ENGINE SUPERCHARGER AND INLET MANIFOLD ARRANGEMENT

Abstract: A multi-cylinder two-stroke cycle engine having a plurality of cylinders (1, 2, 3) arranged in line with each cylinder having at least two inlet ports one on each of the two opposite longitudinal sides of the in-line cylinders (1, 2, 3). Air passages (67, 77) extend along said opposite sides to supply air from a supercharger (not shown) to the respective inlet ports. An air control valve (68) is operable to selectively control air supply to one or both of said air passages (67, 77) whereby optimum combustion conditions are obtained for various engine load/speed conditions. A centrifugal supercharger arrangement is also disclosed, the supercharger being coupled to the engine crankshaft and interposed between the cylinder block and the engine flywheel.

Description: -1- EdNE SUEIEffiHABGER AND INLET MAra_rTLD AREANΞEMΣ-NT This invention relates to engines to be operated with a supercharger and maybe applied to engines operating on either the two stroke or four stroke cycle. There is currently a trend towards the use of supercharged engines in vehicles, particularly in engines of automobiles, and the majority of these employ a turbo-charger, that is a centrifugal compressor driven by a turbine through which the hot exhaust gases from the engine are expanded. Although the performance of turbo-chargers is acceptable, there are problems associated with their use, including the space they occupy in the engine compartment, the heat radiated from the turbine section within the engine compartment, and the relatively high level of servicing required by turbo-chargers. Also there iε a time lag in the response of a turbo-charge to increasing power demands on the engine, particularly when increasing in low to medium speed range. However, as the customer demand increases for greater performance from small displacement engines, it is evident that an effective supercharged engine iε desirable. The object of the present invention iε to provide an engine and supercharger aεεembly which substantially reduces the above disadvantages and iε effective in operation and relatively i*simple and cost effective in manufacture. With this stated object in view, there is provided, by one aspect of the present invention a multi-cylinder internal combustion engine having a cylinder block, a crankshaft having a longitudinal axis and supported in the cylinder block for rotation about said longitudinal axis, a plurality of cylinders in εaid cylinder block arranged in one or more banks, each bank having a plurality of inline cylinderε, a piεton εupported to reciprocate in each cylinder, each piεton being coupled to the crankshaft to effect rotation of the crankshaft in responεe to reciprocation of the pistons, each cylinder in at least one cylinder bank having at least two inlet ports, one on each of the two opposite longitudinal εideε of the respective bank of cylinders, an air passage extending along at least one bank of cylinders and communicating with inlet ports on each cylinder of the cylinder bank on each of the two opposite sideε of the cylinder bank, the air passage of the or each cylinder bank being arranged to receive air from a supercharger, and air control means operable in relation to at leaεt one air paεεage receiving air from the supercharger to selectively supply or vary the rate of supply of air to the inlet portε on one or both sides of the cylinders of that cylinder bank. With another aspect of the present invention in view there iε provided a multi-cylinder internal combustion engine having a cylinder block, a crankshaft having a longitudinal axis and supported in the cylinder block for rotation about εaid longitudinal axiε, a plurality of cylinderε in εaid cylinder block arranged in one or more cylinder banks, each cylinder bank having a plurality of inline cylinders, a piεton εupported to reciprocate in each cylinder, each piεton being coupled to the crankεhaft to effect rotation of the crankshaft in responεe to reciprocation of the piεtonε, a centrifugal supercharger located adjacent one end of*the cylinder block co-axial with the crankshaft, said compressor having a stationery housing non-rotatably secured to the cylinder block and an impeller co-axially drive coupled to the crankshaft. Conveniently the supercharger iε located between the cylinder block and a flywheel mounted on the crankshaft preferably with at leaεt part of the houεing of the centrifugal εupercharger iε formed integral with the cylinder block or a component of the engine εuch aε the crankcase or oil sump, or an adaptor or mounting plate that iε attached to the cylinder block to facilitate mounting of a transmission assembly to the engine. In yet another aspect of the invention there is provided a multi-cylinder supercharged two stroke cycle internal combustion engine having a cylinder block, a crankshaft having a longitudinal axis and supported in the cylinder block for rotation about εaid longitudinal axis, a plurality of cylinders in said cylinder block arranged in an inline formation, a piston εupported to reciprocate in each cylinder, each piεton being coupled to the crankεhaft to effect rotation of the crank in response to reciprocation of the pistons, each cylinder having at least two peripherally spaced inlet ports in the wall of the cylinder cyclically opened and closed by the piston reciprocating in the cylinder, at least one inlet port of each of two adjacent cylinders being located in an opposing relation and each communicating with a portion of a single transfer paεεage interpoεed between said opposing inlet ports, whereby air from the supercharger can be supplied to said two cylinders through the respective opposing inlet ports from εaid εingle transfer paεεage, the timing of the opening and clo-εing of the opposing inlet ports by the reciprocation of the pistons in the adjacent cylinders being arranged so that only one of εaid oppoεing ports is in communication with the εingle transfer port at any one time. Preferably an air delivery port and/or an air inlet port of the compressor is* alεo formed integral with the compressor housing. Where the engine is one that operates on the two stroke cycle, and has inlet ports formed in the wall of some or all of the cylinders of the engine it is preferable that a conduit is provided in the cylinder block to communicate between the air delivery port of the compreεεor housing and at least some of the inlet ports. Where more than one inlet port is provided for each cylinder, with inlet ports on each of the two generally opposite sides of the cylinder block or bank, a single conduit may be provided along one side of the cylinders with pasεageε extending therefrom, within the cylinder block, to the inlet ports on the other εide thereof. Alternatively, reεpective conduits may be provided along each side of the cylinder bank to communicate with the inlet portε on the reεpective εideε thereof. In an engine having two bankε of cylinders arranged in a V formation, one conduit may be provided in the valley between the two banks, to provide air to portε in the cylinderε on either εide of the valley, and reεpective conduitε on the outer side of each bank to provide air to further ports on the outer side of the cylinders. Where a conduit is providing air to two or more side by εide cylinderε of a multi-cylinder engine, a εingle paεεage may communicate portε of adjacent cylinder to the conduit. Thiε arrangement will permit a reduction in the εpacing between the cylinders and improvement in the air flow into the cylinderε. Proviεion may be made to control the flow rates in the reεpective conduitε to achieve a deεired distribution of the air between the portε on the reεpective sides of the cylinder bank. The control provision may be adapted to enable the air distribution to be varied with engine load and/or εpeed, and may be part of an ECU controlled engine management system. The supercharger is preferably of the centrifugal type and iε preferably loca*ted at that end of the engine at which the crankεhaft is coupled to the transmission device that delivers the torque of the engine to the equipment to be driven. The centrifugal supercharger may be located at the flywheel end of the cylinder block and is located between the flywheel and the cylinder block, where it may be conveniently located in or at least in part incorporated into the housing normally provided to encloεe the flywheel and commonly referred to aε the bell housing. Provision may be made to effect cooling of the supercharger by providing coolant circulating passageε within the housing which communicate with the coolant system of the cylinder block. Preferably provision is made especially to cool the high presεure air delivered from the to contribute to the more efficient operation of the engine. The impeller of the εupercharger may be coupled to the crankεhaft of the engine to rotate at the same εpeed aε the crankshaft, or alternatively a suitable speed εtep-up transmission may be provided therebetween. The transmission mechanism may be of the epicyclic traction type, for example of the friction ball type epicyclic drive. The invention will be more readily understood from the following description of one form of engine having the εupercharger incorporated therein aε illuεtrated in the accompanying drawings. In the drawings, Figure 1 is a side view of the engine; Figure 2 iε a plan view from above; Figure 3 iε a sectional view through the rear portion of the cylinder block and the supercharger; Figure 4 iε a εectional view of the cylinder block alolng the line 4-4 in Figue 1; Figure 5 iε a εectional view of the cylinder block along the line 4-4 in Figure 1; Figure 6 iε a diagram relating to the supercharge drive; and Figure 7 is a simplified transverse cross-εec±ional view of a multi-cylinder V engine, incorporating the air distribution system of the invention. Referring now to the drawings, the engine illustrated is of a three cylinder inline single bank configuration operating on the two stroke cycle. The cylinder block 11 has three cylinders formed therein closed at the top by the cylinder head 12. A crankshaft 13 iε journalled in bearingε provided at the lower end of the block 11 with the lower end of the block being closed by the crankcase 14. The crankshaft 13 carrieε a flywheel 15 at the rear end and a pulley 16 at the forward end for driving the various engine accesεorieε, such as alternator and water circulation pump (not shown). The exhaust manifold 18 is attached to one side of the cylinder block 11 to communicate with three exhaust ports provided in the block 11 communicating with the respective cylinderε of the engine. On the oppoεite εide of the cylinder block 11 to the exhaust manifold 18 is an air plenum chamber 19 that communicates with respective inlet ports provided in the cylinder block to communicate with each of the three cylinderε. At the rear of the engine, the εcroll type houεing 20 of a centrifugal supercharger iε formed in part integral with the cylinder block 21, but may be part of an adaptor plate which iε εecured to the cylinder block 11. As seen in Figure 3, the εupercharger εcroll houεing extendε in an arcuate form below the rear portion 14a of the crankcase 14 and includes a forward projecting portion 22 . which co-operates with the air inlet tube 23. The forward projecting portion 22 communicates with the interior of the εcroll houεing 20 at 25 located radially inward of the periphery of the impeller 26 aε iε conventional in a centrifugal type pump compresεor. Internally of the scroll housing 20 the impeller 26 is mounted to rotate concentrically with respect to the crankshaft 13 and is driven thereby through an epicyclic traction type transmiεεion 27 to provide the required εpeed differential between the engine, crankεhaft and the impellor. Further details of the transmisεion 27 are available in the U.S. patent previously referred to herein and are provided hereinafter. The spiral high presεure cavity 28 formed in the εcroll houεing 20 communicated at 29 with the air duct 19 that leads to a plenum chamber 61 (Figure 4) to distribute the air from the supercharger to the respective cylinders of the engine. Aε can be seen the diεpoεition of the centrifugal εupercharger incorporated into the rear portion of the engine block provideε an extremely compact conεtruction whereby the proviεion of the supercharger does not substantially increase the overall longitudinal dimensions of the engine. Also there is a minimal amount of external ducting or piping required to deliver the air to the εupercharger and to deliver the air from the εupercharger to the reεpective engine cylinderε. Aε can be εeen in Figure 3, the impeller 26 of the εupercharger is arranged with a central hub 50 having an internal surface 51 with a concentric annular recess 52 of arcuate crosε-εection. A cylindrical εleeve 54 iε non-rotatably mounted on the extenεion 56 of the cylinder block co-axial with the crankshaft 13. The external cylindrical surface 57 of the εleeve 54 haε a concentric annular recess 55 of arcuate cross-section. When both the εleeve 54 and the impeller hub 50 are co-axially mounted, a plurality of εteel ballε 58 are interpoεed therebetween εeated in the reεpective annular receεεeε 52 and 55. The ballε 58 are mounted in a carrier 59 attached to the flywheel 15 and crankεhaft 13 to rotate therewith. The carrier 59 haε a plurality of apertureε therein to locate the ballε 58 in a equally spaced configuration about the axis of the crankshaft in a manner similar to that used in ball bearings. The frictional load between the balls 58 and the surface of the reεpective annular receεεeε 52 and 55 is sufficient so that, as the crankεhaft and the carrier 59 rotate, the ballε 58 will rotate on their reεpective axes parallel to the axis of the crankshaft and so roll along the surface of the receεε 55 in the sleeve 54. The rotation of the balls 58 on their axes transmits a rotational movement to the hub 50 of the impeller 26 to rotate the impeller on its axis, which correspondε to the crankεhaft axiε, at a rotational εpeed greater than the crankshaft rotational speed. , In the known conεtructionε of the above type of epicyclic friction ball tranεmiεεion, the recesses 52 and 55 are of spherical segmental croεs-εection of a diameter slightly greater than that of the ballε so that the ballε 58 contact the εurfaceε of the receεε substantially in the diametral plane of the balls radial to the crankshaft axis. Thus with the carrier 59 engaging the balls at the mid diameter between the diameters of the contact between the balls and the impeller 26 and the contact between the balls and the εleeve 54, there iε achieved a εpeed εtep-up ratio between the crankεhaft and the impeller of approximately 2:1. However, it has been found that if the recesε 55 in the εleeve 54 iε εhaped to bring the line of contact closer to the line of cntact of the balls with the carrier 59, then the εtep-up ratio can be increaεed εubεtantially above 2:1. Thiε can be achieved by forming the receεε in the εleeve 54 with an undercut cross-section as shown in Figure 6 so the radial distance A from the axis B of the ball 58 to the line of contact C with the recesε 66 in the εleeve 54 is lesε than half the diameter of the ball. The line of contact D between the ball and the receεε 52 in the impeller hub 50 remainε unaltered at the maximum value equal to approximately the full diameter of the ball 58. Thiε ability to obtain a εpeed εtep-up of greater than 2:1 is advantageous in a supercharger drive aε the increaεed εupercharger εpeed at low engine speedε substantially improves the effectivenesε of the supercharger on the engine performance. Referring now to Figure 4 of the drawings, there is shown a cross-εectional view of the engine εhown in Figureε 1 and 2 along the line 4-4 in Figure 1, and with the εupercharger omitted for the purpoεe of εimplicity. Aε can be εeen from Figure 1, thiε cross-sectional view along the line 4-4 is low on the engine block and below the level of the inlet and exhaust ports of the cylinders, which shall be referred to further in connection with Figure 5 of the drawings. The air delivery duct 19 from the supercharger enters the plenum chamber 61 which extends subεtantially the length of the engine. The plenum chamber is an independent component from the engine block, and is secured thereto by appropriate mounting bolts, interposed between the plenum chamber 61 and the cylinder block is a baffle plate 64 having three apertures 63, 65 and 66 therethrough which provide the only communication between the plenum chamber 61 and the interior of the cylinder block. The central aperture 66 in the baffle plate 64 is the only direct communication between the plenum chamber 61 and the cavity 67 in the cylinder block. The plate-type valve 68 is mounted centrally of the aperture 66 on a spindle 69 so that the flow of air from the plenum chamber 61 to the gallery 67 in the cylinder block may be controlled and if desired, completely terminated. The end apertureε 65 and 63 in the baffle plate 64 align with the respective ends 71 and 72 of the loop pasεage 73 formed in the cylinder block. The passage 73 passes across the block at each end thereof as indicated at 75 and 76 communicating with the respective endε of a gallery 77 running the full length of the cylinder block on the other side of the engine and closed on the outer side by the cover plate 78. Extending from the gallerieε 67 and 77 are a plurality of tranεfer passages which communicate the various air inlet ports of the engine cylinderε with the reεpective galleries. The gallery 76 communicates with each of the three pairs of rear transfer paεεageε 80, 81 and 82, which communicate with the respective rear inlet ports of each of the cylindes of the engine. At each end, the gallery 67 communicates with auxilliary passages 83 and 84, which communicate with the outer auxilliary port of the respective end cylinders 3 and 1 of the engine. In the area between the respective adjacent cylinderε there iε further provided auxilliary transfer passages 85 and 86, each of which communicates with two auxilliary ports, one in each of the two adjacent cylinders, as described in more detail hereinafter. The other gallery 77 located on the oppoεite εide of the engine block, thiε being the εide on which the exhauεt portε are alεo located, has two end inlet transfer pasεages 90 and 91 communicating with the respective inlet ports in the end cylinders 1 and 3, and between the adjacent pairs of cylinders 3,2 and 2,1 there are provided two further inlet transfer paεεages 92 and 93, each supplying air to two inlet ports, one provided in each of the two adjacent cylinders. It can be readily seen, from a conεideration of the above described air distribution pasεages, when the control valve 68 is in the closed poεition, no air iε supplied to the air gallery 67 and accordingly no air is provided to the inlet ports in the engine which communicate with the inlet transfer passages 80, 81, 82, 83, 84, 85 and 86. However, air is εupplied through the paεεageε 75 and 76 to the air gallery 77, from which air iε then εupplied to the inlet ports associated with inlet transfer passages 90, 91, 92 and 93. It has been found beneficial to operate the engine with air supplied to the restricted number of inlet ports of the engine in order to obtain appropriate combustion conditions in the cylinders under light loads. It will be appreciated that in order to obtain the desired control over the air flow to the portε on the reεpective oppoεite εides of the cylinder block by the uεe of the passage 73, and to supply air to the inlet portε of two adjacent cylinderε by a εingle transfer pasεage, it iε necessary for the crankcase to be of a construction such that it will co-operate with the lower face of the cylinder block to provide an uninterrupted seal between the crankcaεe and the air supply system of the engine including the air galleries 67 and 77, and a seal between the respective air galleries 67 and 77. Referring now to Figure 5 of the drawings, this is a cross-sectional view through the cylinder block at the level of the various inlet and exhaust ports to the respective cylinders. The inlet and outlet portε are opened and closed by the piston reciprocating in the cylinder in the conventional manner. The twin transfer passages 80, 81 and 82 supply air to the respective pairs of rear inlet ports 100, 101 and 102, these ports being diagonally opposite the exhaust ports 104, 105 and 106 in the correεponding cylinderε. The outer auxilliary tranεfer passages 83 and 84 provide air to the auxilliary ports 108 and 109 of the reεpective end cylinders 3 and 1 of the cylinder block and the inner auxilliary transfer passages 85 and 86 supply air respectively to the pair of ports 110 and 111 and the pair of ports 112 and 113. The transfer passages 90, 91, 92 and 93 each communicate with gallery 77, and the end transfer pasεages 90 and 91 communicate with the outer inlet portε 115 and 116 of the reεpective end cylinderε 1 and 3 while the central tranεfer paεεages 93 and 92 communicate reεpectively with the paired inlet ports 117, 118 and 119, 120, reεpectively. The supplying of air to respective inlet ports of adjacent cylinders in a multi-cylinder two stroke cycle engine from a single transfer port haε not previously been practised, however, it has been found to be practical in a εupercharged engine, wherein the compreεεion preεεure conventionally developed in the crankcase section relating to each cylinder iε not required to effect transfer of the air into the cylinder. However, where the engine iε supercharged a continuous εupply of compreεaed air iε available to the ports without reliance upon crankcase compression which cycles with the reciprocation of the piston. In this regard, it will be appreciated that by providing a single transfer passage servicing the adjacent inlet ports of two adjacent cylinders, the cross-sectional area of the εingle transfer passage can be made greater than would be poεsible if two independent pasεageε were provided in the same space between to service the inlet portε of the reεpective cylinderε. Accordingly, a benefit iε achieved by making the εingle tranεfer paεεage larger in croεε-εection than one of the two paεεageε normally uεed, and yet less than the total crosε-εection of the two passageε it replaceε. In thiε way, the benefitε of a less reεtrictive passage for the air flow can be obtained while also reducing the overall length of the engine. Accordingly, a dual benefit is obtained, whereaε in previouε engineε a benefit in one area could only be achieved with a detrimental effect in the other area. When adjacent inlet portε of adjacent cylinderε have a common tranεfer paεsage aε discussed above, it is necesεary that the timing of the opening and closing of the inlet ports of adjacent cylinders be arranged εo that only one of the inlet portε iε open to receive air from the common tranεfer paεεage at any one time. Thiε arrangement enεureε that the cylinders having inlet ports receiving air from a common transfer pasεage each receiving the required amount of air. If both of the portε were open at the εame time, conditionε may exiεt that would reεult in an uneven air distribution between the two inlet ports εupplied from the common tranεfer passage. Also as the direction of the air flow through the inlet portε iε uεually important in achieving εcavenging of the cylinder, it iε preferable for the piston of one cylinder to close the inlet port theeof while the other inlet port receiving air from the εame transfer port is open. The portion of the piston closing the one inlet port provides part of the surface of the transfer pasεage guiding the air flow to the cylinder with the open inlet port. Referring now to Figure 7 of the drawings, there is shown in simplified form a tranverse croεε-εectional view of a multi-cylinder engine with cylinderε arranged in a 60° V formation providing two bankε of inline cylinderε. The engine operateε on the two-εtroke cycle, preferably with direct fuel injection to the reεpective cylinderε. The engine iε provided with three air conduitε receiving air from a εupercharger, conveniently of the configuration previouεly deεcribed with reference to Figure 3. The three conduits compriεe conduits 30 and 31 located low down on the cylinders on either side of the block. The respective conduits 30 and 31 each run substantially the length of the block so as to be able to provide air to all of the inlet ports located on the respective outer sideε of the cylinder bankε where the exhaust ports are also located. Conveniently, the conduitε 30 and 31 may be interconnected acroεε the engine block at the forward and/or rear end thereof (not εhown) εo that there are balanced conditionε between the air in the reεpective conduits 30 and 31. The conduits 30 and 31 communicate with reεpective tranεfer paεεageε 32 and 33 formed in the wall of the cylinders in each bank to deliver air from the conduitε through the respective inlet ports 34 and 35 to the respective cylinders 36 and 37. The wall 38 bridges between the cylinders n the respective bankε of the V formation to form a central air conduit 39 running the length of the engine block and communicating via reεpective tranεfer passages 40 and 41 with ports 42 and 43 in the cylinderε 36 and 37 in the respective bankε. The condduit 39 formed within the V alεo receive air from the same supercharger unit as provides the air to the cnoduits 30 and 31. In one form of the engine, the conduits 30 and 31 each communicate at the opposite end of the engine and with the central paεεage 39, conveniently at the delivery port of the εupercharger. The conduits 30 and 31 may be isolated from the conduit 39 other than the communication arising from all three passages receiving their air supply from the same supercharger. Further in such a construction a control valve may be provided so that conduit 39 can be isolated from the εupercharger, whereby air is only delivered to the conduits 30 and 31. Further the valve may be of a construction whereby the rate of supply of air to the conduit 39 can be regulated. If deεired the control valve may operate on the cnduitε 30 and 31 and the central conduit 39 is in direct communication with the supercharger. The control of the air supply to the paεεageε 30, 31 and 39 in either of the above manners may be used to asεiεt in the control of the combuεtion and εcavenging proceεε to thereby provide management over the level of exhauεt emissions. In particular, under low load conditions it is appropriate to provide air supply only to the conduitε 30 and 31. A detailed deεcription of the porting and tranεfer paεεageε haε not been provided aε thiε iε readily understood from the previouε deεcription of the single bank of inline cylinderε as εhown in Figureε 1, 2, 4 and 5. The V engine configuration iε baεically two εingle bankε with a common crankεhaft and crankcaεe. In the engine εhown in Figure 7 the conduitε 30 and 31 each correεpond to gallery 77 in Figure 4 and the conduit 39 corresponds to gallery 67. In reference to the control of the air flow to the respective gallerieε or conduitε aε previouεly deεcribed, thiε may be achieved by a valve element, εuch aε by the valve 68, thiε may be by* mechanical actuation from the engine throttle valve or under the control of an electronic engine management εyεtem aε currently uεed widely in vehicle engines.

Claims: THE CLAIMS DEFINING THE INVENTION ARE AS FOLLOWS: 1. A multi-cylinder internal combustion engine having a cylinder block, a crankshaft having a longitudinal axis and supported in the cylinder block for rotation about said longitudinal axiε, a plurality of cylinderε in εaid cylinder block arranged in one or more bankε, each bank having a plurality of inline cylinders, a piston supported to reciprocate in each cylinder, each piεton being coupled to the crankεhaft to effect rotation of the crankεhaft in response to reciprocation of the pistons, a supercharger located at one end of the cylinder block co-axial wi h the crankshaft, said εupercharger having a εtationery houεing non-rotatably εecured to the cylinder block and an impeller co-axially with and drive coupled to the crankεhaft. 2. A multi-cylinder internal combuεtion engine aε claimed in claim 1, wherein the supercharger is interposed between the engine cylinder block and a flywheel mounted on the crankεhaft. 3. A multi-cylinder internal combuεtion engine as claimed in claim 1, including transmiεεion means to drive couple the impeller of the εupercharger to the crankεhaft, the transmission means beirig adapted to rotate the impeller at a rotation speed greater than the crankshaft. 4. A multi-cylinder internal combustion engine as claimed in claim 1, 2 or 3, wherein each cylinder in at least one cylinder bank has at leaεt two inlet portε one on each εide of the longitudinal axis of the reεpective bank of the cylinder, and a reεpective air paεεage extending along each of said two sides of the bank of cylinders, each air passage being arranged to receive air from the supercharger, the inlet ports on the respective side of said cylinder bank being in direct communication only with the air passage on that side of the cylinder bank. 5. A multi-cylinder internal combuεtion engine aε claimed in claim 4, wherein air control meanε are provided to εelectively εupply or vary the rate of εupply of air from the supercharger to one or both of said air passages of each cylinder bank. 6. A multi-cylinder internal combustion engine aε claimed in any one of the preceding claims, wherein at least part of the stationary housing of the supercharger is integral with the cylinder block. 7. A multi-cylinder internal combustion engine aε claimed in claim 4, being a two εtroke cycle engine and having in the wall of each cylinder an exhauεt port, all exhauεt portε in each cylinder bank being located on the one εide of the cylinder bank, each cylinder in the cylinder bank having at leaεt one inlet port in the cylinder wall on the εame εide of εaid cylinder bank aε the exhauεt portε, εaid inlet portε on the exhaust port side of the cylinder bank all being in direct communication with the air passage extending along the same side of the cylinder bank as the exhaust ports. 8. A multi-cylinder internal combuεtion engine aε claimed in claim 7, wherein each cylinder in the cylinder bank haε two inlet ports in the cylinder wall one on each of the two opposite sides of the exhaust port in the longitudinal direction of the cylinder bank. 9. A multi-cylinder two stroke cycle internal combustion engine as claimed in claim 7 or 8, wherein air control means are provided to εelectively εupply or vary the rate of εupply of air from the supercharger to one or both of said air pasεages on the cylinder bank. 10. A multi-cylinder two stroke cycle internal combustion engine as claimed in claim 9, wherein εaid air control meanε iε adapted to εelectively iεolate the air εupply from the εupercharger to the air passage on the opposite εide of the cylinder bank to the exhauεt portε. 11. A multi-cylinder internal combuεtion engine having a cylinder block, a crankshaft having a longitudinal axis and supported in the cylinder block for rotation about said longitudinal axis, a plurality of cylinders in εaid cylinder block arranged in one or more banks, each bank having a plurality of inline cylinders, a piston supported to reciprocate in each cylinder, each piston being coupled to the crankεhaft to effect rotation of the crankεhaft in response to reciprocation of the pistons, each cylinder in at least one cylinder bank having at least two inlet ports, one on each of the two opposite longitudinal sideε of the reεpective bank of cylinderε, and a reεpective air paεεage extending along each of εaid two oppoεite sideε of each cylinder bank, each air paεsage being arranged to receive air from a supercharger, the inlet portε on the respective εideε of εaid cylinder bank being in direct communication only with the air paεεage on that εide of the cylinder bank, and air control meanε operable to selectively supply air or vary the rate of supply of ir from the εupercharger to one or both of εaid air paεεages of each cylinder block. 12. A multi-cylinder internal combuεtion engine as claimed in claim 10, being a two stroke cycle engine and having in the wall of each cylinder an exhaust port, all exhaust ports in each bank being located on the one εide of the bank, each cylinder having at least one inlet port in the cylinder wall on the same side of said bank as the exhaust ports, said inlet port on the exhaust port εide the cylinder bank being in direct communication with the air paεεage extending along the εame side of the cylinder bank as the exhaust ports. 13. A multi-cylinder internal combuεtion engine aε claimed in claim 12, wherein each cylinder in the cylinder bank has two inlet ports in the cylinder wall one on each of the two opposite sides of the exhaust port in the longitudinal direction of the cylinder bank. 14. A multi-cylinder two stroke cycle internal combustion engine as claimed in claim 11, wherein said air control means is adapted to selectively isolate the air εupply from the εupercharger to the air pasεage on the oppoεite εide of the cylinder bank to the exhauεt ports. 15. A multi-cylinder two stroke cycle internal combustion engine having a cylinder block, a crankshaft having a longitudinal axis and supported in the cylinder block for rotation about said longitudinal axis, a plurality of cylinderε in εaid cylinder block arranged in one or more bankε, each bank having a plurality of inline cylinderε, a piεton εupported to reciprocate in each cylinder, each piεton being coupled to the crankεhaft to effect rotation of the crankεhaft in reεponεe to reciprocation of the piεtonε, each cylinder in at leaεt one cylinder bank having at leaεt two peripherally εpaced inlet portε in the wall thereof, one on each εide of the longitudinal axiε of the reεpective bank of cylinderε, an air paεεage extending along at leaεt one bank of cylinderε and communicating with inlet portε on each cylinder of the cylinder bank on each of the two oppoεite sides of the cylinder bank, the air pasεage being arranged to receive air from a supercharger, and air control means operable in relation to the air passage receiving air from the supercharger to selectively supply or vary the rate of supply of air to the inlet ports on one or both sideε of the cylinderε of that cylinder bank. 16. A multi-cylinder internal combustion engine as claimed in any one of the preceding claims 7 to 14, being two banks of cylinders arranged in a V formation, wherein each bank haε an air paεsage extending along the outer side thereof and a εingle air paεεage iε provided between the bank communicating with the inlet ports on the inner side of each bank. 17. A multi-cylinder supercharged two εtroke cycle internal combuεtion engine having a cylinder block, a crankεhaft having a longitudinal axiε and εupported in the cylinder block for rotation about εaid longitudinal axis, a plurality of cylinders in said cylinder block arranged in an inline formation, a piεton εupported to reciprocate in each cylinder, each piεton being coupled to the crankεhaft to effect rotation of the crank in reεponεe to reciprocation of the pistons, each cylinder having at least two peripherally spaced inlet ports in the wall of the cylinder cyclically opened and cloεed by the piεton reciprocating in the cylinder, at leaεt one inlet port of each of two adjacent cylinderε being located in an opposing relation and each communicating with a portion of a single tranεfer paεεage interpoεed between εaid oppoεing inlet portε, whereby air from the εupercharger can be εupplied to εaid two cylinderε through the respective opposing inlet ports from said single transfer paεεage, the timing of the opening and cloεing of the opposing inlet ports by the reciprocation of the pistonε in the adjacent cylinderε being arranged εo that only one of εaid oppoεing portε iε in communication with the εingle transfer port at any one time. 18. A multi-cylinder internal combustion engine as claimed in claim 17, wherein the two adjacent cylinders each have two inlet ports, one inlet port of each cylinder being located in opposing relation on each side of a plane containing the longitudinal axis of the two adjacent cylinders, and respective transfer passage portions on each εide of εaid plane in communication with the oppoεing inlet ports on that side of the plane. 19. A multi-cylinder internal combustion engine aε claimed in any one of claimε 1 to 16 being a two stroke cycle engine wherein the inlet ports are located in the wall of respective cylinders and include two peripherally spaced inlet ports in each cylinder cyclically opened and closed by the piston reciprocating in the cylinder, at least one inlet port of each of two adjacent cylinders being located in an opposing relation and each communicating with a portion of a εingle transfer pasεage interposed between said opposing inlet portε, whereby air from the εupercharger can be εupplied to εaid two cylinderε through the respective opposing inlet ports from said single transfer pasεage, the timing of the opening and cloεing of the opposing inlet ports by the reciprocation of the pistons in the adjacent cylinders being arranged so that only one of said opposing ports is in communication with the single transfer port at any one time.

Inventors: BELL GREGORY BRUCE, SCHLUNKE CHRISTOPHER KIM, BELL, GREGORY, BRUCE, SCHLUNKE, CHRISTOPHER, KIM
Applicants: ORBITAL ENG PTY, ORBITAL ENGINE COMPANY PROPRIETARY LIMITED
Application year: 1990
Main classification: F02D9
IPC codes: F02B25, F02B33, F02B75, F02F1, F02M35