 7A .

. .


7


D, enabling advanced opening and closing of the exhaust port


49


in relation to the intake port


35


. Angle β° is an angle of rotation of crank


70


, corresponding to the piston


9


move from BDC to the piston, where piston


9


closes the exhaust port


49


.




The method of operation of the TSICE on

FIG. 6

is as follows.




At the end of the power stroke, when piston


9


of the power cylinder is at BDC, as shown in

FIG. 6

, crank


71


still has β° to turn, before piston


10


will each BDC.




With piston


9


at BDC, the exhaust port


49


is completely open, allowing the escape of burned gases from cavities


17


and


19


. Piston


10


still has not reached BDC and the intake port


35


is still closed. When piston


9


moves up from BDC, and piston


10


still continues going down to its BDC, the exhaust port


49


starts closing simultaneously with opening of the intake port


35


. At this time a direct-flow scavenging of power cavities takes place. A fresh portion of air-fuel mixture entering through the intake port


35


, fills consequently cavities


19


and


17


, pushing out burned gases through the exhaust port


49


. Compressed air-fuel mixture is delivered to the intake port


35


by the channel


107


from the pumping cavities


18


and


20


. When the piston


10


reaches BDC and opens completely the intake port


35


, piston


9


completely closes the exhaust port


49


, which represents the end of scavenging. The charging of the cavities


19


and


17


with fresh air-fuel mixture continues through the still open intake port


35


, until it is completely closed by the piston


10


, moving up from BDC. After the closing of the port


35


, the air-fuel mixture is compressed in power cavities


17


and


19


. Pistons


9


and


10


, move up, piston


9


reached TDC first, and when it starts going down and piston


10


reaches TDC, ignition of compressed air-fuel mixture happens, initiating a power stroke. While moving up, pistons


9


and


10


create a vacuum in the pumping cavities


18


and


20


. When the piston


9


reaches TDC, it opens the intake port


34


, and the created vacuum induces suction of fresh-air fueled mixture into the pumping cavities


18


and


20


. During the power stroke, moving down, pistons


9


and


10


compress it, and at the end of power stroke, the process of scavenging/charging of the power cavities starts, as described above.




Another embodiment of the present invention, shown in FIG


8


, has two double-sided cylinders


1


and


2


, but unlike the engine on

FIG. 6

, it has all cavities being power cavities, including upper cavities


17


and


19


and lower cavities


18


and


20


. Each pair of cavities has its common combustion chamber


66


and the spark plug


79


. Instead of pumping cavities used in engine on

FIG. 6

, an external source of scavenging is used, like the supercharger


91


, which can be driven by an electric motor or by the engine itself, or by the energy of exhaust gases (turbo-supercharger). The cavities


17


and


18


have exhaust ports


49


and


50


, and the cavities


19


and


20


have intake ports


35


and


36


. Air-fuel mixture from the supercharger


91


is delivered with constant pressure to the intake ports


35


and


36


. The crank


70


of the piston


9


has a crank angle advanced by β° against the crank


71


of the piston


10


, as shown on

FIG. 7

, enabling advanced opening and closing of the exhaust port


49


in relation to the intake port


35


and the exhaust port


50


in relation to the intake port


36


.




The method of operation of the TSICE on

FIG. 8

is as follows.




At the end of the power stroke, when piston


9


of the power cylinder is at BDC, as shown on

FIG. 8

, the crank


71


still has β° to turn, before the piston


10


will reach BDC.




With piston


9


at BDC exhaust port


49


is completely open allowing the escape of burned gases from cavities


17


and


19


. Piston


10


still has not reached BDC and the intake port


35


is still closed. When piston


9


moves up from BDC, and piston


10


still continues going down to BDC, the exhaust port


49


starts closing simultaneously with opening of the intake port


35


, which initiates a direct-flow scavenging of cavities


19


and


17


with pressurized air-fuel mixture from the supercharger. The scavenging continues until the exhaust port


49


is closed. At that moment, the piston


10


reaches BDC, and the intake port


35


remains open until completely closed by piston


10


, moving up from BDC. This allows the supercharger to create excessive pressure of air-fuel mixture inside the cavities


19


and


17


. During the compression stroke the pistons


9


and


10


reach TDC one before another. When piston


10


reaches TDC, the compressed air-fuel mixture is ignited by a spark plug and a power stroke starts. The pistons


9


and


10


go down and after the piston


9


reaches BDC a new cycle begins. Operation of power cavities


18


and


20


goes exactly the same way, as of cavities


17


and


19


, described above, but with the opposite timing. That doubles the amount of power, generated by the TSICE, compared with the TSICE on FIG.


6


. Additional increase of power per liter of displacement is achieved by the use of a supercharger, which makes the coefficient of admission of the power cylinders more than 1.0.




TSICE shown on

FIGS. 9A .

. .


9


D is the third embodiment of the present invention with double-sided cylinders


1


and


2


, where pistons


9


and


10


, reciprocally movable therein, are connected to cranks


70


and


71


. The crank


70


has a crank angle, advanced against crank


71


by α°=180°+β°, as shown on

FIGS. 5A .

. .


5


D, where β° is an angle of rotation of crank


70


, corresponding to the piston


9


move from TDC down to the position when piston


9


closes the exhaust port


50


. The cavities


18


and


19


are power cavities, connected to each other by channel


106


, shown on

FIGS. 9C

,


9


D. The channel


106


represents the common combustion chamber for cavities


18


and


19


, which have the common spark plug


79


, common intake ports


35


, located in cavity


19


, and common exhaust port


50


, located in cavity


18


. Cavities


17


and


20


are pumping cavities. They have individual intake ports


33


and


36


and exhaust ports


49


and


52


, connected to the intake ports


35


by channels


102


and


107


.




The method of operation of the TSICE on

FIGS. 9A .

. .


9


D is as follows.




At the end of a compression stroke, as shown on

FIGS. 9A and 9B

, air-fuel mixture is compressed in the power cavities


18


and


19


and a vacuum is created in the pumping cavities


17


and


20


. When the piston


9


of the power cylinder is at BDC (FIG.


9


A), the intake port


33


opens and vacuum inside the pumping cavity


17


draws in a fresh portion of air-fuel mixture. The crank


71


still has β° to turn, before piston


10


will reach TDC. When that happens (FIG.


9


B), the intake port


36


opens and vacuum inside the pumping cavity


20


draws in a fresh portion of air-fuel mixture. At the same time, air-fuel mixture, compressed in power cavities


18


and


19


is ignited with the spark plug


79


, and a power stroke begins with simultaneous compression of a new portion of air-fuel mixture in the pumping cavities


17


and


20


. When piston


9


, on its way up, reaches TDC (

FIG. 9C

) the exhaust port


50


opens, allowing the release of the burned gases from the power cavities. Since then, both pistons move down: the piston


9


, closing the exhaust port


50


, and the piston


10


, opening the intake ports


35


of power cylinders. Until the exhaust port


50


closes, the direct-flow scavenging/charging of the power cavities


19


and


18


goes on. Compressed in the pumping cavities


17


and


20


, an air-fuel mixture is released through the channels


102


and


107


into the cavity


19


and from there through the channel


106


into the cavity


18


, pushing the rest of the burned gases out of the exhaust port


50


. The process of scavenging ends when the piston


10


reaches BDC and the piston


9


closes the exhaust port


50


(FIG.


9


D). The intake ports


35


remain open and process of charging of the power cylinders continues until piston


10


, moving up from BDC, closes ports


35


, and another compression stroke starts.




An advantage of this version of TSICE is that the phase opposition of the cranks


70


and


71


balances the forces applied to the crankshaft bearings and inertial masses of the engine.




In practical applications for smoother performance this type of engine will include four double-sided cylinders, combined in pairs, as shown on FIG.


9


E.




TSICE according to the present invention, shown on

FIGS. 10A .

. .


10


D, unlike the previous embodiment, has all four cavities of two double-sided cylinders being power cavities. The power cavities


18


and


19


are connected by the channel


106


, as shown on

FIGS. 10C

,


10


D. The power cavities


17


and


20


are connected by the channel


108


, as shown on

FIGS. 10A

,


10


B. Each pair of cavities has its own spark plug


79


. The cavities


18


and


19


have the common intake port


35


and exhaust port


50


. The cavities


17


and


20


have the common intake port


36


and the exhaust port


49


. The crank


70


has a crank angle, advanced against the crank


71


by α°=180°+β°, as shown on

FIGS. 5A .

. .


5


D, where β° is an angle of rotation of the crank


70


, corresponding to the piston


9


move from BDC up to the position when the piston


9


closes the exhaust port


49


. Since cylinders of this TSICE do not have pumping cavities, the external supercharger


91


, connected by the intake manifold


92


to the intake ports, is used for scavenging/charging of the power cavities.




The method of operation of the TSICE on

FIGS. 10A .

. .


10


D is as follows.




When the piston


9


reaches BDC at the end of power stroke, as shown on

FIG. 10A

, the exhaust port


49


opens, allowing the escape of burned gases from the cavities


17


and


20


. During another β° of crankshaft rotation, both pistons move up: the piston


9


moves from BDC, closing the exhaust port


49


, and the piston


10


moves towards TDC, opening the intake port


36


. Until the exhaust port


49


is completely closed, the direct-flow scavenging/charging of the cavities


20


and


17


takes place. Pressurized air-fuel mixture from the supercharger


91


fills the cavities


20


and


17


through the intake port


36


and the channel


108


, pushing the rest of the burned gases out of the exhaust port


49


. The process of scavenging ends, when the piston


10


reaches TDC and the piston


9


closes the exhaust port


49


(FIG.


10


B). The intake port


36


remains open and the process of charging of the power cylinders continues until the piston


10


, moving down from TDC, closes the port


36


and a compression stroke begins in the cavities


17


and


20


. At the time of scavenging/charging of the cavities


17


and


20


, another pair of cavities,


18


and


19


, is at the end of a compression stroke. When the piston


10


reaches TDC, the compressed air-fuel mixture in the cavities


18


and


19


is ignited, initiating in them a power stroke. This gas combustion causes the pistons


9


and


10


to move towards each other, piston


9


to TDC and piston


10


to BDC, compressing a new portion of air-fuel mixture in the cavities


17


and


20


. When the piston


9


reaches TDC (FIG.


10


C), the exhaust port


50


opens, allowing the release of the burned gases from the power cavities


18


and


19


through the channel


106


at the end of a combustion stroke. During another β° of crankshaft rotation, both pistons move down: the piston


9


moves from TDC, closing the exhaust port


50


, and piston


10


moves towards BDC, opening the intake port


35


. Until the exhaust port


50


is completely closed, the direct-flow scavenging/charging of the cavities


18


and


19


takes place. Pressurized air-fuel mixture from the supercharger


91


fills cavities


18


and


19


through the intake port


35


and channel


106


, pushing the rest of the burned gases out of the exhaust port


50


. The process of scavenging ends, when the piston


10


reaches BDC and the piston


9


closes the exhaust port


50


(FIG.


10


D). The intake port


35


remains open and the process of charging of the power cylinders continues until the piston


10


, moving up from BDC, closes the port


35


and a compression stroke begins in the cavities


18


and


19


. At the time of scavenging/charging of the cavities


18


and


19


, another pair of cavities,


17


and


20


, is at the end of a compression stroke. When the piston


10


reaches BDC, a compressed air/fuel mixture in the cavities


17


and


20


is ignited, initiating in them a power stroke. This gas combustion causes the pistons


9


and


10


to move towards each other, the piston


9


to BDC and the piston


10


to TDC, compressing a new portion of air-fuel mixture in the cavities


18


and


19


. When the piston


9


reaches BDC (FIG.


10


A), the process continues, as described above.




All the engines, described above, achieve the object of increasing of power per liter of displacement.




The few shown examples illustrate, how wide can be the variety of applications of present invention, from small appliances, to the huge diesel marine engines.




Many more modifications of the present invention are possible, and among those, described above, TSICE, presented on

FIG. 10

, is considered as the preferred embodiment. Nevertheless, other shown embodiments may be given preference in different applications.




The scope of the invention should be determined by the appended claim, rather than by the examples given.



Claims
  • 1. A two stroke internal combustion engine comprising first power cylinder with a first piston reciprocally movable therein and an intake ports and second power cylinder with a second piston reciprocally movable therein and an exhaust ports, said pistons being connected each to its own crank, with the crank of the second piston having advanced crank angle against the crank of the first piston, enabling advanced opening and closing of the exhaust port in relation to the intake port, said cylinders being double-sided, with upper power cavities and lower power cavities on the opposite sides of the pistons, said cavities interconnected by passages in pairs, with lower power cavities separated from cranks by a transverse partition, and the intake ports of power cavities of the first cylinder connected to a source of scavenging and supercharging, with improvements, including said crank of the second piston having additional advancement of 180° against the crank of the first piston, providing movement of said pistons in opposition to each other, and said passages interconnecting lower power cavity of the first cylinder with upper power cavity of the second cylinder and upper power cavity of the first cylinder with lower power cavity of the second cylinder.
Priority Claims (1)
Number Date Country Kind
98111885 Jun 1998 RU
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Number Name Date Kind
896514 Brundige Aug 1908 A
968636 Aslakson Aug 1910 A
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2706970 Rinne Apr 1955 A
4079705 Buchner Mar 1978 A
4157080 Hill Jun 1979 A
4275689 Ray Jun 1981 A
4312308 Slattery Jan 1982 A
4516539 Andreen May 1985 A
4781155 Brucker Nov 1988 A
5638779 Atmur et al. Jun 1997 A
5862781 Rossle Jan 1999 A