WO2006084542A1 - Rotor-kolben-verbrennungsmotor - Google Patents
Rotor-kolben-verbrennungsmotor Download PDFInfo
- Publication number
- WO2006084542A1 WO2006084542A1 PCT/EP2006/000312 EP2006000312W WO2006084542A1 WO 2006084542 A1 WO2006084542 A1 WO 2006084542A1 EP 2006000312 W EP2006000312 W EP 2006000312W WO 2006084542 A1 WO2006084542 A1 WO 2006084542A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- rotor
- combustion engine
- internal combustion
- engine according
- piston
- Prior art date
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
- F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
- F02B57/08—Engines with star-shaped cylinder arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B13/00—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion
- F01B13/04—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder
- F01B13/06—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement
- F01B13/068—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement the connection of the pistons with an actuated or actuating element being at the inner ends of the cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B15/00—Reciprocating-piston machines or engines with movable cylinders other than provided for in group F01B13/00
- F01B15/02—Reciprocating-piston machines or engines with movable cylinders other than provided for in group F01B13/00 with reciprocating cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B73/00—Combinations of two or more engines, not otherwise provided for
Definitions
- the invention relates to an internal combustion engine according to the preamble of claim 1.
- radial engines in which the cylinders are arranged in a star shape with pistons and the piston rods drive a crankshaft.
- a special form of the radial engine is the recirculation engine, in which the crankshaft is stationary and the cylinders rotate with pistons.
- rotary engines such as the Wankel engine are known in which rotates in an ellipsoidal housing with epithrooid chambers, a rotor that follows the ellipsoidal shape.
- the volume of the individual chambers is changed, and in one revolution of the rotor, the four strokes of the engine are completed, but not optimally segmented.
- the ellipsoidal shape creates differences in chamber volume and so does the four cycles.
- the object of the invention is to provide an internal combustion engine which achieves a high efficiency with a simple construction and smooth running. It is also an object of the invention to avoid the ellipsoidal shape with the The aim of the maximum chamber seals to reduce vibrations to a minimum and to simplify the construction.
- New here is, inter alia, that the combustion of the air / gas mixture is no longer carried out in the cylinders and thus the piston does not ' directly serve the drive, but the cylinders with pistons provide the additional combustion chamber with the compressed air / gas mixture.
- the gas flowing out of the combustion chamber outside the rotor after ignition drives the rotor.
- the rotor-piston internal combustion engine is characterized by being small in size, light in weight but very powerful and yet economical, offering a wide range of engine power control, low fuel consumption and higher ignition timing fuels such as diesel engines , As hydrogen, can burn.
- the rotor-piston-motor has a circular shape of the rotor and built with offset from the center C axis. This eliminates the complicated ellipsoidal movement and allows a good seal of the individual working chambers.
- the completion of the suction, pressing and the ignition of the fuel-air mixture and the discharge of the exhaust gases can be achieved by the Difference in the distances from the axis of the piston group offset from the center (C) of the rotor at point B (center B) to the periphery of the rotor.
- the priming and in the sector of the minimum radius (r min.) The ignition of the fuel-air mixture and the emission of the exhaust gases in one revolution of the rotor are performed.
- the force resulting from the ignition is directed tangentially in the direction of rotation of the rotor, which is predetermined by the combustion chamber, the piston group and the offset center (B).
- FIG. 2 shows a section according to D-D in FIG. 1 - one of the variants for mounting the piston group
- FIG. 3 shows a section according to F-F in FIG. 1,
- FIG. 4 shows a section along E-E in FIG. 1,
- FIG. 5 is an end view of the engine
- FIG. 6 is a top view of the engine
- FIG. 8 Schematic representation of the process of sucking in the fuel-air mixture and the controllable sector (X), which determines its initial torque
- FIG. 9 Schematic representation of the working process and the controllable sector (Y), which determines the initial momentum of the emission of the exhaust gases
- FIG. 10 Circuit diagram of the processes suction (N), injection (M), work (H), discharge of exhaust gases (E), vacuum generation (G).
- the rotor-piston internal combustion engine consisting of three or more mutually parallel, cooperating liquid-cooled housings 1, has - according to Figures 1 to 3 - depending on a housing 1 to which a spark plug 2, an exhaust port 3 and a suction port 4 are mounted.
- the rotor 5 is mounted with two sprockets 14.
- the segments 9 are mounted on both sides of each individual working chamber 11 of the cylinder 6, which serve to seal those.
- the parts of the cylinder 6, which are movably captured in the rotor 5, are spherical from the outside, which fulfills the function of a ball joint.
- the cylinders 6 are radially movable and orbitally overflow and slide on the pistons 8 equipped with smaller pistons 13 (expanders), which in turn are sealed with the segments 9.
- the pistons 8 are movable independently of each other, as shown in FIG. 2, mounted axially.
- the pistons 8 / I and 8 / II store in the housing 1 and the piston 8 / II is stored between and in pistons 8 / and S / 11.
- the bearing of the piston group 8 / I + II + III is from the center C of the rotor 5 offset in point B (offset center B, intersected by the axis 10).
- the pistons 8 are axially immobile relative to the center B and orbital not overflow.
- each piston is reached in the area where exhaust gas discharge begins ( Figure 1).
- the straight line passing through the center C of the rotor and through the offset center B shows exactly this area.
- the combustion chamber 17 is at an angular distance of 30 °, precisely from this straight line in front of the exhaust port. Upon ignition of the fuel-air mixture in the combustion chamber 17, the piston 8 has not quite reached the top dead center.
- the spherically movably received in the rotor 5 cylinder 6) act as balancing arms (Winkelkompensatoren), which compensate for the angular transitions to the various orbitalen positions, which are determined by the offset center B and the circular shape of the rotor 5.
- a smaller piston 13 is structurally predetermined, by which the different load moments are compensated at the different predetermined powers up to the time of ejection of the exhaust gases.
- This smaller piston 13 exerts no influence on the indicator voltage (pressure) formed in the working chamber 11.
- the movement is transmitted tangentially by pressure on the rotor 5 in its direction of movement. This direction of movement is predetermined by the construction of the combustion chamber 17 in the housing 1 and by the piston group displaced from the center C of the rotor 5 and which is mounted in the housing 1 (FIG. 2) (axis 10).
- the cylinder travel (working volume) is changed, and as a result, the power of the engine can be changed during its running.
- the intake 4 is set so constructive that by their selectable positioning in Sector X, the initial torque of the intake of the fuel-air mixture can be changed.
- the function of the motor is realized after switching on the starter and turning the rotor 5. Due to the constructive differences in the distance from the periphery of the rotor 5 to the axis 10 offset from the center C, the cylinders 6 change the volume of the working chambers 11 and depending on their points of contact, the five working processes (see FIG. 10) in one revolution of the Rotor 5 completed.
- the ignition process at the position of the piston (8 / I, see FIG. 1) the working chamber 11 and the combustion chamber 17 meet in the housing 1. At this moment, the fuel-air mixture in the working chamber 11 is maximally pressed. In the meeting with the combustion chamber 17, the fuel-air mixture is pressed into this and ignited immediately.
- the resulting force F acts on the piston head 8 / I 1 and on the rotor 5.
- the force F is distributed tangentially to the rotor 5 in its direction of movement and acts until the moment of expulsion of the exhaust gases through the adjustable discharge opening 3.
- the working chambers 11 in the rotor 5 are positioned at an angular distance of 120 ° from each other.
- the ignition process takes place three times (at an angular distance of 120 °) for one revolution of the rotor 5. This process takes place separately in each of the three housings 1 / R1, R2, R3 of the motor.
- the complete motor consists of three or more housings 1 / R1, R2, R3, which are intermeshed by gear gear 15a and operate synchronously.
- the piston group 8 of each subsequent housing 1 is compared with the previous offset at a certain angle which is proportional to the number of housings 1 in the engine. With three housings 1, each subsequent piston group 8 is positioned offset by 40 ° with respect to the previous one.
- the combination of different housing diameter sizes in the engine allows different power values per individual rotor 5 to be achieved.
- the design thus specified gives, depending on the need and situation, the possibility of automatically selecting the number of housings 1 which participate in the working operation of the engine. As a result, one achieves a lower fuel consumption.
- all housing 1, R1, R2, R3 participate in the working operation of the engine.
- the rotor 5 At rest, the rotor 5 has a certain constructive mass, which has a smaller value overall than during rotation.
- the space of the interior side of the rotor 5 is filled once with oil.
- centrifugal forces which distribute the oil on the inner wall of the rotor 5.
- the rotor 5 has a structurally predetermined relief shape of the inner wall. This causes the sputtering of the oil back into the internal space of the engine. As a result, a new, larger value of the mass of the rotor 5 is produced during rotation. This allows low power consumption at engine startup and higher rotational torque during engine operation.
- the invention belongs to the internal combustion engines of the rotor-piston type and can be used in automobile, aircraft and shipbuilding, for motorcycles, generators, pumps and for driving various transmissions and mechanisms.
- the rotor 5 After starting the rotor-piston engine, the rotor 5 is set in a right rotational movement, wherein the volume of the working chamber 11 during the working process (ignition of the fuel-air mixture in the combustion chamber 17) remains constant.
- the piston 8 does not make any return movement at this moment.
- the pistons 8 serve only to suck in fuel-air mixture in the cylinders 6, and to press into the combustion chamber 17 and expel exhaust gases.
- the entire piston group rotates about the axis 10, which is offset from the center C.
- the ignition of the fuel-air mixture happens outside of the working chambers 11 namely in the combustion chamber 17.
- the piston 8, which has pressed the fuel-air mixture into the combustion chamber 17, forms an angle of 70 ° to the rotor.
- the resulting during detonation force F is directly distributed tangentially by pressure on the rotor 5.
- the piston 8 is not set in return movement due to the detonation, as shown in FIGS. 1 and 3.
- Each individual piston 8 has a smaller piston 13, which absorbs part of the detonation force F at the first moment and thereby enables a balancing (compensation) the different strong detonations at a change in the position of the ejection port 3 or suction port 4 or the center B. It protects the combustion chamber 17 and housing 1 thus from overloading.
- the rotor-piston internal combustion engine consists of 3 rotors 5 and 3 piston groups 8/1, 8 / II, S / i 11 with the associated cylinders 6, a total of 9 pistons 8.
- Each piston 8 is positioned relative to the other structurally given that between them an angle of 40 ° exists. This means that when starting the engine, ignition is performed at intervals of 40 °. This angular distance is accordingly reduced in a possible execution of the engine with 4 rotors 5 proportional to 30 °. (For example: with 5 rotors 5 at 24 °)
- a rotor-piston internal combustion engine has been developed by the invention, which performs no ellipsoidal movement compared to the Wankel engine and has constructive advantages.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL06701294T PL1846646T3 (pl) | 2005-02-08 | 2006-01-16 | Silnik spalinowy z wirującym tłokiem |
JP2007553491A JP2008530413A (ja) | 2005-02-08 | 2006-01-16 | ロータ・ピストン内燃機関 |
US11/884,056 US7673595B2 (en) | 2005-02-08 | 2006-01-16 | Rotor-piston internal combustion engine |
EP06701294A EP1846646B1 (de) | 2005-02-08 | 2006-01-16 | Rotor-kolben-verbrennungsmotor |
AT06701294T ATE520871T1 (de) | 2005-02-08 | 2006-01-16 | Rotor-kolben-verbrennungsmotor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05002570.9 | 2005-02-08 | ||
EP05002570 | 2005-02-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2006084542A1 true WO2006084542A1 (de) | 2006-08-17 |
Family
ID=34933628
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2006/000312 WO2006084542A1 (de) | 2005-02-08 | 2006-01-16 | Rotor-kolben-verbrennungsmotor |
Country Status (8)
Country | Link |
---|---|
US (1) | US7673595B2 (de) |
EP (1) | EP1846646B1 (de) |
JP (1) | JP2008530413A (de) |
AT (1) | ATE520871T1 (de) |
ES (1) | ES2371656T3 (de) |
PL (1) | PL1846646T3 (de) |
RU (1) | RU2392460C2 (de) |
WO (1) | WO2006084542A1 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9057267B2 (en) * | 2005-03-09 | 2015-06-16 | Merton W. Pekrul | Rotary engine swing vane apparatus and method of operation therefor |
DE102006046011B4 (de) * | 2006-09-28 | 2008-07-10 | Alois Tradler | Druckkraftmaschine, insbesondere Brennkraftmaschine, mit einer Ringstruktur |
US8056527B2 (en) | 2008-11-19 | 2011-11-15 | De Oliveira Egidio L | Split-chamber rotary engine |
US8225767B2 (en) * | 2010-03-15 | 2012-07-24 | Tinney Joseph F | Positive displacement rotary system |
BR112012033399A2 (pt) * | 2010-07-06 | 2017-12-05 | Sydney Oliver Ampuero Larry | motor de combustão interna |
US8800501B2 (en) * | 2010-07-20 | 2014-08-12 | Sylvain Berthiaume | Rotating and reciprocating piston device |
RU2472018C2 (ru) * | 2011-03-15 | 2013-01-10 | Сергей Владимирович Пирогов | Роторно-поршневой двигатель |
US9528433B2 (en) * | 2012-04-04 | 2016-12-27 | Fahim Mahmood | Double bars and single wheel rotary combustion engine |
CZ30945U1 (cs) | 2017-06-30 | 2017-08-21 | Stanislav Chromčák | Pístový motor |
RU2731210C2 (ru) * | 2018-10-01 | 2020-08-31 | Владислав Николаевич Мальцев | Двигатель внутреннего сгорания роторно-лопастного типа |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB357979A (en) * | 1930-06-30 | 1931-09-30 | Reginald Warren | An improved fluid pressure pump, engine, or variable speed power transmitter or brake |
FR1600757A (de) * | 1968-12-20 | 1970-07-27 | ||
DE4118938A1 (de) * | 1991-06-08 | 1992-12-10 | Ostermeyer Heinz Juergen | Rotationsschwingkolbenmotor |
FR2750162A1 (fr) * | 1996-06-19 | 1997-12-26 | Turbe Louis Charles | Moteur rotatif |
CA2300584A1 (en) * | 1999-04-08 | 2000-10-08 | Shih-Pin Huang | Internal combustion engine |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1042675A (en) * | 1908-04-09 | 1912-10-29 | William D Sargent | Rotary explosive-motor. |
US975485A (en) * | 1910-01-26 | 1910-11-15 | John A Waltman | Rotary multiple-cylinder internal-combustion engine. |
US2127016A (en) * | 1937-04-21 | 1938-08-16 | Frank A Voiles | Internal combustion engine |
US3665811A (en) * | 1968-07-03 | 1972-05-30 | Gilbert Van Avermaete | Rotary machine |
US3581718A (en) * | 1968-11-14 | 1971-06-01 | David V Petty | Rotary internal combustion engines |
JPS4917962B1 (de) * | 1970-12-07 | 1974-05-07 | ||
ES396667A1 (es) * | 1971-11-04 | 1974-05-16 | Ferragut Rodriguez | Maquina de embolos rotativos. |
US3857371A (en) * | 1973-06-04 | 1974-12-31 | T Gibson | Rotary internal combustion engine |
US4166438A (en) * | 1976-11-11 | 1979-09-04 | Gottschalk Eldon W | Machine with reciprocating pistons and rotating piston carrier |
DE3531208A1 (de) * | 1985-08-31 | 1986-02-27 | Lorenz 7916 Nersingen Fetzer | Verbrennungsturbinenmotor |
US5365892A (en) * | 1987-04-16 | 1994-11-22 | Kienle Gerhard K | Rotary internal combustion engine |
JPH02101050U (de) * | 1989-01-30 | 1990-08-10 | ||
US5123394A (en) * | 1990-05-23 | 1992-06-23 | Warren Ogren | Rotary reciprocating internal combustion engine |
JPH05202759A (ja) * | 1990-12-06 | 1993-08-10 | Shizuo Kimura | ピストンの下に付けたツバで吸入圧縮掃気工程を行なう2サイクルエンジン |
US6253717B1 (en) * | 1999-04-16 | 2001-07-03 | Lonny J. Doyle | Rotary engine |
US6062175A (en) * | 1999-04-20 | 2000-05-16 | Huang; Shih-Pin | Rotating cylinder internal-combustion engine |
JP2004092483A (ja) * | 2002-08-30 | 2004-03-25 | Toyota Motor Corp | エアモータ |
-
2006
- 2006-01-16 US US11/884,056 patent/US7673595B2/en not_active Expired - Fee Related
- 2006-01-16 RU RU2007133506/06A patent/RU2392460C2/ru active
- 2006-01-16 JP JP2007553491A patent/JP2008530413A/ja active Pending
- 2006-01-16 ES ES06701294T patent/ES2371656T3/es active Active
- 2006-01-16 PL PL06701294T patent/PL1846646T3/pl unknown
- 2006-01-16 WO PCT/EP2006/000312 patent/WO2006084542A1/de active Application Filing
- 2006-01-16 AT AT06701294T patent/ATE520871T1/de active
- 2006-01-16 EP EP06701294A patent/EP1846646B1/de not_active Not-in-force
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB357979A (en) * | 1930-06-30 | 1931-09-30 | Reginald Warren | An improved fluid pressure pump, engine, or variable speed power transmitter or brake |
FR1600757A (de) * | 1968-12-20 | 1970-07-27 | ||
DE4118938A1 (de) * | 1991-06-08 | 1992-12-10 | Ostermeyer Heinz Juergen | Rotationsschwingkolbenmotor |
FR2750162A1 (fr) * | 1996-06-19 | 1997-12-26 | Turbe Louis Charles | Moteur rotatif |
CA2300584A1 (en) * | 1999-04-08 | 2000-10-08 | Shih-Pin Huang | Internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
PL1846646T3 (pl) | 2012-01-31 |
RU2392460C2 (ru) | 2010-06-20 |
EP1846646B1 (de) | 2011-08-17 |
ATE520871T1 (de) | 2011-09-15 |
RU2007133506A (ru) | 2009-03-20 |
EP1846646A1 (de) | 2007-10-24 |
US20080121207A1 (en) | 2008-05-29 |
US7673595B2 (en) | 2010-03-09 |
ES2371656T3 (es) | 2012-01-05 |
JP2008530413A (ja) | 2008-08-07 |
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