US1309891A - Compound piston for internal-combustion engines and the llkb - Google Patents
Compound piston for internal-combustion engines and the llkb Download PDFInfo
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- US1309891A US1309891A US1309891DA US1309891A US 1309891 A US1309891 A US 1309891A US 1309891D A US1309891D A US 1309891DA US 1309891 A US1309891 A US 1309891A
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- 150000001875 compounds Chemical class 0.000 title description 44
- 238000002485 combustion reaction Methods 0.000 title description 20
- 230000005540 biological transmission Effects 0.000 description 22
- 238000004880 explosion Methods 0.000 description 20
- 210000000707 Wrist Anatomy 0.000 description 12
- 238000010276 construction Methods 0.000 description 8
- 230000000875 corresponding Effects 0.000 description 4
- 238000003379 elimination reaction Methods 0.000 description 4
- VKYKSIONXSXAKP-UHFFFAOYSA-N Hexamethylenetetramine Chemical compound C1N(C2)CN3CN1CN2C3 VKYKSIONXSXAKP-UHFFFAOYSA-N 0.000 description 2
- 241000282619 Hylobates lar Species 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 230000000994 depressed Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000006011 modification reaction Methods 0.000 description 2
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
- F02B75/28—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
Definitions
- My principal object is to make a piston and piston transmission in two or more parts, each part having an independent stroke, the stroke of one part being ahead of the stroke of the succeeding part delivered at a different angle of thrust to the crank shaft, so as to split up the force of the explosion in internal combustion engines, overcome the dead center, avoid the liability of back-firing, and reduce the vibration, thereby dispensing with the necessity of a fly wheel, which as well known, serves to store energy which is drawn upon when the explosion takes place before the crank shaft has reached the dead center, thus reducing the change or direction of torque.
- Figure 1 is a vertical central section crosswise of the crank shaft and showing a compound piston and piston transmission embodying the principles of my invention, the view being taken on he line 11 of Fig. 2.
- Fig. 2 is a sectional detail on the line 2-2 of Fig. 1.
- Fig. 3 is a diagram illustrating the piston transmission to the crank shaft.
- Fig. 4 is'a side elevation upon an enlarged scale of the compound crank pin bearing.
- Fig. 5 is a sectional detail on the line 5-'5 of Fig. 4.
- Fig. 6 is a perspective of one of the connecting rods.
- Fig. 7 is a perspective of the inner compound piston member.
- Fig. 8 is a perspective of the outer compound'piston member and taken on the line 9-9 of Fig. 10.
- Fig. 9 is a view analogous to Fi 1 and showing a three part piston an piston transmission whereas Figs. 18 show a two part piston and piston transmission.
- Fig. 10 is a view analogous to Fig. 2 and taken on the line 1010 of Fig. 9.
- Fig. 11 is a sectional detail on the line 11-11 of Fig. 10.
- Fig. 12 is a view analogous to Fig. 3.
- Flg. 13 1s a view analogous to Fig. 12 and showing the parts on a quarter stroke
- Fig. 12 shows the parts passing the lar member 2.
- the inner member 1 is provided upon its periphery 3 with ring grooves 4 and when the rings are applied the memher 1 fits in the central opening 5 of the member 2 and the member 2 has a periphery 6 provided with ring grooves 7.
- the periphery 6 of the member 2 fits in the piston cylinder 8.
- the connecting rod 9 is inserted upwardly between internalbearings 10 and 11 of the member 1 and a hollow wrist pin 12 is in serted through the bearings 10 and 11 and through the bearing 13 in the upper end of the connecting rod 9.
- the member 2 is provided with a casing around the opening 5, said casing formin the cylinder 14 for the member 1, there being an annular chamber 15 around the cylinder 14, said chamber 15 being open at the bottom.
- the connecting rod 16 consists of two bars 17 and 18 connected by braces 19 and 20, said braces 19 and 20 being off-set to pass around the connecting rod 9, and bearings 21 and 22 are formed at the upper ends of the bars 17 and 18.
- the bearings-21 and 22 are inserted upwardly into the chamber 15 and a wrist pin 23 is inserted through the member-2 and through the bearings 21 and 22 and through the hollow 24 of the wrist pin 12.
- the hollow 24 is enough larger than the wrist pin 23 to allow the members 1 and 2 to move endwise relative to each other to the desired extent.
- the opening 5 is eccentric relative to the periphery 6 so as to ofl-set the center of the wrist pin 23 relative to the center of the wrist pin 12, thereby giving the connecting rods 9 and 16 different angularities relative to the crank shaft.
- the crank 25 of the crank shaft has the usual crank pin 26 and a compound connecting rod bearing 27 is mounted upon this crank pin.
- the compound connecting rod bearing 27 is a split sleeve having two concentric bearing portions 28 and 29 and an eccentric bearing portion 30.
- the split bearing 31 is formed upon the lower end of the connecting rod 9 and fits the eccentric bearing portion 30 and split bearings 32 and 33 are formed upon the lower ends of the bars 17 and 18 of the connecting rod 16 and fit the concentric bearing portions 28 and 29.
- Keys 34 and 35 are applied to key seats 36 and 37 in the bearings 32 and 33 and corresponding seats 38 and 39 in the bearing portions 28 and 29 so as to hold the compound bearing 27 from rotating relative to the connecting rod 16.
- the bearing 27 is set so that the center 40 of the eccentric portion 30 is substantially on a horizontal plane with the center 41 of the concentric portions 28 and 29, so that when the crank pin 26 is in its elevated position, as in Fig. 1, the center 40 will be ahead of the center 41 with the crank pin traveling in the direction indicated by the arrow 42, and then when the explosion takes place in the chamber 43 and the crank in 26 is close to or on the dead center the caring 30 will have passed the dead center and theimpulse of the explosion coming through the-member 1 and connecting rod 9 to the bearing 30 will assist in carrying the crank pin 26 over the dead center. I As shown in Fig.
- the parts 1 and 2 are off-set to the left while the centers 40 and 41 are off-set to the right, so that the efiective forces of the connecting rods 9 and 16 are crossed, the object being to split up the forces by the divergent angularities, reduce the strain at the point of passing the dead center, reduce the liability of backfiring, that is when the crank pin refuses to pass the dead center and goes backwardly, and reduce the vibration of the engine.
- Fig. 3 the compound piston is twisted a quarter turn relative to the crank shaft in order to show the connections.
- the center 41 is in a direct line between the center 44 of the crank shaft and the piston member 1 and on the dead center.
- the center 41 travels in the line-45 concentric to the crank shaft center 44 while the center 40 travels in. the line 46 eccentric to the center 44.
- the path of travel of the center 40 is considerably longer on the down stroke from the dead center line 47 than on the up stroke and the crankpin leverage is considerably greater.
- the compound piston consists of the central circular member 48, the intermediate annular member 49, and the outer annular member 50 all arranged concentrically and moving longitudinally. relative to each other.
- the crank shaft crank 51 has a compound:
- crank pin consisting-of the concentric bearing face 52, the intermediate eccentric bearing faces 53 and 54, and the outer eccentric bearing faces 55 and 56.
- the center 58 of the eccentric faces53 and 54 and the center 5,-9l'of the eccentric faces 55 and 56 are in a circumferential line with the center 57 atthe front when the crank shaft is moving in the direction indicated by the ar- -will be substantially flush on the faces of their heads.
- crank pin action is broken up into three different parts by the compound crank pin and the impact of the explosion in the chamber 64: is broken up into three diiferent parts by the members 48, 49 and 50 and transmitted to the compound crank pin from three different lines at three different times.
- An internal combustion engine comprising a cylinder, a combustion chamber at one end thereof, a plurality of pistons slid-. ably mounted upon each other, the crosssectional area of any of said pistons being at least-a major part of any other of said pistons, a crank shaft and connecting rods forming a compound transmission from the pistons to the crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being differently timed.
- An internal combustion engine comprising a cylinder, a combustion chamber at one end thereof, a plurality of pistons of substantially equal cross-sectional areas slidably mounted upon each other, a crank shaft, and connecting rods forming a compound transmission from the pistons to the crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being difierently timed.
- a cylinder a plurality of pistons mounted to reciprocate relative to each other therein, a crank shaft, and separate power transmission connecting rods varying in angularity connected to said pistons and to said crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being differently timed.
- An internal combustion engine comprising a cylinder, a combustion chamber at one end thereof, an annularv piston en aging said cylinder, a second piston mounte Within said first piston, the cross sectional areas of said pistons being substantially equal, a crank shaft, and independent transmission connecting rods connebtingsaid pistons to the crank shaft and so arranged that when said pistons are at the extreme end of the movements the lines of direction of the power transmitted to said crank shaft from said pistons pass on opposite sides of the center of the crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being differently timed.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Description
E. GRIFFITH.
COMPOUND PISTON FOR INTERNAL COMBUSTION ENGINES AND THE LIKE.
APPLICATION FILED JUNE 20, I918.
1,309,89 1 Patented July 15, 1919.
3 SHEETS'SHEET l.
WITNESS: 45. INVENTOR.
fi7rzasi'rafia 3k 44 i qw/w/w A TTORNE Y.
E. GRIFFITH.
COMPOUND PISTON FOR INTERNAL COMBUSTION ENGINES AND THE LIKE.
APPLSCATION FILED JUNE 20. I918.
1,399,89 1 Patvntcd July 15, 1919.
3 SHEETS-SHEET 2 Fi'yf W1 TNESS: I N VEN TOR A TTORNE Y.
E. GRIFFITH.
COMPOUND PISTON FOI' INTERNAL COMBUSTION ENGINES AND THE LIKE.
APPLICATION FILED JUNE-I20. I9I8.
Patent-(d July I5, 1919.
3 SHEETS-SHEET 3- W I TNESS:
A TTORNE Y.
ERNEST GRIFFITH, 0]? LONG BEACH, CALIFORNIA, ASSIGNOR 0F ONE-HALF T0 GEORGE D. GILMORE, 0]? LOS ANGELES, CALIFORNIA.
COMPOUND PISTON FOR INTERNAL-COMBUSTION ENGINES AND THE LIKE.
To all whom it may concern:
Be it known that I, ERNEST GRIFFITH, a citizen of the United States, residing at Long Beach, in the county of Los Angeles and State of California, have invented new and useful Improvements in Compound Pistons for Internal-Combustion Engines and the like, of which the following is a specification.
My principal object is to make a piston and piston transmission in two or more parts, each part having an independent stroke, the stroke of one part being ahead of the stroke of the succeeding part delivered at a different angle of thrust to the crank shaft, so as to split up the force of the explosion in internal combustion engines, overcome the dead center, avoid the liability of back-firing, and reduce the vibration, thereby dispensing with the necessity of a fly wheel, which as well known, serves to store energy which is drawn upon when the explosion takes place before the crank shaft has reached the dead center, thus reducing the change or direction of torque. v
Figure 1 is a vertical central section crosswise of the crank shaft and showing a compound piston and piston transmission embodying the principles of my invention, the view being taken on he line 11 of Fig. 2.
Fig. 2 is a sectional detail on the line 2-2 of Fig. 1.
Fig. 3 is a diagram illustrating the piston transmission to the crank shaft.
Fig. 4 is'a side elevation upon an enlarged scale of the compound crank pin bearing.
Fig. 5 is a sectional detail on the line 5-'5 of Fig. 4.
Fig. 6 is a perspective of one of the connecting rods.
Fig. 7 is a perspective of the inner compound piston member.
Fig. 8 is a perspective of the outer compound'piston member and taken on the line 9-9 of Fig. 10.
Fig. 9 is a view analogous to Fi 1 and showing a three part piston an piston transmission whereas Figs. 18 show a two part piston and piston transmission.
' Fig. 10 is a view analogous to Fig. 2 and taken on the line 1010 of Fig. 9.
Fig. 11 is a sectional detail on the line 11-11 of Fig. 10.
Specification of Letters Patent.
Patented J uly 15, 1919.
Application filed June 20, 1918. Serial No. 241,039.
Fig. 12 is a view analogous to Fig. 3. Flg. 13 1s a view analogous to Fig. 12 and showing the parts on a quarter stroke Whereas Fig. 12 shows the parts passing the lar member 2. The inner member 1 is provided upon its periphery 3 with ring grooves 4 and when the rings are applied the memher 1 fits in the central opening 5 of the member 2 and the member 2 has a periphery 6 provided with ring grooves 7. The periphery 6 of the member 2 fits in the piston cylinder 8.
The connecting rod 9 is inserted upwardly between internalbearings 10 and 11 of the member 1 and a hollow wrist pin 12 is in serted through the bearings 10 and 11 and through the bearing 13 in the upper end of the connecting rod 9. The member 2 is provided with a casing around the opening 5, said casing formin the cylinder 14 for the member 1, there being an annular chamber 15 around the cylinder 14, said chamber 15 being open at the bottom. The connecting rod 16 consists of two bars 17 and 18 connected by braces 19 and 20, said braces 19 and 20 being off-set to pass around the connecting rod 9, and bearings 21 and 22 are formed at the upper ends of the bars 17 and 18. The bearings-21 and 22 are inserted upwardly into the chamber 15 and a wrist pin 23 is inserted through the member-2 and through the bearings 21 and 22 and through the hollow 24 of the wrist pin 12. The hollow 24 is enough larger than the wrist pin 23 to allow the members 1 and 2 to move endwise relative to each other to the desired extent. The opening 5 is eccentric relative to the periphery 6 so as to ofl-set the center of the wrist pin 23 relative to the center of the wrist pin 12, thereby giving the connecting rods 9 and 16 different angularities relative to the crank shaft.
The crank 25 of the crank shaft has the usual crank pin 26 and a compound connecting rod bearing 27 is mounted upon this crank pin. The compound connecting rod bearing 27 is a split sleeve having two concentric bearing portions 28 and 29 and an eccentric bearing portion 30. The split bearing 31 is formed upon the lower end of the connecting rod 9 and fits the eccentric bearing portion 30 and split bearings 32 and 33 are formed upon the lower ends of the bars 17 and 18 of the connecting rod 16 and fit the concentric bearing portions 28 and 29. Keys 34 and 35 are applied to key seats 36 and 37 in the bearings 32 and 33 and corresponding seats 38 and 39 in the bearing portions 28 and 29 so as to hold the compound bearing 27 from rotating relative to the connecting rod 16.
In assembling the connecting rods 9 and 16 and the bearing 27 the bearing 27 is set so that the center 40 of the eccentric portion 30 is substantially on a horizontal plane with the center 41 of the concentric portions 28 and 29, so that when the crank pin 26 is in its elevated position, as in Fig. 1, the center 40 will be ahead of the center 41 with the crank pin traveling in the direction indicated by the arrow 42, and then when the explosion takes place in the chamber 43 and the crank in 26 is close to or on the dead center the caring 30 will have passed the dead center and theimpulse of the explosion coming through the-member 1 and connecting rod 9 to the bearing 30 will assist in carrying the crank pin 26 over the dead center. I As shown in Fig. 1 the parts 1 and 2 are off-set to the left while the centers 40 and 41 are off-set to the right, so that the efiective forces of the connecting rods 9 and 16 are crossed, the object being to split up the forces by the divergent angularities, reduce the strain at the point of passing the dead center, reduce the liability of backfiring, that is when the crank pin refuses to pass the dead center and goes backwardly, and reduce the vibration of the engine.
In Fig. 3 the compound piston is twisted a quarter turn relative to the crank shaft in order to show the connections. The center 41 is in a direct line between the center 44 of the crank shaft and the piston member 1 and on the dead center. The center 41 travels in the line-45 concentric to the crank shaft center 44 while the center 40 travels in. the line 46 eccentric to the center 44. The path of travel of the center 40 is considerably longer on the down stroke from the dead center line 47 than on the up stroke and the crankpin leverage is considerably greater. While the relative movements of the members 1 and 2' are only slight, still the impact of the explosion in the chamber 43 is communicated through the member 1 to the eccentric 30 and through the member 2 to the concentrics 28 and 29 and the impulses are delivered over separate lines to different parts and are communicated to the crank shaft at difierent angles and at difierent times. Especial attention is again called'to the fact that the eccentric 30 does not rotate and that its chief purpose is to off-set the centers40 and 41 and change the crank pin angularity. v
In the modification shown in Figs. 913 the compound piston consists of the central circular member 48, the intermediate annular member 49, and the outer annular member 50 all arranged concentrically and moving longitudinally. relative to each other.. The crank shaft crank 51 has a compound:
crank pin consisting-of the concentric bearing face 52, the intermediate eccentric bearing faces 53 and 54, and the outer eccentric bearing faces 55 and 56. Starting from the center 57 of the concentric bearing face 52, the center 58 of the eccentric faces53 and 54 and the center 5,-9l'of the eccentric faces 55 and 56 are in a circumferential line with the center 57 atthe front when the crank shaft is moving in the direction indicated by the ar- -will be substantially flush on the faces of their heads. I
If the parts are standing in the position shown in Figs. 9 and 12, at the time an explosion takes place in the chamber 64 the centers 57 and 58 have passed the dead center line and the center 59 is on the dead center. The impact of the explosion against the piston member 48 will be directed through the connecting rod 61 to the point 57 which is considerably beyond the dead center, and the impact of the explosion Will be communicated through the piston member 49 and connecting rod 62 to the point 58 which is also beyond the dead center, and only a small part of the impact of the explosion will be communicated through the piston rod 63 to the point 59 on the dead center, and the forces exerted at the'points 57 and 58 will easily carry the point 59 over the dead center. In this construction the impulse is broken up into three parts and one or more of the parts is devoted to carrying the other parts over the dead center.
relative to the member 49 and both members 48 and 49 are depressed relative to the member 50, and obviously on the other quarter,
turn the positions will bereversed},
In this construction the members 48, 49
the center 65 and the movements of the compound piston members 48, 49 and 50 are substantially equal but the corresponding movements do not take place in unison.
The crank pin action is broken up into three different parts by the compound crank pin and the impact of the explosion in the chamber 64: is broken up into three diiferent parts by the members 48, 49 and 50 and transmitted to the compound crank pin from three different lines at three different times.
Thus I have produced a compound piston and compound transmission from the piston to the crank shaft.
It is obvious that any desired number of cylinders may be used in connection with a single crank shaft, each cylinder or any desired number of cylinders being provided with compound pistons and compound transmissions.
. Among the leading advantages I expect to derive from this construction is the elimination of or reduction in the. weight of the fly wheel, the reduction of vibration, and the elimination of the tendency to back-fire. These features are especially desirable in aeroplane construction and are more or less desirable in other constructions such as automobiles, motor boats, and the like.
Various changes may be made without departing from the spirit of my invention as claimed.
I claim:
1. An internal combustion engine comprising a cylinder, a combustion chamber at one end thereof, a plurality of pistons slid-. ably mounted upon each other, the crosssectional area of any of said pistons being at least-a major part of any other of said pistons, a crank shaft and connecting rods forming a compound transmission from the pistons to the crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being differently timed. j
An internal combustion engine comprising a cylinder, a combustion chamber at one end thereof, a plurality of pistons of substantially equal cross-sectional areas slidably mounted upon each other, a crank shaft, and connecting rods forming a compound transmission from the pistons to the crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being difierently timed.
3. A cylinder, a plurality of pistons mounted to reciprocate relative to each other therein, a crank shaft, and separate power transmission connecting rods varying in angularity connected to said pistons and to said crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being differently timed.
4. An internal combustion engine comprising a cylinder, a combustion chamber at one end thereof, an annularv piston en aging said cylinder, a second piston mounte Within said first piston, the cross sectional areas of said pistons being substantially equal, a crank shaft, and independent transmission connecting rods connebtingsaid pistons to the crank shaft and so arranged that when said pistons are at the extreme end of the movements the lines of direction of the power transmitted to said crank shaft from said pistons pass on opposite sides of the center of the crank shaft, said connecting rods being of substantially the same lengths and the same strokes, the strokes being differently timed.
In testimony whereof I have signed my name to this specification.
' ERNEST GRIFFITH.
Publications (1)
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US1309891A true US1309891A (en) | 1919-07-15 |
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US1309891D Expired - Lifetime US1309891A (en) | Compound piston for internal-combustion engines and the llkb |
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Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421884A (en) * | 1944-05-08 | 1947-06-10 | Carl L Holmes | Parallel piston engine |
US2458111A (en) * | 1947-02-11 | 1949-01-04 | Soltesz Rudolph | Multiple piston for internalcombustion engines |
US2598630A (en) * | 1945-02-27 | 1952-05-27 | Glen W Winberg | Back-pressure valve |
US3312206A (en) * | 1964-12-09 | 1967-04-04 | Radovic Dusan | Reciprocating engines |
US4096835A (en) * | 1977-01-04 | 1978-06-27 | Charles Edward Lamont | Internal combustion engine method and apparatus |
US4359016A (en) * | 1979-08-13 | 1982-11-16 | Bachmann William V | Internal combustion engine |
US4383508A (en) * | 1978-03-30 | 1983-05-17 | Honda Giken Kogyo Kabushiki Kaisha | Internal combustion engine |
US4489681A (en) * | 1981-12-02 | 1984-12-25 | Jackson Francis W | Multiple piston expansion chamber engine |
US4570580A (en) * | 1981-12-02 | 1986-02-18 | Jackson Francis W | Multiple piston expansion chamber engine |
US4715328A (en) * | 1981-12-02 | 1987-12-29 | Jackson Francis W | Multiple piston expansion chamber engine |
DE4018524A1 (en) * | 1990-06-09 | 1991-12-12 | Gerhard Jedamski | Piston IC engine with double piston - has second piston which operates in central bore of main piston |
US5865092A (en) * | 1997-07-03 | 1999-02-02 | Woudwyk; Anthony D. | Engine connecting rod and double piston assembly |
US6752105B2 (en) * | 2002-08-09 | 2004-06-22 | The United States Of America As Represented By The Administrator Of The United States Environmental Protection Agency | Piston-in-piston variable compression ratio engine |
US20090101004A1 (en) * | 2007-10-19 | 2009-04-23 | Johnson Jerald L | Two part piston for an internal combustion engine |
WO2018151689A1 (en) * | 2017-02-18 | 2018-08-23 | Eden Gizem | Telescopic piston configuration for internal combustion engines |
-
0
- US US1309891D patent/US1309891A/en not_active Expired - Lifetime
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421884A (en) * | 1944-05-08 | 1947-06-10 | Carl L Holmes | Parallel piston engine |
US2598630A (en) * | 1945-02-27 | 1952-05-27 | Glen W Winberg | Back-pressure valve |
US2458111A (en) * | 1947-02-11 | 1949-01-04 | Soltesz Rudolph | Multiple piston for internalcombustion engines |
US3312206A (en) * | 1964-12-09 | 1967-04-04 | Radovic Dusan | Reciprocating engines |
US4096835A (en) * | 1977-01-04 | 1978-06-27 | Charles Edward Lamont | Internal combustion engine method and apparatus |
US4383508A (en) * | 1978-03-30 | 1983-05-17 | Honda Giken Kogyo Kabushiki Kaisha | Internal combustion engine |
US4359016A (en) * | 1979-08-13 | 1982-11-16 | Bachmann William V | Internal combustion engine |
US4489681A (en) * | 1981-12-02 | 1984-12-25 | Jackson Francis W | Multiple piston expansion chamber engine |
US4570580A (en) * | 1981-12-02 | 1986-02-18 | Jackson Francis W | Multiple piston expansion chamber engine |
US4715328A (en) * | 1981-12-02 | 1987-12-29 | Jackson Francis W | Multiple piston expansion chamber engine |
DE4018524A1 (en) * | 1990-06-09 | 1991-12-12 | Gerhard Jedamski | Piston IC engine with double piston - has second piston which operates in central bore of main piston |
US5865092A (en) * | 1997-07-03 | 1999-02-02 | Woudwyk; Anthony D. | Engine connecting rod and double piston assembly |
US6752105B2 (en) * | 2002-08-09 | 2004-06-22 | The United States Of America As Represented By The Administrator Of The United States Environmental Protection Agency | Piston-in-piston variable compression ratio engine |
US20090101004A1 (en) * | 2007-10-19 | 2009-04-23 | Johnson Jerald L | Two part piston for an internal combustion engine |
WO2018151689A1 (en) * | 2017-02-18 | 2018-08-23 | Eden Gizem | Telescopic piston configuration for internal combustion engines |
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