EP0152321B1 - Device for controlling the opening and closing of the combustion chamber of an internal-combustion engine - Google Patents

Device for controlling the opening and closing of the combustion chamber of an internal-combustion engine Download PDF

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Publication number
EP0152321B1
EP0152321B1 EP19850400107 EP85400107A EP0152321B1 EP 0152321 B1 EP0152321 B1 EP 0152321B1 EP 19850400107 EP19850400107 EP 19850400107 EP 85400107 A EP85400107 A EP 85400107A EP 0152321 B1 EP0152321 B1 EP 0152321B1
Authority
EP
European Patent Office
Prior art keywords
inlet
passage
combustion chamber
chamber
combustion
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.)
Expired
Application number
EP19850400107
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German (de)
French (fr)
Other versions
EP0152321A1 (en
Inventor
Jean-Claude Fayard
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.)
Elf Antar France
Original Assignee
Elf France SA
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
Priority claimed from FR8410675A external-priority patent/FR2549490A1/en
Priority claimed from FR8500637A external-priority patent/FR2576060B2/en
Application filed by Elf France SA filed Critical Elf France SA
Priority to AT85400107T priority Critical patent/ATE30456T1/en
Publication of EP0152321A1 publication Critical patent/EP0152321A1/en
Application granted granted Critical
Publication of EP0152321B1 publication Critical patent/EP0152321B1/en
Expired 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
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements
    • F01L7/02Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves
    • F01L7/021Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves with one rotary valve
    • F01L7/022Cylindrical valves having one recess communicating successively with aligned inlet and exhaust ports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements
    • F01L7/16Sealing or packing arrangements specially therefor
    • 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
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • 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

Definitions

  • the present invention applies to a device for controlling the circulation of gases to and from a combustion chamber of an internal combustion engine, constituted by a rotary plug or rotor comprising at least one internal channel or a lateral cut defining passages of 'respective exhaust or intake transverse flow, a passage directly connected to the combustion chamber, the plug being contained in a transverse bore into which opens the orifice of said passage arranged in a sealing ring which is housed in a bore, in which it slides, the sealing ring being applied to the rotor by a continuous contact surface around the orifice of the passage under the effect of the pressure prevailing in the combustion chamber being surrounded by one or several sealing members such as segments, and being provided with means for injecting oil on the plug.
  • the plug is contained in a transverse bore into which opens the orifice connected directly to the combustion chamber and the intake and / or exhaust orifices connected respectively to an exhaust manifold.
  • the passage connected to the combustion chamber is arranged in a sealing ring housed in an applied bore, on the plug by a continuous sealing surface around the orifice connected directly to the combustion chamber, under the effect of the pressure prevailing in the combustion chamber, and surrounded by one or more, sealing members such as segments, this ring being able to slide in the bore and its stroke being limited, on one side, by the plug and, on the other side, by a retaining shoulder.
  • Such combustion engines appear capable of delivering mass powers much higher than known and proven solutions, in particular for small displacement engines, due to the absence of distribution parts subjected to an alternating movement generating a beat limit frequency.
  • the most decisive advantage of this type of distribution lies in the possibility of having exhaust and intake ducts twice the diameter of a conventional valve system, which allows for better filling. and therefore a higher specific power.
  • US-A-4,114,639 describes a rotary valve used for controlling the circulation of gases to and from a combustion chamber of an internal combustion engine and into which the lubricant is supplied using porous plugs between the member of the rotating valve and the inner surface of the valve body supporting this rotating member.
  • the seal between the insert forming an annular seal and the rotating member forming the supply and exhaust distributor cannot be maintained over time. There is in fact no means of placing the insert on the member other than that due to the oil pressure or the combustion pressure of the chamber.
  • This known system has the drawback, in the event of wear on contact between the insert and the rotating member, an exhaust gas leak is established towards the oil supply line and a discharge of lubricating oil, followed by seizure of the rotating contact.
  • One of the aims of the present invention is precisely to overcome these defects of combustion engines with rotary distribution in order to allow the large passage sections offered by this type of their distribution to be used without risking rapid wear and consumption of exaggerated fuel.
  • the sealing ring is crossed at least at its periphery by a pressurized oil circuit heading towards the oil return and capable of ensuring cooling.
  • this ring and the injection means are connected to said oil circuit, pass axially through at least part of the annular section of the ring and open into a continuous annular distribution groove which is formed inside the continuous contact surface established on a strip of small width along the general line of intersection of two cylinders and which opens on the interface existing between this contact surface and the external surface of the rotor.
  • the means for injecting the fluid consist, on the one hand, of an annular oil intake and circulation chamber, delimited between the periphery of the sealing ring and its bore and axially limited at each end by a seal interposed between the outer surface of the sealing ring and the bore and, on the other hand, by at least one supply passage having an outlet opening opening into said interface between the surface continuous sealing and the outer surface of the plug and in that at least one gun sealing segment is interposed between on the one hand the sealing ring and its bore and on the other hand said seal located on the side of the combustion.
  • the annular inlet chamber is traversed by a large flow of pressurized oil directing through an outlet pipe towards another member to be lubricated or the discharge.
  • an end part of at least one supply member for one of the combustion elements crosses in a leaktight manner the cross section of the sealing ring to open into the passage which is connected to the combustion chamber, and in that the adjacent part of said end part is housed with an annular clearance in a supply passage towards the outside of said combustion element, said supply passage being connected to the annular fluid intake chamber.
  • the passage giving rise to the annular clearance is traversed by a flow of the fluid brought to the annular fluid admission chamber.
  • the passage giving rise to the annular clearance is extended towards the outside by an enlarged annular chamber, which is closed by a seal.
  • elastic ring interposed between the supply member and the inner wall of said chamber and delimiting a cooling chamber traversed by said fluid flow.
  • the sealing ring is, on the one hand, made of a soft material having good rubbing qualities with the surface of the plug, for example plastic, and, on the other hand, permanently pushed back on the surface of the plug under a substantially constant pressure by a spring.
  • scraper means lubricating fluid injected into the interface are arranged around the intake orifice connecting the rotor to the intake of the mixture of combustion air and engine fuel, these scraper means being constituted by a sealing ring intake disposed at the periphery of said intake port, which comes into continuous support on the outer surface of the plug and which is capable of isolating the interior of the intake port from the interface between the plug and its bore to limit the entrainment of oil and liquid fuel simultaneously on the surface of the rotating plug.
  • the sealing ring is, on the one hand, made of a soft material having good rubbing qualities with the surface of the plug, for example plastic, and, on the other hand part, permanently pushed back on the surface of the plug under a substantially constant pressure by a spring.
  • the plug has two separate inlet and outlet passages respectively which are capable of successively opening both by rotation of the plug, on the side of the combustion chamber, on the sealing ring and, on the side opposite to the combustion chamber, on outlet orifices which are each offset on the axis of the plug relative to the sealing ring, so as to reduce the entrainment of the fuel to the surface of the plug and the fuel entrained at the intake in the intake passage formed inside the plug.
  • the separate intake or exhaust passages of two neighboring combustion chambers are provided in the plug, opening onto an orifice for communication with the intake or the exhaust which is common to the two adjacent combustion chambers, so as to reduce the number of openings to be provided on the outside face of the plug.
  • the intake circuit of the combustion chamber includes means for removing fuel from the air drawn into the combustion chamber. combustion before the end of admission.
  • the abovementioned suppression means consist of stopping the injection of fuel clearly before the end of the suction phase.
  • the abovementioned suppression means are then preferably constituted by at least one auxiliary passage of air rich in fuel such as an emulsion, formed in the plug and cylinder head of the combustion chamber and the auxiliary passage leads to the interface between the plug and its bore at a point such that it is closed by the rotation of the plug before the main opening (s) (s) of admission not the self.
  • the suppression means are constituted by stopping the injection of fuel clearly before the end of the suction phase.
  • the suppression means are constituted by at least one auxiliary passage of air rich in fuel, formed in the plug and the cylinder head of the combustion chamber and which opens onto the interface between the rotor and its bore in an orifice which is closed off by the rotation of the rotor before the main opening (s) of inlet (s) are self-contained.
  • the passage giving rise to the annular clearance is extended towards the outside by an enlarged annular chamber, said annular chamber being closed by an elastic annular seal which is interposed between the inlet and the inner wall of said chamber and which delimits a cooling chamber through which the lubricating and cooling fluid flows brought in by the injection means.
  • This enlarged part allows a tool to access the feed member.
  • US-A-4,114,639 describes a rotary valve used for controlling the circulation of gases to and from a combustion chamber of an internal combustion engine and into which the lubricant is supplied using porous plugs between the member of rotating valve and the lower surface of the valve body supporting this rotating member.
  • a rotary plug 1 for distributing the exhaust of a combustion chamber 2 of a heat engine is shown at the moment when its internal exhaust channel 3 is opened wide on the combustion chamber 2.
  • the plug 1 turns, continuously and synchronously with the rotation of the engine, in a bore 4 and the exhaust channel 3 is connected to the combustion chamber 2 by a passage 5 of relatively large dimension formed in a ring seal 6 which can slide freely in a bore 7 with an axis substantially parallel to that of the engine cylinder (not shown) or substantially perpendicular to the axis of rotation of the plug 1, so as to ensure good bearing of the surface of contact of the ring 6 on the outer surface 8 of the plug 1.
  • the contact surface 22 between the ring 6 and the plug 1 is established on a strip of small width along the general line of intersection of two cylinders (the exterior surfaces of the wood bucket 1 and ring 6 of different diameters and substantially perpendicular and concurrent axes.
  • the sealing ring 6 which moves with gentle friction in its bore 7 is applied to the outer surface of plug 1 by the single pressure prevailing in combustion chamber 2 and acting on its annular section, increased if necessary by the thrust of a spring with low reaction force such as a washer elastic.
  • this thrust spring (not shown) of the ring 6 on the plug 1 is not essential if there is only a slight clearance or interface i between the end 9 of the ring 6 of the side of the combustion chamber 2 and a retaining shoulder 10 formed at the end of the bore 7 receiving the ring 6.
  • the temperature being relatively high in the interface i because of the proximity of the chamber 2 combustion, the holding over time of a spring member is very random.
  • a gun sealing segment 11 is disposed in a known manner in this interface j and is worn by a groove 12 preferably made in the ring 6. The segment 11 also prevents overheating of the interface j in the direction of the plug 1 and the formation in this interface of deposits which would end up blocking the ring 6 in its bore 7 .
  • the sealing ring 6 is provided with means for injecting a lubricating and cooling fluid, preferably engine lubricating oil pressurized by the engine oil pump, into the interface e between the continuous sealing surface 22 (along the general line of orthogonal intersection of two cylinders of different diameters) around the orifice 3 formed in the plug 1 and the external surface 8 of the plug 1.
  • a lubricating and cooling fluid preferably engine lubricating oil pressurized by the engine oil pump
  • the fluid injection means comprise a line 13 for supplying pressurized oil usually connected to the engine lubrication pump and leading to an annular distribution chamber 14, delimited in the interface j between the periphery of the ring 6 and its bore 7 for example using a cir groove cular 15 formed at the periphery of the sealing ring 6.
  • the chamber 14 can be traversed by a large flow of oil under pressure moving towards another member to be lubricated or discharge via an outlet pipe 16.
  • the chamber 14 is delimited in the interface j by two annular seals 17 and 18 disposed respectively on the side of the combustion chamber 2 and on the side of the plug 1.
  • the annular seals 17 and 18 are preferably made of a resistant elastomeric material for seal housed by elasticity in annular grooves formed on the outer surface of the ring 6 because the gun segment 11 1 and the circulation of oil protect against excessive temperature.
  • the oil distribution chamber 14 is connected to the interface e between the sealing surface of the ring 3 and the external surface 8 of the plug 1 by supply passages 19 made, preferably, by a longitudinal bore. in the thickness of the ring, connected to a transverse bore 20 from the bottom of the circular groove 15.
  • the supply passages 19 can lead to the interface e directly by an outlet chamfer or else in an annular groove continuous distribution 21 formed inside the contact or sealing surface 22 of the ring 6, this in order to better distribute the oil in the interface e.
  • the channel 6 formed inside the rotary valve 1 can be a channel for the admission of fresh gases (normally pressurized air or at atmospheric pressure) fueled or not, or else an exhaust channel combustion gases as described above and that the channel 3 can be replaced, as will be seen hereinafter, by a lateral notch successively filling, during the rotation of the plug, the functions of intake and exhaust passage.
  • tion 2 during the compression and gas combustion phases strongly applies the sealing surface 22 to the outer surface 8 of the plug 1 and reduces the thickness of this oil blade to a minimum value just sufficient to ensure a film of oil between the surface of the plug 1 and the sealing surface 22.
  • the friction hysteresis of the gun segment 11 of the ring 6 on the plug 1 maintains a significant residual application force of the ring 6 on the plug 1.
  • This residual force limits oil leaks between the sealing surface 22 and the surface 8 of the plug at a flow rate just sufficient to ensure a continuous film of oil between the surface 8 of the plug 1 and its guide bore 4.
  • the wear of the sealing surface 22 of the ring 6 is reduced to a minimum value and the risks of seizure at high speed of the ring 6 on the plug 1 are deleted.
  • the temperature of the surface of the plug 1 (moreover generally cooled internally by a longitudinal circulation of water) is considerably reduced and the seal between the plug and its bore 4 is ensured by an oil wedge.
  • the circulation in diversion of the oil between the supply pipe 13 and the outlet pipe 16 ensures an energetic cooling of the sealing ring 6 which could thus in certain application cases be made of a relatively soft material and good rubbing quality such as high strength molded plastic.
  • the sealing ring 6 as well as the plug 1 can be produced, preferably, in the different friction couples usually used in engines such as: cast iron / chrome, cast iron / cast iron, etc., but also in new composite materials , ceramics or other new products.
  • a calibrated orifice (not shown) can be placed on the inlet pipe 13 or on the supply passages 19 in order to limit the flow of oil escaping from the interface e when the pressure drop caused by the passages is insufficient to limit the oil leakage rate.
  • the sealing ring 6 can be made of porous sintered metal with a sealing plating on the surfaces which should not give rise to an exudation of oil, or else as shown in FIG. 2, an annular ring or cartridge 23 made of porous sintered metal, such as bronze, is introduced or molded in a blind housing 19a formed longitudinally in the sealing ring 6.
  • This porous ring 23 is connected by at least one lateral passage 20 to the oil pressure distribution chamber 14.
  • the porous ring 23 thus functions as a pressure drop and oil distribution member in the interface e and as a good-quality rubbing member reducing the friction between the ring 6 and the rotary plug 1. This arrangement which appears suitable for cases where the speed of rotation of the plug 1 is moderate and where vigorous cooling of the sealing ring 6 is not required, reduces oil losses and is generally more economical to implement than the solution shown in fig. 1.
  • FIGS. 3a to 3c schematically represent the most characteristic positions of a plug 1 provided, not with an internal channel, but with a notch 24 intended to ensure the distribution (suction and exhaust) of a combustion chamber 2 of an internal combustion engine operating according to the four-stroke cycle.
  • the notch 24 connects the combustion chamber 2 of the engine (via a sealing ring of the type described in FIGS. 1 and 2 and not shown) to a suction pipe 25 provided with introduction means fuel such as a carburetor or injector, if the engine is operated with a positive ignition.
  • introduction means fuel such as a carburetor or injector
  • the notch 24 of the plug 1 delimits with the guide bore 4 valve 1 a passage chamber 27 of a significant volume and which is then isolated from the intake and exhaust.
  • the chamber 27 was filled during the intake phase with air relatively rich in fuel since it was sucked in after the walls of the suction pipe were saturated with liquid fuel.
  • the air rich in fuel contained in the passage chamber 27 is completely discharged to the exhaust 26, in particular as a result of the arrival of the puff of exhaust gas at the time of setting up communications (not shown) of the combustion chamber 2 with the chamber 27 when the edge 28 of the notch 24 opens onto the passage 5 connected to the combustion chamber 2.
  • FIG. 4 shows, on a larger scale, a solution to reduce fuel and oil losses. Elements identical to those in FIGS. 1 to 3c are given the same reference numbers.
  • oil scraper means are arranged around the air intake orifice on the plug 1.
  • the scraper means are constituted by an intake sealing ring 29 permanently applied to the surface 8 of the plug 1 by a spring 30.
  • the fuel introduction means constituted here by a petrol injector 31 are adjusted so that the injection is cut off well before the end of the combustion air suction phase.
  • the sealing ring 29 housed in the cooled cylinder head 32 of the engine and through which the fresh intake gases pass is neither subjected to high temperatures nor to significant pressure differences (the overpressures and depressions are less than 1 bar) and as a result, it can be made of a good rubbing plastic material such as Teflon.
  • the operation of the embodiment shown in FIG. 4 is described below.
  • the plug 1 rotates in synchronism with the motor and receives from the supply passages 19 and the distribution groove 21 an oil film which is driven on its surface 8.
  • the oil film formed in the interface between the plug and the bore 4 is stopped by the sealing ring 29 substantially of the same width as the main sealing ring 6.
  • the injection of fuel by the injector 31 begins as soon as the edge 28 of the notch 24 leads to the inner passage 33 of the suction ring 29 and stops well before the other edge 34 of the notch 24 reaches the right edge 35 of the passage 5 formed inside the ring 6 and does not cut off the intake.
  • FIGS. 5 and 6 Another embodiment of the device for controlling the circulation of gases to and from an engine combustion chamber is shown in FIGS. 5 and 6 in which the elements and members identical to those of the preceding figures have the same reference numbers.
  • the plug 1 has two separate inlet and outlet passages 36 and 37 respectively. Each of these two passages successively opens by rotation of the plug 1 on the side of the combustion chamber 2 on the ring d seal 6 and, on the opposite side, on orifices which are laterally offset with respect to the seal ring 6.
  • the intake passage 36 opens from one side of the cylinder head onto the suction pipe 25 surrounded by its suction seal ring 29.
  • the exhaust passage 37 opens onto the passage 5 inside the ring 6 and onto the exhaust pipe 26 offset along the axis of the plug 1 with respect to the sealing ring 6.
  • the two intake passages 36 and 36a of two combustion chambers adjacent to an engine lead to a common orifice 38 for communication with the intake pipe 25 common to the two cylinders.
  • This arrangement which also applies to the exhaust ducts and orifices, makes it possible to reduce the number of outlets to be provided in the plug 1 and the cylinder head 32 which constitute as many zones of weakening of the mechanical resistance of these highly stressed members on the mechanical and thermal plans.
  • the intake channel 25 shown in cross section in FIG. 8 and in longitudinal section in FIG. 9, comprises two auxiliary passages 39 and 40 for supplying a fuel-rich mixture such as an air-petrol emulsion obtained by injecting petrol using an injector 31 (conduit 39 in FIG. 9 ) or by an emulsion carburetor 41 (line 40 in fig. 9).
  • a fuel-rich mixture such as an air-petrol emulsion obtained by injecting petrol using an injector 31 (conduit 39 in FIG. 9 ) or by an emulsion carburetor 41 (line 40 in fig. 9).
  • a single auxiliary duct 39 is sufficient to ensure the correct metering of the fuel.
  • the auxiliary conduits 39 and 40 are closed before the enlarged part 25a of the conduit 25 is so and the air sucked in at the end d suction on the large section 25a does not contain fuel and sweeps the passage chamber 27 delimited by the notch 24 to deplete it of almost all the liquid fuel deposited on its walls, so that when this passage chamber is through which the exhaust gases pass, these entrain only a minute quantity of fuel thus unused towards the exhaust pipe 26.
  • FIGS 10 and 11 illustrate the mounting of a supply member connecting the combustion chamber 2 to the outside such as a spark plug 42 used when the heat engine is an internal combustion engine with controlled ignition.
  • a spark plug 42 used when the heat engine is an internal combustion engine with controlled ignition.
  • the spark plug 42 may be replaced by a fuel injector or a glow plug.
  • the spark plug 42 is screwed into a thread 43 formed through a thin wall area 44 of the cylinder head 32 of the engine, so that its electrodes 45 (connected to ground) and 46 protrude slightly from the interior of the combustion chamber 2.
  • most of the combustion chamber in the vicinity of the top dead center of the piston (not shown) is constituted by the passage 5 of relatively large dimension formed in the sealing ring 6.
  • the spark plug 42 is placed in the position shown in FIG. 10, the fuel mixture is ignited relatively poorly because it does not start in a central position relative to the main volume of the combustion chamber at top dead center.
  • Fig. 11 illustrates in section an arrangement of the spark plug 42 (or where appropriate of a fuel injector or of a heating plug) which overcomes the drawbacks of the mounting solution shown in FIG. 10.
  • the sealing ring 6 comprises between two supply passages 19 a thread 43 for receiving the end portion or base 47 of the spark plug 42 which, in the sealed mounting position through this thread crossing the cross section of the ring 6, projects by its electrodes 45 and 46 inside the passage 5 in the vicinity of the wall but substantially at the center of the main combustion chamber formed by this passage 5.
  • the spark plug rod 48 which constitutes the part adjacent to the base 47 crosses with play a relatively narrow passage 49 formed through the wall of the cylinder head 32.
  • the passage 49 is connected to the outside by a bore 50 of larger diameter forming a annular chamber 51 into which the outlet pipe 16 opens.
  • an elastic annular seal 53 is interposed between the wall of the bore 50 and the cylindrical insulator 52 of the outlet terminal 54 of the candle 42.
  • the position of the ring 6, relative to the rotary plug 1, is likely to vary in service as a result of the expansion of the ring 6, variable axial and radial pressure forces on this ring 6 and especially wear progressive sealing surface 22 of this ring in rubbing contact with the surface 8 of the rotor 1, this wear varying lejeu i.
  • the instantaneous (at each explosion) and progressive movements of the ring 6 do not disturb the sealing of the chamber 51 and the position of the spark plug in the cylinder head 32 thanks, on the one hand, to the play in the passage 49 and avoiding any contact between the cylinder head 32 and the spark plug rod 48 and, on the other hand, the elasticity of the annular seal 53 preferably produced in one elastomeric material.
  • the fuel injector could advantageously be cooled while the glow plug should not be or should be as little as possible, which is achievable by placing it in an insulating envelope.
  • the mounting device assembly system shown in FIG. 11 carries out a mechanical and vibratory decoupling between, on the one hand the sealing ring 6 which delimits most of the combustion chamber at the top dead center of the piston and, on the other hand, the cylinder head 32. Thanks to the properties damping the elastomer of the seal 53 and the annular seals 17 and 18, not only the possible vibrations of the ring 6 can not be transmitted to the cylinder head and vice versa but, in addition, these vibrations are damped at their frequency critical by the large mass of elastomer of the joint 53.
  • the spark plug 42 is mounted on the thread 43 of the ring 6 outside the refrigerant circuit passing through the annular chamber 14.
  • the chamber 14 is, by example, placed near the upper end (in the drawing) of the ring 6 and in the vicinity of the interface e, the spark plug base 47 being placed either in the vicinity of the middle of the height of the ring 6 , which is closer to combustion chamber 2.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

La présente invention s'applique à un dispositif de contrôle de la circulation des gaz de et vers une chambre de combustion de moteur à combustion interne, constiué par un boisseau tournant ou rotor comportant au moins un canal intérieur ou une entaille latérale définissant des passages d'écoulement transversal respectifs d'échappement ou d'admission, un passage relié directement à la chambre de combustion, le boisseau étant contenu dans un alésage transversal dans lequel débouche l'orifice dudit passage aménagé dans un anneau d'étanchéité qui est logé dans un alésage, dans lequel il coulisse, l'anneau d'étanchéité étant appliqué sur le rotor par une surface de contact continue autour de l'orifice du passage sous l'effet de la pression régnant dans la chambre de combustion étant entouré d'un ou plusieurs organes d'étanchéité tels que des segments, et étant muni de moyens d'injection d'huile sur le boisseau.The present invention applies to a device for controlling the circulation of gases to and from a combustion chamber of an internal combustion engine, constituted by a rotary plug or rotor comprising at least one internal channel or a lateral cut defining passages of 'respective exhaust or intake transverse flow, a passage directly connected to the combustion chamber, the plug being contained in a transverse bore into which opens the orifice of said passage arranged in a sealing ring which is housed in a bore, in which it slides, the sealing ring being applied to the rotor by a continuous contact surface around the orifice of the passage under the effect of the pressure prevailing in the combustion chamber being surrounded by one or several sealing members such as segments, and being provided with means for injecting oil on the plug.

Selon un mode de réalisation connu de ce type de moteur (demandes de brevet français FR-A-2 531 139 et FR-A-2 531 174) permettant de tourner à des vitesses de rotation élevée, le boisseau est contenu dans un alésage transversal dans lequel débouche l'orifice relié directement à la chambre de combustion et les orifices d'admission et/ou d'échappement reliés respectivement à un collecteur d'échappement. Le passage relié à la chambre de combustion est aménagé dans un anneau d'étanchéité logé dans un alésage appliqué, sur le boisseau par une surface d'étanchéité continue autour de l'orifice relié directement à la chambre de combustion, sous l'effet de la pression régnant dans la chambre de combustion, et entouré d'un ou plusieurs, organes d'étanchéité tels que des segments, cet anneau pouvant coulisser dans l'alésage et sa course étant limitée, d'un côte, par le boisseau et, de l'autre côté, par un épaulement de retenue.According to a known embodiment of this type of motor (French patent applications FR-A-2,531,139 and FR-A-2,531,174) making it possible to rotate at high rotational speeds, the plug is contained in a transverse bore into which opens the orifice connected directly to the combustion chamber and the intake and / or exhaust orifices connected respectively to an exhaust manifold. The passage connected to the combustion chamber is arranged in a sealing ring housed in an applied bore, on the plug by a continuous sealing surface around the orifice connected directly to the combustion chamber, under the effect of the pressure prevailing in the combustion chamber, and surrounded by one or more, sealing members such as segments, this ring being able to slide in the bore and its stroke being limited, on one side, by the plug and, on the other side, by a retaining shoulder.

De tels moteurs à combustion paraissent aptes à délivrer des puissances massiques beaucoup plus élevées que les solutions connues et éprouvées, en particulier pour les moteurs de faible cylindrée, par suite de l'absence de pièces de distribution soumises à un mouvement alternatif générateur d'une fréquence limite de battement. L'avantage le plus décisif de ce type de distribution réside dans la possibilté d'avoir des conduits d'échappement et d'admission de diamètre deux fois plus important qu'un système à soupapes classiques, ce qui perment d'avoir un meilleur remplissage et donc une puissance spécifique plus importante.Such combustion engines appear capable of delivering mass powers much higher than known and proven solutions, in particular for small displacement engines, due to the absence of distribution parts subjected to an alternating movement generating a beat limit frequency. The most decisive advantage of this type of distribution lies in the possibility of having exhaust and intake ducts twice the diameter of a conventional valve system, which allows for better filling. and therefore a higher specific power.

Après une première expérimentation approfondie des dispositifs de distribution à boisseau rotatifs, il s'avère que ces systèmes à rotor de distribution présentent des inconvénients ou des défauts de fonc- tionnemment qui n'ont pas permis d'en exploiter les avantages répertoriés ci-dessus.After a first in-depth experiment with rotary valve distribution devices, it turns out that these distribution rotor systems have drawbacks or operational flaws which have not made it possible to exploit the advantages listed above. .

Parmi ces divers inconvénients, on peut citer les difficultés pour assurer la lubrification et le refroidissement des éléments d'étanchéité, ce qui provoque une usure excessive du boisseau et des éléments et organes d'étanchéité, une consommation de lubrifiant élevée, et peut conduire, dans certains cas limites, au grippage du boisseau dans son alésage.Among these various drawbacks, mention may be made of the difficulties in ensuring the lubrication and cooling of the sealing elements, which causes excessive wear of the plug and of the sealing elements and elements, a high consumption of lubricant, and can lead to, in certain borderline cases, seizure of the bushel in its bore.

Par ailleurs, lorsque la distribution par boisseau rotatif est appliquée à des moteurs à quatre temps, on ne constate pas de diminution de la consommation spécifique de carburant par rapport aux moteurs fonctionnant selon le cylcle à deux temps. Cette surconsommation de carburant paraît due à une séparation insuffisante des conduits ou des phases d'admission et d'échappement qui entraîne:

  • - une dilution des gaz frais par les gaz d'échappement se traduisant par une mauvaise combustion et une pollution plus importante;
  • - une introduction du mélange carburé dans le gaz d'échappement entraînant aussi une augmentation de la pollution et de la consommation spécifique en carburant.
Furthermore, when the rotary valve distribution is applied to four-stroke engines, there is no reduction in the specific fuel consumption compared to engines operating according to the two-stroke cylinder. This overconsumption of fuel appears to be due to an insufficient separation of the ducts or of the intake and exhaust phases which leads to:
  • - dilution of the fresh gases by the exhaust gases, resulting in poor combustion and greater pollution;
  • - introduction of the fuel mixture into the exhaust gas also resulting in an increase in pollution and specific fuel consumption.

US-A-4 114 639 décrit une valve tournante utilisée pour le contrôle de la circulation des gaz de et vers une chambre de combustion de moteur à combustion interne et dans laquelle le lubrifiant est amené à l'aide de bouchons poreux entre l'organe de valve tournant et la surface intérieure de corps de valve supportant cet organe tournant. Cependant l'étanchéité entre l'insert formant joint annulaire et l'organe tournant formant distributeur d'alimentation et déchappement ne peut se maintenir dans le temps. Il n'existe en effet aucun moyen de placage de l'insert sur l'organe autre que celui dû à la pression de l'huile ou à la pression de combustion de la chambre. Ce système connu présente l'inconvénient, en cas d'usure au contact entre l'insert et l'organe tournant qu'il s'établit une fuite de gaz d'échappement vers la conduite d'amenée d'huile et un refoulement de l'huile de graissage, suivi du grippage du contact tournant.US-A-4,114,639 describes a rotary valve used for controlling the circulation of gases to and from a combustion chamber of an internal combustion engine and into which the lubricant is supplied using porous plugs between the member of the rotating valve and the inner surface of the valve body supporting this rotating member. However, the seal between the insert forming an annular seal and the rotating member forming the supply and exhaust distributor cannot be maintained over time. There is in fact no means of placing the insert on the member other than that due to the oil pressure or the combustion pressure of the chamber. This known system has the drawback, in the event of wear on contact between the insert and the rotating member, an exhaust gas leak is established towards the oil supply line and a discharge of lubricating oil, followed by seizure of the rotating contact.

L'un des buts de la présente invention est précisément de pallier ces défauts des moteurs à combustion à distribution rotative afin de permettre d'utiliser les grandes sections de passage qu'offre ce type de leur distribution sans risquer des usures rapides et des consommations de carburant exagérées.One of the aims of the present invention is precisely to overcome these defects of combustion engines with rotary distribution in order to allow the large passage sections offered by this type of their distribution to be used without risking rapid wear and consumption of exaggerated fuel.

A cet effet, selon un premier mode de réalisation de l'invention, l'anneau d'étanchéité est traversé au moins à sa périphérie par un circuit d'huile sous pression se dirigeant vers le retour d'huile et apte à assurer le refroidissement de cet anneau et les moyens d'injection sont branchés sur ledit circuit d'huile, traversent axialement au moins une partie de la section annulaire de l'anneau et débouchent dans une rainure annulaire continue de distribution qui est ménagée à l'intérieur de la surface de contact continue établie sur une bande de faible largeur selon la ligne générale d'intersection de deux cylindres et qui s'ouvre sur l'interface existant entre cette surface de contact et la surface extérieure du rotor.To this end, according to a first embodiment of the invention, the sealing ring is crossed at least at its periphery by a pressurized oil circuit heading towards the oil return and capable of ensuring cooling. of this ring and the injection means are connected to said oil circuit, pass axially through at least part of the annular section of the ring and open into a continuous annular distribution groove which is formed inside the continuous contact surface established on a strip of small width along the general line of intersection of two cylinders and which opens on the interface existing between this contact surface and the external surface of the rotor.

Les moyens d'injection du fluide sont constitués, d'une part, d'une chambre annulaire d'admission et de circulation d'huile, délimitée entre la périphérie de l'anneau d'étanchéité et son alésage et limitée axialement à chaque extrémité par un joint d'étanchéité interposé entre la surface extérieure de l'anneau d'étanchéité et l'alésage et, d'autre part, d'au moins un passage d'amenée présentant un orifice de sortie débouchant dans ladite interface entre la surface d'étanchéité continue et la surface extérieure du boisseau et en ce qu'au moins un segment d'étanchéité de coup de feu est interposé entre d'une part l'anneau d'étanchéité et son alésage et d'autre part ledit joint d'étanchéité situé du côté de la chambre de combustion.The means for injecting the fluid consist, on the one hand, of an annular oil intake and circulation chamber, delimited between the periphery of the sealing ring and its bore and axially limited at each end by a seal interposed between the outer surface of the sealing ring and the bore and, on the other hand, by at least one supply passage having an outlet opening opening into said interface between the surface continuous sealing and the outer surface of the plug and in that at least one gun sealing segment is interposed between on the one hand the sealing ring and its bore and on the other hand said seal located on the side of the combustion.

La chambre annulaire d'admission est parcourue par un débit important d'huile sous pression se dirigeant par une conduite de sortie vers un autre organe à lubrifier ou la décharge.The annular inlet chamber is traversed by a large flow of pressurized oil directing through an outlet pipe towards another member to be lubricated or the discharge.

Selon un autre mode de réalisation du dispositif, une partie d'extrémité d'au moins un organe d'amenée de l'un des éléments de la combustion, par exemple une bougie d'allumage pour un moteur à allumage commandé ou un injecteur et/ou une bougie de chauffage pour un moteur à cycle Diesel, traverse de façon étanche la section transversale de l'anneau d'étancheité pour déboucher dans le passage qui est relié à la chambre de combustion, et en ce que la partie adjacente de ladite partie d'extrémité est logée avec un jeu annulaire dans un passage d'amenée vers l'extérieur dudit élément de la combustion, ledit passage d'amenée étant relié à la chambre annulaire d'admission de fluide.According to another embodiment of the device, an end part of at least one supply member for one of the combustion elements, for example a spark plug for a spark-ignition engine or an injector, and / or a heating plug for a diesel cycle engine, crosses in a leaktight manner the cross section of the sealing ring to open into the passage which is connected to the combustion chamber, and in that the adjacent part of said end part is housed with an annular clearance in a supply passage towards the outside of said combustion element, said supply passage being connected to the annular fluid intake chamber.

En variante, le passage donnant lieu au jeu annulaire est parcouru par un écoulement du fluide amené à la chambre annulaire d'admission de fluide.As a variant, the passage giving rise to the annular clearance is traversed by a flow of the fluid brought to the annular fluid admission chamber.

Lorsque le dispositif de contrôle de la circulation des gas de et vers la chambre de combustion du moteur est appliqué à un moteur thermique le passage donnant lieu au jeu annulaire se prolonge vers l'extérieur par une chambre annulaire élargie, qui est fermée par un joint annulaire élastique interposé entre l'organe d'amenée et la paroi intérieure de ladite chambre et délimitant une chambre de refroidissement parcourue par ledit écoulement de fluide. L'anneau d'étanchéité est, d'une part, réalisé en un matériau mou présentant de bonnes qualités frottantes avec la surface du boisseau par exemple de la matière plastique et, d'autre part, repoussé en permanence sur la surface du boisseau sous une pression sensiblement constante par un ressort.When the device controlling the circulation of gases from and to the combustion chamber of the engine is applied to a heat engine, the passage giving rise to the annular clearance is extended towards the outside by an enlarged annular chamber, which is closed by a seal. elastic ring interposed between the supply member and the inner wall of said chamber and delimiting a cooling chamber traversed by said fluid flow. The sealing ring is, on the one hand, made of a soft material having good rubbing qualities with the surface of the plug, for example plastic, and, on the other hand, permanently pushed back on the surface of the plug under a substantially constant pressure by a spring.

Selon un mode de réalisation de l'invention, appliqué à un moteur thermique où le rotor sert simultanément à contrôler l'échappement du moteur et l'admission du mélange de carburant et d'air de combustion dans la chambre de combustion, des moyens racleurs du fluide lubrifiant injecté dans l'interface sont disposés autour de l'orifice d'admission reliant le rotor à l'admission du mélange d'air de combustion et de carburant du moteur, ces moyens racleurs étant constitués d'un anneau d'étanchéité d'admission disposé à la périphérie dudit orifice d'admission, qui vient en appui continu sur la surface extérieure du boisseau et qui est apte à isoler l'intérieur de l'orifice d'admission de l'interface entre le boisseau et son alésage pour limiter l'entraînement d'huile et simultanément de carburant liquide à la surface du boisseau en rotation.According to one embodiment of the invention, applied to a heat engine where the rotor simultaneously serves to control the exhaust of the engine and the admission of the mixture of fuel and combustion air into the combustion chamber, scraper means lubricating fluid injected into the interface are arranged around the intake orifice connecting the rotor to the intake of the mixture of combustion air and engine fuel, these scraper means being constituted by a sealing ring intake disposed at the periphery of said intake port, which comes into continuous support on the outer surface of the plug and which is capable of isolating the interior of the intake port from the interface between the plug and its bore to limit the entrainment of oil and liquid fuel simultaneously on the surface of the rotating plug.

Selon un autre mode de réalisation de l'invention, l'anneau d'étanchéité est, d'une part, réalisé en un matériau mou présentant de bonnes qualités frottantes avec la surface du boisseau par exemple de la matière plastique et, d'autre part, repoussé en permanence sur la surface du boisseau sous une pression sensiblement constante par un ressort. Selon un autre mode de réalisation de l'invention, le boisseau comporte deux passages séparés d'admission et respectivement d'échappement qui sont susceptibles de déboucher successivement tous les deux par rotation du boisseau, du côté de la chambre de combustion, sur l'anneau d'étanchéité et, du côté opposé à la chambre de combustion, sur des orifices de sortie qui sont chacun décalés sur l'axe du boisseau par rapport à l'anneau d'étanchéité, de manière à diminuer l'entraînement du carburant à la surface du boisseau et du carburant entraîné à l'admission dans le passage d'admission ménagé à l'intérieur du boisseau.According to another embodiment of the invention, the sealing ring is, on the one hand, made of a soft material having good rubbing qualities with the surface of the plug, for example plastic, and, on the other hand part, permanently pushed back on the surface of the plug under a substantially constant pressure by a spring. According to another embodiment of the invention, the plug has two separate inlet and outlet passages respectively which are capable of successively opening both by rotation of the plug, on the side of the combustion chamber, on the sealing ring and, on the side opposite to the combustion chamber, on outlet orifices which are each offset on the axis of the plug relative to the sealing ring, so as to reduce the entrainment of the fuel to the surface of the plug and the fuel entrained at the intake in the intake passage formed inside the plug.

Selon encore un autre mode de réalisation de l'invention, les passages séparés d'admission ou d'échappement de deux chambres de combustion voisines sont ménagés dans le boisseau en débouchant sur un orifice de communication avec l'admission ou l'échappement qui est commun aux deux chambres de combustion voisines, de manière à réduire le nombre d'ouvertures à prévoir sur la face extérieure du boisseau.According to yet another embodiment of the invention, the separate intake or exhaust passages of two neighboring combustion chambers are provided in the plug, opening onto an orifice for communication with the intake or the exhaust which is common to the two adjacent combustion chambers, so as to reduce the number of openings to be provided on the outside face of the plug.

Selon une forme d'exécution de l'invention, appliquée à un moteur thermique fonctionnant selon le cycle à quatre temps, le circuit d'admission de la chambre de combustion comporte des moyens de suppression du carburant dans l'air aspiré dans la chambre de combustion avant la fin de l'admission. Dans le cas où le carburant est introduit par injection dans l'air d'admission, les moyens de suppression précités sont constitués par l'arrét de l'injection de carburant nettement avant la fin de la phase d'aspiration.According to one embodiment of the invention, applied to a heat engine operating according to the four-stroke cycle, the intake circuit of the combustion chamber includes means for removing fuel from the air drawn into the combustion chamber. combustion before the end of admission. In the case where the fuel is introduced by injection into the intake air, the abovementioned suppression means consist of stopping the injection of fuel clearly before the end of the suction phase.

Dans le cas où le carburant est introduit dans la chambre de combustion via un carburateur, les moyens de suppression précités sont alors, de préférence, constitués par au moins un passage auxiliaire d'air riche en carburant tel qu'une émulsion, ménagé dans le boisseau et la culasse de la chambre de combustion et le passage auxiliaire débouche sur l'interface entre le boisseau et son alésage en un point tel qu'il est obturé par la rotation du boisseau avant que la (ou les) ouverture(s) principale(s) d'admission ne le soi(en)t.In the case where the fuel is introduced into the combustion chamber via a carburetor, the abovementioned suppression means are then preferably constituted by at least one auxiliary passage of air rich in fuel such as an emulsion, formed in the plug and cylinder head of the combustion chamber and the auxiliary passage leads to the interface between the plug and its bore at a point such that it is closed by the rotation of the plug before the main opening (s) (s) of admission not the self.

Selon une forme d'éxécution de l'invention, dans le cas où le carburant est introduit par injection dans l'air d'admission, les moyens de suppression sont constitués par l'arrêt de l'injection de carburant nettement avant la fin de la phase d'aspiration.According to one embodiment of the invention, in the case where the fuel is introduced by injection into the intake air, the suppression means are constituted by stopping the injection of fuel clearly before the end of the suction phase.

Selon une autre forme d'éxécution de l'invention, les moyens de suppression sont constitués par au moins un passage auxiliaire d'air riche en carburant, ménagé dans le boisseau et la culasse de la chambre de combustion et qui débouche sur l'interface entre le rotor et son alésage en un orifice qui est obturé par la rotation du rotor avant que la (ou les) ouverture(s) pricipale(s) d'admission ne le soi(en)t.According to another embodiment of the invention, the suppression means are constituted by at least one auxiliary passage of air rich in fuel, formed in the plug and the cylinder head of the combustion chamber and which opens onto the interface between the rotor and its bore in an orifice which is closed off by the rotation of the rotor before the main opening (s) of inlet (s) are self-contained.

Selon une autre variante encore du dispositif selon l'invention, le passage donnant lieu au jeu annulaire se prolonge vers l'extérieur par une chambre annulaire élargie, ladite chambre annulaire étant fermée par un joint annulaire élastique qui est interposé entre l'organe d'amenée et la paroi intérieure de ladite chambre et qui délimite une chambre de refroidissement parcourue par le fluide lubrifiant et réfrigérant amené par les moyens d'injection. Cette partie élargie permet à un outil d'accéder à l'organe d'amenée. US-A-4 114 639 décrit une valve tournante utilisée pour le contrôle de la circulation des gaz de et vers une chambre de combustion de moteur à combustion interne et dans lequelle le lubrifiant est amené à l'aide de bouchons poreux entre l'organe de valve tournant et la surface inférieure du corps de valve supportant cet organe tournant. Cependant l'étanchéité entre l'insert formant joint annulaire et l'organe tournant formant distributeur d'alimentation et d'échappement ne peut se maintenir dans le temps. In n'existe en effet aucun moyen de placage de l'insertsurl'organe autre que celui dû à la pression de l'huile ou à la pression de combustion de la chambre. Ce système connu présente l'inconvénient, en cas d'usure au contact entre l'insert et l'organe tournant qu'il s'établit une fuite de gaz d'échappement vers la conduite d'amenée d'huile et un refoulement de l'huile de graissage, suivi du grippage du contact tournant.According to yet another variant of the device according to the invention, the passage giving rise to the annular clearance is extended towards the outside by an enlarged annular chamber, said annular chamber being closed by an elastic annular seal which is interposed between the inlet and the inner wall of said chamber and which delimits a cooling chamber through which the lubricating and cooling fluid flows brought in by the injection means. This enlarged part allows a tool to access the feed member. US-A-4,114,639 describes a rotary valve used for controlling the circulation of gases to and from a combustion chamber of an internal combustion engine and into which the lubricant is supplied using porous plugs between the member of rotating valve and the lower surface of the valve body supporting this rotating member. However, the seal between the insert forming an annular seal and the rotating member forming the supply and exhaust distributor cannot be maintained over time. There is in fact no means of placing the insert on the organ other than that due to the oil pressure or to the combustion pressure of the chamber. This known system has the drawback, in the event of wear on contact between the insert and the rotating member, an exhaust gas leak is established towards the oil supply line and a discharge of lubricating oil, followed by seizure of the rotating contact.

D'autres buts, avantages et caractéristiques du dispositif de contrôle selon l'invention apparaîtront à la lecture de la description de divers modes de réalisation, faite à titre non limitatif et en ragard du dessin annexé où:

  • les figures 1 et 2 sont des vues en coupe et à grande échelle de deux modes de réalisation du système d'étanchéité selon l'invention entre un boisseau de distribution tournant et une chambre de combustion de moteur;
  • les figures 3a à 3c illustrent schématiquement les principales positions au cours d'un cycle moteurd'un système de distribution à boisseau appliqué à un moteur fonctionnant selon le cycle à quatre temps;
  • la fig. 4 est une vue en coupe à grande échelle du système de distribution à boisseau représenté schématiquement sur les figures 3a à 3c et équipé d'un anneau d'étanchéité d'admission selon l'invention;
  • la fig. 5 est une vue en coupe, toujours à grande échelle, d'un autre mode de réalisation du système de distribution à boisseau selon l'invention comportant des conduits d'admission et d'échappement séparés à l'intérieur du boisseau;
  • la fig. 6 est une vue en coupe avec arrachements selon la ligne VI-VI de la fig. 5, d'une partie du boisseau de distribution d'un moteur comportant plusieurs cylindres parallèles;
  • la fig. 7 est une vue en coupe à grande échelle d'un système de distribution à boisseau selon l'invention dans lequel sont prévus des moyens d'appauvrissement en carburant de l'air aspiré en fin d'admission;
  • les figures 8 et 9 sont des coupes respectivement selon les lignes VIII-VIII et IX-IX du système de distribution représenté à la figure 7;
  • la fig. 10 est une vue en coupe du système d'étanchéité selon l'invention comportant une bougie d'allumage débouchant dans la chambre de combustion;
  • la fig. 11 est une vue en coupe du système d'étanchéité selon l'invention comportant une bougie d'allumage débouchant directement dans le passage de l'anneau d'étanchéité.
Other objects, advantages and characteristics of the control device according to the invention will appear on reading the description of various embodiments, given without limitation and with reference to the appended drawing where:
  • Figures 1 and 2 are sectional views on a large scale of two embodiments of the sealing system according to the invention between a rotating distribution valve and an engine combustion chamber;
  • FIGS. 3a to 3c schematically illustrate the main positions during a motor cycle of a plug distribution system applied to an engine operating according to the four-stroke cycle;
  • fig. 4 is a sectional view on a large scale of the plug distribution system shown diagrammatically in FIGS. 3a to 3c and equipped with an intake sealing ring according to the invention;
  • fig. 5 is a sectional view, still on a large scale, of another embodiment of the valve distribution system according to the invention comprising separate intake and exhaust ducts inside the valve;
  • fig. 6 is a sectional view with cutaway along line VI-VI of FIG. 5, of a part of the valve plug of an engine comprising several parallel cylinders;
  • fig. 7 is a sectional view on a large scale of a plug distribution system according to the invention in which means are provided for depletion of fuel from the air sucked in at the end of intake;
  • Figures 8 and 9 are sections respectively along lines VIII-VIII and IX-IX of the distribution system shown in Figure 7;
  • fig. 10 is a sectional view of the sealing system according to the invention comprising a spark plug opening into the combustion chamber;
  • fig. 11 is a sectional view of the sealing system according to the invention comprising a spark plug opening directly into the passage of the sealing ring.

Sur les figures 1 et 2, un boisseau rotatif 1 de distribution de l'échappement d'une chambre de combustion 2 de moteur thermique est représenté à l'instant où son canal intérieur d'échappement 3 est ouvert en grand sur la chambre de combustion 2. Le boisseau 1 tourne, en continu et de façon synchronisée avec la rotation du moteur, dans un alésage 4 et le canal d'échappement 3 est relié à la chambre de combustion 2 par un passage 5 de ralativement grande dimension ménagé dans un anneau d'étanchéité 6 qui peut coulisser librement dans un alésage 7 d'axe sensiblement parallèle à celui du cylindre moteur (non représenté) ou sensiblement perpendiculaire à l'axe de rotation du boisseau 1, de manière à assurer un bon portage de la surface de contact de l'anneau 6 sur la surface extérieure 8 du boisseau 1. La surface de contact 22 entre l'anneau 6 et le boisseau 1 s'établit sur une bande de faible largeur selon la ligne générale d'intersection de deux cylindres (les surfaces extérieures du boisseau 1 et de l'anneau 6 de diamètres différents et d'axes sensiblement perpendiculaires et concourants. Selon une disposition connue particulièrement efficace parce qu'elle proportionne l'effort d'application de l'anneau d'étanchéité 6 sur le boisseau 1 à la pression à étancher, l'anneau d'étanchéité 6 qui se déplace à frottement doux dans son alésage 7 est appliqué sur la surface extérieure du boisseau 1 par la seule pression régnant dans la chambre de combustion 2 et agissant sur sa section annulaire, majorée le cas échéant de la poussée d'un ressourt à faible effort de réaction tel qu'une rondelle élastique. La présence de ce ressort de poussée (non représenté) de l'anneau 6 sur le boisseau 1 n'est pas indispensable s'il n'existe qu'un faible jeu ou interface i entre l'extrémité 9 de l'anneau 6 du côté de la chambre de combustion 2 et un épaulement de retenue 10 ménagé à l'extrémité de l'alésage 7 recevant l'anneau 6. De plus, la température étant relativement élevée dans l'interface i à cause de la proximité de la chambre de combustion 2, la tenue dans le temps d'un organe de ressort est des plus aléatoires. Afin de supprimer les fuites dans l'interface j entre la superfice extérieure de l'anneau 6 et l'intérieur de son alésage 7, un segment d'étanchéité de coup de feu 11 est disposé de manière connue dans cet interface j et est porté par une rainure 12 ménagée de préférence dans l'anneau 6. Le segment 11 évite également une surchauffe de l'interface j en direction du boisseau 1 et la formation dans cet interface de dépôts qui finiraient par bloquer l'anneau 6 dans son alésage 7.In FIGS. 1 and 2, a rotary plug 1 for distributing the exhaust of a combustion chamber 2 of a heat engine is shown at the moment when its internal exhaust channel 3 is opened wide on the combustion chamber 2. The plug 1 turns, continuously and synchronously with the rotation of the engine, in a bore 4 and the exhaust channel 3 is connected to the combustion chamber 2 by a passage 5 of relatively large dimension formed in a ring seal 6 which can slide freely in a bore 7 with an axis substantially parallel to that of the engine cylinder (not shown) or substantially perpendicular to the axis of rotation of the plug 1, so as to ensure good bearing of the surface of contact of the ring 6 on the outer surface 8 of the plug 1. The contact surface 22 between the ring 6 and the plug 1 is established on a strip of small width along the general line of intersection of two cylinders (the exterior surfaces of the wood bucket 1 and ring 6 of different diameters and substantially perpendicular and concurrent axes. According to a known arrangement which is particularly effective because it provides the force for applying the sealing ring 6 on the plug 1 to the pressure to be sealed, the sealing ring 6 which moves with gentle friction in its bore 7 is applied to the outer surface of plug 1 by the single pressure prevailing in combustion chamber 2 and acting on its annular section, increased if necessary by the thrust of a spring with low reaction force such as a washer elastic. The presence of this thrust spring (not shown) of the ring 6 on the plug 1 is not essential if there is only a slight clearance or interface i between the end 9 of the ring 6 of the side of the combustion chamber 2 and a retaining shoulder 10 formed at the end of the bore 7 receiving the ring 6. In addition, the temperature being relatively high in the interface i because of the proximity of the chamber 2 combustion, the holding over time of a spring member is very random. In order to eliminate leaks in the interface j between the outer surface of the ring 6 and the interior of its bore 7, a gun sealing segment 11 is disposed in a known manner in this interface j and is worn by a groove 12 preferably made in the ring 6. The segment 11 also prevents overheating of the interface j in the direction of the plug 1 and the formation in this interface of deposits which would end up blocking the ring 6 in its bore 7 .

Selon l'invention, l'anneau d'étanchéité 6 est muni de moyens d'injection d'un fluide lubrifiant et réfrigérant, de préférence d'huile de lubrification du moteur mise sous pression par la pompe à huile du moteur, dans l'interface e entre la surface d'étanchéité continue 22 (selon la ligne générale d'intersection orthogonale de deux cylindres de diamètres différents) autour de l'orifice 3 ménagé dans le boisseau 1 et la surface extérieure 8 du boisseau 1.According to the invention, the sealing ring 6 is provided with means for injecting a lubricating and cooling fluid, preferably engine lubricating oil pressurized by the engine oil pump, into the interface e between the continuous sealing surface 22 (along the general line of orthogonal intersection of two cylinders of different diameters) around the orifice 3 formed in the plug 1 and the external surface 8 of the plug 1.

Selon le dispositif représenté à la fig. 1, les moyens d'injection de fluide comportent une conduite 13 d'amenée d'huile sous pression habituellement reliée à la pompe de graissage du moteur et débouchant sur une chambre annulaire de distribution 14, délimitée dans l'interface j entre la périphérie de l'anneau 6 et son alésage 7 par exemple à l'aide d'une rainure circulaire 15 ménagée à la périphérie de l'anneau d'étanchéité 6. Selon une disposition favorisant le refroidissement de l'anneau 6, la chambre 14 peut être parcourue par un débit important d'huile sous pression se dirigeant vers un autre organe à lubrifier ou la décharge par une conduite de sortie 16. La chambre 14 est délimitée dans l'interface j par deux joints d'étanchéité annulaires 17 et 18 disposés respectivement du côté de la chambre de combustion 2 et du côté du boisseau 1. Les joints annulaires 17 et 18 sont, de préférence, réalisés en un matériau élastomère résistant pour joint logé par élasticité dans des rainures annulaires ménagées à la surface extérieure de l'anneau 6 car le segment de coup de feu 11 1 et la circulation de l'huile les protègent contre une température excessive.According to the device shown in fig. 1, the fluid injection means comprise a line 13 for supplying pressurized oil usually connected to the engine lubrication pump and leading to an annular distribution chamber 14, delimited in the interface j between the periphery of the ring 6 and its bore 7 for example using a cir groove cular 15 formed at the periphery of the sealing ring 6. According to an arrangement favoring the cooling of the ring 6, the chamber 14 can be traversed by a large flow of oil under pressure moving towards another member to be lubricated or discharge via an outlet pipe 16. The chamber 14 is delimited in the interface j by two annular seals 17 and 18 disposed respectively on the side of the combustion chamber 2 and on the side of the plug 1. The annular seals 17 and 18 are preferably made of a resistant elastomeric material for seal housed by elasticity in annular grooves formed on the outer surface of the ring 6 because the gun segment 11 1 and the circulation of oil protect against excessive temperature.

La chambre de distribution d'huile 14 est reliée à l'interface e entre la surface d'étanchéité de l'anneau 3 et la surface extérieure 8 du boisseau 1 par des passages d'amenée 19 réalisés, de préférence, par un perçage longitudinal dans l'épaisseur de l'anneau, raccordé à un perçage transversal 20 à partir du fond de la rainure circulaire 15. Les passages d'amenée 19 peuvent déboucher sur l'interface e directement par un chanfrein de sortie ou bien dans une rainure annulaire continue de distribution 21 ménagée à l'intérieur de la surface de contact ou d'étanchéité 22 de l'anneau 6, ceci afin de mieux répartir l'huile dans l'interface e. On doit noter que le canal 6 ménagé à l'intérieur du boisseau rotatif 1 peut être un canal d'admission des gaz frais (normalement de l'air surpressé ou à la pression atmosphérique) carburés ou non, ou bien un canal d'échappement des gaz de combustion comme décrit précédemment et que le canal 3 peut être remplacé, comme on le verra par la suite, par une entaille latérale remplissant successivement au cours de la rotation du boisseau, les fonctions de passage d'admission puis d'échappement.The oil distribution chamber 14 is connected to the interface e between the sealing surface of the ring 3 and the external surface 8 of the plug 1 by supply passages 19 made, preferably, by a longitudinal bore. in the thickness of the ring, connected to a transverse bore 20 from the bottom of the circular groove 15. The supply passages 19 can lead to the interface e directly by an outlet chamfer or else in an annular groove continuous distribution 21 formed inside the contact or sealing surface 22 of the ring 6, this in order to better distribute the oil in the interface e. It should be noted that the channel 6 formed inside the rotary valve 1 can be a channel for the admission of fresh gases (normally pressurized air or at atmospheric pressure) fueled or not, or else an exhaust channel combustion gases as described above and that the channel 3 can be replaced, as will be seen hereinafter, by a lateral notch successively filling, during the rotation of the plug, the functions of intake and exhaust passage.

Le fonctionnement du dispositif de contrôle de la circulation des gaz de et/ou vers une chambre de combustion de moteur, tel que représenté à la fig. 1 va maintenant être explicité. Dès que le moteur est mis en rotation, il entraîne le boisseau 1 en rotation synchrone et il engendre une pression d'huile qui se transmet à la chambre de distribution 14 et à la rainure annulaire 21 pour faire écouler une mince lame d'huile entre la surface d'étanchéité 22 de l'anneau 6 et la surface extérieure mobile 8 du boisseau 1. La pression régnant dans la chambre de combus-The operation of the device for controlling the circulation of gases from and / or to an engine combustion chamber, as shown in FIG. 1 will now be explained. As soon as the motor is put into rotation, it drives the plug 1 in synchronous rotation and it generates an oil pressure which is transmitted to the distribution chamber 14 and to the annular groove 21 to cause a thin blade of oil to flow between the sealing surface 22 of the ring 6 and the movable external surface 8 of the plug 1. The pressure prevailing in the combustion chamber

tion 2 pendant les phases de compression et de combustion des gaz applique fortement la surface d'étanchéité 22 sur la surface extérieure 8 du boisseau 1 et réduit l'épaisseur de cette lame d'huile à une valeur minimale juste suffisante à assurer un film d'huile entre la surface du boisseau 1 et la surface d'étanchéité 22. Pendant les phases de balayage et d'aspiration (pour la marche du moteur selon le cycle à quatre temps) où la pression dans la chambre de combustion 2 est voisine de la pression atmosphérique ou peu supérieure à celle-ci (cas du moteur suralimenté), l'hystérésis de friction du segment de coup de feu 11 de l'anneau 6 sur le boisseau 1 maintient un effort d'application résiduel non négligeable de l'anneau 6 sur le boisseau 1. Cet effort résiduel limite les fuites d'huile entre la surface d'étanchéité 22 et la surface 8 du boisseau à un débit juste suffisant pour assurer un film d'huile continu entre la surface 8 du boisseau 1 et son alésage de guidage 4. Lorsque le canal 3 à l'intérieur du boisseau 1 est un canal d'échappement, les fuites d'huile vers le passage intérieur 3-5 sont emportées vers l'échappement et donc perdues, tandis que lorsque le canal 3 est un canal d'admission, les fuites d'huile vers le passage 5 sont ramenées dans la chambre de combustion 2 et ainsi au moins partiellement réutilisées.tion 2 during the compression and gas combustion phases strongly applies the sealing surface 22 to the outer surface 8 of the plug 1 and reduces the thickness of this oil blade to a minimum value just sufficient to ensure a film of oil between the surface of the plug 1 and the sealing surface 22. During the sweeping and suction phases (for running the engine according to the four-stroke cycle) where the pressure in the combustion chamber 2 is close to atmospheric pressure or slightly higher than this (case of the supercharged engine), the friction hysteresis of the gun segment 11 of the ring 6 on the plug 1 maintains a significant residual application force of the ring 6 on the plug 1. This residual force limits oil leaks between the sealing surface 22 and the surface 8 of the plug at a flow rate just sufficient to ensure a continuous film of oil between the surface 8 of the plug 1 and its guide bore 4. When the can al 3 inside the plug 1 is an exhaust channel, the oil leaks to the interior passage 3-5 are carried to the exhaust and therefore lost, while when the channel 3 is an intake channel , the oil leaks to the passage 5 are brought back into the combustion chamber 2 and thus at least partially reused.

Grâce à la lubrification continue de l'interface e, l'usure de la surface d'étanchéité 22 de l'anneau 6 est réduite à une valeur minimale et les risques de grippage à haut régime de l'anneau 6 sur le boisseau 1 sont supprimés. La température de la surface du boisseau 1 (par ailleurs généralement refroidi intérieurement par une circulation longitudinale d'eau) est considérablement réduite et l'étanchéité entre le boisseau et son alésage 4 est assurée par un coin d'huile. La circulation en dérivation de l'huile entre la conduite d'amenée 13 et la conduite de sortie 16 assure un refroidissement énergique de l'anneau d'étanchéité 6 qui pourrait ainsi dans certains cas d'application être réalisé en un matériau relativement mou et de bonne qualité frottante tel que de la matière plastique moulée à haute résistance.Thanks to the continuous lubrication of the interface e, the wear of the sealing surface 22 of the ring 6 is reduced to a minimum value and the risks of seizure at high speed of the ring 6 on the plug 1 are deleted. The temperature of the surface of the plug 1 (moreover generally cooled internally by a longitudinal circulation of water) is considerably reduced and the seal between the plug and its bore 4 is ensured by an oil wedge. The circulation in diversion of the oil between the supply pipe 13 and the outlet pipe 16 ensures an energetic cooling of the sealing ring 6 which could thus in certain application cases be made of a relatively soft material and good rubbing quality such as high strength molded plastic.

L'anneau d'étanchéité 6 ainsi que le boisseau 1 pourront être réalisés, de préférence, dans les différents couples de frottement habituellement utilisés dans les moteurs tels que: fonte/chrome, fonte/ fonte, etc., mais aussi en matériaux composites nouveaux, céramiques ou autres nouveaux produits. Un orifice calibré (non représenté) peut être disposé sur la conduite d'entrée 13 ou sur les passages d'amenée 19 afin de limiter le débit d'huile s'échappant de l'interface e lorsque la perte de charge provoquée par les passages d'amenée est insuffisante pour limiter le débit de fuite d'huile.The sealing ring 6 as well as the plug 1 can be produced, preferably, in the different friction couples usually used in engines such as: cast iron / chrome, cast iron / cast iron, etc., but also in new composite materials , ceramics or other new products. A calibrated orifice (not shown) can be placed on the inlet pipe 13 or on the supply passages 19 in order to limit the flow of oil escaping from the interface e when the pressure drop caused by the passages is insufficient to limit the oil leakage rate.

Dans le mode de réalisation représenté à la fig. 2, les éléments identiques à ceux représentés à la fig. 1 sont dotés des mêmes numéros de référence. A la différence de la fig. 1, l'anneau d'étancheité 6 peut être réalisé en métal fritté poreux avec un placage d'étanchéité sur les surfaces ne devant pas donner lieu à une exsudation d'huile, ou bien comme représenté à la fig. 2, une bague ou cartouche annulaire 23 en métal fritté poreux, tel que du bronze, est introduite ou moulée dans un logement borgne 19a ménagé longitudinalement dans l'anneau d'étanchéité 6. Cette bague poreuse 23 est reliée par au moins un passage latéral 20 à la chambre 14 de distribution de pression d'huile. La bague poreuse 23 fonctionne ainsi comme un organe de perte de charge et de répartition de l'huile dans l'interface e et comme un organe à bonne qualité frottante réduisant la friction entre la bague 6 et le boisseau rotatif 1. Cette disposition qui paraît convenir pour les cas où la vitesse de rotation du boisseau 1 est modérée et où un refroidissement énergique de l'anneau d'étanchéité 6 n'est pas exigé, diminue les pertes d'huile et se révèle généralement plus économique à mettre en oeuvre que la solution représentée à la fig. 1.In the embodiment shown in FIG. 2, the elements identical to those shown in FIG. 1 have the same reference numbers. Unlike fig. 1, the sealing ring 6 can be made of porous sintered metal with a sealing plating on the surfaces which should not give rise to an exudation of oil, or else as shown in FIG. 2, an annular ring or cartridge 23 made of porous sintered metal, such as bronze, is introduced or molded in a blind housing 19a formed longitudinally in the sealing ring 6. This porous ring 23 is connected by at least one lateral passage 20 to the oil pressure distribution chamber 14. The porous ring 23 thus functions as a pressure drop and oil distribution member in the interface e and as a good-quality rubbing member reducing the friction between the ring 6 and the rotary plug 1. This arrangement which appears suitable for cases where the speed of rotation of the plug 1 is moderate and where vigorous cooling of the sealing ring 6 is not required, reduces oil losses and is generally more economical to implement than the solution shown in fig. 1.

Le figures 3a à 3c représentent schématiquement les positions les plus caractéristiques d'un boisseau 1 muni, non pas d'un canal intérieur, mais d'une entaille 24 destinée à assurer la distribution (aspiration et échappement) d'une chambre de combustion 2 d'un moteur à combustion interne functionnant selon le cycle à quatretemps. A la fig. 3a, on voit que l'entaille 24 relie la chambre de combustion 2 du moteur (via un anneau d'étanchéité du type décrit sur les figures 1 et 2 et non représenté) à une conduite d'aspiration 25 dotée de moyens d'introduction de carburant tel qu'un carburateur ou un injecteur, si le moteur fonctionne avec un allumage commandé. A la fig. 3b, le boisseau 1 a tourné dans le sens trigonométrique et est venu obturer à la fois la conduite d'aspiration 25 et la conduite d'échappement 26. On voit que l'entaille 24 du boisseau 1 délimite avec l'alésage 4 de guidage du boisseau 1 une chambre de passage 27 d'un volume non négligeable et qui est alors isolée de l'admission et de l'échappement. La chambre 27 a été remplie au cours de la phase d'admission par de l'air relativement riche en carburant car aspiré après que les parois du conduit d'aspiration ont été saturées de carburant liquide. On voit à la fig. 3c que l'air riche en carburant contenu dans la chambre de passage 27 est complètement déchargé à l'échappement 26, notamment par suite de l'arrivée de la bouffée de gaz d'échappement au moment de la mise en communications (non représentée) de la chambre de combustion 2 avec la chambre 27 lorsque le bord 28 de l'entaille 24 débouche sur le passage 5 relié à la chambre de combustion 2.FIGS. 3a to 3c schematically represent the most characteristic positions of a plug 1 provided, not with an internal channel, but with a notch 24 intended to ensure the distribution (suction and exhaust) of a combustion chamber 2 of an internal combustion engine operating according to the four-stroke cycle. In fig. 3a, it can be seen that the notch 24 connects the combustion chamber 2 of the engine (via a sealing ring of the type described in FIGS. 1 and 2 and not shown) to a suction pipe 25 provided with introduction means fuel such as a carburetor or injector, if the engine is operated with a positive ignition. In fig. 3b, the plug 1 has turned counterclockwise and has closed both the suction pipe 25 and the exhaust pipe 26. It can be seen that the notch 24 of the plug 1 delimits with the guide bore 4 valve 1 a passage chamber 27 of a significant volume and which is then isolated from the intake and exhaust. The chamber 27 was filled during the intake phase with air relatively rich in fuel since it was sucked in after the walls of the suction pipe were saturated with liquid fuel. We see in fig. 3c that the air rich in fuel contained in the passage chamber 27 is completely discharged to the exhaust 26, in particular as a result of the arrival of the puff of exhaust gas at the time of setting up communications (not shown) of the combustion chamber 2 with the chamber 27 when the edge 28 of the notch 24 opens onto the passage 5 connected to the combustion chamber 2.

Une autre source de surconsommation de carburant lorsque le moteur équipé d'un boisseau rotatif de distribution fonctionne selon le cycle à quatre temps avec alimentation en air carburé, réside dans le fait que le carburant liquide qui coule sur le parois d'aspiration et s'évapore progressivement en direction de la chambre de combustion, est entraîné à la surface du boisseau 1 en direction de l'échappement 26 où les gaz chauds l'évaporent et l'emportent en pure perte dans l'échappement avec le film d'huile déposé par le dispositif de lubrification représenté sur les figures 1 et 2.Another source of overconsumption of fuel when the engine equipped with a rotary distributor valve operates according to the four-stroke cycle with fuel air supply, lies in the fact that the liquid fuel which flows on the suction wall and s' gradually evaporates in the direction of the combustion chamber, is entrained on the surface of the plug 1 in the direction of the exhaust 26 where the hot gases evaporate it and carry it away in pure exhaust in the exhaust with the film of oil deposited by the lubrication device shown in Figures 1 and 2.

La figure 4 représente, à plus grande échelle, une solution permettant de réduire les pertes de carburant et d'huile. Les éléments identiques à ceux des figures 1 à 3c sont dotés des mêmes numéros de référence. Dans ce mode de réalisation, des moyens racleurs d'huile sont disposés autour de l'orifice d'admission d'air sur le boisseau 1. Les moyens racleurs sont constitués par un anneau d'étanchéité d'admission 29 appliqué en permanence sur la surface 8 du boisseau 1 par un ressort 30. Selon une autre disposition de ce mode de réalisation, les moyens d'introduction de carburant constitués ici par un injecteur d'essence 31 sont réglés de telle manière que l'injection soit coupée bien avant la fin de la phase d'aspiration de l'air de combustion. L'anneau d'étanchéité 29 logé dans la culasse refroidie 32 du moteur et traversé par les gaz d'admission frais n'est pas soumis ni à des températures élevées, ni à des différences de pression importantes (les surpressions et dépressions sont inférieures à 1 bar) et en conséquence, il peut être réalisé en une matière plastique de bonne qualité frottante telle que le Téflon.Figure 4 shows, on a larger scale, a solution to reduce fuel and oil losses. Elements identical to those in FIGS. 1 to 3c are given the same reference numbers. In this embodiment, oil scraper means are arranged around the air intake orifice on the plug 1. The scraper means are constituted by an intake sealing ring 29 permanently applied to the surface 8 of the plug 1 by a spring 30. According to another arrangement of this embodiment, the fuel introduction means constituted here by a petrol injector 31 are adjusted so that the injection is cut off well before the end of the combustion air suction phase. The sealing ring 29 housed in the cooled cylinder head 32 of the engine and through which the fresh intake gases pass is neither subjected to high temperatures nor to significant pressure differences (the overpressures and depressions are less than 1 bar) and as a result, it can be made of a good rubbing plastic material such as Teflon.

Le fonctionnement du mode de réalisation représenté à la fig. 4 est décrit-ci-après. Le boisseau 1 tourne en synchronisme avec le moteur et reçoit depuis les passages d'amenée 19 et la rainure de distribution 21 un film d'huile qui est entraîné à sa surface 8. Le film d'huile formé dans l'interface entre le boisseau et l'alésage 4 est arrêté par l'anneau d'étanchéité 29 sensiblement de même largeur que l'anneau d'étanchéité pricipal 6. L'injection du carburant par l'injecteur 31 commence dès que l'arête 28 de l'entaille 24 débouche sur le passage intérieur 33 de l'anneau d'aspiration 29 et s'arrête bien avant que l'autre arête 34 de l'entaille 24 n'atteinge le bord de droite 35 du passage 5 ménagé à l'intérieur de l'anneau 6 et ne coupe l'admission. Dès le début de l'injection du carburant, une partie de celui-ci est vaporisée dans le jet d'air aspiré tandis que l'autre s'arrête sur les parois et est entraînée vers la chambre de combustion 2 en s'évaporant progressivement. Grâce à l'arrêt de l'injection bien avant la fin de l'aspiration (tout en respectant les conditions du mélange quasi stoéchiométrique à la chambre de combustion 2), les parois ne contiennent plus qu'une faible quantité de carburant liquide au moment de la coupure de l'admission et la chambre de passage 27 est très pauvre en carburant. Le carburant liquide qui stagne à l'intérieur du passage 33 est arrêté par le frottement de l'anneau d'étanchéité 29 et ne peut ainsi être entraîné vers l'échappement jusqu'à ce que l'admission de l'air ne reprenne au cycle d'aspiration suivant et n'entraîne dans la chambre de combustion 2 ce carburant liquide qui s'est en grande partie évaporé pendant la suite du cycle moteur. Les dispositions représentées à la fig. 4 réduisent considérablement la quantité de carburant entraînée directement à l'échappement et permettent de réaliser un cycle à quattre temps fonctionnant avec un boisseau à entaille et avec une consommation raisonnable tout en bénéficiant des sections de passage nettement augmentées de la distribution par boisseau tournant.The operation of the embodiment shown in FIG. 4 is described below. The plug 1 rotates in synchronism with the motor and receives from the supply passages 19 and the distribution groove 21 an oil film which is driven on its surface 8. The oil film formed in the interface between the plug and the bore 4 is stopped by the sealing ring 29 substantially of the same width as the main sealing ring 6. The injection of fuel by the injector 31 begins as soon as the edge 28 of the notch 24 leads to the inner passage 33 of the suction ring 29 and stops well before the other edge 34 of the notch 24 reaches the right edge 35 of the passage 5 formed inside the ring 6 and does not cut off the intake. From the start of the injection of the fuel, part of it is vaporized in the jet of aspirated air while the other stops on the walls and is entrained towards the combustion chamber 2 by gradually evaporating . Thanks to the stop of the injection well before the end of the aspiration (while respecting the conditions of the almost stoichiometric mixture in the combustion chamber 2), the walls contain only a small amount of liquid fuel at the time of the intake shutdown and the flow chamber 27 is very poor in fuel. The liquid fuel which stagnates inside the passage 33 is stopped by the friction of the sealing ring 29 and cannot therefore be entrained towards the exhaust until the air intake resumes at following suction cycle and does not carry into the combustion chamber 2 this liquid fuel which has largely evaporated during the rest of the engine cycle. The arrangements shown in fig. 4 considerably reduce the amount of fuel driven directly to the exhaust and allow a four-stroke cycle operating with a notched bushel and with reasonable consumption while benefiting from significantly increased passage sections of the distribution by rotary bushel.

Un autre mode de réalisation du dispositif de contrôle de la circulation des gaz de et vers une chambre de combustion de moteur est représenté sur les figures 5 et 6 où les éléments et les organes identiques à ceux des figures précédentes portent les mêmes numéros de référence. Dans ce mode de réalisation, le boisseau 1 comporte deux passages séparés d'admission et d'échappement respectivement 36 et 37. Chacun de ces deux passages débouche successivement par rotation du boisseau 1 du côté de la chambre de combustion 2 sur l'anneau d'étanchéité 6 et, du côté opposé, surdes orifices qui sont décalés latéralement par rapport à l'anneau d'étanchéité 6. Le passage d'admission 36 débouche d'un côte de la culasse sur la conduite d'aspiration 25 entourée de son anneau d'étanchéité à l'aspiration 29.Another embodiment of the device for controlling the circulation of gases to and from an engine combustion chamber is shown in FIGS. 5 and 6 in which the elements and members identical to those of the preceding figures have the same reference numbers. In this embodiment, the plug 1 has two separate inlet and outlet passages 36 and 37 respectively. Each of these two passages successively opens by rotation of the plug 1 on the side of the combustion chamber 2 on the ring d seal 6 and, on the opposite side, on orifices which are laterally offset with respect to the seal ring 6. The intake passage 36 opens from one side of the cylinder head onto the suction pipe 25 surrounded by its suction seal ring 29.

Lorsque le boisseau 1 a tourné pour venir en position de plein d'échappement, le passage d'échappement 37 débouche sur le passage 5 à l'intérieur de l'anneau 6 et sur la conduite d'échappement 26 décalée selon l'axe du boisseau 1 par rapport à l'anneau d'étanchéité 6.When the plug 1 has turned to come into full exhaust position, the exhaust passage 37 opens onto the passage 5 inside the ring 6 and onto the exhaust pipe 26 offset along the axis of the plug 1 with respect to the sealing ring 6.

Selon le détail de la coupe de la fig. 6, on voit qu'à l'intérieur du boisseau 1, les deux passages d'admission 36 et 36a de deux chambres de combustion voisines d'un moteur (en fait de deux cylindres parallèles d'un moteur) débouchent sur un orifice commun 38 de communication avec la conduite d'admission 25 commune aux deux cylindres.According to the detail of the section of FIG. 6, it can be seen that inside the plug 1, the two intake passages 36 and 36a of two combustion chambers adjacent to an engine (in fact two parallel cylinders of an engine) lead to a common orifice 38 for communication with the intake pipe 25 common to the two cylinders.

Cette disposition qui s'applique aussi aux conduits et orifices d'échappement permet de réduire le nombre de sorties à ménager dans le boisseau 1 et la culasse 32 qui constiuent autant de zones d'affaiblissement de la résistance mécanique de ces organes fortement sollicités sur les plans mécaniques et thermiques.This arrangement, which also applies to the exhaust ducts and orifices, makes it possible to reduce the number of outlets to be provided in the plug 1 and the cylinder head 32 which constitute as many zones of weakening of the mechanical resistance of these highly stressed members on the mechanical and thermal plans.

En revenant à la fig. 5, on comprend qu'au cours de la rotation du moteur et du boisseau 1, la chambre de passage constituée par le conduit d'aspiration 36 ou l'ensemble des conduits d'aspiration 36-36a et 38, peut venir emprisonner de l'air relativement riche en carburant mais ne peut pas se trouver balayée par les gaz d'échappement. Le carburant contenu dans le passage d'aspiration 36 à l'intérieur de boisseau 1 reste donc en place jusqu'à ce que ce passage 36 parvienne à nouveau en position d'aspiration pour l'injecter dans la chambre de combustion 2.Returning to fig. 5, it is understood that during the rotation of the motor and the plug 1, the passage chamber formed by the suction duct 36 or all of the suction ducts 36-36a and 38, can come to trap the air relatively rich in fuel but cannot be swept away by the exhaust gases. The fuel contained in the suction passage 36 inside the valve 1 therefore remains in place until this passage 36 again reaches the suction position in order to inject it into the combustion chamber 2.

Dans le mode de réalisation représenté sur les figures 7 à 9 et où les éléments et organes identiques à ceux des figures précédentes portent les mêmes numéros de référence, on se propose de réduire considérablement la richesse en carburant en fin de période d'aspiration. A cette fin, le canal d'admission 25 représenté en coupe transversale à la fig. 8 et en coupe longitudinale à la fig. 9, comporte deux passages auxiliaires 39 et 40 d'amenée d'un mélange riche en carburant tel qu'une émulsion air-essence obtenue par injection d'essence à l'aide d'un injecteur 31 (conduit 39 à la fig. 9) ou par un carburateur à émulsion 41 (conduit 40 à la fig. 9). Lorsque l'on utilise l'injection d'essence, un seul conduit auxiliaire 39 est suffisant pour assurer le dosage correct du carburant.In the embodiment shown in Figures 7 to 9 and where the elements and bodies identical to those of the previous figures bear the same reference numbers, it is proposed to considerably reduce the fuel richness at the end of the suction period. To this end, the intake channel 25 shown in cross section in FIG. 8 and in longitudinal section in FIG. 9, comprises two auxiliary passages 39 and 40 for supplying a fuel-rich mixture such as an air-petrol emulsion obtained by injecting petrol using an injector 31 (conduit 39 in FIG. 9 ) or by an emulsion carburetor 41 (line 40 in fig. 9). When using petrol injection, a single auxiliary duct 39 is sufficient to ensure the correct metering of the fuel.

Dans ce mode de réalisation, comme on le voit sur la coupe de la fig. 8, au cours de la rotation du boisseau 1 pendant la phase d'admission du moteur à quatre temps, les conduits auxiliaires 39 et 40 sont obturés avant que la partie élargie 25a du conduit 25 ne le soit et l'air aspiré en fin d'aspiration sur la large section 25a ne contient pas de carburant et balaye la chambre de passage 27 délimitée par l'entaille 24 pour l'appauvrir de presque tout le carburant liquide déposé sur ses parois, de telle façon que lorsque cette chambre de passage est traversée par les gaz d'échappement, ceux-ci n'entraînent qu'une quantité infime de carburant ainsi inutilisé vers la conduite d'échappement 26.In this embodiment, as seen in the section of FIG. 8, during the rotation of the plug 1 during the intake phase of the four-stroke engine, the auxiliary conduits 39 and 40 are closed before the enlarged part 25a of the conduit 25 is so and the air sucked in at the end d suction on the large section 25a does not contain fuel and sweeps the passage chamber 27 delimited by the notch 24 to deplete it of almost all the liquid fuel deposited on its walls, so that when this passage chamber is through which the exhaust gases pass, these entrain only a minute quantity of fuel thus unused towards the exhaust pipe 26.

Les figures 10 et 11 illustrent le montage d'un organe d'amenée reliant la chambre de combustion 2 à l'extérieur ettel qu'une bougie d'allumage 42 utilisée lorsque le moteur thermique est un moteur à combustion interne à allumage commandé. Dans le cas d'un moteur à injection de carburant tel qu'un moteur à cycle Diesel, la bougie 42 pourra être remplacée par un injecteur de carburant ou une bougie de préchauffage. Les éléments et organes identiques à ceux des figures précédentes portent, bien entendu, les mêmes numéros de référence.Figures 10 and 11 illustrate the mounting of a supply member connecting the combustion chamber 2 to the outside such as a spark plug 42 used when the heat engine is an internal combustion engine with controlled ignition. In the case of a fuel injection engine such as a diesel cycle engine, the spark plug 42 may be replaced by a fuel injector or a glow plug. Elements and bodies identical to those of the preceding figures, of course, have the same reference numbers.

Si l'on se reporte à la fig. 10, on voit que la bougie 42 est vissée dans un filetage 43 ménagé à travers une zone de paroi mince 44 de la culasse 32 du moteur, de telle façon que ses électrodes 45 (reliée à la masse) et 46 fassent légèrement saillie à l'intérieur de la chambre de combustion 2. Lorsque l'on utilise un moteur à taux de compression élevé, l'essentiel de la chambre de combustion au voisinage du point mort haut du piston (non représenté), est constitué par le passage 5 de relativement grande dimension ménagé dans l'anneau d'étanchéité 6. Lorsque la bougie 42 est placée dans la position représentée à la fig. 10, l'allumage du mélange carburé s'effectue relativement mal car il ne démarre pas en une position centrale par rapport au principal volume de la chambre de combustion au point mort haut.If we refer to fig. 10, it can be seen that the spark plug 42 is screwed into a thread 43 formed through a thin wall area 44 of the cylinder head 32 of the engine, so that its electrodes 45 (connected to ground) and 46 protrude slightly from the interior of the combustion chamber 2. When using an engine with a high compression ratio, most of the combustion chamber in the vicinity of the top dead center of the piston (not shown) is constituted by the passage 5 of relatively large dimension formed in the sealing ring 6. When the spark plug 42 is placed in the position shown in FIG. 10, the fuel mixture is ignited relatively poorly because it does not start in a central position relative to the main volume of the combustion chamber at top dead center.

La fig. 11 illustre en coupe une disposition de la bougie d'allumage 42 (ou le cas échéant d'un injecteur de carburant ou d'une bougie de chauffage) qui remédie aux inconvénients de la solution de montage représentée à la fig. 10. L'anneau d'étanchéité 6 comporte entre deux passages d'amenée 19 un filetage 43 de réception de la partie d'extrémité ou culot 47 de la bougie 42 qui, en position de montage étanche à travers ce filetage traversant la section transversale de l'anneau 6, vient faire saillie par ses électrodes 45 et 46 à l'intérieur du passage 5 au voisinage de la paroi mais sensiblement au centre de la chambre de combustion principale constituée par ce passage 5.Fig. 11 illustrates in section an arrangement of the spark plug 42 (or where appropriate of a fuel injector or of a heating plug) which overcomes the drawbacks of the mounting solution shown in FIG. 10. The sealing ring 6 comprises between two supply passages 19 a thread 43 for receiving the end portion or base 47 of the spark plug 42 which, in the sealed mounting position through this thread crossing the cross section of the ring 6, projects by its electrodes 45 and 46 inside the passage 5 in the vicinity of the wall but substantially at the center of the main combustion chamber formed by this passage 5.

La tige de bougie 48 qui constitue la partie adjacente au culot 47 traverse avec jeu un passage relativement étroit 49 ménagé à travers la paroi de la culasse 32. Le passage 49 est relié à l'extérieur par un alésage 50 de plus grand diamètre formant une chambre annulaire 51 dans laquelle débouche la conduite de sortie 16. Afin d'obturer la chambre annulaire 51, un joint annulaire élastique 53 est interposé entre la paroi de l'alésage 50 et l'isolant cylindrique 52 de la borne de sortie 54 de la bougie 42.The spark plug rod 48 which constitutes the part adjacent to the base 47 crosses with play a relatively narrow passage 49 formed through the wall of the cylinder head 32. The passage 49 is connected to the outside by a bore 50 of larger diameter forming a annular chamber 51 into which the outlet pipe 16 opens. In order to close off the annular chamber 51, an elastic annular seal 53 is interposed between the wall of the bore 50 and the cylindrical insulator 52 of the outlet terminal 54 of the candle 42.

Lorsque le moteur est en fonctionnement, un débit d'huile important et, de préférence réfrigéré préalablement, est amené par la conduite 13 et vient mettre en pression la chambre annulaire de distribution 14 pour faire s'écouler, via les passages d'amenée 19, un faible débit d'huile de lubrification dans l'interface e entre le boisseau rotatif 1 est la surface d'étanchéité 22 de l'anneau 6. Dans le même temps, un débit d'huile plus important s'écoule de la chambre 14 à la chambre 51 via le passage étroit 49. Ce débit d'huile, qui est ensuite évacué à la bâche, refroidit l'anneau 6 et la bougie 42 en agissant de façon très efficace au voisinage de la partie la plus chaude constituée par le culot 47 et les électrodes. La position de l'anneau 6, par rapport au boisseau rotatif 1, est susceptible de varier en service par suite de la dilatation de l'anneau 6, des efforts de pression variables axiaux et radiaux sur cet anneau 6 et surtout de l'usure progressive de la surface d'étanchéité 22 de cet anneau en contact frottant avec la surface 8 du rotor 1, cette usure faisant varier lejeu i. Les déplacements instantanés (à chaque explosion) et progressifs de l'anneau 6 ne perturbent pas l'étanchéité de la chambre 51 et la position de la bougie dans la culasse 32 grâce, d'une part au jeu ménagé dans le passage 49 et évitant tout contact entre la culasse 32 et la tige de bougie 48 et, d'autre part, à l'élasticité du joint annulaire 53 réalisé de préférence en un matériau élastomère. On notera que si l'on applique le mode de réalisation de la fig. 11 à un moteur Diésel, l'injecteur de carburant pourra avantageusement être rofroidi tandis que la bougie de préchauffage ne doit pas l'être ou doit l'être le moins possible, ce qui est réalisable en la plaçant dans une enveloppe isolante.When the engine is running, a large flow of oil, preferably refrigerated beforehand, is brought in through line 13 and pressurizes the annular distribution chamber 14 to make it flow, via the inlet passages 19 , a low flow of lubricating oil in the interface e between the rotary plug 1 is the sealing surface 22 of the ring 6. At the same time, a greater flow of oil flows from the chamber 14 to the chamber 51 via the narrow passage 49. This oil flow, which is then evacuated to the tarpaulin, cools the ring 6 and the spark plug 42 by acting very effectively in the vicinity of the hottest part constituted by the base 47 and the electrodes. The position of the ring 6, relative to the rotary plug 1, is likely to vary in service as a result of the expansion of the ring 6, variable axial and radial pressure forces on this ring 6 and especially wear progressive sealing surface 22 of this ring in rubbing contact with the surface 8 of the rotor 1, this wear varying lejeu i. The instantaneous (at each explosion) and progressive movements of the ring 6 do not disturb the sealing of the chamber 51 and the position of the spark plug in the cylinder head 32 thanks, on the one hand, to the play in the passage 49 and avoiding any contact between the cylinder head 32 and the spark plug rod 48 and, on the other hand, the elasticity of the annular seal 53 preferably produced in one elastomeric material. Note that if we apply the embodiment of FIG. 11 to a diesel engine, the fuel injector could advantageously be cooled while the glow plug should not be or should be as little as possible, which is achievable by placing it in an insulating envelope.

Le système de montage d'organe d'amenée représenté à la fig. 11 réalise un découplage mécanique et vibratoire entre, d'une part l'anneau d'étanchéité 6 qui délimite l'essentiel de la chambre de combustion au point mort haut du piston et, d'autre part, la culasse 32. Grâce aux propriétés d'amortissement de l'élastomère du joint 53 et des joints annulaires 17 et 18, non seulement les vibrations éventuelles de l'anneau 6 ne peuvent pas se transmettre à la culasse et réciproquement mais, en plus, ces vibrations sont amorties à leur fréquence critique par la masse importante d'élastomère du joint 53.The mounting device assembly system shown in FIG. 11 carries out a mechanical and vibratory decoupling between, on the one hand the sealing ring 6 which delimits most of the combustion chamber at the top dead center of the piston and, on the other hand, the cylinder head 32. Thanks to the properties damping the elastomer of the seal 53 and the annular seals 17 and 18, not only the possible vibrations of the ring 6 can not be transmitted to the cylinder head and vice versa but, in addition, these vibrations are damped at their frequency critical by the large mass of elastomer of the joint 53.

Pour des raisons de simplification, on peut bien entendu, monter la bougie 42 sur le filetage 43 de l'anneau 6 hors du circuit de fluide réfrigérant passant par la chambre annulaire 14. Il suffit, pour cela, que la chambre 14 soit, par exemple, placée à proximité de l'extrémité supérieure (sur le dessin) de l'anneau 6 et au voisinage de l'interface e, le culot de bougie 47 venant se placer soit au voisinage du milieu de la hauteur de l'anneau 6, soit plus à proximité de la chambre de combustion 2.For reasons of simplification, it is of course possible to mount the spark plug 42 on the thread 43 of the ring 6 outside the refrigerant circuit passing through the annular chamber 14. For this, it suffices that the chamber 14 is, by example, placed near the upper end (in the drawing) of the ring 6 and in the vicinity of the interface e, the spark plug base 47 being placed either in the vicinity of the middle of the height of the ring 6 , which is closer to combustion chamber 2.

Claims (13)

1. Device for controlling the flow of the gas issuing from and flowing into the combustion chamber (2) of an internal combustion engine, constituted by a rotative valve cock or rotor (1) comprising at least one inner channel (3) or a lateral cut (24) defining transverse exhaust or inlet flow passages, respectively, a passage (5) directly connected to the combustion chamber (2), said valve cock (1) being enclosed in a transverse bore (4) into which opens the orifice of said passage formed in a sealing ring (6) which is placed in a bore (7) wherein it slides, said sealing ring (6) being applied onto the rotor (1) by a continuous contact surface (22) around the orifice of said passage (5) under the effect of the pressure prevailing within said combustion chamber (2) and surrounded by one or more sealing elements (11) such as sealing segments, while being provided with injection means (19, 23) for injecting oil onto said valve cock (1), characterized in that said sealing ring (6) is crossed through, at least at its periphery, by a pressure oil circuit (13, 14, 16) directed toward the oil collector and adapted to cool said ring (6), and in that said injection means (19, 32) which are connected to said oil circuit (13, 14, 16) cross axially at least a portion of the annular section of said ring (6) and open into an uninterrupted annular distributing groove (21) provided within the continuous contact surface (22) defined on a strip of small width along the general intersecting line of two cylinders, while opening at the interface (e) existing between said contact surface (22) and the outer surface (8) of said rotor (1).
2. Device according to claim 1, characterized in that said fluid injection means are constituted, on the one hand, by an annular oil inlet and circulating chamber (14) delimited between the periphery of the sealing ring (6) and its bore (7) and limited axially at each end by a seal (17, 18) interposed between the outer surface of the sealing ring and the bore (7) and, on the other hand, by at least one inlet passage (19) having an outlet orifice that opens at said interface (e) between the continuous sealing surface (22) and the outer surface (8) of said valve cock (1), and in that at least one flame sealing segment (11) is interposed between, on the one hand, said sealing ring (6) and its bore (7) and, on the other hand, said seal (17) located on the side of the combustion chamber (2).
3. Device according to claim 2, characterized in that the annular inlet chamber (14) is crossed through by a high rate pressure oil flow directed through an outlet conduit (16) toward another organ to be lubricated or toward the oil outlet.
4. Device according to any one of claims 2 and 3, characterized in that an end portion (45, 46, 47) of at least one organ for feeding one of the combustion elements, such as a sparking-plug (42) for a motor with controlled ignition, or an injector and/or a heating plug for a Diesel engine tightly extends through the cross-section of the sealing ring (6) and opens into the passage (5) which is connected to the combustion chamber, and in that the portion (48) adjacent to said end portion is mounted with an annular clearance in an inlet passage (49) directing said combustion element outwardly, said inlet passage (49) being connected to the annular fluid inlet chamber (14).
5. Device according to claim 4, characterized in that the passage (49) determining said annular clearance is crossed through by a flow of the fluid introduced into said annular fluid inlet chamber (14).
6. Device according to claim 5, characterized in that said passage (49) determining said annular clearance extends outwardly in the form of an enlar- gened annular chamber (52) which is closed by an elastic annular seal (53) interposed between the inlet organ (42) and the inner wall (50) of said chamber (51) and delimiting a cooling chamber (14, 19, 51) through which passes said fluid flow.
7. Device according to any one of claims 1 to 6, applied to a combustion motor, wherein the rotor (1) is used at the same time for controlling the motor exhaust and the inlet of the fuel-plus-air mixture into the combustion chamber, characterized in that means for scraping the fluid lubricant injected at the interface (e) are arranged about the inlet orifice connecting the rotor (1) to the combustion air and fuel mixture inlet of the motor, said scraping means being constituted by an inlet sealing ring (29) provided at the periphery of said inlet orifice and continuously bearing on the outer surface (8) of said rotor (1), said scraping means being adapted to isolate the inside of the inlet orifice with respect to the interface between said valve cock (1) and its bore, so as to limit the amount of oil carried along by the liquid fuel at the surface (8) of the rotating valve cock (1).
8. Device according to claim 7, characterized in that the sealing ring (29) is made, on the one hand, of a soft material having satisfactory friction properties with respect to the surface of said valve cock, such as plastic material, and is, on the other hand, continuously pushed onto the surface of said valve cock under the effect of the substantially constant pressure of a spring (30).
9. Device according to any one of claims 1 to 8, characterized in that said valve cock (1) comprises two separate inlet and exhaust passages (36, 37), respectively, which are adapted to open successively, both of them, through the rotation of the valve cock (1), on said sealing ring (6), on the side of the combustion chamber (2), and, on the side opposite to the combustion chamber (2), into outlet orifices each one of which is offset along the axis of the valve cock (2) with respect to said sealing ring (6), so as to decrease the amount of fuel carried off at the surface of the valve cock, as well as the amount of fuel carried off at the inlet into said inlet passage (27) provided within said valve cock.
10. Device according to claim 9, characterized in that said separate inlet or exhaust passages (36, 37) for two adjacent combustion chambers are provided in said valve cock and open into an orifice (38) communicating with the inlet or the exhaust that is common to said two adjacent combustion chambers, so as to reduce the number of orifices required on the outer surface of said valve cock.
11. Device according to any one of claims 1 to 10, applied to a four-stroke combustion motor, characterized in that the inlet circuit of the combustion chamber (2) comprises means for cutting off the fuel in the air aspired into the combustion chamber prior to the termination the inlet process.
12. Device according to claim 11, characterized in that when the fuel is introduced by injection into the inlet air, said cutting-off means are constituted by completely cutting off the fuel injection well prior to the termination of the aspiration phase.
13. Device according to claim 11 or 12, characterized in that the cutting-off means are constituted by at least one auxiliary passage (39, 40) for air with a high fuel content, said passage being provided in the valve cock (1) and the head (32) of the combustion chamber and opening at the interface between the rotor (1) and its bore (4) into an orifice which is sealed by the rotation of the rotor (1 ) prior to the sealing of the main inlet opening(s) (25).
EP19850400107 1984-02-03 1985-01-23 Device for controlling the opening and closing of the combustion chamber of an internal-combustion engine Expired EP0152321B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT85400107T ATE30456T1 (en) 1984-02-03 1985-01-23 SYSTEM FOR CONTROL OF THE OPENING AND CLOSING OF THE COMBUSTION CHAMBER OF AN ENGINE.

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR8410675A FR2549490A1 (en) 1983-07-23 1984-02-03 PROCESS FOR THE MANUFACTURE OF A LOW ALLOY STEEL FORGED PART
FR8410675 1984-02-03
FR8500637A FR2576060B2 (en) 1985-01-17 1985-01-17 DEVICE FOR CONTROLLING THE GAS CIRCULATION FROM AND / OR TO A COMBUSTION CHAMBER OF AN INTERNAL COMBUSTION ENGINE
FR8500637 1985-01-17

Publications (2)

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EP0152321A1 EP0152321A1 (en) 1985-08-21
EP0152321B1 true EP0152321B1 (en) 1987-10-28

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EP19850400107 Expired EP0152321B1 (en) 1984-02-03 1985-01-23 Device for controlling the opening and closing of the combustion chamber of an internal-combustion engine

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JP (1) JPS60198315A (en)
BE (1) BE901637A (en)
DE (1) DE3560844D1 (en)

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Publication number Priority date Publication date Assignee Title
FR2643417B1 (en) * 1989-02-17 1991-03-29 Elf France VALVE ASSEMBLY FOR EXPLOSION ENGINES
GB9000306D0 (en) * 1990-01-06 1990-03-07 Bullivant Nicholas T Rotary valve
ES2249068B1 (en) * 2002-06-10 2007-06-01 Antonio Ferreres Lopez ROTARY DISTRIBUTION VALVE.
DE102005000034A1 (en) * 2005-04-15 2006-10-19 Ford Global Technologies, LLC, Dearborn Rotary slide valve for opening and/or closing of liquid and/or gas conducting connection to combustion chamber, has sealing unit arranged with sealing lip such that lip in closed valve position is brought into position resting against body
US11242933B2 (en) * 2019-06-03 2022-02-08 Fisher Controls International Llc Floating valve seat for a rotary control valve for use in severe service applications

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Publication number Priority date Publication date Assignee Title
FR628533A (en) * 1927-02-04 1927-10-25 Porter Engine Dev Inc Improvements to internal combustion engines
FR747013A (en) * 1932-08-02 1933-06-09 Distribution by rotary slide valve for internal combustion engines
DE902918C (en) * 1942-11-12 1954-01-28 Charlotte Heylandt Geb Wachter Sealing of the movable cylinder base in cylindrical rotary valves
US4114639A (en) * 1973-09-07 1978-09-19 Cross Manufacturing Company (1938) Ltd. Lubricated rotary valve with concentric sealing rings
EP0100713B1 (en) * 1982-07-27 1986-11-12 Guy Negre Sealing element for a gas-cycle control device for a combustion chamber

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BE901637A (en) 1985-08-01
JPH0457845B2 (en) 1992-09-14
JPS60198315A (en) 1985-10-07
DE3560844D1 (en) 1987-12-03
EP0152321A1 (en) 1985-08-21

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