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WO2007132071A1 - Lubrication and cooling of rotary piston engines - Google Patents

Lubrication and cooling of rotary piston engines Download PDF

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Publication number
WO2007132071A1
WO2007132071A1 PCT/FR2006/001069 FR2006001069W WO2007132071A1 WO 2007132071 A1 WO2007132071 A1 WO 2007132071A1 FR 2006001069 W FR2006001069 W FR 2006001069W WO 2007132071 A1 WO2007132071 A1 WO 2007132071A1
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WO
WIPO (PCT)
Prior art keywords
rotor
oil
machine according
cylindrical
bore
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.)
Ceased
Application number
PCT/FR2006/001069
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French (fr)
Inventor
Roland Raso
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MRCC INDUSTRIES Sas
Original Assignee
MRCC INDUSTRIES Sas
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Filing date
Publication date
Application filed by MRCC INDUSTRIES Sas filed Critical MRCC INDUSTRIES Sas
Priority to PCT/FR2006/001069 priority Critical patent/WO2007132071A1/en
Publication of WO2007132071A1 publication Critical patent/WO2007132071A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • 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
    • F01C1/02Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F01C1/063Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them
    • 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
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/04Lubrication

Definitions

  • the present invention relates to improvements relating to a rotary piston machine used in particular as a heat engine. More specifically, the present invention aims to improve the lubrication and cooling of a thermal machine of the type described in patent EP 748 415 and in US Patent 5,992,371.
  • This machine comprises a motor unit in which is machined a cylindrical bore in which are interposed two rotors forming with the cylindrical bore two diametrically opposed working chambers in each of which evolves a gaseous mixture according to the phases of a suitable thermodynamic cycle.
  • One of the rotors is driven in a continuous rotational movement while the other is animated by an intermittent rotational movement at a speed double that of the rotor with continuous movement so as to achieve cyclic volumic variations of the two. working rooms.
  • the continuously moving rotor has a central bore passing therethrough and two diametrically opposed recesses.
  • the rotor with intermittent movement is constituted by a cylindrical shaft rotatably mounted in the central bore of the rotor with continuous movement and by two vanes integral with the shaft arranged diametrically opposite pistons, and engaged in the recesses of the rotor movement continued.
  • Each of these pallets delimits with the corresponding recess, a working chamber in which evolves a gas mixture and a passive rear chamber.
  • a hydraulic pump hydraulically connected to a hydraulic motor coupled to the intermittently operating rotor.
  • a valve mechanism which ensures the opening of the circuit during the intake and expansion phases to release the rotation of the intermittent rotor and its closure during the compression phases and exhaust to rotate the intermittent rotor during these phases.
  • the intermittent rotor is also mechanically associated with an angular stop mechanism opposing its backward rotation during the intake and expansion phases.
  • each rotor comprises at least one lubricating means capable of delivering a metered quantity of lubricating fluid on the surfaces of each working chamber in front of the sealing segments considering the direction of rotation of the rotors.
  • each lubricating means is constituted by:
  • At least one lubricator connected to a lubricant supply circuit and having a lubricating head with a lubricating orifice held in abutment against the surface to be lubricated by an elastic member, - and at least one hollow form formed in said surface, in the path of the orifice of the greaser head to fill said recessed form of lubricating fluid.
  • FIG. 1 is a longitudinal sectional view of a machine according to the invention
  • FIG. 2 is a cross-sectional view along the line AA of FIG. 1,
  • FIG. 3 is a perspective view of a rotor with continuous movement
  • FIG. 4 is a front view of an intermittently moving rotor
  • FIG. 5 is a sectional view along line BB of FIG. 4,
  • FIG. 6 is a sectional view of a lubricator
  • FIG. 7 is a partial view in longitudinal section of a rotor with continuous movement
  • FIG. 8 is a view in longitudinal section of the two rotors mounted one inside the other
  • the bore 2 of the engine block 1 comprises two hydrodynamic bearings 20 spaced apart from each other for supporting the rotor 3 with continuous movement.
  • This rotor constitutes the power output shaft of the engine.
  • Each recess 8 that comprises the rotor with continuous movement 3, in a section perpendicular to the axis of said rotor conforms to the contour of a circular crown sector.
  • the recess 8 has a cross section of rectangular or square shape.
  • the recess 8 opens into the bore 7.
  • the rotor 4 with intermittent movement is supported by two hydrodynamic bearings 21 mounted at a distance from each other each in a housing coaxial with the bore 7 of the rotor 3.
  • the shaft 9 of the rotor 4 is provided with a longitudinal through bore 4a.
  • the rotor 3 with continuous movement accomplishes about a quarter turn.
  • the rotor 4 with intermittent movement during the phases of admission of the gaseous mixture into each working and expansion chamber of the gases is secured by a non-return mechanism to remain angularly fixed relative to the engine block at least in the backward direction, while during each of the compression phases of the gaseous mixture and the exhaust of the flue gases it is subjected by a motion transmission means to perform approximately one half-turn relative to the engine block 1.
  • the rotor with movement intermittent 4 performed relative to the rotor with continuous movement 3 about a quarter turn.
  • each radial recess 8 of the rotor with continuous movement 3 on the outer cylindrical surface of this rotor 3, and on the cylindrical surface of the axial bore 7 that comprises the latter, are formed respectively an external sealing barrier 11 and a barrier internal sealing 12.
  • each pallet of the intermittent rotor comprises at least one sealing barrier 13, the latter being formed continuously on the radial lateral banks 10a of the pallet 10 and on the front edge 10b of the latter.
  • the outer 11 and inner 12 sealing gates each comprise two arcuate circumferential side portions disposed respectively on either side of the radial recesses and at least one rectilinear part extending from one to the other part. lateral.
  • the external sealing barrier 11 of the continuous-motion rotor 3 is supported on the cylindrical surface of the bore 2 of the engine block 1, and the internal sealing barrier 12 that comprises the continuously-moving rotor 3 is supported on the cylindrical surface of the shaft 9 of the intermittently moving rotor 3.
  • Each sealing barrier 13 formed on each pallet 10 of the rotor with intermittent movement bears on the lateral faces of the corresponding recess 8 and on the cylindrical face of the bore 2 of the engine block.
  • each rotor 3, 4 comprises at least one lubricating means capable of delivering a metered quantity of lubricating fluid. on the surfaces of each working chamber in front of the sealing segments by considering the direction of rotation of the rotors, said lubricating means being fed by an oil circuit comprising an external oil pump.
  • each greasing means is constituted by at least one grease fitting 22 mounted in a bore made in the rotor 3, 4 corresponding.
  • This lubricator is connected to a delivery circuit of a lubricating fluid and comprises a lubricating head 23 with a lubricating orifice 24 held in abutment against the corresponding surface of the working chamber by an elastic member 25.
  • the lubricating means is also formed by recessed shapes formed in the surfaces of the working chamber, on the path of the orifice of the head of the nipples to receive lubricating fluid.
  • these recessed shapes are micro-cavities capable of retaining the lubricating fluid, formed by surface treatment such as honing.
  • each grease nipple 22 has a cylindrical tubular body comprising, perpendicular to its longitudinal axis, a convex end face in a truncated cone forming the head 23, said body being pierced axially from one side of a delivery channel. of oil at the orifice 24 of the truncated cone head.
  • the elastic member 25 keeps the head 23 of the grease nipple 22 applied against the corresponding surface of the working chamber 5.
  • the lubrication orifice 24 is normally closed off by this surface and the oil can not escape. However, as soon as it is facing a cavity of this surface, the oil can then escape and fill the cavity. The oil present in this cavity will then be swept by the associated segment to be spread over the entire corresponding surface of the working chamber 5.
  • the tubular body of the grease nipple 22 has a counterbore for receiving the associated elastic member, said elastic member 25 being constituted by a spring with non-contiguous turns.
  • the oil supply channel opens into this counterbore.
  • the nipples 22 associated with the intermittent rotor 4 are mounted in bores made in each pallet 10 and opening into the side faces 10a thereof. Still according to this arrangement, said bores are in communication with channels made in the rotor 4 with intermittent movement and opening into the axial bore 4a of the shaft of said rotor to the right, each, of an oil distribution groove performed in an oil distribution ring 28 mounted in the bore 4a. As is understood, two oil distribution rings 28 are provided respectively associated with the lubricators 22 that comprise the two radial banks 10a of the pallet 10.
  • This shaft is also equipped with radial channels 29 opening on the one hand into the bore 4a, the right of the oil distribution groove of the oil distribution ring 28, and secondly in its outer cylindrical face, to the right of an oil supply chamber 30 formed in a ring rotated in the rotor with continuous movement, this ring advantageously constituting the body of the hydrodynamic bearing 21.
  • the bearing body 21 comprises an oil chamber supplied with oil by the oil circuit.
  • two hydrodynamic bearings 21 are provided. Each bearing ensures the rotational guidance of the intermittently moving rotor 4 in the rotor with continuous movement 3.
  • the grease nipples 22 of the rotor with continuous movement 3 are mounted in cylindrical bores made in the body of said rotor 3 and opening for some on the outer cylindrical face of said rotor and for the others on the inner cylindrical face. of this rotor.
  • These bores are in communication with oil supply channels 32 formed in the rotor with continuous movement, parallel to its longitudinal axis, said channels 32 for supplying oil also supplying oil to the hydrodynamic bearings 21 supporting the rotor with intermittent movement in the rotor with continuous movement and the hydrodynamic bearings 20 supporting the rotor with continuous movement 3 in the engine block 1, said longitudinal channels being supplied with oil by an external pump via one or several rotary joints.
  • the oil circuit also ensures the cooling of the engine.
  • the oil circuit comprises one or more longitudinal return channels formed in the rotor with continuous movement 3 and each longitudinal feed and / or return channel is equipped with a means adapted to create a turbulent flow regime of oil to increase the degree of heat transfer between the rotor 3 and this oil.
  • This means capable of creating the turbulent regime present in the corresponding channel, in the flow path of the oil a series of reliefs.
  • the means capable of creating a turbulent regime forces the oil to follow a helical path in the corresponding channel. This increases the length of the path of the oil flow and its speed in the corresponding channel and consequently its effectiveness.
  • the means capable of creating a turbulent regime and forcing the oil to follow a helical path may be constituted by an axial pin 33 occupying a central position in the channel and by a helical structure 34 wound around the central pin 33 and extending longitudinally along the entire length of the pin and extending radially from said pin 33 to the cylindrical inner face of said channel.
  • the rotor with continuous movement 3 is associated with a hydrodynamic axial stop 35 fed by the oil circuit, interposed between the engine block 1 and the rotor 3 with continuous movement.
  • This hydrodynamic axial stop 35 is intended to contain the axial movements of the rotor with continuous movement 3.
  • This axial abutment 35 has two opposed active bearing faces 351 provided with several cavities 352 for the formation of oil wedges .
  • the oil circuit provides, as is understood, several functions, namely a lubrication function, a cooling function for the rotors and a feed function for the hydrodynamic bearings 20, 21. It goes without saying that the present invention can receive all the arrangements and variants of the field of technical equivalents without departing from the scope of this patent.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Abstract

The heat engine concerned comprises a cylinder block in which a cylindrical borehole is formed, said borehole containing two coaxially mounted rotors penetrating thereinto, one rotor (3) rotating continuously and the other intermittently. Together with the cylindrical borehole, said rotors define two working chambers in which a gaseous mixture forms according to an appropriate thermodynamic cycle. The sealing of the chambers is ensured by the segmentation created by sealing barriers mounted on the two rotors. At least the continuously moving rotor (3) comprises at least one pressurised oil circuit especially for ensuring the oiling, by means of oilers (22), of the segmentation (11, 12) associated with the continuously moving rotor (3) and the segmentation associated with the intermittently moving rotor.

Description

LUBRIFICATION ET REFROIDISSEMENT DES MACHINES A PISTONS ROTATIFS LUBRICATION AND COOLING OF ROTARY PISTON MACHINES

La présente invention a pour objet des perfectionnements relatifs à une machine à pistons rotatifs utilisable notamment en tant que moteur thermique. Plus précisément la présente invention vise à améliorer le graissage et le refroidissement d'une machine thermique du type de celle décrite dans le brevet EP 748 415 et dans le brevet US 5 992 371.The present invention relates to improvements relating to a rotary piston machine used in particular as a heat engine. More specifically, the present invention aims to improve the lubrication and cooling of a thermal machine of the type described in patent EP 748 415 and in US Patent 5,992,371.

Cette machine comporte un bloc moteur dans lequel est usiné un alésage cylindrique dans lequel sont montés en interpénétration deux rotors formant avec l'alésage cylindrique deux chambres de travail diamétralement opposées dans chacune desquelles évolue un mélange gazeux selon les phases d'un cycle thermodynamique approprié. L'un des rotors est animé d'un mouvement de rotation continu tandis que l'autre est animé d'un mouvement de rotation intermittent selon une vitesse double de celle du rotor à mouvement continu de façon à réaliser des variations volumiques, cycliques des deux chambres de travail. Le rotor à mouvement continu présente un alésage central le traversant de part en part et deux évidements diamétralement opposés. Le rotor à mouvement intermittent est constitué par un arbre cylindrique monté en rotation dans l'alésage central du rotor à mouvement continu et par deux palettes solidaires de l'arbre disposées de manière diamétralement opposées formant pistons, et engagées dans les évidements du rotor à mouvement continu. Chacune de ces palettes délimite avec l'évidement correspondant, une chambre de travail dans laquelle évolue un mélange gazeux et une chambre arrière passive.This machine comprises a motor unit in which is machined a cylindrical bore in which are interposed two rotors forming with the cylindrical bore two diametrically opposed working chambers in each of which evolves a gaseous mixture according to the phases of a suitable thermodynamic cycle. One of the rotors is driven in a continuous rotational movement while the other is animated by an intermittent rotational movement at a speed double that of the rotor with continuous movement so as to achieve cyclic volumic variations of the two. working rooms. The continuously moving rotor has a central bore passing therethrough and two diametrically opposed recesses. The rotor with intermittent movement is constituted by a cylindrical shaft rotatably mounted in the central bore of the rotor with continuous movement and by two vanes integral with the shaft arranged diametrically opposite pistons, and engaged in the recesses of the rotor movement continued. Each of these pallets delimits with the corresponding recess, a working chamber in which evolves a gas mixture and a passive rear chamber.

À ce rotor à mouvement continu est accouplée une pompe hydraulique connectée hydrauliquement à un moteur hydraulique accouplé au rotor à fonctionnement intermittent. Sur le circuit hydraulique entre la pompe et le moteur est prévu un mécanisme de clapets qui assure l'ouverture du circuit pendant les phases d'admission et de détente afin de libérer la rotation du rotor à mouvement intermittent et sa fermeture pendant les phases de compression et d'échappement afin d'entraîner en rotation le rotor à mouvement intermittent pendant ces phases. Le rotor à mouvement intermittent est par ailleurs mécaniquement associé à un mécanisme de butée angulaire s'opposant à sa rotation rétrogire pendant les phases d'admission et de détente.To this continuously moving rotor is coupled a hydraulic pump hydraulically connected to a hydraulic motor coupled to the intermittently operating rotor. On the hydraulic circuit between the pump and the engine is provided a valve mechanism which ensures the opening of the circuit during the intake and expansion phases to release the rotation of the intermittent rotor and its closure during the compression phases and exhaust to rotate the intermittent rotor during these phases. The intermittent rotor is also mechanically associated with an angular stop mechanism opposing its backward rotation during the intake and expansion phases.

Le but de l'invention est notamment d'améliorer le graissage et le refroidissement de ce type de moteur. À cet effet le moteur du genre précité se caractérise essentiellement en ce que chaque rotor comporte au moins un moyen de graissage apte à délivrer une quantité dosée de fluide de lubrification sur les surfaces de chaque chambre de travail en avant des segments d'étanchéité en considérant le sens de rotation des rotors. Selon une autre caractéristique de l'invention, chaque moyen de graissage est constitué par :The object of the invention is in particular to improve the lubrication and cooling of this type of engine. For this purpose the engine of the aforementioned type is essentially characterized in that each rotor comprises at least one lubricating means capable of delivering a metered quantity of lubricating fluid on the surfaces of each working chamber in front of the sealing segments considering the direction of rotation of the rotors. According to another characteristic of the invention, each lubricating means is constituted by:

- au moins un graisseur connecté à un circuit de délivrance d'un fluide de graissage et comportant une tête de graissage avec un orifice de graissage maintenu en appui contre la surface à lubrifier par un organe élastique, - et au moins une forme en creux formée dans ladite surface, sur la trajectoire de l'orifice de la tête du graisseur pour remplir ladite forme en creux de fluide de graissage.- At least one lubricator connected to a lubricant supply circuit and having a lubricating head with a lubricating orifice held in abutment against the surface to be lubricated by an elastic member, - and at least one hollow form formed in said surface, in the path of the orifice of the greaser head to fill said recessed form of lubricating fluid.

D'autres avantages, buts et caractéristiques de l'invention apparaîtront à la lecture de la description d'une forme préférée de réalisation donnée à titre d'exemple non limitatif en se référant aux dessins annexés en lesquels :Other advantages, aims and features of the invention will appear on reading the description of a preferred embodiment given by way of non-limiting example with reference to the appended drawings in which:

- la figure 1 est une vue en coupe longitudinale d'une machine selon l'invention,FIG. 1 is a longitudinal sectional view of a machine according to the invention,

- la figure 2 est une vue en coupe transversale selon la ligne AA de la figure 1 ,FIG. 2 is a cross-sectional view along the line AA of FIG. 1,

- la figure 3 est une vue en perspective d'un rotor à mouvement continu,FIG. 3 is a perspective view of a rotor with continuous movement,

- la figure 4 est une vue de face d'un rotor à mouvement intermittent, - la figure 5 est une vue en coupe selon la ligne BB de la figure 4,FIG. 4 is a front view of an intermittently moving rotor, FIG. 5 is a sectional view along line BB of FIG. 4,

- la figure 6 est une vue en coupe d'un graisseur,FIG. 6 is a sectional view of a lubricator,

- la figure 7 est une vue partielle en coupe longitudinale d'un rotor à mouvement continu,FIG. 7 is a partial view in longitudinal section of a rotor with continuous movement,

- la figure 8 est une vue en coupe longitudinale des deux rotors montés l'un dans l'autre,FIG. 8 is a view in longitudinal section of the two rotors mounted one inside the other,

- la figure 9 est une vue en coupe selon la ligne CC de la figure 8, - la figure 10 est une vue de face d'une butée hydraulique. Telle que représentée, la machine à pistons rotatifs selon l'invention, est utilisable principalement en tant que moteur thermique à allumage commandé ou diesel comprend un bloc moteur 1 dans lequel est réalisé un alésage cylindrique 2 dans lequel sont montés de manière coaxiale en interpénétration deux rotors 3, 4 dont un, le rotor 3 est à mouvement de rotation continu et présente un perçage axial 7 et deux évidements radiaux 8, diamétralement opposés, débouchant d'une part dans le perçage axial et d'autre part dans la surface cylindrique externe et dont l'autre rotor, le rotor 4 est à mouvement intermittent et comprend un arbre cylindrique 9 engagé de manière libre en rotation dans le perçage axial 7 du rotor à mouvement continu, et deux palettes radiales 10 diamétralement opposées, formant piston, fixées à l'arbre 9 et engagées dans les évidements radiaux 8 de façon à pouvoir s'y déplacer angulairement, chacune des dites palettes formant avec l'évidement radial 8 correspondant et avec l'alésage 2 du bloc moteur 1 en considérant le sens de rotation des rotors, une chambre avant ou chambre de travail 5 et une chambre arrière ou chambre passive 6. Ces chambres 5, 6, par rotation des rotors, sont assujetties à tourner autour de l'axe géométrique de l'alésage 2 du bloc moteur. Un mélange gazeux est séquentiellement introduit dans la chambre de travail 5 pour évoluer selon les phases d'un cycle thermodynamique en vue de produire un travail mécanique.- Figure 9 is a sectional view along the line CC of Figure 8, - Figure 10 is a front view of a hydraulic stop. As shown, the rotary piston machine according to the invention can be used mainly as a spark ignition engine or diesel engine comprises a motor unit 1 in which is formed a cylindrical bore 2 in which are coaxially mounted interpenetration two rotors 3, 4, one of which, the rotor 3 is in a continuous rotational movement and has an axial bore 7 and two diametrically opposite radial recesses 8, opening on the one hand in the axial bore and on the other hand in the outer cylindrical surface and whose other rotor, the rotor 4 is intermittently moving and comprises a cylindrical shaft 9 freely rotatably engaged in the axial bore 7 of the rotor with continuous movement, and two diametrically opposed radial vanes 10, forming a piston, fixed to the shaft 9 and engaged in the radial recesses 8 so as to be able to move angularly, each of said pallets forming with the évi corresponding radial direction 8 and with the bore 2 of the engine block 1 by considering the direction of rotation of the rotors, a front chamber or working chamber 5 and a rear chamber or passive chamber 6. These chambers 5, 6, by rotation of the rotors , are subject to rotate around the geometric axis of the bore 2 of the engine block. A gaseous mixture is sequentially introduced into the working chamber 5 to evolve according to the phases of a thermodynamic cycle in order to produce a mechanical work.

L'alésage 2 du bloc moteur 1 comporte deux paliers hydrodynamiques 20 distants l'un de l'autre destinés à supporter le rotor 3 à mouvement continu. Ce rotor constitue l'arbre de sortie de puissance du moteur.The bore 2 of the engine block 1 comprises two hydrodynamic bearings 20 spaced apart from each other for supporting the rotor 3 with continuous movement. This rotor constitutes the power output shaft of the engine.

Chaque évidement 8 que comporte le rotor à mouvement continu 3, selon une section perpendiculaire à l'axe dudit rotor épouse le contour d'un secteur de couronne circulaire. Suivant une section contenant l'axe longitudinal du rotor, l'évidement 8 présente une section droite de forme rectangulaire ou carrée. Comme on peut le voir sur les figures jointes l'évidement 8 débouche dans l'alésage 7. Par son arbre 9, le rotor 4 à mouvement intermittent est supporté par deux paliers hydrodynamiques 21 montés à distance l'un de l'autre chacun dans un logement coaxial au perçage 7 du rotor 3.Each recess 8 that comprises the rotor with continuous movement 3, in a section perpendicular to the axis of said rotor conforms to the contour of a circular crown sector. According to a section containing the longitudinal axis of the rotor, the recess 8 has a cross section of rectangular or square shape. As can be seen in the accompanying figures, the recess 8 opens into the bore 7. Through its shaft 9, the rotor 4 with intermittent movement is supported by two hydrodynamic bearings 21 mounted at a distance from each other each in a housing coaxial with the bore 7 of the rotor 3.

L'arbre 9 du rotor 4 est doté d'un alésage longitudinal traversant 4a. Lors de chacune des quatre phases du cycle thermodynamique, à savoir, admission, compression, allumage-détente ou combustion-détente, échappement, le rotor 3 à mouvement continu accompli environ un quart de tour. Le rotor 4 à mouvement intermittent pendant les phases d'admission du mélange gazeux dans chaque chambre de travail et de détente des gaz est assujetti par un mécanisme anti-retour à demeurer angulairement fixe par rapport au bloc moteur au moins dans le sens rétrogire, tandis que pendant chacune des phases de compression du mélange gazeux et d'échappement des gaz brûlés il est assujetti par un moyen de transmission de mouvement à accomplir environ un demi-tour par rapport au bloc moteur 1. Pendant ces deux phases, le rotor à mouvement intermittent 4 accompli par rapport au rotor à mouvement continu 3 environ un quart de tour.The shaft 9 of the rotor 4 is provided with a longitudinal through bore 4a. During each of the four phases of the thermodynamic cycle, namely, admission, compression, ignition-expansion or combustion-expansion, exhaust, the rotor 3 with continuous movement accomplishes about a quarter turn. The rotor 4 with intermittent movement during the phases of admission of the gaseous mixture into each working and expansion chamber of the gases is secured by a non-return mechanism to remain angularly fixed relative to the engine block at least in the backward direction, while during each of the compression phases of the gaseous mixture and the exhaust of the flue gases it is subjected by a motion transmission means to perform approximately one half-turn relative to the engine block 1. During these two phases, the rotor with movement intermittent 4 performed relative to the rotor with continuous movement 3 about a quarter turn.

Autour de chaque évidement radial 8 du rotor à mouvement continu 3, sur la surface cylindrique externe de ce rotor 3, et sur la surface cylindrique du perçage axial 7 que comporte ce dernier, sont formées respectivement une barrière d'étanchéité externe 11 et une barrière d'étanchéité interne 12.Around each radial recess 8 of the rotor with continuous movement 3, on the outer cylindrical surface of this rotor 3, and on the cylindrical surface of the axial bore 7 that comprises the latter, are formed respectively an external sealing barrier 11 and a barrier internal sealing 12.

De plus, chaque palette du rotor à mouvement intermittent comporte au moins une barrière d'étanchéité 13, cette dernière étant formée de manière continue sur les rives latérales radiales 10a de la palette 10 et sur la rive frontale 10b de cette dernière.In addition, each pallet of the intermittent rotor comprises at least one sealing barrier 13, the latter being formed continuously on the radial lateral banks 10a of the pallet 10 and on the front edge 10b of the latter.

Les barrières d'étanchéité externe 11 et interne 12 comporte chacune deux parties latérales en arc de circonférence de cercle disposées respectivement de part et d'autre des évidements radiaux et au moins une partie rectiligne s'étendant de l'une à l'autre partie latérale. La barrière d'étanchéité externe 11 du rotor à mouvement continu 3 prend appui sur la surface cylindrique de l'alésage 2 du bloc moteur 1 , et la barrière d'étanchéité interne 12 que comporte le rotor à mouvement continu 3, prend appui sur la surface cylindrique de l'arbre 9 du rotor à mouvement intermittent 3.The outer 11 and inner 12 sealing gates each comprise two arcuate circumferential side portions disposed respectively on either side of the radial recesses and at least one rectilinear part extending from one to the other part. lateral. The external sealing barrier 11 of the continuous-motion rotor 3 is supported on the cylindrical surface of the bore 2 of the engine block 1, and the internal sealing barrier 12 that comprises the continuously-moving rotor 3 is supported on the cylindrical surface of the shaft 9 of the intermittently moving rotor 3.

Chaque barrière d'étanchéité 13 formée sur chaque palette 10 du rotor à mouvement intermittent prend appui sur les faces latérales de l'évidement 8 correspondant et sur la face cylindrique de l'alésage 2 du bloc moteur.Each sealing barrier 13 formed on each pallet 10 of the rotor with intermittent movement bears on the lateral faces of the corresponding recess 8 and on the cylindrical face of the bore 2 of the engine block.

Conformément à l'invention, chaque rotor 3, 4 comporte au moins un moyen de graissage apte à délivrer une quantité dosée de fluide de lubrification sur les surfaces de chaque chambre de travail en avant des segments d'étanchéité en considérant le sens de rotation des rotors, ce moyen de graissage étant alimenté par un circuit d'huile comportant une pompe à huile externe. Préférentiellement chaque moyen de graissage est constitué par au moins un graisseur 22 monté dans un alésage pratiqué dans le rotor 3, 4 correspondant. Ce graisseur est connecté à un circuit de délivrance d'un fluide de graissage et comporte une tête de graissage 23 avec un orifice de graissage 24 maintenu en appui contre la surface correspondante de la chambre de travail par un organe élastique 25. Le moyen de graissage est également constitué par des formes en creux formées dans les surfaces de la chambre de travail, sur la trajectoire de l'orifice de la tête des graisseurs pour recevoir du fluide de graissage.According to the invention, each rotor 3, 4 comprises at least one lubricating means capable of delivering a metered quantity of lubricating fluid. on the surfaces of each working chamber in front of the sealing segments by considering the direction of rotation of the rotors, said lubricating means being fed by an oil circuit comprising an external oil pump. Preferably each greasing means is constituted by at least one grease fitting 22 mounted in a bore made in the rotor 3, 4 corresponding. This lubricator is connected to a delivery circuit of a lubricating fluid and comprises a lubricating head 23 with a lubricating orifice 24 held in abutment against the corresponding surface of the working chamber by an elastic member 25. The lubricating means is also formed by recessed shapes formed in the surfaces of the working chamber, on the path of the orifice of the head of the nipples to receive lubricating fluid.

Préférentiellement ces formes en creux sont des micro-cavités aptes à retenir le fluide de graissage, formées par traitement de surface tel que honage.Preferably these recessed shapes are micro-cavities capable of retaining the lubricating fluid, formed by surface treatment such as honing.

Dans la forme préférée de réalisation, chaque graisseur 22 présente un corps tubulaire cylindrique comprenant perpendiculairement à son axe longitudinal une face terminale convexe en tronc de cône formant la tête 23, ledit corps étant percé axialement de part en part d'un canal d'amenée d'huile à l'orifice 24 de la tête en tronc de cône.In the preferred embodiment, each grease nipple 22 has a cylindrical tubular body comprising, perpendicular to its longitudinal axis, a convex end face in a truncated cone forming the head 23, said body being pierced axially from one side of a delivery channel. of oil at the orifice 24 of the truncated cone head.

L'organe élastique 25 permet de maintenir la tête 23 du graisseur 22 appliquée contre la surface correspondante de la chambre de travail 5. L'orifice de graissage 24 se trouve normalement obturé par cette surface et l'huile ne peut s'échapper. En revanche dès qu'il se trouve en regard d'une cavité de cette surface, l'huile peut alors s'échapper et remplir cette cavité. L'huile présente dans cette cavité sera ensuite balayée par le segment associé pour être étalé sur toute la surface correspondante de la chambre de travail 5.The elastic member 25 keeps the head 23 of the grease nipple 22 applied against the corresponding surface of the working chamber 5. The lubrication orifice 24 is normally closed off by this surface and the oil can not escape. However, as soon as it is facing a cavity of this surface, the oil can then escape and fill the cavity. The oil present in this cavity will then be swept by the associated segment to be spread over the entire corresponding surface of the working chamber 5.

Toujours selon la forme préférée de réalisation, le corps tubulaire du graisseur 22, présente un lamage pour recevoir l'organe élastique associé, ledit organe élastique 25 étant constitué par un ressort à spires non jointives. Comme on peut le voir, le canal d'amenée d'huile débouche dans ce lamage.Still according to the preferred embodiment, the tubular body of the grease nipple 22 has a counterbore for receiving the associated elastic member, said elastic member 25 being constituted by a spring with non-contiguous turns. As can be seen, the oil supply channel opens into this counterbore.

Dans la forme préférée d'exécution, les graisseurs 22 associés au rotor à mouvement intermittent 4 sont montés dans des alésages pratiqués dans chaque palette 10 et débouchant dans les faces latérales 10a de ces dernières. Toujours selon cette disposition, les dits alésages sont en communication avec des canaux pratiqués dans le rotor 4 à mouvement intermittent et débouchant dans l'alésage axial 4a de l'arbre dudit rotor au droit, chacun, d'une rainure de distribution d'huile pratiquée dans une bague 28 de distribution d'huile montée dans l'alésage 4a. Comme on le comprend sont prévues deux bagues de distribution d'huile 28 associées respectivement aux graisseurs 22 que comportent les deux rives radiales 10a de la palette 10. Cet arbre est par ailleurs équipé de canaux radiaux 29 débouchant d'une part dans l'alésage interne 4a, au droit de la rainure de distribution d'huile de la bague de distribution d'huile 28, et d'autre part dans sa face cylindrique externe, au droit d'une chambre d'alimentation en huile 30 formée dans une bague calée en rotation dans le rotor à mouvement continu, cette bague constituant avantageusement le corps du palier hydrodynamique 21. Le corps de palier 21 comporte une chambre à huile alimentée en huile par le circuit d'huile. Comme on le comprend sont prévus deux paliers hydrodynamiques 21. Chaque palier assure le guidage en rotation du rotor à mouvement intermittent 4 dans le rotor à mouvement continu 3.In the preferred embodiment, the nipples 22 associated with the intermittent rotor 4 are mounted in bores made in each pallet 10 and opening into the side faces 10a thereof. Still according to this arrangement, said bores are in communication with channels made in the rotor 4 with intermittent movement and opening into the axial bore 4a of the shaft of said rotor to the right, each, of an oil distribution groove performed in an oil distribution ring 28 mounted in the bore 4a. As is understood, two oil distribution rings 28 are provided respectively associated with the lubricators 22 that comprise the two radial banks 10a of the pallet 10. This shaft is also equipped with radial channels 29 opening on the one hand into the bore 4a, the right of the oil distribution groove of the oil distribution ring 28, and secondly in its outer cylindrical face, to the right of an oil supply chamber 30 formed in a ring rotated in the rotor with continuous movement, this ring advantageously constituting the body of the hydrodynamic bearing 21. The bearing body 21 comprises an oil chamber supplied with oil by the oil circuit. As is understood, two hydrodynamic bearings 21 are provided. Each bearing ensures the rotational guidance of the intermittently moving rotor 4 in the rotor with continuous movement 3.

Toujours selon la forme préférée de réalisation, les graisseurs 22 du rotor à mouvement continu 3 sont montés dans des alésages cylindriques pratiqués dans le corps dudit rotor 3 et débouchant pour certains sur la face cylindrique externe dudit rotor et pour les autres sur la face cylindrique interne de ce rotor. Ces alésages sont en communication avec des canaux d'amenée d'huile 32 pratiqués dans le rotor à mouvement continu, parallèlement à son axe longitudinal, les dits canaux 32 d'amenée d'huile assurant aussi l'alimentation en huile des paliers hydrodynamiques 21 support du rotor à mouvement intermittent dans le rotor à mouvement continu et des paliers hydrodynamiques 20 support du rotor à mouvement continu 3 dans le bloc moteur 1 , les dits canaux longitudinaux étant alimentés en huile par une pompe externe via un ou des joints tournants. Avantageusement le circuit d'huile assure également le refroidissement du moteur. À cet effet le circuit d'huile comprend un ou plusieurs canaux de retour, longitudinaux formés dans le rotor à mouvement continu 3 et chaque canal longitudinal d'alimentation et/ou de retour est équipé d'un moyen apte à créer un régime turbulent d'écoulement d'huile afin d'augmenter le degré de transfert thermique entre le rotor 3 et cette huile. Ce moyen apte à créer le régime turbulent présente dans le canal correspondant, sur le trajet d'écoulement de l'huile une série de reliefs. Selon une forme préférée de réalisation, le moyen apte à créer un régime turbulent force l'huile à suivre un trajet en hélice dans le canal correspondant. On augmente ainsi la longueur du trajet du flux d'huile et sa vitesse dans le canal correspondant et par voie de conséquence son efficacité.Still according to the preferred embodiment, the grease nipples 22 of the rotor with continuous movement 3 are mounted in cylindrical bores made in the body of said rotor 3 and opening for some on the outer cylindrical face of said rotor and for the others on the inner cylindrical face. of this rotor. These bores are in communication with oil supply channels 32 formed in the rotor with continuous movement, parallel to its longitudinal axis, said channels 32 for supplying oil also supplying oil to the hydrodynamic bearings 21 supporting the rotor with intermittent movement in the rotor with continuous movement and the hydrodynamic bearings 20 supporting the rotor with continuous movement 3 in the engine block 1, said longitudinal channels being supplied with oil by an external pump via one or several rotary joints. Advantageously, the oil circuit also ensures the cooling of the engine. For this purpose the oil circuit comprises one or more longitudinal return channels formed in the rotor with continuous movement 3 and each longitudinal feed and / or return channel is equipped with a means adapted to create a turbulent flow regime of oil to increase the degree of heat transfer between the rotor 3 and this oil. This means capable of creating the turbulent regime present in the corresponding channel, in the flow path of the oil a series of reliefs. According to a preferred embodiment, the means capable of creating a turbulent regime forces the oil to follow a helical path in the corresponding channel. This increases the length of the path of the oil flow and its speed in the corresponding channel and consequently its effectiveness.

Dans la pratique, le moyen apte à créer un régime turbulent et à forcer l'huile à suivre un trajet en hélice pourra être constitué par une broche axiale 33 occupant une position centrale dans le canal et par une structure en hélice 34 enroulée autour de la broche centrale 33 et s'étendant longitudinalement sur toute la longueur de la broche et s'étendant radialement de ladite broche 33 à la face interne cylindrique dudit canal. Toujours selon la forme préférée de réalisation, au rotor à mouvement continu 3 est associée une butée axiale hydrodynamique 35 alimentée par le circuit d'huile, interposée entre le bloc moteur 1 et le rotor 3 à mouvement continu. Cette butée axiale hydrodynamique 35 a pour but de contenir les mouvements axiaux du rotor à mouvement continu 3. Cette butée axiale 35 présente deux faces actives d'appui, opposées, 351 pourvues de plusieurs cavités 352 en vue de la formation de coins d'huile.In practice, the means capable of creating a turbulent regime and forcing the oil to follow a helical path may be constituted by an axial pin 33 occupying a central position in the channel and by a helical structure 34 wound around the central pin 33 and extending longitudinally along the entire length of the pin and extending radially from said pin 33 to the cylindrical inner face of said channel. Still according to the preferred embodiment, the rotor with continuous movement 3 is associated with a hydrodynamic axial stop 35 fed by the oil circuit, interposed between the engine block 1 and the rotor 3 with continuous movement. This hydrodynamic axial stop 35 is intended to contain the axial movements of the rotor with continuous movement 3. This axial abutment 35 has two opposed active bearing faces 351 provided with several cavities 352 for the formation of oil wedges .

Le circuit d'huile assure comme on le comprend plusieurs fonctions à savoir une fonction de graissage, une fonction de refroidissement des rotors et une fonction d'alimentation des paliers hydrodynamiques 20, 21. II va de soi que la présente invention peut recevoir tous les aménagements et variantes du domaine des équivalents techniques sans pour autant sortir du cadre du présent brevet. The oil circuit provides, as is understood, several functions, namely a lubrication function, a cooling function for the rotors and a feed function for the hydrodynamic bearings 20, 21. It goes without saying that the present invention can receive all the arrangements and variants of the field of technical equivalents without departing from the scope of this patent.

Claims

Revendications.Claims. 1/ Machine thermique à pistons rotatifs utilisable notamment en tant que moteur thermique comportant un bloc moteur (1) dans lequel est formé un alésage cylindrique (2) dans lequel sont montés de manière coaxiale en interpénétration deux rotors dont un (3) est à mouvement de rotation continu et présente un perçage axial (7) et au moins un évidement radial (8) débouchant d'une part dans le perçage axial (7) et d'autre part dans la surface cylindrique externe et dont l'autre rotor (4) est à mouvement intermittent et comprend d'une part un arbre cylindrique (9) engagé de manière libre en rotation dans le perçage (7) du rotor à mouvement continu, et d'autre part au moins une palette radiale (10) formant piston fixée à l'arbre (9) et engagée dans l'évidement radial (8) de façon à pouvoir s'y déplacer angulairement, ledit arbre (9) étant traversé de part en part d'un alésage cylindrique (4a) axial et ladite palette (10) ou piston formant avec l'évidement radial (8) du rotor à mouvement continu (3) et avec l'alésage (2) du bloc moteur (1 ) en considérant le sens de rotation des rotors (3, 4) une chambre arrière (6) ou chambre passive et une chambre avant (5) ou chambre de travail (5, 6), lesquelles chambres, par rotation des rotors sont assujetties à tourner autour de l'axe géométrique de l'alésage (2) du bloc moteur, un mélange gazeux étant séquentiellement introduit dans la chambre de travail pour évoluer selon les phases d'un cycle thermodynamique en vue de produire un travail mécanique et des barrières d'étanchéité (11 , 12, 13) étant formées autour de l'évidement radial (8) du rotor (3) à mouvement continu respectivement sur la surface cylindrique externe de rotor pour former une barrière d'étanchéité externe (11) et sur la surface cylindrique du perçage axial du rotor pour former une barrière d'étanchéité interne (12), ainsi que sur les rives radiales (10a) et la rive frontale de la palette du rotor à mouvement intermittent, lesdites barrières d'étanchéité (11 , 12, 13) étant constituées par des segments aboutés les uns autres et montés dans des rainures formées dans le rotor à mouvement continu et dans les rives radiales et frontale de la palette du rotor à mouvement intermittent, caractérisée en ce qu'au moins le rotor à mouvement continu (3) comporte au moins un circuit d'huile sous pression pour notamment assurer notamment le graissage de la segmentation (11 , 12,13) associée au rotor à mouvement continu (3) et au rotor à mouvement intermittent (4). 2/ Machine selon la revendication 1 , caractérisée en ce que chaque rotor comporte au moins un moyen de graissage apte à délivrer une quantité dosée de fluide de lubrification sur les surfaces de chaque chambre de travail en avant des segments d'étanchéité en considérant le sens de rotation des rotors, ce moyen de graissage étant alimenté par le circuit d'huile sous pression.1 / Rotary piston heat engine usable in particular as a heat engine comprising an engine block (1) in which is formed a cylindrical bore (2) in which are coaxially mounted interpenetration two rotors of which one (3) is moving continuous rotation and has an axial bore (7) and at least one radial recess (8) opening on the one hand in the axial bore (7) and on the other hand in the outer cylindrical surface and the other rotor (4 ) is intermittent and comprises on the one hand a cylindrical shaft (9) freely rotatably engaged in the bore (7) of the continuously moving rotor, and on the other hand at least one radial vane (10) forming a piston fixed to the shaft (9) and engaged in the radial recess (8) so as to be able to move angularly, said shaft (9) being traversed right through a cylindrical bore (4a) axial and said pallet (10) or piston forming with the radial recess ( 8) of the rotor with continuous movement (3) and with the bore (2) of the engine block (1) by considering the direction of rotation of the rotors (3, 4) a rear chamber (6) or passive chamber and a front chamber (5) or working chamber (5, 6), which chambers, by rotation of the rotors are subject to rotate about the geometric axis of the bore (2) of the engine block, a gas mixture being sequentially introduced into the chamber working to evolve according to the phases of a thermodynamic cycle to produce a mechanical work and sealing barriers (11, 12, 13) being formed around the radial recess (8) of the rotor (3) with movement continuously on the outer cylindrical rotor surface to form an outer sealing barrier (11) and on the cylindrical surface of the axial bore of the rotor to form an inner sealing barrier (12), as well as on the radial banks (10a). ) and the front edge of the moving rotor pallet intermittent, said sealing barriers (11, 12, 13) being constituted by abutting segments one another and mounted in grooves formed in the rotor with continuous movement and in the radial and frontal banks of the rotor blade with motion intermittent, characterized in that at least the continuous-motion rotor (3) comprises at least one pressurized oil circuit, in particular to ensure in particular the lubrication of the segmentation (11, 12, 13) associated with the rotor with continuous movement ( 3) and the intermittent rotor (4). 2 / Machine according to claim 1, characterized in that each rotor comprises at least one greasing means adapted to deliver a metered quantity of lubricating fluid on the surfaces of each working chamber in front of the sealing segments in consideration of the direction rotation of the rotors, the lubricating means being fed by the pressurized oil circuit. 3/ Machine selon la revendication précédente, caractérisée en ce que chaque moyen de graissage est constitué par :3 / Machine according to the preceding claim, characterized in that each greasing means is constituted by: - au moins un graisseur (22) connecté à un circuit de délivrance d'un fluide de graissage et comportant une tête de graissage (23) avec un orifice de graissage (24) maintenu en appui, contre la surface à lubrifier, par un organe élastique (25),at least one lubricator (22) connected to a lubricating fluid supplying circuit and comprising a lubricating head (23) with a lubricating orifice (24) held in abutment against the surface to be lubricated, by an organ elastic (25), - et au moins une forme en creux formée dans ladite surface, sur la trajectoire de l'orifice (24) de la tête (23) du graisseur (22) pour remplir ladite forme en creux de fluide de graissage. 4/ Machine selon la revendication 3, caractérisée en ce que les surfaces de la chambre de travail (5), sont traitées de façon à présenter des micro-cavités aptes à retenir l'huile de graissage.and at least one recessed shape formed in said surface, on the path of the orifice (24) of the head (23) of the grease nipple (22) to fill said hollow form with lubricating fluid. 4 / Machine according to claim 3, characterized in that the surfaces of the working chamber (5), are treated so as to have micro-cavities adapted to retain the lubricating oil. 5/ Machine selon la revendication 3 ou la revendication 4, caractérisée en ce que chaque graisseur (22) présente un corps tubulaire cylindrique comprenant perpendiculairement à son axe longitudinal une face terminale convexe en tronc de cône, ledit corps étant percé axialement de part en part d'un canal d'amenée d'huile à la tête bombée.5 / Machine according to claim 3 or claim 4, characterized in that each grease (22) has a cylindrical tubular body comprising perpendicularly to its longitudinal axis a convex end face truncated cone, said body being pierced axially from one side to the other an oil feed channel to the convex head. 6/ Machine selon la revendication 5, caractérisée en ce que le corps tubulaire du graisseur, présente un lamage formé dans le canal d'amenée d'huile, prévu pour recevoir l'organe élastique associé (25), ledit organe élastique étant constitué par un ressort à spires non jointives.6 / Machine according to claim 5, characterized in that the tubular body of the grease nipple, has a recess formed in the oil supply channel, adapted to receive the associated elastic member (25), said elastic member being constituted by a spring with non-contiguous turns. 7/ Machine selon l'une quelconque des revendications 3 à 6, caractérisée en ce que les graisseurs (22) associés au rotor à mouvement intermittent sont montés dans des alésages pratiqués dans chaque palette (10) et débouchant dans les faces latérales de ces dernières, les dits alésages sont en communication avec des canaux pratiqués dans le rotor à mouvement intermittent (4) et débouchant dans l'alésage axial (4a) de l'arbre (9) dudit rotor (4) au droit, chacun, d'une rainure de distribution d'huile pratiquée dans une bague de distribution d'huile (28) montée dans l'alésage (4a) de l'arbre (9) du rotor à mouvement intermittent (4), ledit arbre (9) étant par ailleurs équipé de canaux radiaux (29) débouchant d'une part dans l'alésage interne (4a), au droit de la rainure de distribution d'huile de la bague de distribution d'huile (28) et d'autre part dans sa face cylindrique externe au droit d'une chambre (30) d'alimentation en huile formée dans une bague calée en rotation dans le rotor à mouvement continu, cette bague constituant le corps d'un palier hydrodynamique (21 ), ledit corps de palier étant équipé d'une chambre à huile alimentée en huile par le circuit d'huile. 8/ Machine selon l'une quelconque des revendications 3 à 7, caractérisée en ce que les graisseurs (22) du rotor à mouvement continu (3) sont montés dans des alésages cylindriques pratiqués dans le corps dudit rotor et débouchant pour certains sur la face cylindrique externe dudit rotor et pour les autres sur la face cylindrique interne, les dits alésages étant en communication avec des canaux (32) d'amenée d'huile pratiqués dans ledit rotor (3), parallèlement à son axe longitudinal, les dits canaux d'amenée d'huile (32) assurant l'alimentation en huile des paliers hydrodynamique (21) support du rotor à mouvement intermittent dans le rotor à mouvement continu et de paliers hydrodynamique (20) support du rotor à mouvement continu (3) dans le bloc moteur (1), les dits canaux longitudinaux (32) étant alimentés en huile par une pompe externe via un joint tournant.7 / Machine according to any one of claims 3 to 6, characterized in that the grease nipples (22) associated with the rotor with intermittent movement are mounted in bores made in each pallet (10) and opening into the side faces of the latter said bores are in communication with channels in the intermittently-moving rotor (4) and opening into the axial bore (4a) of the shaft (9) of said rotor (4) to the right, each, of a groove for dispensing oil practiced in a oil distribution ring (28) mounted in the bore (4a) of the shaft (9) of the intermittently moving rotor (4), said shaft (9) being furthermore equipped with radial channels (29) opening a part in the internal bore (4a), in line with the oil distribution groove of the oil distribution ring (28) and secondly in its external cylindrical face with the right of a chamber ( 30) of oil supply formed in a ring set in rotation in the rotor with continuous movement, this ring constituting the body of a hydrodynamic bearing (21), said bearing body being equipped with an oil chamber supplied with oil by the oil circuit. 8 / Machine according to any one of claims 3 to 7, characterized in that the grease nipples (22) of the rotor with continuous movement (3) are mounted in cylindrical bores made in the body of said rotor and opening for some on the face cylindrical external of said rotor and for the others on the inner cylindrical face, said bores being in communication with channels (32) for supplying oil in said rotor (3), parallel to its longitudinal axis, said channels of supplying oil (32) supplying oil to hydrodynamic bearings (21) supporting the rotor with intermittent motion in the rotor with continuous movement and hydrodynamic bearings (20) supporting the rotor with continuous movement (3) in the motor block (1), said longitudinal channels (32) being supplied with oil by an external pump via a rotary joint. 9/ Machine selon l'une quelconque des revendications précédentes, caractérisée en ce que le circuit d'huile assure également le refroidissement du moteur. 10/ Machine selon la revendication 9, caractérisée en ce que le circuit d'huile sous pression comprend un ou plusieurs canaux de retour, longitudinaux formés dans le rotor à mouvement continu.9 / Machine according to any one of the preceding claims, characterized in that the oil circuit also ensures the cooling of the engine. 10 / Machine according to claim 9, characterized in that the pressurized oil circuit comprises one or more longitudinal return channels formed in the rotor with continuous movement. 11/ Machine selon la revendication précédente, caractérisé en ce que chaque canal longitudinal d'alimentation et/ou de retour est équipé d'un moyen apte à créer un régime turbulent d'écoulement d'huile afin d'augmenter le degré de transfert thermique entre le rotor (3) et l'huile de refroidissement, ledit moyen apte à créer le régime turbulent présentant dans le canal correspondant une série de reliefs. 12/ Machine selon la 11 , caractérisée en ce que le moyen apte à créer le régime turbulent force l'huile à suivre un trajet en hélice dans le canal correspondant.11 / Machine according to the preceding claim, characterized in that each longitudinal supply and / or return channel is equipped with means capable of creating a turbulent flow of oil flow in order to increase the degree of heat transfer between the rotor (3) and the cooling oil, said means adapted to create the turbulent regime having in the corresponding channel a series of reliefs. 12 / Machine according to 11, characterized in that the means adapted to create the turbulent regime forces the oil to follow a helical path in the corresponding channel. 13/ Machine selon la revendication précédente, caractérisée en ce que le moyen apte à créer un régime turbulent et à forcer l'huile à suivre un trajet en hélice est constitué par une broche axiale (33) occupant une position centrale dans le canal et par une structure (34) en hélice enroulée autour de la broche centrale et s'étendant longitudinalement sur toute la longueur de la broche et s'étendant radialement de ladite broche à la face interne cylindrique dudit canal. 14/ Machine selon l'une quelconque des revendications précédentes, caractérisée en ce qu'au rotor à mouvement continu est associée une butée axiale (35) hydrodynamique alimentée par le circuit d'huile, interposée entre le bloc moteur (1 ) et le rotor à mouvement continu (3) pour contenir les mouvements axiaux du rotor à mouvement continu (3). 15/ Machine selon la revendication 14, caractérisée en ce que la butée axiale (35) présente deux faces actives d'appui, opposées (351 ) pourvues de plusieurs cavités (352) en vue de la formation de coins d'huile. 13 / Machine according to the preceding claim, characterized in that the means adapted to create a turbulent regime and to force the oil to follow a helical path is constituted by an axial pin (33) occupying a central position in the channel and by a helical structure (34) wound around the central spindle and extending longitudinally along the entire length of the spindle and extending radially from said spindle to the cylindrical inner face of said channel. 14 / Machine according to any one of the preceding claims, characterized in that the continuous rotor is associated with a axial stop (35) hydrodynamic powered by the oil circuit, interposed between the engine block (1) and the rotor continuous motion device (3) for containing the axial movements of the continuously moving rotor (3). 15 / Machine according to claim 14, characterized in that the axial abutment (35) has two opposed active bearing faces (351) provided with several cavities (352) for the formation of oil wedges.
PCT/FR2006/001069 2006-05-12 2006-05-12 Lubrication and cooling of rotary piston engines Ceased WO2007132071A1 (en)

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Citations (6)

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Publication number Priority date Publication date Assignee Title
GB128419A (en) * 1918-07-02 1919-06-26 Martin Ling-Bevington Improvements in and relating to Rotary Engines, Pumps, Blowers and the like.
GB1205584A (en) * 1967-02-20 1970-09-16 Ehrlich Engineering Ltd Oscillating vane machines
DE2537742A1 (en) * 1975-08-14 1977-02-17 Sulzer Ag LUBRICATION DEVICE OF A PISTON ENGINE
US5324182A (en) * 1989-02-03 1994-06-28 Huschang Sabet Rotating piston internal combustion engine with ring gear elastically coupled to the housing
DE10220015A1 (en) * 2001-05-07 2002-11-21 Man B & W Diesel As Kopenhagen Injecting lubricating oil into internal combustion engine cylinder involves storing oil in chamber between non-return valve and dosing valve until pressure in chamber exceeds opening pressure
FR2880912A1 (en) * 2005-01-17 2006-07-21 Mrcc Ind Sa Heat engine e.g. diesel engine, has continuous and intermittent rotation rotors with lubricators supplied by oil circuit to deliver lubrication fluid on surfaces of working chambers in front of sealing segments associated to rotors

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB128419A (en) * 1918-07-02 1919-06-26 Martin Ling-Bevington Improvements in and relating to Rotary Engines, Pumps, Blowers and the like.
GB1205584A (en) * 1967-02-20 1970-09-16 Ehrlich Engineering Ltd Oscillating vane machines
DE2537742A1 (en) * 1975-08-14 1977-02-17 Sulzer Ag LUBRICATION DEVICE OF A PISTON ENGINE
US5324182A (en) * 1989-02-03 1994-06-28 Huschang Sabet Rotating piston internal combustion engine with ring gear elastically coupled to the housing
DE10220015A1 (en) * 2001-05-07 2002-11-21 Man B & W Diesel As Kopenhagen Injecting lubricating oil into internal combustion engine cylinder involves storing oil in chamber between non-return valve and dosing valve until pressure in chamber exceeds opening pressure
FR2880912A1 (en) * 2005-01-17 2006-07-21 Mrcc Ind Sa Heat engine e.g. diesel engine, has continuous and intermittent rotation rotors with lubricators supplied by oil circuit to deliver lubrication fluid on surfaces of working chambers in front of sealing segments associated to rotors

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