US1145820A - Internal-combustion engine. - Google Patents
Internal-combustion engine. Download PDFInfo
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- US1145820A US1145820A US62201411A US1911622014A US1145820A US 1145820 A US1145820 A US 1145820A US 62201411 A US62201411 A US 62201411A US 1911622014 A US1911622014 A US 1911622014A US 1145820 A US1145820 A US 1145820A
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- 238000002485 combustion reaction Methods 0.000 title description 14
- 239000000203 mixture Substances 0.000 description 13
- 239000007789 gas Substances 0.000 description 7
- 238000004880 explosion Methods 0.000 description 5
- 239000012530 fluid Substances 0.000 description 5
- 238000010276 construction Methods 0.000 description 3
- 239000002360 explosive Substances 0.000 description 3
- 238000007906 compression Methods 0.000 description 2
- 230000002000 scavenging effect Effects 0.000 description 2
- MWPLVEDNUUSJAV-UHFFFAOYSA-N anthracene Chemical compound C1=CC=CC2=CC3=CC=CC=C3C=C21 MWPLVEDNUUSJAV-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000003190 augmentative effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 230000036461 convulsion Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000003534 oscillatory effect Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
Definitions
- SHEETSSHEET 3 Ti I Z5/UU 25 3 22 I 5028 ll 25 3 ZZ U Z8 JJ 25 LVVENTOR: F f/ Summl'I/ lV/T/VESSES:
- T FRANK H. SUMMERIL
- cer- 'tain new and useful Improvements in Internal-Combustion Engines of which the following is a specification.
- This invention relates to improvements in internal combustion engines of the type in which a pair of coactive pistons are disposed in one cylinder to be impelled in opposite directions by the explosion of an interposed charge of combustible gas.
- the principal object of my invention is to provide an engine of simple construction in which the opposed pistons in each cylinder have a relatively unbalanced movement for the purpose of timing the opening and closing periods of the admission and exhaust ports so as to prevent waste of explosive mixture. and to promote the thorough scavenging of the cylinder after each explosion.
- the unbalanced movements of the pistons are attained by displacement of their crankconnections around the shaft, at an angle of less than one hundred and eighty degrees, whereby, when the two pistons have reached the end of their strokes, the said connections will extend approximately at equal angles at opposite sides of the dead centers in the crank-motion.
- the pistons will be at all times, in a position to effectively carry the crank shaft past its dead centers and the speed of the engine will thus be materially increased.
- Another object of the invention is to provide means whereby the charge admitted into the cylinder at one time may be increased to approximately twice its volume, by adjustment of a valve ap lied between the Patented July b, 1915.
- Figure 1 represents a longitudinal sectional view of the engine, Fig. 2, a longitudinal section taken through one of the cylinders along the line 2-2, Fig. 1, the pistons having been omitted to more clearly show the positions of the various ports.
- Fig. 3 a composite view showing transverse sections taken respectively along the lines 33 and 5-5, Fig. 2, Fig. 4, a transverse section along the line 4-4:, Fig. 2, Figs. 5
- the engine as shown in the drawings, operating on the well known two-cycle principle, is composed of two cylinders 2, each provided with two opposed pistons 3 and 4, the stems of which are, by means of link-connections 5 operatively associated with double cranks on a shaft 6 which is rotatably mounted between the two cylinders, in parallel relation to their axes.
- the cranks are preferably constructed in the form of disks 7 which have an oscillatory movement in crank-cases 8, between two collars 9 which are keyed to the shaft 6.
- crank connection between the shaft and the pistons may be, made of a character different from that shown in the drawings, and, specifically, do not form part, of the present invention.
- the two cylinders 2,' which, as usual, are closed by means of heads 2, are provided at their ends with jackets which are horizontally divided into two compartments by I takes place and which, by means of a contive stroke of the respective piston 3, is conduit 13-is connected with the carbureter or other suitable supply of combustible gas.
- the separated upper compartments 14 at the same end of the cylinders each provide a transfer chamber through which the mixture compressed and displaced during the effecducted into the space between the two pistons.
- the connected lower compartments at the opposite end of the two cylinders constitutean air-receiving chamber 15 which may be connected with either the atmosphere orthe carbureter by the ad ustment of a three-way valve 16 applied at the intersection of.
- a conduit 17 wh ich opens into the chamber, and a pipe 38 which connects with the carbureter conduit 13, and the separated upper compartments 18 at the same end of the cylinders, each constitute an air-transfer chamber through which air compressed and displacedduring the effective-stroke of the respective piston 4 is conducted intothe space between the two pistons during vthescavenging period in the cycle of operations.
- the surge chamber a'nd' the air receiving chamber may be formed-either by enlargements of the lower compartments of the cylinder jackets or they may be providedby separate receptacles of suitable construction which are connected with the respective jacketcompartments by means of conduits.
- the mixture-receiving or surge-chamber-l2 connects with the interior of the cylinder bya plurality of ports 22 disposed at the end of the chamber remote from the adj acen't end.
- the mixture transfer-chamber- 14 connects with the interior of the cylinder, at one of its ends by 'meansiof a series of ports 23 through which the gases flow from the cylinderinto the said chamber during the outward stroke of the piston, and at itsopposite end by ports 24 through which the said gases'are discharged into the space between the pistons when the corresponding piston reaches. the end of its outward stroke.
- air receiving chamber 15 connects at its innermost end with the interior of the cylinder by means of ports 25 and the air transfer chamber 18 is connected with the cylin-' der by means of ports 26 through which air contained in the cylinder, passes into the ter of the cylinder, are formed slightly in advance of the corresponding ends of the ports 27 so that during outward movement of the piston 4, the exhaust will open a moment before the scavenging air is introduced into the cylinder.
- the pistons 3 and 4 which are preferably .of the hollow type as shown in the drawings, divide the cylinder into three compartments, namely, the explosion-compartment 30, between the two pistons, a mixture-compression compartment 31 between the piston 3 and the adj acentend of the cylinder and an air compression compartment 32 between the opposite end of the cylinder and the piston 4. (See Fig. 5.)
- the cranks which connect the pistons of each cylinder with the shaft 6, are, as mentioned hereinbefore, displaced around the shaft at an angle of less than one hundred and eighty degrees, an angle of from one hundred and ten to one-hundred and When the pistons are substantially at the end of their strokes, as is shown in Figs. 5 and 9 of the drawings, their cranks extend at equal angles at o posite sides of the dead centers in the cran movement, which are designated in the said figures by the letter 0.
- the scavenge ports 27 are uncovered with the result that the air contained in the ,ylinder compartment 32 and the transfer chamber 18, which had been compressed during the outward movement of the piston past the ports 25, is forced into the space between the pistons, which thus is scavenged until during the return movement of the piston 4 the scavenge ports are again closed which occurs before the exhaust ports are completely covered, (see Figs. 7 and 8). Shortly before the last action takes place the mixture admission ports 24 are uncovered by the piston 3, which at the commencement of its outward movement had closed the ports 22 through which the mixture contained in the surge chamber had entered the cylindercompartment 31.
- the volume of the charge may be instantlv augmented by connecting the air-receiving chamber 15 with the carbureter in place of with the open air by adjustment of the valve 16, when mixture will be introduced into the'space between the pistons through the scavenge-ports 27 as well as through the charge-admission ports 24.
- a cylinder having admission ports at opposite sides of its center and an exhaust port at one side of the same, a rotary shaft, opposed pistons within the said cylinder in operative connection with the said shaftja source of motive fluid in communication with one of said admission ports, and means for connecting the other admission port with either the atmosphere or the said source.
- a cylinder having at one side of its centera charge-admission port and at the other side of the center an exhaust port, a scavengeport and an air discharge port in continuous communication with the latter by a bypass, and an air admission port positioned between the said communicating ports, a rotary shaft, and opposed pistons having unbalanced movements of equal length within the said cylinder, in operative connection with the said shaft, the several ports being positioned so that during movement of the pistons the said exhaust port and the said scavenge port are uncovered and again covered before the admission port is opened for the admission of a fresh charge between the pistons.
- a cylinder having at one side of its center a charge admission port and at the other side of the same, an exhaust port, a scavenge port and an air discharge port in continuous communication by a by-pass, and an air admission port positioned between the said communicating ports, a rotary shaft, opposed pistons within the said cylinder in operative connection with the said shaft, a source of motive fluid in connection with the charge-admission port, and means for connecting the air-admission portwith either the atmosphere or the said source.
- inder having at one of its ends, a jacket partitioned into an air receiving chamber and an air transfer-chamber, a rotary shaft, and opposed pistons within the said cylinder in operative connection with the said shaft, said cylinder having at one side of its center a charge-admission port and at the opposite side of the center, an exhaust port, a scavenge port and an air-discharge port in communication with said transfer chamber, and an air-admission port disposed between the last named ports in communication with the said air receiving chamber.
- a cylinder having jackets at opposite ends thereof, and each partitioned into two compartments, the compartments in one of said jackets constituting respectively a surge chamber and a mixture transfer chamber and those in the other jacket, an air receiving chamber and an air-transfer chamber, a rotary shaft, and opposed pistons having unbalanced movements within the cylinder in operative connection with said shaft, the said cylinder having at one side of its center an exhaust port, at the same side, a scavenge port and an air discharge port in a c'yl communication with the air-transfer cham- &
- a cylinder having jackets at opposite ends thereof, and each partitioned into two compartments, the compartments in one of said 1ackets constituting respectively a surge chamber and a mixture transfer chamber and those in the other jacket, an air receiving chamber.
- the said cylinder having at one side of its center, an exhaust port, at the same side, a scavenge port and an air discharge port in communication with the air-transfer chamber and an air admission port disposed between the last named ports in communication with the air-receiving chamber, and at the opposite side of its center, a discharge ort and an admission port in communicatlon with the mixturetransfer chamber and an admission port positioned between the said ports in communication with the surge chamber, a source of a motive fluid in communication with the said surge "chamber and the said receiving -.chamber, and a valve for connecting the latter with either said source or the atmosphere.
- two cylinders each having at one side of its center a charge admission port and at the other side of the center an exhaust port, a scavenge port and'an air discharge port in communication with the latter by a by-pass, and an air admission port disposed between said communicating ports, anair-receiving chamber in communication withthe air admission ports of the two cylinders and provided by communicating jackets which partly surround the cylinders, a rotary shaft, and opposed pistons within said cylinders in operative connectlon with said-shaft.
- cylinders each having at one side of its center a chargeadmission port and at the other side of the center an exhaust port, a scavenge port and an air discharge port in communication with the latter by a by-pass, and an air admission port disposed, between said communicating ports, an air-receiving cham- -ber in communication with the air admission ports of the two cylinders, a rotary shaft, and opposed pistons within said cylillilders in operative connection with said s a t.
- a cylinder having at one side of its center an exhaust port and at the opposite side of the same, 'an-admission port and a therewith communicating discharge port, a rotary shaft, and opposed pistons in said cylinder having crank connections with said shaft, the said connections and the said ports being arranged so that when the exhaust opening is covered by movement of one of said pistons in one direction, the said discharge port is opened for the admission of a charge of explosive mixture between the pistons, by movement of the other piston in the same direction.
- a cylinder having at one side of its center, a charge-admission port and at the other side of its center, an exhaust port, a scavenge port and an air discharge port in communication with the latter by a by-pass, and an air admission port posltioned between the said communicating ports, a rotary shaft, and opposed pistons having unbalanced movements of equal length in the said cylinder, in operative connection with said shaft,
- the several ports being positioned so that during movement of the pistons, the said exhaust port and the said scavenge port are FRANK n. SUMMERIL.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
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- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
F. H. SUMMERIL.
INTERNAL COMBUSTION ENGINE.
APPLICATION FILED APR. 19, I91! Patented July 6, 1915.
3 SHEETS-SHEET l mmmm [.YVENTOR. 60/77/776/ 7 N h b X F \d\ H m NIH. N |1.|.. I H N N m H I Q "n g z H AMQL I\ 5 I l I I II I 2 MN m m h. QN%\ v n M WW 0% F. H. SUMMERIL. INTERNAL COMBUSTION ENGINE. APPLICATION FILED APR-197.1911.
Patented July 6, 1915.
3 SHEETS-.SHEET 2- ZW/TNESSES:
INVEN TOR. M. R
ATTORNEY.
F. H. SUMMERIL. INTERNAL COMBUSTION ENGINE.
APPLICATION FILED APR. 19, 1911.
Patented July 6, 1915.
3 SHEETSSHEET 3 Ti I Z5/UU 25 3 22 I 5028 ll 25 3 ZZ U Z8 JJ 25 LVVENTOR: F f/ Summl'I/ lV/T/VESSES:
FRANK H. SUMMERIL, F DENVER, COLORADO.
INTERNAL-COMBUSTION ENGINE.
iaaaaao.
To all whom it may concern Be it known that T, FRANK H. SUMMERIL, a citizen of the United States of America, residing at Denver, in the county of Denver and State of Colorado, have invented cer- 'tain new and useful Improvements in Internal-Combustion Engines, of which the following is a specification.
This invention relates to improvements in internal combustion engines of the type in which a pair of coactive pistons are disposed in one cylinder to be impelled in opposite directions by the explosion of an interposed charge of combustible gas.
- The principal object of my invention is to provide an engine of simple construction in which the opposed pistons in each cylinder have a relatively unbalanced movement for the purpose of timing the opening and closing periods of the admission and exhaust ports so as to prevent waste of explosive mixture. and to promote the thorough scavenging of the cylinder after each explosion.
The unbalanced movements of the pistons are attained by displacement of their crankconnections around the shaft, at an angle of less than one hundred and eighty degrees, whereby, when the two pistons have reached the end of their strokes, the said connections will extend approximately at equal angles at opposite sides of the dead centers in the crank-motion. Byreason of their unbalanced movements, the pistons will be at all times, in a position to effectively carry the crank shaft past its dead centers and the speed of the engine will thus be materially increased.
Further objects of my invention reside in the provision of a surge chamber in which the mixture obtained from the carbureter or other source of supply, is stored be-. fore being admitted into the part of the cylinder between the two pistons, for the purposes of relieving the carbureter of the detrimental jerks to which it is ordinarily subjected, of promoting the intimate intermixture of the explosive gas and oxygen and of heating the mixture by contact with the outer wall of the cylinder before being admitted into the part thereof in which the explosion takes place.
Another object of the invention is to provide means whereby the charge admitted into the cylinder at one time may be increased to approximately twice its volume, by adjustment of a valve ap lied between the Patented July b, 1915.
Serial No. 622,014.
carbureter and the cylinder, whenever an lncrease in the load on the engine, demands a proportionately greater impellent force.
The above and other minor objects all of which will fully appear in the following description, are attained by the mechanism llustrated in the accompanying drawings in the various views of which like parts are similarly designated, and in which,
Figure 1 represents a longitudinal sectional view of the engine, Fig. 2, a longitudinal section taken through one of the cylinders along the line 2-2, Fig. 1, the pistons having been omitted to more clearly show the positions of the various ports. Fig. 3, a composite view showing transverse sections taken respectively along the lines 33 and 5-5, Fig. 2, Fig. 4, a transverse section along the line 4-4:, Fig. 2, Figs. 5
to 12 inclusive, diagrammatic views showing the positions of the opposed pistons and their respective cranks, with relation to the exhaust and admission ports at the distinctive' points in the cycle of operations.
The engine, as shown in the drawings, operating on the well known two-cycle principle, is composed of two cylinders 2, each provided with two opposed pistons 3 and 4, the stems of which are, by means of link-connections 5 operatively associated with double cranks on a shaft 6 which is rotatably mounted between the two cylinders, in parallel relation to their axes. The cranks are preferably constructed in the form of disks 7 which have an oscillatory movement in crank-cases 8, between two collars 9 which are keyed to the shaft 6. I
wish it understood, however, that the crank connection between the shaft and the pistons may be, made of a character different from that shown in the drawings, and, specifically, do not form part, of the present invention.
The two cylinders 2,'which, as usual, are closed by means of heads 2, are provided at their ends with jackets which are horizontally divided into two compartments by I takes place and which, by means of a contive stroke of the respective piston 3, is conduit 13-is connected with the carbureter or other suitable supply of combustible gas.
'The separated upper compartments 14 at the same end of the cylinders each provide a transfer chamber through which the mixture compressed and displaced during the effecducted into the space between the two pistons. The connected lower compartments at the opposite end of the two cylinders constitutean air-receiving chamber 15 which may be connected with either the atmosphere orthe carbureter by the ad ustment of a three-way valve 16 applied at the intersection of. a conduit 17 wh ich opens into the chamber, and a pipe 38 which connects with the carbureter conduit 13, and the separated upper compartments 18 at the same end of the cylinders, each constitute an air-transfer chamber through which air compressed and displacedduring the effective-stroke of the respective piston 4 is conducted intothe space between the two pistons during vthescavenging period in the cycle of operations.
In engines of the single piston type the surge chamber a'nd' the air receiving chamber may be formed-either by enlargements of the lower compartments of the cylinder jackets or they may be providedby separate receptacles of suitable construction which are connected with the respective jacketcompartments by means of conduits.
:Inasmu'ch as in engines of the two-cylinder type theactions of the pistons in one cylinder are identical to those. of the pistons "in the other, it will only be necessary to explain in' thefollowing part of'the description, the operation of the "PI'SCOIIS of one cylinder independent from that of the pistons in the other. The mixture-receiving or surge-chamber-l2 connects with the interior of the cylinder bya plurality of ports 22 disposed at the end of the chamber remote from the adj acen't end. of the cylinder, and the mixture transfer-chamber- 14 connects with the interior of the cylinder, at one of its ends by 'meansiof a series of ports 23 through which the gases flow from the cylinderinto the said chamber during the outward stroke of the piston, and at itsopposite end by ports 24 through which the said gases'are discharged into the space between the pistons when the corresponding piston reaches. the end of its outward stroke. The
Having thus described the mechanical construction of my improved engine, I will now proceed to explain the operation thereof, reference being had to the diagrammatic views shown in Figs. 5 to 12 inclusive of the drawings. Commencing at the time the explosion of the gases in the compartment 30 takes place, when the pistons are substantially at theend of their inward strokes and the cranks extend at equal angles from the dead center, as shown in Fig. 5, it will be observed that the piston 4, whose crank-connection was forward of the dead center with relation to the direction of rotation of the shaft,'will uncover the exhaust ports 28 before the other piston has reached the admission ports 24, so that the exhaust of the spent gases will take place before a new charge is admitted, (see Fig. 6). The airinlet ports 25 are at this time covered and after the exhaust ports are partly opened,
the scavenge ports 27 are uncovered with the result that the air contained in the ,ylinder compartment 32 and the transfer chamber 18, which had been compressed during the outward movement of the piston past the ports 25, is forced into the space between the pistons, which thus is scavenged until during the return movement of the piston 4 the scavenge ports are again closed which occurs before the exhaust ports are completely covered, (see Figs. 7 and 8). Shortly before the last action takes place the mixture admission ports 24 are uncovered by the piston 3, which at the commencement of its outward movement had closed the ports 22 through which the mixture contained in the surge chamber had entered the cylindercompartment 31. The mixture contained within the said compartment and the transfer chamber 14, which was compressed during the outward movement of the piston, is thus forcibly introduced into the space between the two pistons until during the re turn stroke of the piston 3, the admission ports 24 are again closed when the charge contained between the two pistons is compressed by the movements of the latter toward the center of the cylinder, until they have reassumed their original position shown in Fig. 5, when it is ignited. The positions of the pistons shown in the last mentioned figure, have been referred to as being substantially at the end of the'inward strokes, for the reason that, as'shown in Figs. 11 and 12, the piston 4 in moving past the dead center momentarily approaches the center of the cylinder closer before it reaches the position which'it occupies when the explosion takes place. During the inward movements of the two pistons past the ports 22 and 25, new mixture and airare drawn into the chambers 12 and 15, and when the load on the engine increases, the volume of the charge may be instantlv augmented by connecting the air-receiving chamber 15 with the carbureter in place of with the open air by adjustment of the valve 16, when mixture will be introduced into the'space between the pistons through the scavenge-ports 27 as well as through the charge-admission ports 24.
Having thus described my invention what I claim and desire to secure by Letters-Patent is 1. In an internal combustion engine a cylinder having admission ports at opposite sides of its center and an exhaust port at one side of the same, a rotary shaft, opposed pistons within the said cylinder in operative connection with the said shaft, a source of motive fluid in continuous communication with one of said admission ports, and a valve-controlled connection between the said source and the other admission port.
2. In an internal combustion engine, a cylinder having admission ports at opposite sides of its center and an exhaust port at one side of the same, a rotary shaft, opposed pistons within the said cylinder in operative connection with the said shaftja source of motive fluid in communication with one of said admission ports, and means for connecting the other admission port with either the atmosphere or the said source.
8. In an internal combustion engine, a cylinder having at one side of its centera charge-admission port and at the other side of the center an exhaust port, a scavengeport and an air discharge port in continuous communication with the latter by a bypass, and an air admission port positioned between the said communicating ports, a rotary shaft, and opposed pistons having unbalanced movements of equal length within the said cylinder, in operative connection with the said shaft, the several ports being positioned so that during movement of the pistons the said exhaust port and the said scavenge port are uncovered and again covered before the admission port is opened for the admission of a fresh charge between the pistons.
4. In an internal combustion engine, a cylinder having at one side of its center a charge admission port and at the other side of the same, an exhaust port, a scavenge port and an air discharge port in continuous communication by a by-pass, and an air admission port positioned between the said communicating ports, a rotary shaft, opposed pistons within the said cylinder in operative connection with the said shaft, a source of motive fluid in connection with the charge-admission port, and means for connecting the air-admission portwith either the atmosphere or the said source.
5. In an internal combustion engine, inder having at one of its ends, a jacket partitioned into an air receiving chamber and an air transfer-chamber, a rotary shaft, and opposed pistons within the said cylinder in operative connection with the said shaft, said cylinder having at one side of its center a charge-admission port and at the opposite side of the center, an exhaust port, a scavenge port and an air-discharge port in communication with said transfer chamber, and an air-admission port disposed between the last named ports in communication with the said air receiving chamber.
6. In an internal combustion engine, a cylinder having jackets at opposite ends thereof, and each partitioned into two compartments, the compartments in one of said jackets constituting respectively a surge chamber and a mixture transfer chamber and those in the other jacket, an air receiving chamber and an air-transfer chamber, a rotary shaft, and opposed pistons having unbalanced movements within the cylinder in operative connection with said shaft, the said cylinder having at one side of its center an exhaust port, at the same side, a scavenge port and an air discharge port in a c'yl communication with the air-transfer cham- &
' chamber.
7. In an internal combustlon engine, a cylinder having jackets at opposite ends thereof, and each partitioned into two compartments, the compartments in one of said 1ackets constituting respectively a surge chamber and a mixture transfer chamber and those in the other jacket, an air receiving chamber.
andan air-transfer chamber, arotary shaft,
- and opposed pistons having unbalanced movements within the cylinder in operative connection with said shaft, the said cylinder having at one side of its center, an exhaust port, at the same side, a scavenge port and an air discharge port in communication with the air-transfer chamber and an air admission port disposed between the last named ports in communication with the air-receiving chamber, and at the opposite side of its center, a discharge ort and an admission port in communicatlon with the mixturetransfer chamber and an admission port positioned between the said ports in communication with the surge chamber, a source of a motive fluid in communication with the said surge "chamber and the said receiving -.chamber, and a valve for connecting the latter with either said source or the atmosphere.
8. In an internal combustion engine, two cylinders each having at one side of its center a charge admission port and at the other side of the center an exhaust port, a scavenge port and'an air discharge port in communication with the latter by a by-pass, and an air admission port disposed between said communicating ports, anair-receiving chamber in communication withthe air admission ports of the two cylinders and provided by communicating jackets which partly surround the cylinders, a rotary shaft, and opposed pistons within said cylinders in operative connectlon with said-shaft.
9. In an internal combustion engine, two
cylinders each having at one side of its center a chargeadmission port and at the other side of the center an exhaust port, a scavenge port and an air discharge port in communication with the latter by a by-pass, and an air admission port disposed, between said communicating ports, an air-receiving cham- -ber in communication with the air admission ports of the two cylinders, a rotary shaft, and opposed pistons within said cylillilders in operative connection with said s a t.
cylinder, a rotary shaft and a pair of opposed pistons of equal lengths .having un balanced movements of equal length within the said cylinder, in operative connection with the said shaft, the said cylinder having ports which are disposed to be covered and uncovered by the said pistons for the successive admission and discharge of fluid to and from the space between the pistons.
11. In an internal combustion engine, a cylinder having at one side of its center an exhaust port and at the opposite side of the same, 'an-admission port and a therewith communicating discharge port, a rotary shaft, and opposed pistons in said cylinder having crank connections with said shaft, the said connections and the said ports being arranged so that when the exhaust opening is covered by movement of one of said pistons in one direction, the said discharge port is opened for the admission of a charge of explosive mixture between the pistons, by movement of the other piston in the same direction.
12. In an internal combustion engine, a cylinder having at one side of its center, a charge-admission port and at the other side of its center, an exhaust port, a scavenge port and an air discharge port in communication with the latter by a by-pass, and an air admission port posltioned between the said communicating ports, a rotary shaft, and opposed pistons having unbalanced movements of equal length in the said cylinder, in operative connection with said shaft,
the several ports being positioned so that during movement of the pistons, the said exhaust port and the said scavenge port are FRANK n. SUMMERIL.
Witnessesi L. RHOADEB, G. RQLLANDET.
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US62201411A US1145820A (en) | 1911-04-19 | 1911-04-19 | Internal-combustion engine. |
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US62201411A US1145820A (en) | 1911-04-19 | 1911-04-19 | Internal-combustion engine. |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421868A (en) * | 1943-04-23 | 1947-06-10 | Ransom Y Bovee | Barrel type engine |
US2565272A (en) * | 1947-04-07 | 1951-08-21 | Steel Products Eng Co | Power gas generator, including crankless engine |
US2768616A (en) * | 1951-10-25 | 1956-10-30 | Thomas B Danckwortt | Two cycle opposed piston internal combustion engine |
US2875738A (en) * | 1948-10-13 | 1959-03-03 | Rieseler Helene | Two-stroke cycle internal combustion engine with opposed pistons |
US4996953A (en) * | 1990-04-02 | 1991-03-05 | Buck Erik S | Two plus two stroke opposed piston heat engine |
US7219633B1 (en) | 2005-03-21 | 2007-05-22 | Mcleod Robert A | Compression ignition rotating cylinder engine |
US20160265428A1 (en) * | 2013-10-22 | 2016-09-15 | Chris Kiarash Montebello | Rotary piston engine with external explosion/expansion chamber |
US20200063559A1 (en) * | 2018-08-22 | 2020-02-27 | Toyota Jidosha Kabushiki Kaisha | Opposed-piston engine |
-
1911
- 1911-04-19 US US62201411A patent/US1145820A/en not_active Expired - Lifetime
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421868A (en) * | 1943-04-23 | 1947-06-10 | Ransom Y Bovee | Barrel type engine |
US2565272A (en) * | 1947-04-07 | 1951-08-21 | Steel Products Eng Co | Power gas generator, including crankless engine |
US2875738A (en) * | 1948-10-13 | 1959-03-03 | Rieseler Helene | Two-stroke cycle internal combustion engine with opposed pistons |
US2768616A (en) * | 1951-10-25 | 1956-10-30 | Thomas B Danckwortt | Two cycle opposed piston internal combustion engine |
US4996953A (en) * | 1990-04-02 | 1991-03-05 | Buck Erik S | Two plus two stroke opposed piston heat engine |
US7219633B1 (en) | 2005-03-21 | 2007-05-22 | Mcleod Robert A | Compression ignition rotating cylinder engine |
US20160265428A1 (en) * | 2013-10-22 | 2016-09-15 | Chris Kiarash Montebello | Rotary piston engine with external explosion/expansion chamber |
US20200063559A1 (en) * | 2018-08-22 | 2020-02-27 | Toyota Jidosha Kabushiki Kaisha | Opposed-piston engine |
CN110857660A (en) * | 2018-08-22 | 2020-03-03 | 丰田自动车株式会社 | Opposed piston engine |
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