WO2000034635A1 - Rotary piston combustion engine - Google Patents
Rotary piston combustion engine Download PDFInfo
- Publication number
- WO2000034635A1 WO2000034635A1 PCT/FI1999/000994 FI9900994W WO0034635A1 WO 2000034635 A1 WO2000034635 A1 WO 2000034635A1 FI 9900994 W FI9900994 W FI 9900994W WO 0034635 A1 WO0034635 A1 WO 0034635A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- piston
- main cylinder
- engine
- valves
- valve
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 15
- 238000004880 explosion Methods 0.000 claims abstract description 32
- 239000007789 gas Substances 0.000 claims abstract description 15
- 239000000567 combustion gas Substances 0.000 claims abstract description 12
- 239000000203 mixture Substances 0.000 claims abstract description 8
- 230000006835 compression Effects 0.000 claims description 18
- 238000007906 compression Methods 0.000 claims description 18
- 230000033001 locomotion Effects 0.000 claims description 13
- 230000007423 decrease Effects 0.000 description 12
- 238000007789 sealing Methods 0.000 description 9
- 238000013459 approach Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/08—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
- F01C1/12—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type
- F01C1/14—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F01C1/20—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with dissimilar tooth forms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/36—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having both the movements defined in sub-groups F01C1/22 and F01C1/24
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
- F01C1/46—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the outer member
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B2053/005—Wankel engines
Definitions
- the invention relates to a 4-phase combustion engine equipped with a rotary piston, mainly meant to function as a gasoline using engine.
- the embodiment of the engine consists of a main cylinder body, in which there is a rotating piston rotor comprising a piston attached to a cylindrical body having a fixed shaft in the middle.
- the shaft functions as the driving shaft of the engine.
- the engine is operated by two valves, which either open or close the room existing between the engine body and the piston body.
- the rotation of the piston is achieved when the gas mixture compressed into explosion volume is closed in between both the valves in such a way that also the piston stays in between the valves.
- US patent US-3745979 presents a triangular piston structure, where the pistons move radially inside an elliptical cylinder, where the piston pushes the gas ahead into a storage tank closed by valves. From the storage tank the gas expands to the explosion chamber formed by the former piston. The volume of the explosion chamber increases while combustion gas is led into it. In this structure the pressure in the combustion chamber is smaller than in the storage tank, which decreases the motor efficiency compared to the invention.
- Patent publication DE 3926061 Al presents a motor body and rotor structure similar to the invention but with a different operation.
- the motor consists of two pairs of pistons, which function by means of eight valves each in turn in such a way that when one pair of pistons is rotating the other one is standing still. According to this functioning principle it is very difficult to construct a functional motor and thus a detailed structure of the motor has not been presented.
- a so called main cylinder has been made into the engine body and its both ends have been closed by planes forming end walls.
- a revolving piston fastened to a cylindrical piston body, which has a fixed shaft in the middle, which thus functions as a driving shaft of the engine.
- the engine is operated by two valves.
- the valves are located in cylinders crossing the main cylinder in such a way that the outer surface of the valves either combines with the cylinder surface of the main cylinder or the valves close the room existing between the engine body and the piston body.
- the rotating motion of the piston inside the main cylinder is achieved when first the combustion gases compressed into the explosion volume are closed into the room existing between the closed valves in such a way that also the piston remains between the valves. After this the combustion gases are moved from the front side of the piston to its back side through a groove which is wider than the piston in the direction of the cylinder circumference and which is made into the surface of the main cylinder where the explosion chamber is located. While the piston is approaching the valve ahead, it pushes the combustion gases through the groove to the back side of the piston.. A little before the piston touches the valve ahead the explosion takes place and the valve opens. At this stage the front edge of the piston has passed over the groove and it touches the surface of the main cylinder thus closing the combustion chamber. This is followed by the working phase of the engine in which the piston revolves in the main cylinder about 290°.
- FIG. 1 is a cross-section of the engine a little before the explosion
- FIG. 2 is a cross-section of the engine at the moment of the explosion
- FIG. 3 is a cross-section of the engine a little after the explosion
- FIG. 4 is a cross-section of the engine a little before the suction-/ exhaust phase
- FIG. 5 is a cross-section of the engine at the beginning of the suction-/ exhaust phase
- FIG. 6 is a cross-section of the engine during the suction-/ exhaust phase
- FIG. 7 is a cross-section of the engine a little before the compression phase
- FIG. 8 is a cross-section of the engine at the beginning of the compression phase
- FIG. 9 is a cross-section of the engine a little before the end of the compression phase
- FIG. 10 is a cross-section of the engine at the end of the compression phase
- FIG. 11 illustrates a different structure of the engine
- FIG. 12 illustrates the operation mechanism of the valves and the pressure adjustment piston
- FIG. 13 illustrates a perspective picture of the cross-section of the engine
- Figures 1 - 10 illustrate the cross-section of the engine in its different phases of operation.
- the engine body 1 where the main cylinder 2 is located; in the main cylinder the rotating cylindrical piston body 3, onto which the piston 4 is attached; the fixed shaft 5 in the middle of the piston body; the suction- /exhaust valve 6, which rotates in the valve cylinder 7 crossing the main cylinder on the shaft 8; the pressure valve 9, which turns back and forth on the shaft 10 in the valve cylinder 11 crossing the main cylinder in such a way that around the shaft into the engine body has been made a cylinder surface 12 by length about l A of a circle, which combines with the inner surface of the pressure valve; into the surface of the main cylinder at the explosion chamber has been made a groove 13 wider than the piston; the pressure adjustment cylinder 14; the pressure adjustment piston 15; the suction channel 16; the exhaust channel 17; the front sealing part 18 in the main cylinder; the back sealing part 19 in the main cylinder and on the cylinder surfaces of the sealing
- FIG. 1 demonstrates the engine a little before explosion.
- the piston 4 is in the explosion chamber between the valves 6 and 9 in such a way that there exists a small gap between the piston 4 and the pressure valve 9.
- the valve 9 starts to open.
- the purpose of the gap is to give time for the opening of the valve.
- the gap decreases to zero a little after the front edge of the piston 4 has touched the back sealing part 19 in the main cylinder.
- the rest of the combustion gas has moved to the back side of the piston 4 through the small wedge shaped groove 19a in the cylinder surface of the back sealing part 19 and the explosion can take place.
- the valve 6 moves to the suction-/ exhaust position.
- the transition stage is illustrated in figure 4.
- the valve has turned to such a position in which its surface combines with the main cylinder surface 2 and so the piston 4 is able to pass the valve.
- the valve turns to the beginning of the suction-/ exhaust phase, which is illustrated in figure 5.
- both the suction channel 16 and the exhaust channel 17 are simultaneously open in such a way that the valve at the same time closes the connection between the channels. Due to the former the engine carries out simultaneously both the suction- and the exhaust phases in the way that when the back side of the piston sucks air mixture its front side pushes away the exhaust gases.
- the engine starts the compression phase, which begins in such a way that first the suction-/ exhaust valve turns to the position, where the surface of the valve combines with the cylinder surface of the main cylinder 2.
- piston 4 passes the valve.
- This stage is illustrated in figure 7.
- the valve operating mechanism has been designed in such a way that the valve also stays in this position during the whole phase.
- the piston 4 also passes the pressure valve 9, which closes immediately after this.
- the essential compression phase begins from this stage, where the compression is started by compressing the gas mixture against the pressure valve 9. This has been illustrated in figure 8.
- the pressure valve closes the room between the main cylinder 2 and the piston body 3 in such a way that engine body 1 is partly around the shaft 10 thus forming about l A of a cylinder surface in such a way that the inner cylinder surface of the pressure valve combines with the cylinder surface 12 in the body and at the same time the outer surface of the valve touches the cylinder body 3 of the piston.
- a low pressure area is created behind the piston. Its creation is prohibited in such a way that a N-shaped replacement air channel 20 is built inside the pressure valve, through which the piston sucks replacement air.
- the exhaust channel during working phase which is marked in figure 3 as: "2. poisto".
- Figure 9 illustrates the engine a little before the compression phase ends. In this stage the back edge of the piston has passed the middle point of the suction-/ exhaust valve and the valve starts to turn to the position it has during explosion.
- Figure 10 illustrates the engine immediately after the compression phase. A little before the compression phase ends, a small low pressure area is created between the back side of the piston and the valve 6. This low pressure area causes decrease in the motor efficiency, if it has to be filled with the expansion of the already compressed gas mixture. The pressure loss is eliminated, when at the same time that the compressed gas mixture expands into the low pressure area, the pressure adjustment piston 15 decreases the volume with an amount * corresponding to the expansion. The even transition of the pressure to the low pressure area is carried out through a wedge shaped groove 18a on the sealing part of the cylinder.
- one edge of the suction-/ exhaust valve 6 touches the valve cylinder 7 and the other edge touches the piston body 3.
- the valve forms "a back wall" for the compressed explosion gas.
- the explosion gas can be moved from the front side of the piston 4 to its back side. This is carried out through the groove 13, as mentioned before.
- Figure 11 illustrates a modification of the engine, in which the groove 13 has been transferred from the main cylinder surface into its side walls.
- the cylinder area of the sealing part 18 in the main cylinder surface can be enlarged which makes a better sealing between the piston and the cylinder surface.
- Figure 12 illustrates the operation mechanism of the valves 6 and 9 and the pressure adjustment piston 13.
- the following parts can be distinguished in the picture:
- the driving shaft 5 and fixed to it a tooth wheel 21 connected with a chain 22 to a tooth wheel 23; an auxiliary shaft 24, which is fixed to a cam plate 26, which moves the pressure valve 9 by a valve lever 27; to the auxiliary shaft 24 fixed a cam plate 28, which moves the suction-/ exhaust valve 6 by a valve lever 29; in different planes on the driving shaft 5 the suction-/ exhaust valve 6 levers 30, 31, 32; the pressure valve 9 lever 33; counterparts 30a, 31a, 32a, 33a for the valve levers and the springs 34, 35, 36 for returning the motion.
- the engine carries out all the four operation phases during three revolutions, since the suction- and exhaust phases take place simultaneously. Due to this every separate motion of the valve or the pressure adjustment piston takes place only once while the piston rotates three revolutions. Part of these motions can be carried out by the valve levers 30, 31, 32, 33, which are fixed straight to the driving shaft, but part of the motions must be carried out by cam plates 25, 26, 27, since they turn only once during the time that the piston rotates three revolutions. For this reason the driving shaft has a cog wheel 21 with a gear ratio 1 : 3 to the cog wheel 23 on the auxiliary shaft 24. To the cog wheel 23 has been fixed three cam plates25, 26, 28, the eccentric shape of which controls the operation of the pressure adjustment piston and the valves.
- the cam plate 25 controls the operation of the pressure adjustment piston 15 in such a way that it decreases the explosion volume during the stage mentioned before and closes the groove 13 during the start of the suction-/ exhaust phase.
- the cam plate 26 closes the pressure valve 9 by the valve lever 27 and keeps it closed up to the explosion phase and then the cam plate releases the valve to open.
- the cam shaft 28 moves the valve lever 29 in such a way that the valve 6 is transferred from the compression phase to the explosion phase, (pictures 9, 10)
- the rest of the motions of the valves is achieved by the valve levers attached to the driving shaft 5 of the main cylinder. From these motions the levers 30 and 31 rotate the valve 6 from the working phase to the suction-/ exhaust phase by means of the counterparts 30a, 31a.
- Figure 13 illustrates a cross-section of the perspective picture of the engine, where the groove 13 in the main cylinder has been totally substituted by the groove 13a in the side walls of the engine, through which the explosion gas is transferred from the front side of the piston 4 to its back side, as the arrows show.
- the engine has been described as a gasoline engine, but it can also be adapted to run by other fuels correspondingly, like the present Otto-motor. It can also be turned into a Diesel version by adding to it a front chamber.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Valve Device For Special Equipments (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/857,649 US6543406B1 (en) | 1998-12-07 | 1999-01-12 | Rotary piston combustion engine |
JP2000587059A JP2002531765A (en) | 1998-12-07 | 1999-12-01 | Rotary piston combustion engine |
EP99958223A EP1137872A1 (en) | 1998-12-07 | 1999-12-01 | Rotary piston combustion engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FI982637 | 1998-12-07 | ||
FI982637A FI107826B (en) | 1998-12-07 | 1998-12-07 | Internal combustion engine with rotary piston |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2000034635A1 true WO2000034635A1 (en) | 2000-06-15 |
Family
ID=8553054
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FI1999/000994 WO2000034635A1 (en) | 1998-12-07 | 1999-12-01 | Rotary piston combustion engine |
Country Status (5)
Country | Link |
---|---|
US (1) | US6543406B1 (en) |
EP (1) | EP1137872A1 (en) |
JP (1) | JP2002531765A (en) |
FI (1) | FI107826B (en) |
WO (1) | WO2000034635A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009104111A1 (en) * | 2008-02-22 | 2009-08-27 | Szaraniec, Christoph | Rotor-piston internal combustion engine |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005038212A1 (en) * | 2003-10-15 | 2005-04-28 | Han Young Park | Rotary engine |
CN102220901B (en) * | 2005-12-01 | 2014-05-07 | 大卫·D·格雷 | Rotary combustion apparatus |
US20100050981A1 (en) * | 2008-09-04 | 2010-03-04 | Ivas Richard T | Rotary internal combustion engine |
ITFR20090014A1 (en) * | 2009-05-15 | 2010-11-16 | Aldo Salvatore Coraggio | TOPOLOGY AND FUNCTIONING OF A ROTARY VOLUMETRIC MACHINE WITH FIXED, RADIAL AND CONCENTRIC SCOOP COMPARED TO THE ROTATION AXIS AND WITH ABSOLUTE ABSENCE OF MECHANICAL DETAILS SUBJECT TO CHANGE OF MOTION. |
WO2012057838A2 (en) * | 2010-10-27 | 2012-05-03 | Jesus Vazquez | Rotary valve continuous flow expansible chamber dynamic and positive displacement rotary devices |
US20130228149A1 (en) | 2012-03-01 | 2013-09-05 | Heping Ma | Rotary Internal Combustion Engine |
US9664048B2 (en) | 2012-08-23 | 2017-05-30 | Mallen Research Limited Partnership | Positive displacement rotary devices with uniform tolerances |
US9664047B2 (en) | 2012-08-23 | 2017-05-30 | Mallen Research Limited Partnership | Positive displacement rotary devices with uniquely configured voids |
US8956134B2 (en) | 2012-08-23 | 2015-02-17 | Mallen Research Limited | Fixed-vane positive displacement rotary devices |
NO337492B1 (en) * | 2014-06-04 | 2016-04-25 | Erik Michelsen | Rotary Engine |
CN105545465B (en) * | 2016-02-22 | 2018-10-30 | 丁阳 | Automobile internal combustion type circumference rotary engine |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1406140A (en) * | 1919-11-24 | 1922-02-07 | Anderson Axel Julius | Rotary engine |
US1637958A (en) * | 1926-01-13 | 1927-08-02 | Frederick M Newson | Internal-combustion engine |
US2070631A (en) * | 1936-01-25 | 1937-02-16 | Sunderland Morton | Rotary internal combustion engine |
US2412949A (en) * | 1942-09-14 | 1946-12-24 | Kyle And Company Inc | Rotary engine |
US3692002A (en) * | 1971-02-08 | 1972-09-19 | Robert H Williams | Rotary internal combustion engine |
US3739754A (en) * | 1970-12-03 | 1973-06-19 | A Nutku | Rotating-piston toroidal machine with rotating-disc abutment |
US3745979A (en) * | 1971-09-27 | 1973-07-17 | R Williams | Rotary combustion engine |
US4086881A (en) * | 1975-08-05 | 1978-05-02 | Fabrique Nationale Herstal S.A., En Abrege Fn | Rotary engine |
GB2212216A (en) * | 1987-11-09 | 1989-07-19 | Donald Kirk Anderson | A rotary combustion engine |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1311858A (en) * | 1919-07-29 | Sheet | ||
US896485A (en) * | 1906-07-23 | 1908-08-18 | James Tinlin | Internal-combustion engine. |
US892201A (en) * | 1907-06-18 | 1908-06-30 | Andrew W Welsh | Rotary engine. |
US1226745A (en) * | 1914-10-19 | 1917-05-22 | Frederick A Brooks | Rotary engine. |
US2198130A (en) * | 1937-11-29 | 1940-04-23 | Walter A Schweiger | Internal combustion engine |
US2571642A (en) * | 1948-02-27 | 1951-10-16 | Yancy Joseph | Rotary internal-combustion engine |
US2722201A (en) * | 1953-08-14 | 1955-11-01 | John K Muse | Rotary internal combustion engine |
US2977939A (en) * | 1960-01-19 | 1961-04-04 | Fearing Alfred | Rotary internal combustion engines |
US3699930A (en) * | 1971-11-08 | 1972-10-24 | Earl G Bunce | Rotary internal combustion engine |
US3913532A (en) * | 1973-11-05 | 1975-10-21 | Frentzel Dev Inc | Rotary engine |
US3935840A (en) * | 1974-08-07 | 1976-02-03 | Fisher John H | Rotary engine |
US4423710A (en) * | 1981-11-09 | 1984-01-03 | Williams Robert H | High compression rotary engine |
US5797366A (en) * | 1996-11-01 | 1998-08-25 | New Devices Engineering A.K.O. Ltd. | Toroidal internal combustion engine |
US6132197A (en) * | 1996-11-01 | 2000-10-17 | Medis El Ltd | Toroidal internal combustion engine |
US6298821B1 (en) * | 1999-04-12 | 2001-10-09 | Alexander Alexandrovich Bolonkin | Bolonkin rotary engine |
-
1998
- 1998-12-07 FI FI982637A patent/FI107826B/en active
-
1999
- 1999-01-12 US US09/857,649 patent/US6543406B1/en not_active Expired - Fee Related
- 1999-12-01 JP JP2000587059A patent/JP2002531765A/en active Pending
- 1999-12-01 WO PCT/FI1999/000994 patent/WO2000034635A1/en not_active Application Discontinuation
- 1999-12-01 EP EP99958223A patent/EP1137872A1/en not_active Withdrawn
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1406140A (en) * | 1919-11-24 | 1922-02-07 | Anderson Axel Julius | Rotary engine |
US1637958A (en) * | 1926-01-13 | 1927-08-02 | Frederick M Newson | Internal-combustion engine |
US2070631A (en) * | 1936-01-25 | 1937-02-16 | Sunderland Morton | Rotary internal combustion engine |
US2412949A (en) * | 1942-09-14 | 1946-12-24 | Kyle And Company Inc | Rotary engine |
US3739754A (en) * | 1970-12-03 | 1973-06-19 | A Nutku | Rotating-piston toroidal machine with rotating-disc abutment |
US3692002A (en) * | 1971-02-08 | 1972-09-19 | Robert H Williams | Rotary internal combustion engine |
US3745979A (en) * | 1971-09-27 | 1973-07-17 | R Williams | Rotary combustion engine |
US4086881A (en) * | 1975-08-05 | 1978-05-02 | Fabrique Nationale Herstal S.A., En Abrege Fn | Rotary engine |
GB2212216A (en) * | 1987-11-09 | 1989-07-19 | Donald Kirk Anderson | A rotary combustion engine |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009104111A1 (en) * | 2008-02-22 | 2009-08-27 | Szaraniec, Christoph | Rotor-piston internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
JP2002531765A (en) | 2002-09-24 |
FI107826B (en) | 2001-10-15 |
EP1137872A1 (en) | 2001-10-04 |
US6543406B1 (en) | 2003-04-08 |
FI982637A0 (en) | 1998-12-07 |
FI982637A (en) | 2000-06-08 |
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