FR2651828A1 - Engine with a rotary piston - Google Patents

Engine with a rotary piston Download PDF

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Publication number
FR2651828A1
FR2651828A1 FR8912006A FR8912006A FR2651828A1 FR 2651828 A1 FR2651828 A1 FR 2651828A1 FR 8912006 A FR8912006 A FR 8912006A FR 8912006 A FR8912006 A FR 8912006A FR 2651828 A1 FR2651828 A1 FR 2651828A1
Authority
FR
France
Prior art keywords
rotary piston
caps
piston
engine
housing
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.)
Pending
Application number
FR8912006A
Other languages
French (fr)
Inventor
Lassee
Guy
Marie
Robert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LASSEE GUY
Original Assignee
LASSEE GUY
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by LASSEE GUY filed Critical LASSEE GUY
Priority to FR8912006A priority Critical patent/FR2651828A1/en
Publication of FR2651828A1 publication Critical patent/FR2651828A1/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-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
    • F01C1/40Rotary-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
    • F01C1/44Rotary-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 inner member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The innovation relates to an engine with a rotary piston. It is characterised by a case (1) having the shape of two semicircles joined together so that they are slightly separated, and closed by two caps which are traversed at their centre by a shaft (3) on which is fixed a rotary piston (2) equipped with four articulated and guided arms (4.5.6.7.) which create chambers (10.12.13.14.) with the internal casing of the case. The variation in the volume of these chambers brings together the conditions necessary for the operation of a compression-ignition or spark-ignition internal combustion engine.

Description

Depuis plusieurs années, de nombreuses études ont été effectuées sur les moteurs à pistons rotatifs. Seuls quelques moteurs de ce genre ont été commercialisés et à ce jour, ils n'arrivent pas à concurencer les moteurs à pistons alternatifs. For several years, numerous studies have been carried out on rotary piston engines. Only a few such engines have been marketed and to date they cannot compete with reciprocating piston engines.

La présente invention, par sa simplicité, ne devant pas poser de problèmes techniques -insurmontables, devrait permettre la construction d'un moteur à piston rotatif compétitif. The present invention, by its simplicity, should not pose -insurmountable technical problems, should allow the construction of a competitive rotary piston engine.

Le principe de fonctionnement est le suivant:
Un axe traverse en son centre le carter constituant l'enveloppe du moteur, fermé par deux chapeaux. Ce carter a la forme de deux de deux demi-cercles reliés de façon légèrement écartés. Sur cet axe est fixé un piston rotatif muni de quatre bras usinés de telle façon que les sommets de ces bras soient les arcs d'un cercle imaginaire ayant pour centre le milieu de l'axe et que ces arcs, lors de leur rotation, affleurent les parties aplaties du carter. Sur une des faces de chaque bras, un piston oscillant est articulé et, l'autre face est usinée de façon à permettre l'oscillation de la tête de piston. Les chapeaux de carter sont rainurés à une distance constante des parois du carter et, la partie intérieure des têtes de piston est munie d'ergots sur lesquels sont fixées des pièces qui coulisseront dans ces rainures.L'angle extérieur des têtes de piston est donc toujours en contact avec la paroi du carter.
The operating principle is as follows:
An axis crosses in its center the casing constituting the envelope of the engine, closed by two caps. This housing has the form of two of two semicircles connected in a slightly spaced manner. On this axis is fixed a rotary piston provided with four arms machined in such a way that the vertices of these arms are the arcs of an imaginary circle having for center the center of the axis and that these arcs, during their rotation, are flush the flattened parts of the housing. On one face of each arm, an oscillating piston is articulated and, the other face is machined so as to allow the oscillation of the piston head. The crankcases are grooved at a constant distance from the walls of the crankcase and, the interior part of the piston heads is provided with lugs on which are fixed parts which will slide in these grooves. The outside angle of the piston heads is therefore always in contact with the housing wall.

La figure 1 représente, en coupe, une vue intérieure du moteur
La figure 2 représente la partie intérieure du chapeau de carter
La fifure 3 représente une vue en perspective d'un piston oscillant.
Figure 1 shows, in section, an interior view of the engine
Figure 2 shows the inner part of the crankcase cap
The fifure 3 represents a perspective view of an oscillating piston.

A l'intérieur du carter I, le piston rotatif 2, fixé sur l'axe 3, tourne dans le sens de la flèche F. Lors de cette rotation selon la figure 1, le piston 4, guidé par la rainure 8 des chapeaux et la pièce baladeuse de l'ergot 9, crée une chambre 10 entre les pistons 4 et 7, en aspirant du mélange en Il. En même temps, la chambre 12, créé précédemment entre les pistons 4 et 5, commence à se compresser. La chambre 13 formée par les pistons 5 et 6 est complètement compressée et c'est ltexplosion-détente; la chambre 14 formée par les pistons 6 et 7 commence l'évacuation des gaz brûlés en 15. Inside the housing I, the rotary piston 2, fixed on the axis 3, rotates in the direction of the arrow F. During this rotation according to FIG. 1, the piston 4, guided by the groove 8 of the caps and the wandering part of the lug 9, creates a chamber 10 between the pistons 4 and 7, by sucking mixture in It. At the same time, the chamber 12, previously created between the pistons 4 and 5, begins to compress. The chamber 13 formed by the pistons 5 and 6 is completely compressed and it is explosion-detent; the chamber 14 formed by the pistons 6 and 7 begins the evacuation of the burnt gases at 15.

Les quatre temps du moteur à explosion sont donc simultanés. The four times of the internal combustion engine are therefore simultaneous.

La face du piston exposée à l'explosion sera légèrement creusée en son centre pour recevoir une poussée perpendiculaire à cette face (20). Afin de supprimer les compressions dans les logements des pistons oscillants, les chapeaux seront percés de façon circulaire 15 (fig.2), à la base des logements de ces pistons. Pour assurer l'étanchéité des chambres, les pistons seront munis d'au moins un joint 16 sur les faces latérales, allant de l'axe du piston oscillant, jusqu'à la tête côté intérieur, et d'un joint 17 passant par l'angle extérieur de la tête de piston et rejoignant le joint 16. Les bras du piston rotatif auront également au moins un joint d'étanchéité 18 entre les chapeaux et des garnitures d'épousement 19 entre les têtes de piston. The face of the piston exposed to the explosion will be slightly hollowed out in its center to receive a thrust perpendicular to this face (20). In order to eliminate the compressions in the housings of the oscillating pistons, the caps will be drilled in a circular manner 15 (fig. 2), at the base of the housings of these pistons. To ensure the tightness of the chambers, the pistons will be provided with at least one seal 16 on the lateral faces, going from the axis of the oscillating piston, to the head on the interior side, and with a seal 17 passing through the external angle of the piston head and joining the seal 16. The arms of the rotary piston will also have at least one seal 18 between the caps and marrying fittings 19 between the piston heads.

Selon la description de fonctionnement de ce moteur, on peut, en fonction de l'écartement donné aux deux demi-cercles du carter, faire varier les compressions afin d'obtenir un moteur à explosion ou un moteur fonctionnant comme un moteur diésel.  According to the operating description of this engine, it is possible, depending on the spacing given to the two semicircles of the casing, to vary the compressions in order to obtain an internal combustion engine or an engine operating as a diesel engine.

Claims (4)

REVENDICATIONS 1. Moteur à piston rotatif, caractérisé par le fait qu'un piston rotatif (2) muni de quatre pistons oscillants (4;5;6;7) fixés sur ses quatre bras, logé centralement dans un carter en forme de deux demi-cercles reliés-écartés en fonction des compressions à obtenir. Le carter est fermé par deux chapeaux(fig.2), traversés en leur centre par l'axe du piston rotatif, comportant des rainures ou tout autre moyen de guidage(8) à distance constante des parois de carter; rainures dans lesquelles coulissent les pièces de guidage(9) des têtes de pistons oscillants. 1. Rotary piston motor, characterized in that a rotary piston (2) provided with four oscillating pistons (4; 5; 6; 7) fixed on its four arms, housed centrally in a casing in the form of two half connected-spread circles depending on the compressions to be obtained. The housing is closed by two caps (fig. 2), crossed at their center by the axis of the rotary piston, comprising grooves or any other guide means (8) at constant distance from the housing walls; grooves in which the guide parts (9) of the oscillating piston heads slide. 2. Moteur caractérisé selon la revendication 1, par le fait que les faces latérales des bras du piston rotatif touchent de manière étanche, par l'intermédiaire de joints (18), les parois des chapeaux de carter. 2. Motor characterized according to claim 1, in that the lateral faces of the arms of the rotary piston sealingly touch, by means of seals (18), the walls of the casing caps. 3. Moteur caractérisé selon l'une quelconque des revendications 1 et 2 par le fait que les pistons oscillants touchent de manière étanche la paroi du carter et les parois des chapeaux par l'intermédiaire de joints ( 16.17 ). 3. Motor characterized according to any one of claims 1 and 2 in that the oscillating pistons sealingly touch the wall of the housing and the walls of the caps by means of seals (16.17). 4. Moteur caractérisé selon l'une quelconque des revendications 1,2 et 3 par le fait que les pistons oscillants sont creusés dans la face exposée à l'explosion pour recevoir une poussée perpendiculaire à cette face (20).  4. Motor characterized according to any one of claims 1,2 and 3 in that the oscillating pistons are hollowed out in the face exposed to the explosion to receive a thrust perpendicular to this face (20).
FR8912006A 1989-09-11 1989-09-11 Engine with a rotary piston Pending FR2651828A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8912006A FR2651828A1 (en) 1989-09-11 1989-09-11 Engine with a rotary piston

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8912006A FR2651828A1 (en) 1989-09-11 1989-09-11 Engine with a rotary piston

Publications (1)

Publication Number Publication Date
FR2651828A1 true FR2651828A1 (en) 1991-03-15

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Family Applications (1)

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FR (1) FR2651828A1 (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995008699A1 (en) * 1993-09-22 1995-03-30 Eric Edward Austin A rotary vane engine
WO1995016116A1 (en) * 1993-12-06 1995-06-15 Christopher Bernard Wade Rotary engine
FR2720785A1 (en) * 1994-06-03 1995-12-08 Roger Coulmeau Four stroke rotary ignition engine
FR2760787A1 (en) * 1997-03-12 1998-09-18 Max Anglade IC engine with cylindrical rotor used for two- or four- stroke engine, pump, compressor or hydraulic motor
US6457450B1 (en) * 2000-03-01 2002-10-01 Jury Mikhaylovich Luzhkov Ju. M. Luzhkov rotary-turbine internal combustion engine
US6668767B1 (en) * 1999-09-08 2003-12-30 Sanchez Talero John Alejandro Internal combustion engine rotatory (turbovolante)
US6776135B1 (en) * 2003-03-03 2004-08-17 Tsung-Yun Chen Rotary engine
US7143737B2 (en) * 2002-09-25 2006-12-05 Dong-Hyun Kim Rotary engine
JP2008516148A (en) * 2004-10-07 2008-05-15 ジャイロトン・インコーポレーテッド Multilobe rotationally asymmetric compression / expansion engine
US20150040854A1 (en) * 2013-08-12 2015-02-12 Jung-Kuang Chou Rotary Engine
EP3947913A4 (en) * 2019-03-29 2022-12-21 Genesis Advanced Technology Inc. Expandable pistons

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1790256A (en) * 1927-11-28 1931-01-27 Corwin R Wright Internal-combustion engine
GB1070592A (en) * 1962-11-22 1967-06-01 Johann Geiger Improvements in and relating to rotary piston internal combustion engines
FR2121906A5 (en) * 1971-01-11 1972-08-25 Woywode Karl
DE2319257A1 (en) * 1973-04-16 1974-10-31 Joseph Rogl ROTARY PISTON ENGINE
DE2801511A1 (en) * 1978-01-12 1979-07-19 Karl Woywode Four stroke rotary IC engine - has pivoting vanes on central rotor guided by pins in grooves in stator end plates

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1790256A (en) * 1927-11-28 1931-01-27 Corwin R Wright Internal-combustion engine
GB1070592A (en) * 1962-11-22 1967-06-01 Johann Geiger Improvements in and relating to rotary piston internal combustion engines
FR2121906A5 (en) * 1971-01-11 1972-08-25 Woywode Karl
DE2319257A1 (en) * 1973-04-16 1974-10-31 Joseph Rogl ROTARY PISTON ENGINE
DE2801511A1 (en) * 1978-01-12 1979-07-19 Karl Woywode Four stroke rotary IC engine - has pivoting vanes on central rotor guided by pins in grooves in stator end plates

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995008699A1 (en) * 1993-09-22 1995-03-30 Eric Edward Austin A rotary vane engine
WO1995016116A1 (en) * 1993-12-06 1995-06-15 Christopher Bernard Wade Rotary engine
FR2720785A1 (en) * 1994-06-03 1995-12-08 Roger Coulmeau Four stroke rotary ignition engine
FR2760787A1 (en) * 1997-03-12 1998-09-18 Max Anglade IC engine with cylindrical rotor used for two- or four- stroke engine, pump, compressor or hydraulic motor
US6668767B1 (en) * 1999-09-08 2003-12-30 Sanchez Talero John Alejandro Internal combustion engine rotatory (turbovolante)
US6457450B1 (en) * 2000-03-01 2002-10-01 Jury Mikhaylovich Luzhkov Ju. M. Luzhkov rotary-turbine internal combustion engine
US7143737B2 (en) * 2002-09-25 2006-12-05 Dong-Hyun Kim Rotary engine
US6776135B1 (en) * 2003-03-03 2004-08-17 Tsung-Yun Chen Rotary engine
JP2008516148A (en) * 2004-10-07 2008-05-15 ジャイロトン・インコーポレーテッド Multilobe rotationally asymmetric compression / expansion engine
US20150040854A1 (en) * 2013-08-12 2015-02-12 Jung-Kuang Chou Rotary Engine
US9556788B2 (en) * 2013-08-12 2017-01-31 Jung-Kuang Chou Rotary engine
EP3947913A4 (en) * 2019-03-29 2022-12-21 Genesis Advanced Technology Inc. Expandable pistons

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