WO1993011343A1 - Moteur birotatif - Google Patents

Moteur birotatif Download PDF

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Publication number
WO1993011343A1
WO1993011343A1 PCT/AU1992/000635 AU9200635W WO9311343A1 WO 1993011343 A1 WO1993011343 A1 WO 1993011343A1 AU 9200635 W AU9200635 W AU 9200635W WO 9311343 A1 WO9311343 A1 WO 9311343A1
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WO
WIPO (PCT)
Prior art keywords
cylinder
transfer
exhaust
engine
motor
Prior art date
Application number
PCT/AU1992/000635
Other languages
English (en)
Inventor
John Peter Gahan
Original Assignee
John Peter Gahan
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by John Peter Gahan filed Critical John Peter Gahan
Publication of WO1993011343A1 publication Critical patent/WO1993011343A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B13/00—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion
    • F01B13/04—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder
    • F01B13/06—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement
    • F01B13/068—Reciprocating-piston machines or engines with rotating cylinders in order to obtain the reciprocating-piston motion with more than one cylinder in star arrangement the connection of the pistons with an actuated or actuating element being at the inner ends of the cylinders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
    • F02B57/04—Control of cylinder-charge admission or exhaust

Definitions

  • This invention relates to motors of the rotary type including a housing, a cylinder block supported to move within the housing containing a plurality of cylinders varying in volume, in sequence, in response to the relative movement between the piston members and the housing.
  • the motor may be in the form of a heat engine operating on internal or external combustion or a hydraulic or pneumatic motor.
  • motor of the rotary type including a cylinder block rotatab mounted within a cylinder housing, a shaft journalled for rotation in said housing, piston members rotatably supporte on the shaft for rotary motion in the cylinder housing as t shaft and the cylinder block rotate and a plurality of cylinders arranged to define chambers between the housing a the piston members that vary in volume, in sequence, in response to the relative movement between the piston member and the housing.
  • the housing is formed by a peripheral wall and opposed end walls, with each cylinder supported on the central carrier for rotational movement.
  • the central carrier being supported on two bearings, one on each of the respective end walls.
  • the piston may have a rod portion extending from the piston base, through a gas/oil seal, to the crankshaft bearing.
  • the crankshaft is connected to the central carrier by epicyclic gears giving a 2:1 reduction.
  • One complete revolution of the crankshaft causes 180° rotation of the cylinder block.
  • the bearing pads may be formed as an integral part of the piston rod, with or without a surface coating of bearin material, or may be an insert attached thereto.
  • the insert may be made entirely of suitable bearing material, such as phosphor bronze, or may be made of any other material of suitable mechanical and thermal properties with a layer of suitable bearing material on the bearing face.
  • the insert is attached to the rod, since the latter experiences less thermal distortion during engine operation and hence provides a more constant reference for the insert.
  • the present invention is particularly applicable to internal combustion engines wherein the cylinders are supported in the housing for rotation in a direction normal to the plane of the crankshaft as is, and the pistons are connected to the crankshaft so that each piston may move relative thereto in a direction normal to the direction of reciprocation of the eccentric bearing.
  • the piston member provided with seals around its circular edge, fitting snugl into the rotating cylinder, allowing for running clearance.
  • FIG. 1 is a perspective, part section view of a two stroke, rotary engine according to a first embodiment of the invention
  • Fig. 2 is a vertical section view through the engine of Fig. 1
  • Fig. 3 is a horizontal section view through the engine of Fig. 1
  • Fig. 4 is an end section view along lines C-C through the engine of Fig. 1
  • Fig. 5 is an end section view along line D-D of the engine of Fig. 1
  • Fig. 6 is a vertical section through the engine o a second embodiment of the invention
  • Fig. 7 is a horizontal section through the engine of the second embodiment
  • Fig. 8 is a cross-sectional view through the engine of the second embodiment.
  • Fig. 9 is a further cross-section view through th engine of a second embodiment.
  • Fig. 10 is a vertical section through the cylinders of the engine of the second embodiment,
  • Fig. 11 is a horizontal section through the cylinders of the engine of the second embodiment
  • Fig. 12 is a plan view of the inlet cylinders sealing ring of the engine of the second embodiment with selected cross sectional views therethrough
  • Fig. 13 is a plan view of the inlet casing-side sealing ring and exhaust sealing plate and support pads together with selected cross- sectional views therethrough
  • Fig. 14 is a side section view through the exhaust manifold in vertical and horizontal section.
  • Fig. 15 is a side section view through an engine cylinder and port of the second embodiment illustrating a first position of operation
  • Fig. 16 is a side sectional view as for Fig. 15 an showing a second position of operation
  • Fig. 17 is a side section view as in Fig.
  • Fig. 18 is a side section view as for Fig. 15 and illustrating a fourth position of operation
  • Fig. 19 is a side section view as in Fig. 15 and showing a fifth position of operation of the engine of the second embodiment
  • Fig. 20 is a side section view comparing the pisto rings of the engine of the second embodiment to conventional piston rings
  • Fig. 21 is a plan view of sealing arrangements of the engine of the second embodiment including the cylinder seal ring and the end plate seal ring
  • Fig. 22 is a side section view through the casing of the engine of the second embodiment illustrating the relationshipe between the air and transfer tracks according to the second embodiment
  • Fig. 23 is a plan view of an exhaust sealing ring according to the second embodiment of the invention
  • Fig. 24 is a side section view of a piston and cylinder housing according to a second embodiment of the invention.
  • Fig. 25 is an in section view of an engine according to a third embodiment of the invention
  • Fig. 26 is an alternative view of the end section of Fig. 24,
  • Fig. 27 is a vertical section view through the engine according to a third embodiment.
  • Fig. 28 is a horizontal section through the engine according to a third embodiment
  • Fig. 29 is a plan view of a cylinder side sealing ring according to a third embodiment of the invention.
  • Fig. 30 is a plan view of a case side sealing rin according to a third embodiment of the invention
  • Fig. 31 is a perspective view of a half portion o the crank case of the engine according to third embodiment
  • Fig. 32 is a vertical section view of an engine according to a fourth embodiment of the invention
  • Fig. 33 is a horizontal section of the engine according to a fourth embodiment of the invention, Fig.
  • an engine 110 according to the first embodiment comprises an engine casing 111 within which rotates a crank shaft 113 and a central carrier or cylinder block 114.
  • Pistons 115 reciprocate within cylinders 116 within th central carrier/cylinder block 114 thereby causing relative rotation of both the cylinder block 114 and of crank shaft 113 with respect to engine casing 111.
  • the crank shaft 113 is geared to casing 111 by epicyciic gears 117 of ratio 2:1.
  • epicyciic gears 117 of ratio 2:1.
  • the epicyclic gears 117 give a ratio of 2:1 between the central carrier 114 of the cylinders and the crank shaft.
  • the central carrier 114 is mounted on bearings to maintain the running clearance betwee the cylinders and the casing.
  • the central carrier 114 is in two parts 114A, 114B, bolted together to clamp the split seals 118 around the connecting rods 119 and allowing the piston 115 and connecting rod 119 to be one piece for greate strength.
  • induction is accomplished by the under side 122 of the piston 115 drawing gas through the inlet port 120 when it is in line with the inlet tract 121.
  • the port is closed by the seal betwee the inlet and transfer tracts pressing against the cylinder block by spring pressure.
  • the gas is compressed and as the piston reaches T.D.C., or thereabouts, • the spark plug 125, a the appropriate position in the engine casing 111, is timed to ignite the mixture.
  • the power stroke continues until the exhaust port 126 is uncovered by the rotating cylinder at a point just before B.D.C. This permits a much longer use of the available energy than is common in traditional engines.
  • the uncovering of the exhaust port 126 allows the gas to escape instantaneously under its own pressure, lifting th exhaust valve 127 automatically off its seals.
  • the other exhaust valve remains closed to prevent the gas exhausting directly to atmosphere.
  • the rotary valve open 124 after the exhaust port has closed, allowing the charge t enter the cylinder and avoiding any possibility of fresh charge escaping down the exhaust pipe 128.
  • the rotary valve 124 closes when the cylinder has passed by and the gas is then compressed by the piston in preparation for the next power stroke.
  • the engine is described with carburettor and spark-plu ignition but fuel injection and /or diesel principles may be used.
  • the engine may be air and/or liquid cooled.
  • the port timing is controlled by the side of the cylinder casing, not the peripheral passing of the cylinder nor the movement of the piston itself.
  • the exhaust valves are paired because the cylinders are offset, with one valve for each pair of opposed cylinders.
  • the valves can be pressure released (as shown) or timed mechanically as in conventional engines. The reason for a valve at all is because the exhaust gas could escape from one cylinder and then exhaust directly to atmosphere through the other open port, instead of travelling down the exhaus pipe to the silencer.
  • a second embodiment of the invention will now be described with reference to Figs. 6 to 21.
  • Figs. 6 to 11 illustrate various sectional views of an engine according to a second embodiment of the invention.
  • the major difference as compared with the first embodiment is that the sealing rings are constructed differently (refer detailed description in respect of Figs. 20 and 21 later in this specification) .
  • the ignition strip is chamfered on its leading edge s that when the cylinders expand, the top of the spark plug pushes the high tension copper strip, against spring pressure, into the cavity in the housing without jamming.
  • One high tension lead for each-strip is required because.of the staggered cylinders, which is why they are independently sprung.
  • the length of the strip allows the required ignitio advance without the need for separate pick ups, etc.
  • Figs. 6 to 11 the sealing rings have been drawn superimposed upon each other.
  • crank shaft 1 having a crank pi 2 and journalled for rotation in main bearing 3.
  • a planetar gear arrangement comprising crank shaft gear 4, idler gear 5 and crank case gear 6 place the crank case 7 in rotary engagement with crank shaft 1.
  • Piston and connecting rod 8 act to cause rotary motion of crank shaft 1 via crank pin 2.
  • Piston and connecting rod 8 are mounted for sliding, reciprocating motion within cylinder 9.
  • Piston ring(s) 13 act to seal piston and connecting rod 8 against the inside surfaces of cylinder 9. Additional sealing mechanisms, as illustrated, include connecting rod seal 14, crank case seal 15, inlet port seal 16, transfer port seal 17, inlet tract seal 18, transfer tract seal 19, inlet casing-side sealing ring spacing rubber 20, inlet casing-side sealing ring 21, inlet cylinder-side sealing ri 22, exhaust sealing plate 23, exhaust sealing ring stabilising pad 24, exhaust sealing ring 25.
  • the porting arrangement to pass combustion gases into and out of cylinder 9 includes inlet cylinder-side sealing ring inlet orifice 26, inlet cylinder-side sealing ring transfer orifice 27, inlet casing-side sealing ring inlet orifice 28, inlet casing-side sealing ring inner transfer orifice 29, inlet casing-side sealing ring outer transfer orifice 30 inlet casing-side sealing ring air orifice 31, exhaust sealing ring orifice 32 and exhaust sealing plate orifice 33.
  • Exhaust gases pass through exhaust manifold 35 sealed by exhaust manifold sealing ring 34 and pass out via exhaust pipe 39.
  • the engine is modular in nature being defined by parallel end casings 48 spaced at both ends from each other by end casing spacer 47. These components are held together by engine bolt 49 as illustrated.
  • Crank shaft 1 protrudes rotatably through both opposed faces of the end casings 48 whereby the engine can be used as a single module as illustrated in Fig. 6 or can form a single module of an interconnected series of modules connected together via cran shaft 1.
  • Fuel and air communicate within the engine via inlet tract 36, transfer tract 37 and air tract 38. Fuel is mixed with air via carburettor 50.
  • Compressed fuel and air mixture is ignited within cylinder 9 by means of spark plug 40 which is in rotary, . conductive communication with high tension lead 41 via high tension copper strip 42.
  • a pressure spring 44 maintains electrical contact between the top of spark plug 40 and the high tension copper strip 42.
  • the copper strip 42 is insulated from the high tension housing 46 by means of insulating pad 43 and the assembly is retained by retaining plate 45 as best seen in Fig. 8.
  • inlet cylinder-side sealing ring dowel location hole 51 and inlet casing-side sealing ring dowel locating hole 52 which receive locating dowels therewithin.
  • a single engine module comprises, ideally, two pairs of cylinders 9 located on diametrically opposed sides of crank shaft 1 and coacting so as to urge rotation of crank shaft 1.
  • Section A in Fig. 12 is the cross-section of the inlet cylinder sealing ring, taken through the inlet and transfer orifice, showing the grooves for the rubber "0" rings for gas sealing against the cylinder.
  • the cylinder has similar grooves machined around the ports to accept these "0" rings.
  • Section B in Fig. 12. is the cross-section through one of the eight dowel locating holes. The dowels are pressed into the cylinder at the appropriate points and the inlet cylinder sealing ring sits on them, allowing it to float in and out, but not to rotate. When assembled, the cylinder an casing inlet sealing rings are kept pressed together because the rubber "0" rings are under compression. That is to say that the assembled clearance between the cylinder and case i less than the uncompressed thickness of the sealing rings an rubber "0" rings.
  • the two inlet sealing rings, both casing and cylinder, are Teflon coated on their mating surfaces.
  • Section C is Fig. 12 is the cross-section of the exhaust cylinder sealing ring taken through the exhaust outlet.
  • the exhaust manifold, bolted to the cylinders, has the same function as the dowels on the inlet ring.
  • Fig. 13 illustrates the respective positions of inlet casing side sealing ring and the exhaust sealing plate and support pads.
  • Section D in Fig. 13 is the cross-section of the exhaust sealing plate taken through the exhaust outlet.
  • the plate is ceramic coated on its rubbing surface, as are the support pads. They are sunk into the engine case to ensure that they remain in the correct position.
  • ceramic coated steel pad 24 is adapted to stabilise the exhaust cylinder side sealing ring.
  • Section E in Fig. 13 is a cross-section of the inlet casing-side ring taken through the inlet and transfer tracks showing the grooves for the rubber sealing rings.
  • Section F in Fig. 13 is a cross-section of the inlet casing side sealing ring taken through the inlet track and one of the three dowel locating holes.
  • Section G in Fig. 13 is a hole for the air inlet so it does not need a rubber seal. It is not one of the dowel locating holes.
  • the exhaust manifold is on the leading edge of the cylinder for coaling air so it is not on the centre line of the cylinders.
  • Fig. 14 they have been drawn sectioned in the vertical and horizontal sections. On the vertical and horizontal sections the exhaust manifold has been drawn one square further out than it actually is for explanatory purposes - so that the exhaust sealing ring is clear of the inlet sealing rings.
  • Fig. 14 illustrates their relationship as it really is.
  • the exhaust manifold is "T" shaped so that there is an exhaust pipe on each side (as also there are two carburettors) .
  • the exhaust manifold By making the exhaust manifold "L” shaped, it is possible to have the carburettors and the exhaust on the same side for fitting into a car for example with the clutch on the other side. Or, as above with one carburettor and one exhaust on opposite sides.
  • Fig. 15 shows the piston on the power stroke.
  • the exhaust pipe 39 is already open to the exhaust manifold 35 b the exhaust sealing plate orifice 33 lining up with the exhaust sealing ring orifice 32. This is done before the piston 8 uncovers the exhaust part 12 so that the minimum restriction is offered to the exhausting gas.
  • the exhaust sealing ring 25 has a smaller diameter outlet 32 than the diameter of the exhaust manifold 35 to ensure that the highe gas pressure on the cylinder side forces the exhaust sealing ring 25 firmly against the ceramic coated exhaust sealing plate 23 to seal it effectively.
  • the exhaust manifold sealing rings 34 act in the same way as piston rings to ensure an effective seal between the exhaust sealing ring 25 and the exhaust manifold.
  • the under side of the piston is compressing the fresh charge into the transfer track 37.
  • Fig. 16 shows the piston 8 approaching B.D.C. after th high pressure gas in the cylinder 9 has been released down the exhaust pipe 39.
  • the transfer port 11 had been uncovered by the piston 8 after the exhaust port 12 had opened, the transfer of fresh gas was stopped by the inlet casing-side sealing ring 21.
  • the transfer port 11 is opened directly to atmosphere by the inlet casing-side sealing ring air orifice 31 lining up with inlet cylinder- side sealing ring transfer orifice 27, allowing fresh cold air to pass across the top of the piston 8 having been induced into the cylinder 9 by the low pressure created by the exhausting gas.
  • Fig. 17 shows the piston 8 at B.D.C. where the exhaust sealing ring orifice 32 the inlet cylinder-side sealing ring transfer orifice 27 and the inlet cylinder-side sealing ring inlet orifice 26 are all closed.
  • Fig. 18 shows the piston 8 commencing the compression stroke.
  • the transfer port 11 is open to the transfer tract 37 by the inlet cylinder-side sealing ring transfer orifice 27 lining up with the inlet casing-side sealing ring outer transfer orifice 30.
  • the transferred gas cannot escape to pollute the exhaust because the exhaust sealing ring orifice 32 is closed by the ceramic coated exhaust sealing plate 23.
  • the underside of the piston 8 commences the induction stroke.
  • Fig. 19 shows the piston 8 has closed the exhaust port 12 at which point the exhaust sealing ring 25 may be opened to atmosphere for cooling purposes.
  • the air passages in the casing are referred to as "tracts”, in the cylinder as “ports” and in the seal rings as “orifices”.
  • Fig. 20 shows the cylinder head being separate from the cylinder with conventional piston rings 13 being situated on the upper outer part of the cylinder, being covered by the skirt of the cylinder head. That is the cylinder head fits over and around the top of (or the outer end of) the cylinder. After ignition, the pressure in the cylinder forces the pistons inwards and the cylinder head outwards against the casing.
  • the cylinder head should be coated on its outer edge with heat resistant low friction material, such as silicon nitride. Lubrication of the rubbing surface can be achieved by a low pressure, total loss oil supply to the inside of the engine casing, through very small holes drilled at any number of required points.
  • Fig. 21 shows the side-port seals. It is a variation on the first embodiment in that the original sealing rings were required to rub against the moving cylinder.
  • the syste of Fig. 21 uses a separate plate 53, teflon coated, with holes 54 machined in it to line up with the original ports 5 in the cylinder and/or end plates.
  • Fig. 21 In the enlargement in Fig. 21 of the rubber ring and groove, it can be seen that the ring is only partly entered into each groove for location whilst allowing pressure on th assembly to ensure continued sealing.
  • the plate is located in its position by at least the steel dowel pins 55, sunk into the cylinder and into the sealing plate 53.
  • the pin locating hole is blind so that th steel dowel pin does not touch the rubbing/sealing surface o the plate.
  • the ring is held in position by (a) gasket sealant and (b) pressure upon assembly ensuring that the sealing ring is pressed firmly against its mating surface but not too much to actually close the gas around th rubber ring.
  • This sealing system can be used on the end plate tract as well whereby it is possible to have both plates floating and rubbing against each other.
  • Each seal ring is a full circle ensuring contact at all times.
  • a system for desmodronic valve operation can be used for actuating the exhaust valves.
  • a positive stop mechanism can be used for the gearbox if space is limited.
  • the engine of the second embodiment has been simplified somewhat as compared with that of the first embodiment.
  • the side seals, pistons and induction system are the same.
  • the engine of the second embodiment allows for separate cylinder heads and no outside casing.
  • gas will not be directed externally to the rotary valve but will enter the cylinder by a port opened towards the end of the piston stroke (similar to an ordinary two stroke engine).
  • the gas will exhaust by a similar port on the opposite side, opened before the tranfer port (as is also normal two stroke practice) .
  • a difference in the side seals is that there is also another transfer tract 58, concentric with and outside the original transfer tract 37, to direct the gas back into the cylinder instead of around the outside to the rotary valve 124.
  • Fig. 22 shows that the air port 57 is opened to atmosphere after the exhaust port 12 has opened but closes at the same time.
  • Fig. 23 illustrates a ceramic coated exhaust sealing ring 59 bolted to the cylinder block.
  • the ports line up wit the ports described with reference to Fig. 22.
  • the inlet/transfer sealing ring is similar to the exhaust ring except that it has two ports. It is pinned, not bolted and is urged against the other plate by spring pressure.
  • the sealing ring is teflon coated.
  • Fig. 24 highlights the location of the differences in connection of the exhaust tracts, transfer tracts and inlet and air tracts to the cylinder volume in respect of the second embodiment of the invention.
  • the inlet/transfer tract is the same as for the first embodiment but is now located o one side only.
  • this arrangement of the second embodiment includes the following features:- 1. Because of the heat, only one side of the engine will be used for induction and transfer. The other side will be only for exhaust. 2. Because the transferred gas enters by another cylinder port, another transfer tract is required. This is joined to the original transfer tract by a groove machined in the engine casing.
  • Figs. 24 to 28 inclusive highlight variations to the basic engine design of the second embodiment whereby an amended design according to a third embodiment results.
  • Fig. 24 is an end section view of the engine similar to that of Fig. 8 but showing a change in spark plug 40 angle relative to the housing so as to reduce the overall diameter of the engine.
  • Figs. 26 and 27 are vertical and horizontal views respectively similar to that of Figs. 10 and 11 but showing exhaust ports and manifolds more clearly.
  • Fig. 25 is an end section view similar to Fig. 24 but including four symmetrically spaces retaining grooves adapted to receive and retain springs located between the sealing rings to enhance the sealing efficiency when there is insufficient gas pressure to achieve the same effect. This modification requires additional lubrication.
  • An example of the pressure spring 62 is shown in the inset to Fig. 25. There are four springs for the exhaust and four springs for the inlet.
  • Fig. 31 illustrates one half of the engine crank case of the second embodiment adapted to incorporate two split oil seals placed back to back, the inner seal as an oil seal and the outer seal as a gas seal.
  • ancillary chamber 64 is defined in the space around the piston between the larger diameter piston base and the small diameter outer cylinder.
  • the maximum volume of the ancillary chamber 64 is ideally half the volume of the connecting rod between the piston base and the crank case when the piston is at top dead centre (TDC) . If the ancillary chamber 64 is made of larger capacity than this then the engine will be effectively super charged.
  • the piston 8 and the connecting rod can be made as one piece (refer Figs. 15 to 19 of the second embodiment). Alternatively, they can be made separately if it is designed to reduce their total weight.
  • the cylinders 9 can be made in two parts, a larger diameter component and a smaller diameter component, for ease of assembly.
  • the smaller diameter outer cylinder may have rings like piston rings inserted at its inner end whereby instead of pressing outwards as piston rings normally do they will press against the piston to form a seal for an ancillary chamber. In an alternative position a heat resistant seal can be screwed into position at a location where the outer piston rings never reach.
  • the valve timing for the third embodiment is generally as for the second embodiment except as follows.
  • the third embodiment differs in that, at low revolutions, there is time for all the compressed, transferred gas to enter the cylinder before the piston closes the transfer port. At higher revolutions some of the compressed gas may be trapped in the transfer port.
  • no residual fresh charge is exhausted when the air tract is opened.
  • the induction/transfer sealing ring because it is much wider than in the second embodiment, is made ideally in three parts.
  • The. vertical section of Fig. 27 and the horizontal section of Fig. 28 show these connecting tracts covered with a sealing plate bolted to the end plates.
  • the transfer tracts have been shortened to prevent any high pressure gas returning to the following cylinder (which is at a lower pressure) instead of going to the transfer port where it should be.
  • the length of these tracts, the port timing and the like may be altered to suit specific power requirements.
  • the nature of the design of the third embodiment makes it difficult to be run as a diesel engine but with altered porting steam energisation is possible. Similarly, fuel injection can be utilised instead of a carburetter based system.
  • the ignition timing may be controlled from the crank shaft side of the engine with two sets of contacts placed 180° part. Each contact will control one part of opposed cylinders and the timing may be varied by an automotive centrifugal advance mechanism.
  • the arrangement is such that it is possible to turn the engine by rotating the cylinders by taking the drive from the cylinder block.
  • this modification as illustrated in Figs. 32 and 33, there is insufficient room to connect the carburettors directly to the main inlet tracts so they are connected to the ancillary inlet tracts. This is allowable as both tracts are in communication with each other.
  • the primary features which differentiate the fourth embodiment from the earlier embodiments include the longer main bearing bolted to the end plate which is opened out to accept the longer main bearing as well as the lengthened crank case with an oil seal.
  • the driving gear is bolted to the crank case and held by a key way (not shown).
  • the engine oil still drains through the crank case but instead of going to the drain tract (not shown in Figs. 32 and 33) it exits into the drive case to lubricate the gears. It will drain back to the sump via an external pipe (not shown) .
  • a slot must be cut into the outer main bearing case between the bolts to allow the mating gear to mesh with the driving gear and the complete transmission must be contained in an oil tight casing.
  • the outer main bearing case has been shown somewhat off centre for ease of bolting to the existing bolt holes.
  • engine drive can be taken from the shaft e.g. for conventional car-type applications.
  • the drive can be taken from the crank case gear or the shaft for motorcycle applications.
  • Fig. 34 illustrates an arrangement for porting the exhaust gases from the engine to the external environment.
  • the arrangement can be used with- any one of the embodiments illustrated so far.
  • the exhaust sealing plate 68 may be sun into the end plate/side plate or alternatively spaced away from it and secured by bolts.
  • a short exhaust tube 69 may be attached to the plate by welding or screwing. Enough clearance should be allowed around the exhaust tube 69 to allow the free passage of cooling air. This reduces the contact area between the exhaust sealing plate and the end plate to a minimum thus reducing heat transfer and distortion.
  • the main exhaust pipe (not shown) may be clamped to the protruding exhaust tube.
  • port timing may be changed as also the tract length and positioning (with relative changes to the sealing ring orifice) in accordance with experimental data obtained in relation to parameters such as gas velocity, port shape and the length of the engine and the desired speed limit.
  • the engine By positioning the combustion chamber to the side of the cylinders, the engine can be adapted for diesel or steam operation. Use as a steam engine will require port relocation. All sealing rings would need to be ceramic coated for steam engine operation. INDUSTRIAL APPLICABILITY
  • the invention may be applied to an internal combustion engine, a heat engine operating on internal or external combustion, hydraulic or pneumatic motors and steam engines of the rotary type.

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

Abstract

Moteur rotatif (110) comprenant un bloc de culasse qui est monté rotatif dans un carter de cylindre (111). Le bloc de culasse comporte des cylindres (116) dans lequel des éléments (115) de piston sont supportés rotatifs sur un autre (113) tourillonné de manière à tourner dans le carter (111). Les éléments (115) de piston et le carter (111) définissent des chambres de travail dont le volume varie en réaction à leurs déplacements relatifs pour induire une charge pré-comprimée issue du dessous des éléments (115) de piston, par l'intermédiaire d'un orifice de transfert. Des paires décalées de cylindres opposés (116) sont associées à des soupapes d'échappement décalées de manière identique, chaque soupape étant associée à une paire.
PCT/AU1992/000635 1991-11-29 1992-11-27 Moteur birotatif WO1993011343A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AUPK9790 1991-11-29
AUPK979091 1991-11-29

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WO1993011343A1 true WO1993011343A1 (fr) 1993-06-10

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999018332A1 (fr) * 1997-10-06 1999-04-15 John Peter Gahan Moteur rotatif a deux temps
WO1999067367A1 (fr) * 1998-06-22 1999-12-29 Regents Of The University Of Minnesota ADN CODANT ACETYLE CoA CARBOXYLASE DE L'AVOINE
WO2012089621A1 (fr) * 2010-12-29 2012-07-05 Becker Otto Hermann Moteur à combustion interne pourvu de cylindres rotatifs

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GB537824A (en) * 1938-12-29 1941-07-08 Mawen Motor Corp Improvements in or relating to four-stroke cycle rotary internal combustion engines
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US3517651A (en) * 1969-03-11 1970-06-30 Graybill Ind Inc Rotary two-cycle engine
DE2166418A1 (de) * 1971-11-15 1974-01-10 Motoren Forschungs Gmbh Verbrennungskraftmotor mit wenigstens einem sich in einem stator drehenden zylinder
US3865093A (en) * 1971-11-04 1975-02-11 Rodriguez Miguel Ferragut Machine driven by rotary pistons
GB1446852A (en) * 1972-08-12 1976-08-18 Anidyne Corp Rotary machines
US4010719A (en) * 1973-05-04 1977-03-08 Lappa Cleto L Rotary internal combustion engine

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2273900A (en) * 1937-02-05 1942-02-24 Nils Gustaf Hezekiel Frenne Internal combustion engine
US2242231A (en) * 1937-02-12 1941-05-20 Cantoni Humbert Denis Jean Internal combustion engine
GB537824A (en) * 1938-12-29 1941-07-08 Mawen Motor Corp Improvements in or relating to four-stroke cycle rotary internal combustion engines
US3517651A (en) * 1969-03-11 1970-06-30 Graybill Ind Inc Rotary two-cycle engine
US3865093A (en) * 1971-11-04 1975-02-11 Rodriguez Miguel Ferragut Machine driven by rotary pistons
DE2166418A1 (de) * 1971-11-15 1974-01-10 Motoren Forschungs Gmbh Verbrennungskraftmotor mit wenigstens einem sich in einem stator drehenden zylinder
GB1446852A (en) * 1972-08-12 1976-08-18 Anidyne Corp Rotary machines
US4010719A (en) * 1973-05-04 1977-03-08 Lappa Cleto L Rotary internal combustion engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999018332A1 (fr) * 1997-10-06 1999-04-15 John Peter Gahan Moteur rotatif a deux temps
CN1113150C (zh) * 1997-10-06 2003-07-02 约翰·彼得·加恩 旋转式二冲程发动机
WO1999067367A1 (fr) * 1998-06-22 1999-12-29 Regents Of The University Of Minnesota ADN CODANT ACETYLE CoA CARBOXYLASE DE L'AVOINE
WO2012089621A1 (fr) * 2010-12-29 2012-07-05 Becker Otto Hermann Moteur à combustion interne pourvu de cylindres rotatifs

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