US2769435A - Two stroke cycle internal combustion engine with pump compression - Google Patents
Two stroke cycle internal combustion engine with pump compression Download PDFInfo
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- US2769435A US2769435A US213109A US21310951A US2769435A US 2769435 A US2769435 A US 2769435A US 213109 A US213109 A US 213109A US 21310951 A US21310951 A US 21310951A US 2769435 A US2769435 A US 2769435A
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- 230000006835 compression Effects 0.000 title description 25
- 238000007906 compression Methods 0.000 title description 25
- 238000002485 combustion reaction Methods 0.000 title description 15
- 239000000446 fuel Substances 0.000 description 30
- 239000004215 Carbon black (E152) Substances 0.000 description 3
- 125000004122 cyclic group Chemical group 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 229930195733 hydrocarbon Natural products 0.000 description 3
- 150000002430 hydrocarbons Chemical class 0.000 description 3
- 239000000203 mixture Substances 0.000 description 2
- RZZPDXZPRHQOCG-OJAKKHQRSA-O CDP-choline(1+) Chemical compound O[C@@H]1[C@H](O)[C@@H](COP(O)(=O)OP(O)(=O)OCC[N+](C)(C)C)O[C@H]1N1C(=O)N=C(N)C=C1 RZZPDXZPRHQOCG-OJAKKHQRSA-O 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000007865 diluting Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Images
Classifications
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- 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
- F02B1/00—Engines characterised by fuel-air mixture compression
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- 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
- F02B2700/02—Four stroke engines
- F02B2700/023—Four stroke engines with measures for charging, increasing the power
-
- 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
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
Definitions
- Figure l is a sectional elevation taken through cooperative fuel-combustion and air-compressing cylinders of the engine.
- Figure 2 is a fragmentary plan View taken at the line 2--2 in Figure l.
- Figure 3 is a partly sectional View taken at the line 3--3 in Figure 2.
- Figure 4 is a section taken at the broken line 4 4 in Figure 2.
- a divided cycle is used, with primary and secondary cylinders 1 and 14 respectively.
- the primary cylinders 1 compress air to the desired high pressure, forcing the air through a check valve 2 into and through a transfer passage 3 to the transfer valve 4 in the secondary cylinder head 5.
- a damper 7 provided in the air intake passage 8 to the head of the primary cylinder 1 is closable as a valve to shut off the air supply through the passage 8, whereby the outward (suction) stroke of the piston 9 in the cylinder 1 may create a high degree of vacuum in the cylinder until the piston uncovers the port 6 as the stroke ends.
- the damper 7 is arranged to be closed only during a starting of the engine when the engine parts are relatively cold, and the elect is to provide such a high velocity impact flow of air into the raried air of the cylinder through the open port 6 as the suction stroke ends as will so preheat the air charge in the cylinder that the addition to the air of the heat of compression in the succeeding compression stroke will provide the delivery of air to the secondary (power) cylinder 14 through the passage 3 at such a relatively high temperature that a starting of the cold engine may be readily effected without need for the more complicated auxiliary starting devices heretofore used in the art.
- the valve 7 is opened and left open, and the port 6 thereafter functions to insure the provision of the fullest possible charge of air at substantially atmospheric pressure in the chamber of the cylinder 1 at the end of each suction stroke.
- the primary piston 9 and the cylinder head 10 and the passage 3 may be appropriately insulated, as respectively indicated at 11 and 12 and 13, to provide for a maximum retention of the heat of compression provided with the air delivered directly through the passage 3 to the corresponding secondary cylinder 14 which comprises a working cylinder of the engine.
- the air intake Valve for the ICC passage 8 and the discharge valve 2 for the compressor' cylinder 1 are of the spring-loaded type, and are operative at ports in the cylinder head to reduce terminal (compression) clearance to a minimum, it being noted that the valve for the passage 8 is under mechanical control and that the valve 2 comprises a pressure-opened check valve.
- a working (secondary) cylinder 14 provides a combustion-and-expansion chamber having its capacity at the end of the power stroke greater than the capacity of the compression chamber of the compressor (primary) cylinder 1 at the end of an air-intake stroke, whereby the temperature and pressure of the exhaust gases are less than if the air compression ratio in the compressor equaled the working expansion ratio in the power cylinder, and an important improvement in the efficiency of the use of the hydro-carbon fuel results.
- the ratio of the capacity of the power cylinder to that of the compressor cylinder is approximately 1.5 to 1.
- valves 4 and 16 and 18 of the power cylinder are of the poppet type and respectively have usual springloaded stems 4 and 16' and 18' which are operative in appropriate cyclic synchronism from the engine shaft.
- This fuel-throttling control does not alter the compression ratio in the power cylinder as the power output of the engine varies.
- Combustion in the power cylinder 14 starts in that part of the mixture that had the best proportion of fuel and air, and continues as heated fresh air is supplied by the primary piston 1 through the open said transfer valve until transfer valve 4 closes, or the fuel content is consumed.
- the crank pins 23 are so arranged that the secondary piston 17 is traveling outward while the primary piston is still on the compression stroke supplying air to the secondary cylinder 14. l prefer about 40 lag in the primary crank pin.
- the action of the piston 9 of the air compressor cylinder 1 preferably lags behind the action of the piston 17 of the power cylinder 14 by about 40, this being accomplished in the present structure, in which the pistons of the respective cylinders are operative from the same crank pin, by disposing the unitarily related cylinders 1 and 14 to have their axes intersecting in the axis of the common crank shaft at an included angle of the order of 40, this relation being shown in Figure l of the drawings in which, in terms of the indicated direction of rotation of the crank shaft, the piston 17 has begun its working stroke and the cornpression stroke of the piston 9 remains to be completed, both by reason of the disposal of the common crank pin Y axis in the bisection line of said lag angle.
- crank shaft in accordance with the indicated arrange-Y ment of Figure l.
- the full compression of the cornbustion-supporting air before fuel is introduced into it permits the operation of the engine at an optimum comlression ratio which is greater than that possible in a working'cylinder in which fuel is added before compression is completed; the present power cylinder is able to operate at the relatively high compression ratio of about l2 to 1.
- the operation of this engine at such a high compression ratio is made possible Vby the novel feature that the fuel is introduced into the power cylinder as ex- Vhaust ends and before the precompressed and heated air is introduced from the air compressor 1.
- a power cylinder having a piston reciprocatively operative therein, an air compression cylinder having a piston reciprocatively operative therein, means providing a passage directly connecting the cylinders solely through their heads for a direct delivery of compressed air from the compression cylinder to the power cylinder, a normally closed springloaded pressure-controlled check valve operative inthe inlet end of said passage, a normally closed spring-loaded poppet valve operative at the discharge end of said passage, anrinlet port for fuel under pressure at the head of the power cylinder, a normally closed spring-loaded poppet valve operative at said fuel inlet port, and means arranged for actuation in cyclic synchronism with the movement of the piston of the power cylinder to successively open the fuel inlet valve and the air inlet valve when and after the piston has reached the limit of its stroke adjacent the head.
- a structure in accordance with claim l having a pump means supplying partially carbureted hydrocarbon fuel at the fuel inlet port whereby the compressed air subsequently received by the cylinder through the opened air inlet port is arranged to progressively supply a major portion of the required combustion-supporting air to the delivered fuel.
- a power cylinder having a piston reciprocatively operative therein, an air compression cylinder having a piston reciprocatively operative therein, means providing a passage directly connecting the cylinders solely through theirrheads for a direct delivery of compressed Vair from the compression cylinder to the power cylinder, a normally closed springloaded pressure-controlled check valve operative in the inlet end of said passage, a normally closedfspng-loaded poppet valve operative at the discharge'end of said passage, anV inlet port for fuel under pressure at the head of the power cylinder, a normally closed spring-loaded poppet valve operative at said fuel inlet port, an exhaust port provided in the head of the power cylinder, a normally closed spring-loaded poppet valve operative at said exhaust port, and mechanical means arranged for actuation in cyclic synchronism with the movement of the piston of the power cylinder to sequentially open and close the exhaust Valve as the piston approaches the end ofits stroke adjacent the cylinder head and to open the fuel inlet valve substantially
- a power cylinder having a piston operative therein, an air compressionV cylinder having a piston operative therein for providing compressed air at a relatively high pressure, means providing an air-delivery passage directly connecting the cylinders solely at their heads, normally closed check valves at the extremities of said passage, a normally open intake duct terminating at an intake port in the head of said air compression cylinder, a normally closed springloaded intake check valve at said intake port for opening during subatmospheric pressure conditions in the cylinder, a normally open valve in said duct for setting to shut off the air supply through'the duct during a starting of the engine, and an unvalved air intake port in -the cylinder side intermediately of its length.
- a structure in accordance with claim 4 having a pump means deriving partially carbureted hydrocarbon fuel from a carburetor and delivering the same at the fuel inlet port, and means beyond the pump adjustable to vary the amount of air in the carbureted fuel delivered at said fuel inlet port.
- a power cylinder having a piston operative therein, an air compressor cylinder having a piston operative therein for providing the power cylinder with solely compressed air at a relatively high pressure while retaining the heat of its compression, means providing anair-delivery passage directly connecting the cylinders at their head ends, normally closed check valves at the extremities of said passage, a duct providing justable choke valve in said duct for setting to shut oi the air supply through the Vduct during a starting of the engine and an unvalved air intake port in the side of the compressor and arranged for its uncovering by the retracted compressor piston while the ⁇ latter is at substantially the end of its intake stroke.
- a cylinder having a piston operative therein for providing compressed air at a relatively high pressure, means providing an air-delivery passage from the cylinder head, a normally closed pressurecontrolled check valve operative at the intake end of said passage, a normally open air supply duct terminating at a port in the head of said cylinder, a normally closed spring-loaded poppet valve operative at said port for opening during sub-atmospheric pressure conditions in the cylinder, an unvalved air supply port in the cylinder side intermediately of its length and arranged for its uncovering by the retracted piston for directly connecting the cylinder with the atmosphere for the admission of air to the cylinder between its head and the piston during a limited portion of the piston suction stroke, and a normally open shut-off valve in said air supply duct arranged for its setting to temporarily and fully shut oilE the air supply through the duct fora charging of the cylinder with air received solely through said side supply port and before compression.
- a power cylinder having a piston operative therein, an air compressor cylinder having a piston operative therein for providing the power cylinder With solely compressed air at a relatively high pressure which retains the heat of its compression, means providing an airdelivery passage directly connecting the cylinders at their closed spring-loaded intake check valve at said intakeV port for openingV during sub-atmospheric pressure conditions in the cylinder, a normally open valve in said duct for setting to'shut oif the air supply through the duct during a starting of the engine, and means operative to l initiate the delivery of carbureted fuel to the powerrcylinder at the end of the exhaust stroke of its piston and before the admission of the compressed air from the compressor cylinder to the power cylinder.
- a power cylinder having a piston operative therein in exhaust and Working strokes thereof, an air compression cylinder having a working space which is appreciably less than the Working space of the power cylinder and having a piston op erative therein with its suction and compression strokes of the same length as the strokes of the piston in the power cylinder, means providing an air-delivery passage directly connecting the cylinders solely at their heads, normally closed check valves at the extremities of said passage, an intake duct terminating at an intake port in the head of said air compression cylinder, a normally closed spring-loaded intake check valve at said intake port for opening during sub-atmospheric pressure conditions in the cylinder, and ⁇ an unvalved air intake port in the cylinder side intermediately of its length and directly connected with atmosphere.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
Nov. 6, 1956 c. E. cAss TWO STROKE CYCLE INTERNAL COMBUSTION ENGINE WITH PUMP COMPRESSION 2 Sheets-Sheet l Filed Feb. 28, 1951 r o @E 2 wwwa/A Isl l 1 INI" www ' l NVENTOR W4Q-u Nov. 6, 1956 c. E. cAss Two STROKE CYCLE INTERNAL coMBusTroN ENGINE WITH PUMP COR/[PRESSION 2 Sheets-Sheet; 2
Filed Feb. 28, 1951 INVENTOR United States Patent C) TWO STROKE CYCLE INTERNAL COMBUST ION ENGINE WITH PUMP COMPRESSIUN Charles E. Cass, Roseburg, Greg.
Application February 28, 1951, Serial No. 213,109
9 Claims. (Cl. 123-68) This invention relates to the production of power in internal combustion engines of the reciprocating piston type, arranged as shown in the accompanying drawings and more fully described as follows:
Its objectives are better fuel economy and the use of gasoline, oil fuel or alcohol in lightweight engines.
The invention possesses other objects and features of advantage, some of which, with the foregoing, will be set forth or be apparent in the following description thereof, and in the accompanying drawings, in which:
Figure l is a sectional elevation taken through cooperative fuel-combustion and air-compressing cylinders of the engine.
Figure 2 is a fragmentary plan View taken at the line 2--2 in Figure l.
Figure 3 is a partly sectional View taken at the line 3--3 in Figure 2.
Figure 4 is a section taken at the broken line 4 4 in Figure 2.
A divided cycle is used, with primary and secondary cylinders 1 and 14 respectively. The primary cylinders 1 compress air to the desired high pressure, forcing the air through a check valve 2 into and through a transfer passage 3 to the transfer valve 4 in the secondary cylinder head 5. I prefer that the primary cylinder have an auxiliary port 6 at the outer end of piston travel, to admit extra air.
A damper 7 provided in the air intake passage 8 to the head of the primary cylinder 1 is closable as a valve to shut off the air supply through the passage 8, whereby the outward (suction) stroke of the piston 9 in the cylinder 1 may create a high degree of vacuum in the cylinder until the piston uncovers the port 6 as the stroke ends. The damper 7 is arranged to be closed only during a starting of the engine when the engine parts are relatively cold, and the elect is to provide such a high velocity impact flow of air into the raried air of the cylinder through the open port 6 as the suction stroke ends as will so preheat the air charge in the cylinder that the addition to the air of the heat of compression in the succeeding compression stroke will provide the delivery of air to the secondary (power) cylinder 14 through the passage 3 at such a relatively high temperature that a starting of the cold engine may be readily effected without need for the more complicated auxiliary starting devices heretofore used in the art. After the started engine is running hot, the valve 7 is opened and left open, and the port 6 thereafter functions to insure the provision of the fullest possible charge of air at substantially atmospheric pressure in the chamber of the cylinder 1 at the end of each suction stroke.
The primary piston 9 and the cylinder head 10 and the passage 3 may be appropriately insulated, as respectively indicated at 11 and 12 and 13, to provide for a maximum retention of the heat of compression provided with the air delivered directly through the passage 3 to the corresponding secondary cylinder 14 which comprises a working cylinder of the engine. The air intake Valve for the ICC passage 8 and the discharge valve 2 for the compressor' cylinder 1 are of the spring-loaded type, and are operative at ports in the cylinder head to reduce terminal (compression) clearance to a minimum, it being noted that the valve for the passage 8 is under mechanical control and that the valve 2 comprises a pressure-opened check valve.
A working (secondary) cylinder 14 provides a combustion-and-expansion chamber having its capacity at the end of the power stroke greater than the capacity of the compression chamber of the compressor (primary) cylinder 1 at the end of an air-intake stroke, whereby the temperature and pressure of the exhaust gases are less than if the air compression ratio in the compressor equaled the working expansion ratio in the power cylinder, and an important improvement in the efficiency of the use of the hydro-carbon fuel results. In the present structure, the ratio of the capacity of the power cylinder to that of the compressor cylinder is approximately 1.5 to 1.
Part of the exhaust gas passes through ports 15 in the secondary cylinder at the outer end of piston travel, to give rapid exit of exhaust, and reduce heat load on exhaust valve, which opens after piston uncovers exhaust port 15. On the exhaust stroke, piston 17 travels almost to cylinder head 5 forcing out nearly all burned gas and leaving a very small combustion space, exhaust valve 16 closes before secondary piston 17 reaches inner end of piston travel, the fuel charge is admitted into the combustion chamber through valve 1S at or near inner end of secondary piston travel. Then compressed air charge is admitted into the combustion chamber through valve 4 mixing with the fuel thereby diffusing and diluting the fuel charge and rapidly bringing the mixture to high pressure, also adding some heat by impact of the air stream.
The valves 4 and 16 and 18 of the power cylinder are of the poppet type and respectively have usual springloaded stems 4 and 16' and 18' which are operative in appropriate cyclic synchronism from the engine shaft.
I prefer to supply the fuel for each power cylinder 14 from an individual pump, such as the piston pump 19, which draws partiallyV carbureted fuel from a carburetor (not shown) through a passage 20 provided with an adjustable control valve 21 which is cooperative with a valve in a branch passage 22 for varying the proportion of air in the air-borne fuel delivered to and from the pump 19 comprising the throttle control for the fuel supply to the power cylinder. This fuel-throttling control does not alter the compression ratio in the power cylinder as the power output of the engine varies.
Combustion in the power cylinder 14 starts in that part of the mixture that had the best proportion of fuel and air, and continues as heated fresh air is supplied by the primary piston 1 through the open said transfer valve until transfer valve 4 closes, or the fuel content is consumed. The crank pins 23 are so arranged that the secondary piston 17 is traveling outward while the primary piston is still on the compression stroke supplying air to the secondary cylinder 14. l prefer about 40 lag in the primary crank pin. The action of the piston 9 of the air compressor cylinder 1 preferably lags behind the action of the piston 17 of the power cylinder 14 by about 40, this being accomplished in the present structure, in which the pistons of the respective cylinders are operative from the same crank pin, by disposing the unitarily related cylinders 1 and 14 to have their axes intersecting in the axis of the common crank shaft at an included angle of the order of 40, this relation being shown in Figure l of the drawings in which, in terms of the indicated direction of rotation of the crank shaft, the piston 17 has begun its working stroke and the cornpression stroke of the piston 9 remains to be completed, both by reason of the disposal of the common crank pin Y axis in the bisection line of said lag angle.
crank shaft, in accordance with the indicated arrange-Y ment of Figure l. Y
In the present engine, the full compression of the cornbustion-supporting air before fuel is introduced into it permits the operation of the engine at an optimum comlression ratio which is greater than that possible in a working'cylinder in which fuel is added before compression is completed; the present power cylinder is able to operate at the relatively high compression ratio of about l2 to 1. The operation of this engine at such a high compression ratio is made possible Vby the novel feature that the fuel is introduced into the power cylinder as ex- Vhaust ends and before the precompressed and heated air is introduced from the air compressor 1. Also, noting by reference to the relation of parts shown in Figure l of the Y drawings, that the fuel valve has just closed and that the air supply valve from the compressor has just opened, it will be understood that combustion has been initiated by the cylinder pressure which it almost instantly created by the inow of hot` compressed Vair into the confined space between the piston and the cylinder head.
I claim:
l. In an internal Vcombustion engine, a power cylinder having a piston reciprocatively operative therein, an air compression cylinder having a piston reciprocatively operative therein, means providing a passage directly connecting the cylinders solely through their heads for a direct delivery of compressed air from the compression cylinder to the power cylinder, a normally closed springloaded pressure-controlled check valve operative inthe inlet end of said passage, a normally closed spring-loaded poppet valve operative at the discharge end of said passage, anrinlet port for fuel under pressure at the head of the power cylinder, a normally closed spring-loaded poppet valve operative at said fuel inlet port, and means arranged for actuation in cyclic synchronism with the movement of the piston of the power cylinder to successively open the fuel inlet valve and the air inlet valve when and after the piston has reached the limit of its stroke adjacent the head.
2. A structure in accordance with claim l having a pump means supplying partially carbureted hydrocarbon fuel at the fuel inlet port whereby the compressed air subsequently received by the cylinder through the opened air inlet port is arranged to progressively supply a major portion of the required combustion-supporting air to the delivered fuel. Y
, 3. In an internal combustion engine, a power cylinder having a piston reciprocatively operative therein, an air compression cylinder having a piston reciprocatively operative therein, means providing a passage directly connecting the cylinders solely through theirrheads for a direct delivery of compressed Vair from the compression cylinder to the power cylinder, a normally closed springloaded pressure-controlled check valve operative in the inlet end of said passage, a normally closedfspng-loaded poppet valve operative at the discharge'end of said passage, anV inlet port for fuel under pressure at the head of the power cylinder, a normally closed spring-loaded poppet valve operative at said fuel inlet port, an exhaust port provided in the head of the power cylinder, a normally closed spring-loaded poppet valve operative at said exhaust port, and mechanical means arranged for actuation in cyclic synchronism with the movement of the piston of the power cylinder to sequentially open and close the exhaust Valve as the piston approaches the end ofits stroke adjacent the cylinder head and to open the fuel inlet valve substantially at said end of the piston stroke and to finally open the'air inlet valve during a portion of the return stroke of the piston.
4. In an internal combustion engine, a power cylinder having a piston operative therein, an air compressionV cylinder having a piston operative therein for providing compressed air at a relatively high pressure, means providing an air-delivery passage directly connecting the cylinders solely at their heads, normally closed check valves at the extremities of said passage, a normally open intake duct terminating at an intake port in the head of said air compression cylinder, a normally closed springloaded intake check valve at said intake port for opening during subatmospheric pressure conditions in the cylinder, a normally open valve in said duct for setting to shut off the air supply through'the duct during a starting of the engine, and an unvalved air intake port in -the cylinder side intermediately of its length.
5. A structure in accordance with claim 4 having a pump means deriving partially carbureted hydrocarbon fuel from a carburetor and delivering the same at the fuel inlet port, and means beyond the pump adjustable to vary the amount of air in the carbureted fuel delivered at said fuel inlet port. i
6. In an internal combustion engine, a power cylinder having a piston operative therein, an air compressor cylinder having a piston operative therein for providing the power cylinder with solely compressed air at a relatively high pressure while retaining the heat of its compression, means providing anair-delivery passage directly connecting the cylinders at their head ends, normally closed check valves at the extremities of said passage, a duct providing justable choke valve in said duct for setting to shut oi the air supply through the Vduct during a starting of the engine and an unvalved air intake port in the side of the compressor and arranged for its uncovering by the retracted compressor piston while the `latter is at substantially the end of its intake stroke. p
7. In an air compressor, a cylinder having a piston operative therein for providing compressed air at a relatively high pressure, means providing an air-delivery passage from the cylinder head, a normally closed pressurecontrolled check valve operative at the intake end of said passage, a normally open air supply duct terminating at a port in the head of said cylinder, a normally closed spring-loaded poppet valve operative at said port for opening during sub-atmospheric pressure conditions in the cylinder, an unvalved air supply port in the cylinder side intermediately of its length and arranged for its uncovering by the retracted piston for directly connecting the cylinder with the atmosphere for the admission of air to the cylinder between its head and the piston during a limited portion of the piston suction stroke, and a normally open shut-off valve in said air supply duct arranged for its setting to temporarily and fully shut oilE the air supply through the duct fora charging of the cylinder with air received solely through said side supply port and before compression.
8. In an internal combustion engine of the two-stroke J cycle type, a power cylinder having a piston operative therein, an air compressor cylinder having a piston operative therein for providing the power cylinder With solely compressed air at a relatively high pressure which retains the heat of its compression, means providing an airdelivery passage directly connecting the cylinders at their closed spring-loaded intake check valve at said intakeV port for openingV during sub-atmospheric pressure conditions in the cylinder, a normally open valve in said duct for setting to'shut oif the air supply through the duct during a starting of the engine, and means operative to l initiate the delivery of carbureted fuel to the powerrcylinder at the end of the exhaust stroke of its piston and before the admission of the compressed air from the compressor cylinder to the power cylinder.
9. In an internal combustion engine, a power cylinder having a piston operative therein in exhaust and Working strokes thereof, an air compression cylinder having a working space which is appreciably less than the Working space of the power cylinder and having a piston op erative therein with its suction and compression strokes of the same length as the strokes of the piston in the power cylinder, means providing an air-delivery passage directly connecting the cylinders solely at their heads, normally closed check valves at the extremities of said passage, an intake duct terminating at an intake port in the head of said air compression cylinder, a normally closed spring-loaded intake check valve at said intake port for opening during sub-atmospheric pressure conditions in the cylinder, and `an unvalved air intake port in the cylinder side intermediately of its length and directly connected with atmosphere.
References Cited in the tile of this patent UNITED STATES PATENTS 543,094 Hopkins July 23, 1895 6 Niebling May 25, Mewes Sept. 26, Bronder Apr. 30, Schumm et al June 4, Reichenbach Sept. 10, Wallmann July 7, Brandstetter et al. Ian. 26, Johnson Apr. 27, Bolton Dec. 25, Wolfard June 3, Ensign a May 5, Dodge Dec. 13, Maniscalco Oct. 27, Javal May 30, Rose Aug.V 28, Mallory Apr. 6,
FOREIGN PATENTS Switzerland Nov. 28, Great Britain July 7,
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US213109A US2769435A (en) | 1951-02-28 | 1951-02-28 | Two stroke cycle internal combustion engine with pump compression |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US213109A US2769435A (en) | 1951-02-28 | 1951-02-28 | Two stroke cycle internal combustion engine with pump compression |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2769435A true US2769435A (en) | 1956-11-06 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US213109A Expired - Lifetime US2769435A (en) | 1951-02-28 | 1951-02-28 | Two stroke cycle internal combustion engine with pump compression |
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| US (1) | US2769435A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2873574A (en) * | 1956-05-16 | 1959-02-17 | Clara M Long | Combination hot air and internal combustion engine |
| US4344405A (en) * | 1980-12-22 | 1982-08-17 | Zaharis Edward J | Internal combustion engine |
| US7121232B1 (en) * | 1999-10-25 | 2006-10-17 | Timo Tapani Janhunen | Method in an internal combustion engine and an internal combustion engine |
| US20090199829A1 (en) * | 2003-06-20 | 2009-08-13 | Branyon David P | Split-Cycle Four-Stroke Engine |
| US20130319380A1 (en) * | 2012-05-30 | 2013-12-05 | GM Global Technology Operations LLC | Integrated intake manifold and compressor |
| US20190078510A1 (en) * | 2017-09-12 | 2019-03-14 | James T. Ganley | High-Efficiency Two-Stroke Internal Combustion Engine |
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| US733350A (en) * | 1897-10-15 | 1903-07-07 | Wallmann Engine Company | Internal-combustion engine. |
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| US2873574A (en) * | 1956-05-16 | 1959-02-17 | Clara M Long | Combination hot air and internal combustion engine |
| US4344405A (en) * | 1980-12-22 | 1982-08-17 | Zaharis Edward J | Internal combustion engine |
| US7121232B1 (en) * | 1999-10-25 | 2006-10-17 | Timo Tapani Janhunen | Method in an internal combustion engine and an internal combustion engine |
| US20090199829A1 (en) * | 2003-06-20 | 2009-08-13 | Branyon David P | Split-Cycle Four-Stroke Engine |
| US8006656B2 (en) * | 2003-06-20 | 2011-08-30 | Scuderi Group, Llc | Split-cycle four-stroke engine |
| US20130319380A1 (en) * | 2012-05-30 | 2013-12-05 | GM Global Technology Operations LLC | Integrated intake manifold and compressor |
| US9103304B2 (en) * | 2012-05-30 | 2015-08-11 | GM Global Technology Operations LLC | Integrated intake manifold and compressor |
| US20190078510A1 (en) * | 2017-09-12 | 2019-03-14 | James T. Ganley | High-Efficiency Two-Stroke Internal Combustion Engine |
| US10352233B2 (en) * | 2017-09-12 | 2019-07-16 | James T. Ganley | High-efficiency two-stroke internal combustion engine |
| EP3665374A4 (en) * | 2017-09-12 | 2021-04-14 | Ganley, James, T. | HIGH EFFICIENCY TWO STROKE INTERNAL COMBUSTION ENGINE |
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