US3351045A - Two-cycle internal combustion engine - Google Patents
Two-cycle internal combustion engine Download PDFInfo
- Publication number
- US3351045A US3351045A US627211A US62721167A US3351045A US 3351045 A US3351045 A US 3351045A US 627211 A US627211 A US 627211A US 62721167 A US62721167 A US 62721167A US 3351045 A US3351045 A US 3351045A
- Authority
- US
- United States
- Prior art keywords
- cylinder
- cylinders
- crankcase
- fuel
- internal combustion
- 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
- 238000002485 combustion reaction Methods 0.000 title description 4
- 239000000203 mixture Substances 0.000 description 14
- 230000000875 corresponding effect Effects 0.000 description 7
- 230000006835 compression Effects 0.000 description 6
- 238000007906 compression Methods 0.000 description 6
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 230000002000 scavenging effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
-
- 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
-
- 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
- F02B2700/00—Measures relating to the combustion process without indication of the kind of fuel or with more than one fuel
- F02B2700/03—Two stroke engines
- F02B2700/037—Scavenging or charging channels or openings
Definitions
- This invention relates to a two-cycle internal combustion engine having one or more pairs of cylinders and in which the cylinders of each pair are arranged in siamese fashion with the crankcase for one cylinder adjacent the side of the other cylinder in each instance, the engine having two separate synchronized crankshafts which may drive either a common output shaft or separate driveshafts, one for each crankshaft, geared to a common output shaft.
- the invention utilizes crankcase compression for charging the cylinders with fuel-air mixture and in carrying out the invention the fuel-air mixture from one crankcase is fed directly through a port in the common wall into the adjacent cylinder.
- the invention eliminates the conventional transfer passage between the crank chambers and the cylinders.
- the resulting reduction in crankcase compression volume improves the eifective compression ratio of the pistons in the crank chambers, which in turn, results in greater pumping capacity per cubic inch of piston displacement.
- each crank chamber greatly reduces the time required to transfer the fuel air charge. This is particularly important at higher r.p.m. when, in order to achieve efiicient cylinder charging, large volumes of fuel-air vapor must be transferred from the crank chambers into the cylinders in the very short intervals during which the transfer ports are open.
- the siamesed configuration is more compact, more practical in dimensional proportions and is structurally more rigid and lighter in weight than an in-line or V engine of the same piston displacement and the same number of cylinders.
- FIGURE 1 is a schematic section taken on a transverse plane axially of a pair of siamesed cylinders
- FIG. 2 is a schematic side elevation of the engine of FIGURE 1 with a portion of the housing removed;
- FIG. 3 is a schematic elevation looking toward the end of one of the cylinders.
- the engine illustrated comprises two cylinders 1 and 2 arranged in siamesed fashion with the crankcase 3 for cylinder 1 adjacent to cylinder 2, and with the crankcase 4 for cylinder 2 adjacent to cylinder 1.
- Cylinder 1 and crankcase 3 have a common wall 5 between the same, and cylinder 2 and crankcase 4 have a common wall 6 between the same.
- a piston 7 operates in cylinder 1 and a piston 8 operates in cylinder 2 to drive the corresponding crankshafts 9 and 10 by means of corresponding connecting rods 11 and 12.
- the fuel-air mixture is supplied to the crankcases by any suitable carburetor means such as the carburetors 13 and 14 for the respective crankcases 3 and 4.
- the fuelair mixture is compressed in both crankcases 3 and 4 as the pistons 7 and 8 move outwardly of their respective cylinders and toward the corresponding crankcases.
- Exhaust from cylinder 1 is through a discharge port 17 in the cylinder wall opposite to transfer port 15, and exhaust from cylinder 2 is through a discharge port 18 in the cylinder wall opposite to transfer port 16.
- each piston 7 and 8 is shaped to provide a shield 19 between the corresponding exhaust and transfer or intake ports which directs the flow of compressed fuelair mixture upwardly and facilitates the escape of exhaust gases from the cylinder during scavenging.
- crankshafts 9 and 10 may be geared to drive a central output shaft 20, as shown, or a separate drive shaft for each crankshaft may be geared to a common output shaft.
- Suitable water cooling passages are provided for the engine, and also suitable ignition means are provided as indicated by the spark plugs 21.
- the invention as illustrated eliminates long transfer passages for the fuel-air mix and reduces the compression volume of the two crankcases 3 and 4 which thereby results in improved pumping action for the fuel-air mix and generally higher compression ratios for the engine.
- the short transfer ports 15 and 16 eliminate corners which generally increase the friction to the flow of fuel air mix to the cylinders, and provide a direct charging of the individual cylinders from the corresponding adjacent crankcase.
- the direct transfer from one crankcase to the adjacent cylinder substantially reduces the time required for charging the cylinder with the fuel-air mix, a feature particularly important at high speeds.
- the invention may be employed either in engines employing cross-scavenging of the cylinders as shown in FIG. 1, or in engines employing loop-scavenging of the cylinders, not shown.
- the engine is more compact than conventional twocycle engines, and has greater structural rigidity.
- a two-cycle internal combustion engine utilizing crankcase compression of fuel-air mixture and comprising a pair of cylinders disposed in a parallel siamese arrangement with the separate crankcase for each cylinder adjacent to and having a common wall with the opposite cylinder, one. or more exhaust ports for each cylinder in a wall other than the corresponding common wall, one or more transfer intake ports for each cylinder directly through the corresponding common wall, a piston in each cylinder adapted to uncover and cover said ports in the cycle of operation of the engine, and means driven by said pistons and connecting the same whereby the recip- 4 rocal cycle of said pistons are correlated to provide for substantially simultaneous firing of the cylinders.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
Nov. 7, 1967 c. KNUTH 3,351,045
TWO-CYCLE INTERNAL GOMBUSTION ENGINE Filed March 50, 1967 Fig. 3 INVENTOR CARL NUTH fla wa 5% Afl'arneys United States Patent 3,351,045 TWO-CYCLE INTERNAL COMBUSTION ENGINE Carl Knuth, Fond du Lac, Wis., assignor to Brunswick Corporation, Chicago, 11]., a corporation of Delaware Filed Mar. 30, 1967, Ser. No. 627,211 1 Claim. (Cl. 123-52) ABSTRACT OF THE DISCLOSURE A two-cycle engine in which the cylinders are arranged in siamese pairs with a common wall between the crankcase of one cylinder and the opposite cylinder in each instance. A transfer opening through the common wall providcs for admission of fuel-air mixture directly from the crankcase of one to the opposite cylinder. The pistons operate separate synchronized crankshafts in response to simultaneous firing of the fuel-air mixture in the two cylinders.
This invention relates to a two-cycle internal combustion engine having one or more pairs of cylinders and in which the cylinders of each pair are arranged in siamese fashion with the crankcase for one cylinder adjacent the side of the other cylinder in each instance, the engine having two separate synchronized crankshafts which may drive either a common output shaft or separate driveshafts, one for each crankshaft, geared to a common output shaft.
The invention utilizes crankcase compression for charging the cylinders with fuel-air mixture and in carrying out the invention the fuel-air mixture from one crankcase is fed directly through a port in the common wall into the adjacent cylinder.
The invention eliminates the conventional transfer passage between the crank chambers and the cylinders. The resulting reduction in crankcase compression volume improves the eifective compression ratio of the pistons in the crank chambers, which in turn, results in greater pumping capacity per cubic inch of piston displacement.
The elimination of the transfer passages and the direct induction of the fuel-air charge from each crank chamber directly into its adjacent cylinder minimizes flow friction and turbulence, thus further increasing the volumetric efiiciency of the engine.
The proximity of each crank chamber to its co-acting cylinder greatly reduces the time required to transfer the fuel air charge. This is particularly important at higher r.p.m. when, in order to achieve efiicient cylinder charging, large volumes of fuel-air vapor must be transferred from the crank chambers into the cylinders in the very short intervals during which the transfer ports are open.
The siamesed configuration is more compact, more practical in dimensional proportions and is structurally more rigid and lighter in weight than an in-line or V engine of the same piston displacement and the same number of cylinders.
The accompanying drawing illustrates the best mode presently contemplated by the inventor for carrying out the invention.
In the drawing:
FIGURE 1 is a schematic section taken on a transverse plane axially of a pair of siamesed cylinders;
FIG. 2 is a schematic side elevation of the engine of FIGURE 1 with a portion of the housing removed; and
FIG. 3 is a schematic elevation looking toward the end of one of the cylinders.
The engine illustrated comprises two cylinders 1 and 2 arranged in siamesed fashion with the crankcase 3 for cylinder 1 adjacent to cylinder 2, and with the crankcase 4 for cylinder 2 adjacent to cylinder 1.
Cylinder 1 and crankcase 3 have a common wall 5 between the same, and cylinder 2 and crankcase 4 have a common wall 6 between the same.
A piston 7 operates in cylinder 1 and a piston 8 operates in cylinder 2 to drive the corresponding crankshafts 9 and 10 by means of corresponding connecting rods 11 and 12.
The fuel-air mixture is supplied to the crankcases by any suitable carburetor means such as the carburetors 13 and 14 for the respective crankcases 3 and 4. The fuelair mixture is compressed in both crankcases 3 and 4 as the pistons 7 and 8 move outwardly of their respective cylinders and toward the corresponding crankcases.
When piston 7 uncovers a transfer port 15 through the common wall 5 compressed fuel-air mix is forced from crankcase 4 through the port into cylinder 1 to charge the same. At the same time piston 8 uncovers a transfer port 16 through the common wall 6 and compressed fuelair mix is forced from crankcase 3 through the port into cylinder 2 to charge the same.
Exhaust from cylinder 1 is through a discharge port 17 in the cylinder wall opposite to transfer port 15, and exhaust from cylinder 2 is through a discharge port 18 in the cylinder wall opposite to transfer port 16.
The top of each piston 7 and 8 is shaped to provide a shield 19 between the corresponding exhaust and transfer or intake ports which directs the flow of compressed fuelair mixture upwardly and facilitates the escape of exhaust gases from the cylinder during scavenging.
The crankshafts 9 and 10 may be geared to drive a central output shaft 20, as shown, or a separate drive shaft for each crankshaft may be geared to a common output shaft.
Suitable water cooling passages, not shown, are provided for the engine, and also suitable ignition means are provided as indicated by the spark plugs 21.
The invention as illustrated eliminates long transfer passages for the fuel-air mix and reduces the compression volume of the two crankcases 3 and 4 which thereby results in improved pumping action for the fuel-air mix and generally higher compression ratios for the engine.
The short transfer ports 15 and 16 eliminate corners which generally increase the friction to the flow of fuel air mix to the cylinders, and provide a direct charging of the individual cylinders from the corresponding adjacent crankcase.
The direct transfer from one crankcase to the adjacent cylinder substantially reduces the time required for charging the cylinder with the fuel-air mix, a feature particularly important at high speeds.
The invention may be employed either in engines employing cross-scavenging of the cylinders as shown in FIG. 1, or in engines employing loop-scavenging of the cylinders, not shown.
The engine is more compact than conventional twocycle engines, and has greater structural rigidity.
Various modes of carrying out the invention are contemplated as being within the scope of the following claim particularly pointing out and distinctly claiming the sub ject matter which is regarded as the invention.
I claim:
A two-cycle internal combustion engine utilizing crankcase compression of fuel-air mixture and comprising a pair of cylinders disposed in a parallel siamese arrangement with the separate crankcase for each cylinder adjacent to and having a common wall with the opposite cylinder, one. or more exhaust ports for each cylinder in a wall other than the corresponding common wall, one or more transfer intake ports for each cylinder directly through the corresponding common wall, a piston in each cylinder adapted to uncover and cover said ports in the cycle of operation of the engine, and means driven by said pistons and connecting the same whereby the recip- 4 rocal cycle of said pistons are correlated to provide for substantially simultaneous firing of the cylinders.
No references cited.
5 MARK M. NEWMAN, Primary Examiner.
WENDELL E. BURNS, Examiner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US627211A US3351045A (en) | 1967-03-30 | 1967-03-30 | Two-cycle internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US627211A US3351045A (en) | 1967-03-30 | 1967-03-30 | Two-cycle internal combustion engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3351045A true US3351045A (en) | 1967-11-07 |
Family
ID=24513700
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US627211A Expired - Lifetime US3351045A (en) | 1967-03-30 | 1967-03-30 | Two-cycle internal combustion engine |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3351045A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3384058A (en) * | 1967-04-21 | 1968-05-21 | Brunswick Corp | Overhead camshaft engine |
| US4938175A (en) * | 1987-11-12 | 1990-07-03 | Offmar S.N.C. Di Matta Emiliano & Matta Luigi | Engine, particularly for ultralight aircraft |
| ITRM20130356A1 (en) * | 2013-06-21 | 2014-12-22 | Ingranaggio Di Marco De Martino | COMPACT VOLUMETRIC INTERNAL COMBUSTION ENGINE. |
-
1967
- 1967-03-30 US US627211A patent/US3351045A/en not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| None * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3384058A (en) * | 1967-04-21 | 1968-05-21 | Brunswick Corp | Overhead camshaft engine |
| US4938175A (en) * | 1987-11-12 | 1990-07-03 | Offmar S.N.C. Di Matta Emiliano & Matta Luigi | Engine, particularly for ultralight aircraft |
| ITRM20130356A1 (en) * | 2013-06-21 | 2014-12-22 | Ingranaggio Di Marco De Martino | COMPACT VOLUMETRIC INTERNAL COMBUSTION ENGINE. |
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