EP2841737A1 - Piston engine with a variable compression ratio - Google Patents
Piston engine with a variable compression ratioInfo
- Publication number
- EP2841737A1 EP2841737A1 EP13723531.3A EP13723531A EP2841737A1 EP 2841737 A1 EP2841737 A1 EP 2841737A1 EP 13723531 A EP13723531 A EP 13723531A EP 2841737 A1 EP2841737 A1 EP 2841737A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sleeve
- cylinder liner
- cylinder
- engine
- piston
- 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.)
- Granted
Links
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
- F02B75/04—Engines with variable distances between pistons at top dead-centre positions and cylinder heads
- F02B75/041—Engines with variable distances between pistons at top dead-centre positions and cylinder heads by means of cylinder or cylinderhead positioning
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D15/00—Varying compression ratio
- F02D15/04—Varying compression ratio by alteration of volume of compression space without changing piston stroke
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/04—Engines with variable distances between pistons at top dead-centre positions and cylinder heads
Definitions
- the present invention relates to a piston engine with a variable compression ratio, as defined in the preamble of claim 1 .
- variable compression ratio With a variable compression ratio, the performance of a piston engine can be optimized in different operating conditions. Especially in engines in which different fuels are used, the possibility to use different compression ratios provides significant benefits.
- Different solutions are known for implementing the variable compression ratio.
- the cylinder head can be provided with an additional volume that can be selectively used.
- a problem with this solution is that the crevice volume is increased, which leads to increased emissions.
- Another solution is to use a cylinder liner that can be moved in relation to the engine block. With this solution, no additional crevice volume is created, and the need for additional equipment in the cylinder head can be avoided.
- many of the prior art solutions are complicated and the adjustment of the compression ratio takes a lot of time.
- the object of the present invention is to provide an improved piston engine with a variable compression ratio.
- the engine comprises an engine block, at least one cylinder, which cylinder is provided with a cylinder liner that is arranged partly inside the engine block, a reciprocating piston that is arranged inside the cylinder liner, a cylinder head that is arranged above the cylinder liner and attached to the engine block, and means for adjusting the volume of the combustion chamber of the cylinder by moving the cylinder liner in its axial direction in relation to the engine block.
- the means for adjusting the volume of the combustion chamber comprise a rotatable sleeve that is arranged around the upper end of the cylinder liner, and means for transforming the rotational movement of the sleeve into linear movement of the cylinder liner.
- the compression ratio can be changed very quickly. In some cases, it can take even less than a minute to adjust the compression ratio.
- the sleeve is provided with a thread on its inner circumference and the outer circumference of the cylinder liner is provided with a thread that is engaged with the thread of the sleeve. With this arrangement, the compression ratio can be adjusted even steplessly.
- an end surface of the sleeve is provided with alternating elevated sections and cuttings, and the engine is provided with a mating surface that is provided with similar alternating elevated sections and cuttings and engaged with the end surface of the sleeve.
- the mating surface can be arranged in a ring that is arranged around the cylinder liner.
- the ring can be attached to the cylinder liner between the sleeve and the upper end of the cylinder liner or between the engine block and the sleeve.
- the engine is provided with means for rotating the sleeve.
- the rotating means can comprise a hydraulic cylinder and a push rod that is connected to the piston of the hydraulic cylinder.
- the cylinder head is attached to the engine block with hydraulic locking means.
- the hydraulic locking means enable much quicker adjustment of the compression ratio than conventional bolts.
- Fig. 1 shows a piston engine with a variable compression ratio.
- Fig. 2 shows a cross-sectional view of the engine of Fig. 1 .
- Fig. 3 shows a cross-sectional view of the engine of Fig. 1 when a different compression ratio is in use.
- Fig. 4 shows means for rotating an adjustment sleeve according to an embodiment of the invention.
- Fig. 5 shows the means for rotating an adjustment sleeve when a different compression ratio is in use.
- Fig. 6 shows parts that are used for moving a cylinder liner.
- Fig. 7 shows a cross-sectional view of a piston engine according to another embodiment of the invention.
- Fig. 8 shows the engine of Fig. 7 when a different compression ratio is in use.
- figure 1 is shown a simplified illustration of a piston engine according to an embodiment the invention.
- three cylinders 2 are shown, but the engine can comprise any reasonable number of cylinders.
- the engine of figure 1 is an in-line engine, but the engine could also be, for instance, a V-engine.
- the engine is a large internal combustion engine, such as a main or an auxiliary engine of a ship or an engine that is used at a power plant for producing electricity.
- FIGS. 2 and 3 show a cross-sectional view of the engine of figure 1 , but the description below applies also to the embodiment of figures 7 and 8.
- the engine comprises an engine block 1 , into which the cylinders 2 are arranged.
- Each cylinder 2 of the engine is provided with a cylinder liner 2a that is arranged partly inside the engine block 1 .
- the upper end of the cylinder liner 2a is above the upper surface of the engine block 1 .
- a reciprocating piston 3 is arranged inside the cylinder liner 2a.
- the piston 3 is connected to a crankshaft (not shown) that is supported with bearings to the engine block 1 .
- a cylinder head 4 is arranged above the cylinder liner 2a and rests against the upper end of the cylinder liner 2a.
- the cylinder head 4 is attached to engine block 1 by means of hydraulic locking means 13. Because of the hydraulic locking means 13, the cylinder head 4 can be quickly released from the engine block 1 . If quick release is not needed, also conventional bolts can be used for attaching the cylinder head 4 to the engine block 1 .
- the walls of the cylinder 2, the bottom surface of the cylinder head 4 and the piston 5 define a combustion chamber 5.
- the engine is provided with means for adjusting the volume of the combustion chamber 5 of the cylinder 2 by moving the cylinder liner 2a in its axial direction in relation to the engine block 1 .
- the means for adjusting the volume of the combustion chamber 5 comprise a rotatable sleeve 6 that is arranged around the upper end of the cyl- inder liner 2a, and means for transforming the rotational movement of the sleeve 6 into linear movement of the cylinder liner 2a.
- the sleeve 6 rests against the engine block 1 .
- the construction of the sleeve 6 is shown in more detail in figure 6.
- the upper end surface of the sleeve 6 is provided with alternating elevated sections 6a and cuttings 6b. Each elevated section 6a is connected to the adjacent cuttings 6b with chamfered sections 6c.
- the engine is also provided with a mating surface 10, which is provided with similar elevated sections 7a and cuttings 7b. Also the elevated sections 7a of the mating surface 10 are connected to the adjacent cuttings 7b with chamfered sections 7c.
- the mating surface 10 is part of a ring 7, which is shown in more detail in figure 6.
- the mating surface 10 of the ring 7 is arranged against the upper surface of the sleeve 6.
- the ring 7 is arranged between the sleeve 6 and the upper end of the cylinder liner 2a.
- the upper end of the cylinder liner 2a is provided with an elbow 2c, which rests against the other surface of the ring 7.
- the ring 7 thus supports the cylinder lin- er 2a in the vertical direction.
- the ring 7 is attached to the cylinder liner 2a in a rotationally fixed manner, and the ring 7 can thus not rotate in relation to the cylinder liner 2a.
- the cylinder liner 2a In figure 2, the cylinder liner 2a is in its lowermost position, and consequently the volume of the combustion chamber 5 is as small as possible.
- a high compression mode of the engine is thus in use. In the high compression mode, the elevated sections 7a of the ring 7 are against the cuttings 6b of the sleeve 6.
- the cylinder head 4 needs to be released from the engine block 1 .
- the hydraulic locking means 13 are thus unlocked, and the cylinder head 4 is allowed to move in the vertical direction.
- the sleeve 6 is rotated.
- the chamfered sections 6c of the sleeve 6 become engaged with the chamfered sections 7c of the ring 7.
- the rotating sleeve 6 thus starts pushing the ring 7 upwards, which ring 7 pushes the cylinder liner 2a upwards.
- the rotational movement of the sleeve 6 is thus transformed into linear movement of the cylinder liner 2a.
- the sleeve 6 and the ring 7 can also be provided with elevated sections 6a, 6b of different heights. This kind of arrangement allows more than two different compression ratios. When the sleeve 6 is rotated by an angle that corresponds the width of one elevated section 6a, the compression ratio is changed by one step. Further rotation of the sleeve 6 causes an additional change of the compression ratio.
- the ring 7 could be arranged between the engine block 1 and the sleeve 6.
- the mating surface 10 of the ring 7 would face the sleeve 6, and that end surface of the sleeve 6 which is provided with the elevated sections 6a and the cuttings 6b would be arranged against the mating surface 10 of the ring 7.
- the sleeve 6 would have a plain surface against the elbow 2c of the cylinder liner 2a.
- the ring 7 would be attached in a rotationally fixed manner to the engine block 1 .
- valve mechanism needs to be adapted to the moving cylinder head 4, for instance by using hydraulic valve actuators instead of mechanical valve opening arrange- ments.
- FIGS 7 and 8 is shown a piston engine according to another embodiment of the invention.
- the engine is provided with a rotatable sleeve 6 and means for transforming the rotational movement of the sleeve 6 into linear movement of the cylinder liner 2a.
- the inner circumference of the sleeve 6 is provided with a thread 8.
- a similar thread 9 is arranged on the outer circumference of the cylinder liner 2a, and the thread 9 of the cylinder liner 2a is engaged with the thread 8 of the sleeve 6.
- the cylinder liner 2a is fixed in a rotationally fixed manner to the engine block 1 .
- FIGS 4 and 5 are shown means for rotating the sleeve 6.
- the rotating means can be used in connection with both the embodiments of figures 2 and 3 and figures 7 and 8.
- the rotating means comprise a hydraulic cylinder 1 1 and a push rod 12.
- the hydraulic cylinder 1 1 is attached to the engine block 1 and the push rod 12 is connected to the piston 1 1 a of the hydraulic cylinder 1 1 .
- the sleeve 6 comprises an arm 14, to which the push rod 12 is pivoted.
- the hydraulic cylinder 1 1 needs to be provided with a control arrangement that allows several different positions of the piston 1 1 a.
- a certain position of the piston 1 1 a of the hydraulic cylinder 1 1 corresponds to a certain volume of the combustion chamber 5.
- some kind of a gear mechanism can be used for rotating the sleeve.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FI20125437A FI20125437A7 (en) | 2012-04-23 | 2012-04-23 | Piston engine with a variable compression ratio |
| PCT/FI2013/050437 WO2013160541A1 (en) | 2012-04-23 | 2013-04-19 | Piston engine with a variable compression ratio |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2841737A1 true EP2841737A1 (en) | 2015-03-04 |
| EP2841737B1 EP2841737B1 (en) | 2016-03-30 |
Family
ID=48464026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP13723531.3A Active EP2841737B1 (en) | 2012-04-23 | 2013-04-19 | Piston engine with a variable compression ratio |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP2841737B1 (en) |
| FI (1) | FI20125437A7 (en) |
| WO (1) | WO2013160541A1 (en) |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US943598A (en) * | 1908-11-27 | 1909-12-14 | Ingle Hovey | Internal-combustion engine. |
| US1360366A (en) * | 1918-07-13 | 1920-11-30 | James A Charter | Variable-compression gas-engine |
| US1429164A (en) * | 1921-03-22 | 1922-09-12 | John T Ramsey | Internal-combustion engine |
| JP2005133612A (en) * | 2003-10-29 | 2005-05-26 | Toyota Motor Corp | Variable compression ratio internal combustion engine |
-
2012
- 2012-04-23 FI FI20125437A patent/FI20125437A7/en not_active Application Discontinuation
-
2013
- 2013-04-19 EP EP13723531.3A patent/EP2841737B1/en active Active
- 2013-04-19 WO PCT/FI2013/050437 patent/WO2013160541A1/en not_active Ceased
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2013160541A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| FI20125437L (en) | 2013-10-24 |
| WO2013160541A1 (en) | 2013-10-31 |
| FI20125437A7 (en) | 2013-10-24 |
| EP2841737B1 (en) | 2016-03-30 |
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