EP2391801A2 - Drehkolbenmotor mit einem ringförmigen rotor - Google Patents
Drehkolbenmotor mit einem ringförmigen rotorInfo
- Publication number
- EP2391801A2 EP2391801A2 EP09740176A EP09740176A EP2391801A2 EP 2391801 A2 EP2391801 A2 EP 2391801A2 EP 09740176 A EP09740176 A EP 09740176A EP 09740176 A EP09740176 A EP 09740176A EP 2391801 A2 EP2391801 A2 EP 2391801A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- stator
- engine
- compression
- pistons
- 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.)
- Withdrawn
Links
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
- F01C3/00—Rotary-piston machines or engines with non-parallel axes of movement of co-operating members
- F01C3/02—Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged at an angle of 90 degrees
-
- 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
- F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
- F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
Definitions
- the present invention relates to rotary engines with gasoline or compressed air based on the rotational movement of a rotor, and relates in particular to a rotary motor with a circular rotor.
- the engines of the vehicles used today are internal combustion engines comprising reciprocating pistons in which the engine force is produced by the explosion of a mixture of air and fuel such as fuel. petrol.
- Each piston that is in a cylinder is pushed violently by the explosion ert causes the rotation of a crankshaft via a connecting rod.
- these engines have a major disadvantage that the stroke of the piston in the cylinder is limited to about 8 cm.
- the lever arm of the crankshaft is limited to about 4 cm, and therefore, all the motor force is on these 4 cm of the lever arm, which significantly limits the engine torque.
- the rotary engine has a slightly more complex operation than the traditional piston engine. Unlike an internal combustion engine that operates through pistons, the rotary engine uses a rotor. Unlike the internal combustion engine, the rotary engine has neither crankshaft nor crankshaft. There are advantages to using a rotary engine rather than the reciprocating engine. First, this engine having no reciprocating parts, its balancing is excellent, which ensures a private operation of vibrations, thereby limiting the noise level regardless of the speed of rotation. Then, this engine causes less vibration since all the parts follow the same path, because they turn in the same direction. In addition, since there are fewer moving parts in the engine, the rotary motor is more reliable.
- a known engine of this type includes a rotor that orbits within an oval-shaped housing.
- the main element of this engine, the rotor is a triangular object flanked in the center of the engine. This rotor performs an almost oval orbit inside the housing called stator. At each rotation, the ends of the rotor are always in contact with the stator. These contacts thus form the compression chambers, three in all.
- a crank consisting of two toothed gears: one large and one small. The large gear couples with the small gear to define the rotor path in the crankcase.
- the object of the invention is to provide a rotary rotor rotating motor around a stator and having a perfect seal that does not require the use of a lubricant.
- Another object of the invention is to provide a rotary rotor rotating motor around a stator and allowing a motor torque depending on the diameter of the rotor and much larger than that of existing engines
- the object of the invention is therefore a rotary motor comprising a circular stator, a circular rotor rotating around the stator, the rotor and the stator being separated by a circular cylinder, and at least one element with 2 flanges.
- the rotor comprises two compression pistons attached to the inner surface of the rotor, these two pistons being located at the two ends of a first diameter of the rotor and kept substantially in contact with the outer surface of the stator.
- the stator comprises a recess at each end of a diameter, each recess forming a compression chamber with the compression piston at the end of the recess in the direction of rotation of the rotor and one of the flanges of the element 2 flanges said cheek flange, the motor force being applied to the compression piston when the pressure of the gases inside the compression chamber is suddenly raised to a determined value.
- the engine according to the invention is used as a combustion engine in which each of the recesses comprises a fuel delivery pipe and a spark plug, the fuel being injected into the compression chamber.
- each of the recesses comprises a fuel delivery pipe and a spark plug, the fuel being injected into the compression chamber.
- the fuel delivery pipe when the compression piston is in front of the recess and that the transit flanges and yoke of the flanged element are closed, and the spark plug being activated when the compression piston is at the end of the compression chamber, the transit flange being open, so that the explosion of the mixture of air and gasoline in the compression chamber produces the motor force on the compression piston.
- the motor according to the invention is used as a compressed air motor.
- each of the recesses comprises a compressed air supply pipe, the compressed air being injected into the compression chamber associated with each recess when the compression piston is at the end of the compression chamber, the transit flange being open, so as to produce the same motor force as the explosion of the mixture of air and gasoline of the same engine.
- FIGS. 1A, 1B, 1C and 1D are sectional views of the motor showing each of the components of the invention. motor for 4 successive positions of the engine when the latter has rotated in each position by 90 ° counterclockwise with respect to the previous position;
- Figure 2 is a perspective view of the element with 2 flanges;
- FIGS. 3A, 3B and 3C are sectional views showing the progression of the compression piston in the compression chamber from its entry into the chamber until the explosion of the mixture of air and gasoline;
- FIG. 4 is a sectional view of the motor perpendicular to the section of FIG. 1A showing the rotor surrounding the stator and the 2 flanged elements as well as driving these elements by a belt from the axis of the rotor.
- the rotary engine in which the engine is an internal combustion engine represented in FIGS. 1A, 1B, 1C and 1D comprises a stator 10 around which a rotor 12 rotates. is rotated anti-clockwise about an axis 13. The stator and the rotor are separated by a space constituting the cylinder.
- the engine comprises four pistons fixed to the inner surface of the rotor 12: two compression pistons 16 and 18 located at the two ends of a rotor diameter and two intake and exhaust pistons 20 and 22 located at the two ends of a diameter perpendicular to the previous one and therefore to 90 ° of the 2 compression pistons.
- each flanged element comprises two flanges.
- the flanged element 24 illustrated in Figure 2 comprises a transit flange 32 and a yoke flange 34 connected by a rotary drive mechanism.
- the transit flange 32 serves for the passage of gases in the cylinder 14 at the rear of the piston.
- the 2 flanged elements 24 and 26 seen in section in Figures IA to ID are rotated by the rotation of the rotor.
- the axis 13 of the rotor 12 in rotary motion drives the axis 36 associated with the flanged element 24 and the axis 38 associated with the flanged element 26 by means of a belt 40.
- Each of the axes 36 and 38 respectively drives each of the pins 28 and 30 of the associated flange member by means of a deflection device, not shown in Figure 2, which consists of 2 gears at 45 ° to their axis, thus allowing transforming a rotational movement about the axis 36 or 38 into a rotational movement about the perpendicular axis 28 or 30 respectively.
- the stator 10 has two recesses 42 and 44 located at the two ends of a diameter. Each of these two recesses comprises a fuel delivery pipe, the pipe 46 for the recess 42 and the pipe 48 for the recess 44, as well as a spark plug 50 for the recess 42 and a candle
- the flanges of the flanged element 24 form a closed compression chamber 54 in which the compression piston 16 is located.
- gasoline supply via the pipe 46 is activated and the mixture of air and gasoline is formed in the chamber thus formed.
- FIG. 3A the compression piston 16 arrives at the beginning of the chamber 54. Thanks to the opening of the cylinder head flange 34 while the transit flange is closed. The air in chamber 54 begins to compress. Then, when the piston 16 has arrived in the middle of the chamber 54, that is to say in front of the recess 42, the 2 flanges 32 and 34 are closed and the gasoline is injected into the chamber through the pipe 46 as shown in Figure 3B. Finally, when the piston 16 reaches the end of the chamber, the transit flange 32 is in its open portion and the spark plug 50 is activated so as to cause the explosion in the chamber 54 as illustrated in FIG. 3C. This explosion makes it possible to exert a motor force on the piston 16 and thus to drive the rotor in rotation.
- the compression piston 16 When the engine is in the position shown in FIG. 1C, the compression piston 16 has rotated 180 ° since the explosion. The intake / exhaust piston 22 is then in front of the recess 42 of the stator. The volume 56 of the flue gases is at its maximum expansion level and the flue gas begins to escape through the exhaust port 58. The air that entered the cylinder occupies the part 60 which is its volume. maximum between the compression piston 18 and the flange cylinder 34 closed. When the engine is in the position shown in FIG ID, the compression piston 16 has already performed H turn. The air in the portion 56 continues to escape through the exhaust port 58. The volume of the cylinder portion 60 begins to be compressed as it is trapped between the transit flange 32 (the flange cylinder head is open) and the intake / exhaust piston 18.
- FIG. 4 which represents the motor in section A-A of FIG. 1A
- the transit flange of the flanged element 24 and the flange of the flanged element 26 are seen. Note that the two elements flanges 24 and 26 being offset by 180 °, the transit flange of one is in alignment with the cylinder head flange of the other and vice versa.
- the rotor 12 which comprises the two compression pistons 16 and 18 rotates around the stator 10.
- the rotor is rotated about the axis 13 and the two flanged elements 24 and 26 are rotated around their respective axes 28 and 30. These are rotated by the rotary movement of the rotor 12 about its axis 13 which rotates 2 primary axes 36 and 38 by means of the belt 40.
- the axes 36 and 38 communicate the rotational movement respectively to the axes 28 and 30 by means of angle deflectors 60 and 62.
- the diameter of the axes 36 and 38 is equal to half the diameter of the axis 13.
- the axes 36 and 38 being driven by the belt 40, their rotation speed is twice the speed of rotation of the rotor 12. It would be possible to rotate the flanged elements at the same speed as the rotor. But this would require having 4 recesses in each flange instead of 2 as is the case in the embodiment described above. One could even have a single flanged element rotating at the same speed as the rotor. But the diameter of the flanged element should be double, which would increase the size.
- the motor which has just been described has a motor torque which is a function of the diameter of the rotor.
- the rotor may have a diameter of 40 cm, which allows to obtain a motor torque 5 times greater than the engine torque of an alternating motor whose piston stroke is 8 cm.
- the rotary engine just described comprises a spring (not shown) located at the rear of each piston which keeps the piston in contact with the surface of the stator. As the speed increases after the engine has been started, the springs compress with centrifugal force and the pistons move slightly away from the stator surface. When the optimum speed is reached, this speed is such that there is a speed-induced sealing without the need for contact. When the engine is stopped, the pistons retract to come into contact with the stator surface and seal at startup. Since there is no friction on the rotor when it rotates, it is not necessary to put lubricant.
- a ventilation device at the rear of the engine forces the air to pass inside the engine so as to cool all rotating parts.
- the preferred embodiment is a rotary explosion engine, it is possible to operate the engine with compressed air.
- a compressed air inlet pipe for each stator recess, the pipe 64 for the recess 42 and the pipe 66 for the recess 44.
- a simple contactor is sufficient to remove fuel injection by the petrol inlet pipes 46 and 48 and open the compressed air supply pipes 64 and 66.
- the compressed air is at a pressure of about 30 bar which corresponds to the gas pressure after explosion in the chamber.
- the compressed air is injected into the compression chamber when the compression piston is at the end of the compression chamber, the transit flange being open and producing the same motor force as the explosion of the compression chamber. mixture of air and gasoline from the same engine.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Supercharger (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0900392A FR2941740B1 (fr) | 2009-01-30 | 2009-01-30 | Moteur rotatif a rotor circulaire |
PCT/FR2009/001104 WO2010086516A2 (fr) | 2009-01-30 | 2009-09-18 | Moteur rotatif à rotor circulaire |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2391801A2 true EP2391801A2 (de) | 2011-12-07 |
Family
ID=40933744
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09740176A Withdrawn EP2391801A2 (de) | 2009-01-30 | 2009-09-18 | Drehkolbenmotor mit einem ringförmigen rotor |
Country Status (5)
Country | Link |
---|---|
US (1) | US8689763B2 (de) |
EP (1) | EP2391801A2 (de) |
JP (1) | JP2012516408A (de) |
FR (1) | FR2941740B1 (de) |
WO (1) | WO2010086516A2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3086689A1 (fr) | 2018-10-01 | 2020-04-03 | Patrice Christian Philippe Charles Chevalier | Moteur a hydrogene a chambre torique et cylindree variable, et procedes associes |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0815766D0 (en) * | 2008-08-29 | 2008-10-08 | Lontra Ltd | Rotary piston and cylinder devices |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE339761C (de) * | 1920-01-20 | 1921-08-06 | Reinhard Alt | Verbrennungskraftmaschine mit zwei in einem Ringzylinder kreisenden Kolben |
DE1114825B (de) * | 1960-02-03 | 1961-10-12 | Walter Rosch | Umlaufende Kraft- und Arbeitsmaschine |
DE1553050C3 (de) * | 1965-03-01 | 1979-10-04 | George Anthony Mount Martha Victoria Fairbairn (Australien) | Rotationskolbenmaschine mit einem Ringzylinder |
US3739754A (en) * | 1970-12-03 | 1973-06-19 | A Nutku | Rotating-piston toroidal machine with rotating-disc abutment |
DE2304333A1 (de) * | 1973-01-30 | 1974-08-01 | Agropol Ag | Kreisringkolbenmaschine |
DE3146782A1 (de) * | 1981-11-25 | 1983-06-01 | Peter 8650 Kulmbach Leitholf | Rotationskolbenmaschine |
US5131359A (en) * | 1989-11-09 | 1992-07-21 | Gomm Thiel J | Rotating head and piston engine |
DE29522008U1 (de) * | 1995-01-19 | 1999-07-29 | Raab, Anton Gerhard, 80686 München | Kraftmaschine |
GB2333561B (en) * | 1998-01-21 | 2002-03-20 | John Edward Archer | Rotary machine |
US20050045841A1 (en) * | 2003-08-25 | 2005-03-03 | Hartman Delbert Lee | Transverse disc motor |
US7059294B2 (en) * | 2004-05-27 | 2006-06-13 | Wright Innovations, Llc | Orbital engine |
US8151759B2 (en) * | 2006-08-24 | 2012-04-10 | Wright Innovations, Llc | Orbital engine |
-
2009
- 2009-01-30 FR FR0900392A patent/FR2941740B1/fr not_active Expired - Fee Related
- 2009-09-18 EP EP09740176A patent/EP2391801A2/de not_active Withdrawn
- 2009-09-18 US US13/147,058 patent/US8689763B2/en not_active Expired - Fee Related
- 2009-09-18 WO PCT/FR2009/001104 patent/WO2010086516A2/fr active Application Filing
- 2009-09-18 JP JP2011546900A patent/JP2012516408A/ja not_active Withdrawn
Non-Patent Citations (1)
Title |
---|
See references of WO2010086516A2 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3086689A1 (fr) | 2018-10-01 | 2020-04-03 | Patrice Christian Philippe Charles Chevalier | Moteur a hydrogene a chambre torique et cylindree variable, et procedes associes |
Also Published As
Publication number | Publication date |
---|---|
US20120023917A1 (en) | 2012-02-02 |
FR2941740B1 (fr) | 2011-02-11 |
WO2010086516A2 (fr) | 2010-08-05 |
WO2010086516A3 (fr) | 2010-09-30 |
US8689763B2 (en) | 2014-04-08 |
FR2941740A1 (fr) | 2010-08-06 |
JP2012516408A (ja) | 2012-07-19 |
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Legal Events
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18D | Application deemed to be withdrawn |
Effective date: 20140716 |