US2395110A - Two-cycle engine - Google Patents
Two-cycle engine Download PDFInfo
- Publication number
- US2395110A US2395110A US535974A US53597444A US2395110A US 2395110 A US2395110 A US 2395110A US 535974 A US535974 A US 535974A US 53597444 A US53597444 A US 53597444A US 2395110 A US2395110 A US 2395110A
- Authority
- US
- United States
- Prior art keywords
- cylinder
- piston
- exhaust
- inlet
- exhaust port
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000007789 gas Substances 0.000 description 18
- 238000001816 cooling Methods 0.000 description 4
- 239000000446 fuel Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000002000 scavenging effect Effects 0.000 description 2
- 230000005465 channeling Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000266 injurious effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000010408 sweeping Methods 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
- F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
- F02B25/14—Engines characterised by using fresh charge for scavenging cylinders using reverse-flow scavenging, e.g. with both outlet and inlet ports arranged near bottom of piston stroke
- F02B25/18—Engines characterised by using fresh charge for scavenging cylinders using reverse-flow scavenging, e.g. with both outlet and inlet ports arranged near bottom of piston stroke the charge flowing upward essentially along cylinder wall adjacent the inlet ports, e.g. by means of deflection rib on piston
-
- 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
- This invention relates to gas engines of the two cycle type and has for its object the construction and'organization of the parts in a manner to obtain improved efllciency in operation, economy in manufacture and durability in use.
- a particular feature of improvement is in the provision of means for guarding against the injurious eiIects from the hot exhaust gases at certain vital areas which when overheated reduce the efficiency of operation and shorten the life oi the parts.
- a further object is to obtain better scavenging of the cylinder by the discharge of the spent gases without undue mixing thereof with the incoming fresh charge and to accomplish this by a relatively simple and inexpensive modification of the piston head in combination with a special arrangement and location of the inlet and exhaust ports.
- a further object is to provide in an engine having inlet and exhaust ports at the same side of the cylinder and uncovered by the piston simultaneously or in overlapping sequence, means for channeling the incoming flow of fresh gas largely separate from the exhaust gas until said incoming gas builds up a pressure at the opposite side of the cylinder for sweeping out the last remnants of the spent gases.
- Fig. i is a vertical section of so much of the engine cylinder and associated parts as is necessary for understanding of the present invention
- Fig. 2 is a horizontal section through the cylinder on line 2-4 Fig. 1;
- Fig. 3 is a fragmentary vertical section through the cylinder wall on line M Fig. 2 adjacent an inlet port and showing the piston at the top of the exhaust port;
- Fig. 4 is a detail section through a top part of the cylinder on line 4--4 Fig. 2 to show the overhanging lip of the baflle wall.
- the cylinder of the engine comprises the main casing I provided with cooling fins 2 and'a head 3 bolted thereto as shown.
- the usual ignition device 4 is mounted through the cylinder head.
- the cylinder casing is preferably provided with a metal liner 5 forming an inner cylindrical wall for said cylinder within which reciprocates the piston 6 having its usual connecting rod I.
- the lower part of the engine is not shown since this ill said exhaust port 8.
- these two inlet ports are on the same level with each other but are preferably located entirely below the exhaust port. by which is meant that the top edge of each inlet port is slightly below the bottom edge of the exhaust port.
- the piston is designed to uncover both'the exhaust port and the inlet ports during the lower end or dwell portion of its outward stroke.
- the solid head or top ll of the piston is gouged out from the top and sides into lower step portions l2 and i3, one at each side.
- each of the lower step portions l2 and i3 being exposed at opposite sides of the piston are designed to register respectively with the inlet ports 9 and II] for a similar purpose.
- the threshold of each lower step such as l4 and I5 is a suillcient'distance below the top H of the piston so that said inlet *ports will be completely uncovered by said lower steps at the same time that the exhaust port is completely uncovered by the top I I of the piston, namely at the lower dead center of the piston stroke.
- the exhaust port start its opening phase slightly in advance of the opening of the inlet ports and for this purpose the lower steps are designed with the drop distance below the top'as shown and the top edges of said inlet ports are at a short distance below the bottom edge of the exhaust port as shown in the drawing.
- Each of the lower steps II and i2 is shaped in the nature of a ramp sloping upwardly from its lowermost part at the threshold l4 and I5 respectively to the top H of the piston at the other side thereof remote from the exhaust port.
- Inlet fuel passages 15 and I! may be formed as cored-out portions of the cylinder casing as shown so as to lead from the lower crank chamber (not shown) upwardly to communicate respectively with each inlet port 9 and In.
- Other and different forms of inlet fuel conduits leading to the inlet ports may be provided if desired. It will be noted that inlet charge of gaseous fuel is directed by its inlet port or ports horizontally across the threshold of the respective step H or I and will im-' pinge against the inner side wall such as 22 of said step (see Fig. 4).
- This wall 22 will direct the flow of the inlet charge toward the side of the cylinder which is remote from the exhaust port.
- the latter is preferably formed with an overhanging lip 23 (see Fig.4).
- the exhaust pipe or manifold I 8 extends as shown in Fig. 1 through a cutaway portion of the cylinder case without coming in direct contact therewith and is held firmly abutted against the inner liner 5 of said cylinder.
- Lugs 24 remote from the inner abutting end of said exhaust manifold l8 are provided as shown whereby the manifold may be securely fastened to the engine case I by bolts 25.
- An air space or clearance is thus provided between said exhaust pipe and cylinder case I in the vicinity of said exhaust opening.
- the purpose of this construction is to offer as much resistance as possible to the conduction of heat from the hot exhaust gases directly into the cylinder case I.
- This area of the cylinder case in the vicinity of the exhaust pipe or manifold is one of the most diflicult parts of the engineto keep from becoming overheated, and the means herein disclosed will in large part remedy this trouble.
- This cooling effect will be greatly enhanced by having the cooling air draft through the fins 2 in a horizontal direction transversely across the exhaust pipe 18.
- the piston is provided with the usual piston rings such as 20 and 2! and it will be noted that the uppermost piston ring 20 can be no higher than slightly below the threshold l4 and I5 of the lower step portions of said piston.
- This conditional circumstance of my design locates the piston ring 20 considerably below the top H of the piston, with the result that when said top ll of the piston begins to uncover the exhaust port (see Fig. 3) the uppermost piston ring 20 has 5 type of engine the uppermost piston ring will be exposed to a direct contact with said hot gases of the exhaust when the exhaust port is partly opened by the piston and the extreme heat from such direct contact in a short time destroys the 10 usefulness of said uppermost piston ring.
- the incoming charge of gas will be directed by the ramps l2 and I3 toward the opposite side of the cylinder and with an upward sweep toward the top of the cylinder where the streams Join together and create a pressure for 20pushing out the spent gases through the exhaust port 8. It will be observed as indicated by the small arrows that the incoming streams of gas are guided in a direction generally opposite to that of the outgoing gas stream but are prevented from directly mixing with said outgoing gas stream by the baffle side walls of each ramp portion l2 and I3. By this means a cleaner fresh charge is introduced into the cylinder and a more complete discharge of the spent gases i effected than in usual engines of this type.
- a two cycle engine comprising a cylinder having a main casing with cooling means for said casing and a metallic liner forming an inner wall for said cylinder, said liner having an exhaust port therethrough arranged for being uncovered by a piston reciprocable in said cylinder and an exhaust pipe extended through said main casing of the cylinder without substantial contact therewith and held down directly against said inner liner of the cylinder adjacent the exhaust port for conducting away the exhaust gases from the interior of said cylinder and thereby preventing the hot exhaust gases from making contact with any part of said cylinder casing.
Description
Feb. 19, 1946. M FORREST 2,395,110
TWO CYCLE ENGINE Filed May 17, '1944 INVENTOR MAR/1 A. fb/wfsr BY www- ATTORNEYS Patented Feb. 19, 1946 UNITED STATES PATENT orrlcs TWO-CYCLE ENGINE Mark L. Forrest, Framingliam, Mass. Application May 17, 1944, Serial No. 535,974
1 Claim.
This invention relates to gas engines of the two cycle type and has for its object the construction and'organization of the parts in a manner to obtain improved efllciency in operation, economy in manufacture and durability in use.
A particular feature of improvement is in the provision of means for guarding against the injurious eiIects from the hot exhaust gases at certain vital areas which when overheated reduce the efficiency of operation and shorten the life oi the parts.
A further object is to obtain better scavenging of the cylinder by the discharge of the spent gases without undue mixing thereof with the incoming fresh charge and to accomplish this by a relatively simple and inexpensive modification of the piston head in combination with a special arrangement and location of the inlet and exhaust ports.
A further object is to provide in an engine having inlet and exhaust ports at the same side of the cylinder and uncovered by the piston simultaneously or in overlapping sequence, means for channeling the incoming flow of fresh gas largely separate from the exhaust gas until said incoming gas builds up a pressure at the opposite side of the cylinder for sweeping out the last remnants of the spent gases.
Further objects and advantages of my invention will become apparent from the following specification taken in connection with the accompanying drawing which shows a preferred embodiment of my invention and in which:
Fig. i is a vertical section of so much of the engine cylinder and associated parts as is necessary for understanding of the present invention;
Fig. 2 is a horizontal section through the cylinder on line 2-4 Fig. 1;
Fig. 3 is a fragmentary vertical section through the cylinder wall on line M Fig. 2 adjacent an inlet port and showing the piston at the top of the exhaust port; and
Fig. 4 is a detail section through a top part of the cylinder on line 4--4 Fig. 2 to show the overhanging lip of the baflle wall.
Referring more particularly to the drawing the cylinder of the engine comprises the main casing I provided with cooling fins 2 and'a head 3 bolted thereto as shown. The usual ignition device 4 is mounted through the cylinder head. The cylinder casing is preferably provided with a metal liner 5 forming an inner cylindrical wall for said cylinder within which reciprocates the piston 6 having its usual connecting rod I. The lower part of the engine is not shown since this ill said exhaust port 8. Considering the engine as in upright position these two inlet ports are on the same level with each other but are preferably located entirely below the exhaust port. by which is meant that the top edge of each inlet port is slightly below the bottom edge of the exhaust port.
The piston is designed to uncover both'the exhaust port and the inlet ports during the lower end or dwell portion of its outward stroke. For this purpose the solid head or top ll of the piston is gouged out from the top and sides into lower step portions l2 and i3, one at each side.
of the centrally located unrelieved top portion H. The central top portion ll of the piston registers with the exhaust port 8'so that this part of the piston covers and uncovers said exhaust port while each of the lower step portions l2 and i3 being exposed at opposite sides of the piston are designed to register respectively with the inlet ports 9 and II] for a similar purpose. As shown in the drawing the threshold of each lower step such as l4 and I5 is a suillcient'distance below the top H of the piston so that said inlet *ports will be completely uncovered by said lower steps at the same time that the exhaust port is completely uncovered by the top I I of the piston, namely at the lower dead center of the piston stroke. However it is preferable to have the exhaust port start its opening phase slightly in advance of the opening of the inlet ports and for this purpose the lower steps are designed with the drop distance below the top'as shown and the top edges of said inlet ports are at a short distance below the bottom edge of the exhaust port as shown in the drawing.
Each of the lower steps II and i2 is shaped in the nature of a ramp sloping upwardly from its lowermost part at the threshold l4 and I5 respectively to the top H of the piston at the other side thereof remote from the exhaust port.
It will be observed from Fig. 2 that these ramps converge toward one another from their lower to their upper ends, the latter merging into the top surface II of the piston. Inlet fuel passages 15 and I! may be formed as cored-out portions of the cylinder casing as shown so as to lead from the lower crank chamber (not shown) upwardly to communicate respectively with each inlet port 9 and In. Other and different forms of inlet fuel conduits leading to the inlet ports may be provided if desired. It will be noted that inlet charge of gaseous fuel is directed by its inlet port or ports horizontally across the threshold of the respective step H or I and will im-' pinge against the inner side wall such as 22 of said step (see Fig. 4). This wall 22 will direct the flow of the inlet charge toward the side of the cylinder which is remote from the exhaust port. As a further hindrance to the flow of inlet gas over the top edge of said wall 22, the latter is preferably formed with an overhanging lip 23 (see Fig.4).
The exhaust pipe or manifold I 8 extends as shown in Fig. 1 through a cutaway portion of the cylinder case without coming in direct contact therewith and is held firmly abutted against the inner liner 5 of said cylinder. Lugs 24 remote from the inner abutting end of said exhaust manifold l8 are provided as shown whereby the manifold may be securely fastened to the engine case I by bolts 25. An air space or clearance is thus provided between said exhaust pipe and cylinder case I in the vicinity of said exhaust opening. The purpose of this construction is to offer as much resistance as possible to the conduction of heat from the hot exhaust gases directly into the cylinder case I. This area of the cylinder case in the vicinity of the exhaust pipe or manifold is one of the most diflicult parts of the engineto keep from becoming overheated, and the means herein disclosed will in large part remedy this trouble. This cooling effect will be greatly enhanced by having the cooling air draft through the fins 2 in a horizontal direction transversely across the exhaust pipe 18.
The piston is provided with the usual piston rings such as 20 and 2! and it will be noted that the uppermost piston ring 20 can be no higher than slightly below the threshold l4 and I5 of the lower step portions of said piston. This conditional circumstance of my design locates the piston ring 20 considerably below the top H of the piston, with the result that when said top ll of the piston begins to uncover the exhaust port (see Fig. 3) the uppermost piston ring 20 has 5 type of engine the uppermost piston ring will be exposed to a direct contact with said hot gases of the exhaust when the exhaust port is partly opened by the piston and the extreme heat from such direct contact in a short time destroys the 10 usefulness of said uppermost piston ring.
The scavenging operation of my engine will be clearly understood from the foregoing description but may be briefly reviewed as follows:
When the exhaust and inlet ports are opened,
16 as in Fig. 1, the incoming charge of gas will be directed by the ramps l2 and I3 toward the opposite side of the cylinder and with an upward sweep toward the top of the cylinder where the streams Join together and create a pressure for 20pushing out the spent gases through the exhaust port 8. It will be observed as indicated by the small arrows that the incoming streams of gas are guided in a direction generally opposite to that of the outgoing gas stream but are prevented from directly mixing with said outgoing gas stream by the baffle side walls of each ramp portion l2 and I3. By this means a cleaner fresh charge is introduced into the cylinder and a more complete discharge of the spent gases i effected than in usual engines of this type.
It will be understood that the present disclosure and specific description of a suitable embodiment for-carrying out my invention is for purposes of illustration and that equivalent variations thereof may be employed within the scope of the invention as hereinafter claimed.
What I claim is:
A two cycle engine comprising a cylinder having a main casing with cooling means for said casing and a metallic liner forming an inner wall for said cylinder, said liner having an exhaust port therethrough arranged for being uncovered by a piston reciprocable in said cylinder and an exhaust pipe extended through said main casing of the cylinder without substantial contact therewith and held down directly against said inner liner of the cylinder adjacent the exhaust port for conducting away the exhaust gases from the interior of said cylinder and thereby preventing the hot exhaust gases from making contact with any part of said cylinder casing.
MARK L. FORREST.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US535974A US2395110A (en) | 1944-05-17 | 1944-05-17 | Two-cycle engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US535974A US2395110A (en) | 1944-05-17 | 1944-05-17 | Two-cycle engine |
Publications (1)
Publication Number | Publication Date |
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US2395110A true US2395110A (en) | 1946-02-19 |
Family
ID=24136584
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US535974A Expired - Lifetime US2395110A (en) | 1944-05-17 | 1944-05-17 | Two-cycle engine |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2720195A (en) * | 1954-04-16 | 1955-10-11 | Gen Motors Corp | Two-cycle engine |
US2737171A (en) * | 1952-11-13 | 1956-03-06 | Torre Pier Luigi | Cylinders of two-cycle motors |
US3242913A (en) * | 1963-04-24 | 1966-03-29 | Max G Fiedler | Compression ignition engine |
US4016850A (en) * | 1974-02-22 | 1977-04-12 | Brunswick Corporation | Ported cylinder construction for a two-cycle engine |
US4191156A (en) * | 1976-12-30 | 1980-03-04 | Piaggio & C. S.P.A. | Two-stroke, water-cooled internal combustion engine having the cylinder liners removable from the cylinder block |
US4793305A (en) * | 1987-07-16 | 1988-12-27 | Dresser Industries, Inc. | High turbulence combustion chamber for turbocharged lean burn gaseous fueled engine |
-
1944
- 1944-05-17 US US535974A patent/US2395110A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2737171A (en) * | 1952-11-13 | 1956-03-06 | Torre Pier Luigi | Cylinders of two-cycle motors |
US2720195A (en) * | 1954-04-16 | 1955-10-11 | Gen Motors Corp | Two-cycle engine |
US3242913A (en) * | 1963-04-24 | 1966-03-29 | Max G Fiedler | Compression ignition engine |
US4016850A (en) * | 1974-02-22 | 1977-04-12 | Brunswick Corporation | Ported cylinder construction for a two-cycle engine |
US4191156A (en) * | 1976-12-30 | 1980-03-04 | Piaggio & C. S.P.A. | Two-stroke, water-cooled internal combustion engine having the cylinder liners removable from the cylinder block |
US4793305A (en) * | 1987-07-16 | 1988-12-27 | Dresser Industries, Inc. | High turbulence combustion chamber for turbocharged lean burn gaseous fueled engine |
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