Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
  • F01L7/00—Rotary or oscillatory slide valve-gear or valve arrangements
  • F01L7/02—Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves
  • F01L7/021—Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves with one rotary valve
  • F01L7/023—Cylindrical valves having a hollow or partly hollow body allowing axial inlet or exhaust fluid circulation
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
  • F01L7/00—Rotary or oscillatory slide valve-gear or valve arrangements
  • F01L7/02—Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves
  • F01L7/021—Rotary or oscillatory slide valve-gear or valve arrangements with cylindrical, sleeve, or part-annularly shaped valves with one rotary valve
  • F01L7/024—Cylindrical valves comprising radial inlet and axial outlet or axial inlet and radial outlet
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
  • F01L7/00—Rotary or oscillatory slide valve-gear or valve arrangements
  • F01L7/16—Sealing or packing arrangements specially therefor
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
  • F01L2301/00—Using particular materials
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
  • F01L2301/00—Using particular materials
  • F01L2301/02—Using ceramic materials

Definitions

• the present invention relates to a valve for a rotary valve internal combustion engine and manufacture thereof.
• a valve for a rotary valve internal combustion engine and manufacture thereof relates to axial flow rotary valves with internal cooling and incorporating both an inlet port and an exhaust port in the same valve.
• the present invention relates to axial flow rotary valves incorporating an inlet and an exhaust port in the same valve. These ports terminate as openings in the periphery of the valve. During rotation these openings periodically align with a similar window in the cylinder head allowing the passage of gas from the valve to the cylinder and vice versa.
• Rotary valves which run with a small predetermined clearance to the cylinder head bore were developed to address the problem of thermal and mechanical deflection of the valve, which had plagued rotary valve development for the most part of the 20th century.
• Rotary valves were traditionally sealed by the use of a close fitting stationary sleeve around the outer diameter of the valve. These sleeves function to gas seal the combustion chamber, and in the case of valves incorporating both inlet and exhaust ports to seal between the ports. These arrangements failed because they were unable to cope with the inevitable thermal and mechanical distortion of the valve which invariably resulted in seizure of the valve in the sleeve. Although many attempts were made to design sleeves that overcome this problem, none were commercialised.
• the valve was designed to run with a small clearance to the cylinder head bore and the combustion chamber was sealed by means of a floating array of seals arranged around the window in the cylinder head.
• a floating array of seals arranged around the window in the cylinder head.
• Thermal distortion generally results in a "permanent" distorted valve shape that rotates with the valve, if a thermally induced high point on the valve makes contact with the cylinder head bore the contact point will rotate with the valve generating considerable heat in the valve at the point of contact. This type of contact typically results in seizure of the valve in the cylinder head bore.
• Axial flow rotary valves incorporating both inlet and exhaust ports in the same valve are the most demanding category of rotary valve from a thermal distortion perspective.
• the hot exhaust port at the other end is the cool inlet port and the periphery is part subject to combustion, part subject to exhaust flow and part subject to inlet flow. Further, the presence of two ports in the same valve dramatically reduces the space available for valve cooling passages.
• Cooling passages are an essential requirement for all rotary valves with the possible exception of those with very low power outputs.
• some prior art patent documents only show the rotary valve constructional and cooling details schematically, as these details were not relevant to the disclosure.
• a typical example of this is US Patent 5,509,386 (Wallis et al).
• FIG. 10 A rotary valve constructed similarly to that of US Patent 5,509,386 (Wallis et al) is shown in Figs. 10 and 11 of the present specification. Important features of this valve are the complex cooling passages completely isolating the inlet and exhaust ports from each other and extending into the area adjacent the exhaust trailing edge 34 (refer Fig. 11).
• Fig. 12 is an isometric view of the core necessary to manufacture the cooling passage in this valve by a casting process. This core is exceedingly complex with thin wall sections and can only be manufactured using ceramic, which is very fragile, expensive and difficult to remove from the casting.
• This valve is typical of previous prior art valves in that it is manufactured as a steel casting with cored internal cooling passages. In practise these valves are extremely difficult to cast and require use of the investment casting process which further increases the complexity and cost.
• US Patent 2,158,386 shows cooling details of an axial flow rotary valve incorporating both inlet and exhaust ports in the same valve. Cooling is provided in a manner similar to that of the prior art rotary valve shown in Figs. 10 and 11 of the present specification including cooling of exhaust trailing edge.
• the cooling passages in the valve shown in US Patent 2,158,386 (Sykes) are however much larger than those of the valve shown in Figs. 10 and 11, and therefore make the process of manufacturing the casting somewhat easier.
• the problem with this valve is the very small ports that result from this approach.
• Both the inlet and exhaust ports have a diameter that is smaller than 50% of the valve outside diameter.
• valve 10 and 11 has an inlet port with a diameter that is 80% of the valve outer diameter and an exhaust port with a diameter that is 70% of the valve outside diameter.
• the valve shown in US Patent 2,158,386 will have an inlet flow area of less than 40% that of a valve as shown in Figs 10 and 11 having the same outside diameter.
• the breathing capacity of such a valve would be so low as to render it inefficient compared to modern poppet valve technology.
• the diameter of the valve is the critical design issue as it determines the position of the spark plug and the shape of the combustion chamber. The greater the valve diameter the further the sparkplug must be located from the centre of the cylinder. From a combustion perspective the optimum spark plug position is the centre of the cylinder.
• prior art rotary valves of the type shown in Figs. 10 and 11 tend to be structurally inefficient with low stiffness to weight ratio.
• Prior art rotary valves such as that shown in US Patent 5,509,386 (Wallis et al) show axially disposed passages even if they were, as discussed previously, only schematic.
• the axial passage of this valve has a large circumferential length and there is connection between the inner and outer walls 40, 39 (Fig. 11 ) at the circumferential ends of this axial passage only. This is the source of its structural inefficiency.
• the rotary valve in Fig. 11 has an axial passage 21a extending circumferentially from adjacent the exhaust port leading edge 35 to the inlet port 3.
• the resulting structure formed by the outer wall 39, axial passage 21a and inner walls 40 of the valve is inherently flexible as the inner and outer walls are not tied together can therefore move independently of each other. This arrangement results in a very poor stiffness to weight ratio.
• the aspect ratio of an axially extending passage is defined as the maximum circumferential length of the passage divided by the minimum radial height between the radial extremities of the axial passage and the adjacent surface of either the inner or outer wall, which ever is the closer.
• the radial wall thickness of outer wall 39 is 3.5mm
• the radial wall thickness of inner wall 40 is 2mm
• the circumferential length of axial passage 21 a is 70mm giving axial passage 21 a an aspect ratio of thirty five to one (35:1).
• the outside diameter of the valve must be a minimum consistent with the required minimum flow area in both the inlet and exhaust ports.
• the valve must be sufficiently stiff such that under maximum combustion load the deflection is less than the predetermined small clearance.
• the valve cooling and the valve construction must be such to ensure that the thermal distortion is less than the predetermined small clearance.
• the valve cooling and construction must be such that valve distortion due to mechanical load does not add to the thermal distortion. Otherwise, the predetermined small clearance would have to be larger than necessary.
• the present invention seeks to overcome one or more of the disadvantages associated with the abovementioned prior art rotary valves that have internal cooling passages cast therein.
• the present invention consists of an axial flow rotary valve for an internal combustion engine, said valve being adapted to rotate about an axis within a bore in the cylinder head of said engine, one end of said valve being an inlet end and the other end being an exhaust end, said valve comprising a centre portion having a cylindrical periphery, an inlet portion smaller in diameter than said centre portion, extending between said centre portion and said inlet end, an exhaust portion smaller in diameter than said centre portion, extending between said centre portion and said exhaust end, an inlet port extending from said inlet end and terminating as an inlet opening in the periphery of said centre portion, and an exhaust port extending from said exhaust end and terminating as an exhaust opening in the periphery of said centre portion, characterised in that said centre portion has at least one elongate passage communicating between said inlet portion and said exhaust portion, said passage being disposed circumferentially outside said openings and radially outside at least one of said inlet and exhaust portions.
• said passage has an aspect ratio smaller than 10:1.
• At least one end of said centre portion has an annular valve seat extending radially inwards from said cylindrical periphery and at least a portion of said passage is radially outside the inside diameter of said annular valve seat.
• said centre portion has at least one annular cavity, axially outside said inlet and exhaust openings, having an annular opening radially inside of said annular valve seat, and an end of said passage terminates at said cavity.
• said at least one elongate passage comprises a plurality of circumferentially spaced apart elongate passages.
• At least one of said passages is adjacent the trailing edge of said exhaust opening.
• each of said passages has a substantially circular section and extends in a substantially axial direction.
• said inlet and exhaust ports are separated by a common wall having no internal passages.
• said elongate passage is a coolant passage.
• said valve is manufactured from a single solid piece of material.
• said valve is manufactured from an inner body and at least one outer body, said outer body at least partially surrounding said inner body and attached thereto such that said passage is formed at the interface between said bodies.
• the present invention consists of a method of manufacturing a rotary valve in accordance with the first aspect of the present invention, from an unfinished valve having an oversize centre portion stepping radially inwards at both ends, comprising the steps of:
• the present invention consists of a rotary valve assembly for an internal combustion engine, comprising a rotary valve in accordance with the first aspect of the invention, a cylinder head having a bore in which said valve is supported by bearing means and rotates with a small predetermined clearance between said bore and said centre portion of said valve, said inlet and exhaust openings of said valve periodically communicating with a window in said bore, and first and second sealing rings flexibly sealed to said bore and biased axially inwards against first and second valve seats respectively formed by opposite ends of said centre portion.
• said rotary valve assembly further comprising a heat insulation barrier in the exhaust port of said valve covering at least a portion of the common wall separating said inlet and exhaust ports of said valve.
• Fig.1 is a sectional view of an axial flow rotary valve internal combustion engine in accordance with a first preferred embodiment of the present invention.
• Fig. 2 is a partial cross sectional view along II - II of the engine depicted in Fig.1 where the clearance between the valve and the cylinder head bore has been exaggerated for clarity.
• Fig. 3 is a partial cross sectional view through an axial flow rotary valve in the early stages of manufacture according to the present invention.
• Fig. 4 is a partial cross sectional view as in Fig.3 but with the valve at a later stage of manufacture.
• Fig. 5 is a partial cross sectional view as in Fig.3 and Fig.4 but with the valve at the end of manufacture.
• Fig. 6 is an isometric view of a rotary valve according to a second preferred embodiment of the present invention, manufactured from two pieces.
• Fig. 7 is a cross sectional view through a rotary valve showing details of a heat insulation method for the exhaust port according to the present invention.
• Fig. 8 is an isometric view of the sheet metal baffle used to insulate the common wall and the exhaust port of the valve shown in Fig. 7.
• Fig. 9 is an isometric axial sectional view through the centre of the rotary valve shown in Fig. 1.
• Fig. 10 is an isometric axial sectional view through the centre of a prior art rotary valve.
• Fig. 11 is an isometric transverse sectional view through the centre of the prior art rotary valve shown in Fig. 10.
• Fig. 12 is an isometric view of the core required to manufacture the cooling passages in the prior art valve shown in Figs. 10 and 11.
• Fig. 1 depicts a first embodiment of a rotary valve assembly according to the present invention comprising a valve 1 and a cylinder head 2.
• Valve 1 has an inlet port 3 and an exhaust port 4.
• Valve 1 has a centre portion 5 of constant diameter with an inlet portion 9 of reduced diameter on one side and exhaust portion 16 of reduced diameter on the other side.
• Inlet portion 9 extends between centre portion 5 and the inlet end 42 of valve 1.
• Exhaust portion 16 extends between centre portion 5 and the exhaust end 43 of valve 1.
• Inlet port 3 extends from inlet end 42 of valve 1 and terminates at inlet opening 6 in the periphery of centre portion 5.
• Exhaust port 4 extends from exhaust end 43 and terminates at exhaust opening 7 in the periphery of centre portion 5.
• Inlet port 3 and exhaust port 4 are separated by a common wall 23.
• Valve 1 is supported by bearings 8 to rotate about axis 10 in cylinder head 2.
• Bearings 8 support the periphery of inlet portion 9 and exhaust portion 16. Bearings 8 allow valve 1 to rotate about axis 10 whilst maintaining a small running clearance between the periphery of centre portion 5 and bore 11 of cylinder head 2.
• Cylinder head 2 is mounted on top of cylinder block 12. Piston 13 reciprocates in cylinder 14. As valve 1 rotates in cylinder head 2, inlet opening 6 and exhaust opening 7 periodically communicate with window 15 in cylinder head 2, allowing the passage of fluids between valve 1 and cylinder 14.
• Valve cooling and lubricating oil is prevented from entering the zone between the periphery of centre portion 5 and the bore 11 by two face seal arrangements comprising valve sealing rings 18, O-rings 20, annular valve seats 17 and face seal springs 19.
• Centre portion 5 extends axially a small distance past the axial extremities of window 15.
• Valve 1 steps radially inward either side of centre portion 5 forming radial faces that form valve seats 17 against which valve sealing rings 18 are axially inwardly preloaded by face seal springs 19.
• Valve sealing rings 18 are slidingly sealed against cylinder head bore 11 by means of O-rings 20.
• a plurality of small axially extending elongate axial passages 21 allow cooling oil to pass through valve 1 close to the surface of centre portion 5. Passages 21 extend axially beyond the axial extremities of inlet opening 6 and exhaust opening 7, and communicate between inlet portion 9 and exhaust portion 16. Cooling oil enters and exits the centre portion 5 through the annular gaps between the inside diameter of valve seats 17 and the radially adjacent valve surfaces 24. Immediately axially inboard of valve seats 17 are annular cavities 22 providing access to axial passages 21. Axial passages 21 terminate at annular cavities 22, and each annular cavity 22 has an annular opening radially inside of valve seats 17. Annular cavities 22 are axially outside of inlet opening 6 and exhaust opening 7. Fig. 9 shows an isometric sectional view of valve 1.
• Axial passages 21 have a small aspect ratio.
• axial passages 21 are formed by drilled holes, typically the hole diameter is 2mm and the radial wall thickness between the radial extremity of the hole and the adjacent surface is 1.5mm giving axial passages 21 an aspect ratio of 1.33 (ie. 2mm/1.5mm). This ensures that the inner and outer walls are always effectively tied together and act as a very efficient beam. Unlike the prior art valves any movement of the common wall 23 is directly reacted by both the inner and outer walls.
• axial passages 21 are approximately equally circumferentially spaced apart and are located at a constant radius from axis 10 close to the surface of cylindrical portion 5.
• Axial passages 21 are disposed circumferentially outside inlet opening 6 and exhaust opening 7, including several of axial passages 21 being located in the bridge 32 of valve 1.
• Bridge 32 is formed by the portion of the periphery of centre portion 5 that spans between the inlet opening leading edge 33 and the exhaust opening trailing edge 34.
• Axial passages 21 are wholly disposed radially outside the extremities of both the periphery of inlet portion 9 and the periphery of exhaust portion 16.
• the axial passages may be radially outside the extremities of only one of the inlet or the exhaust portions. It is necessary for the axial passages to be radially outside at least one of the inlet or exhaust portions so that access is available to machine the axial passages.
• Axial passages 21 are small in diameter and are typically less than 2mm diameter. As there is no known means of casting such passages they must be machined into valve 1. Axial passages 21 must be close to the surface of cylindrical portion 5 to minimize the heat path between the surface of the valve subject to heat input from the combustion chamber and axial passages 21.
• Axial passages 21 can easily be provided adjacent exhaust trailing edge 34. In prior art arrangements this was only possible by extending the cooling passage between the inlet and exhaust port.
• a single common wall 23 separates the inlet port 3 from the exhaust port 4, replacing the typical prior art arrangement of two walls separated by an internal cooling passage with a consequent saving of material and weight.
• axial passages 21 The requirement to position axial passages 21 close to the surface of centre portion 5 is in conflict with the requirement to form valve seats 17 of adequate radial depth at both ends of centre portion 5.
• the radial extremities of axial passages 21 are located radially within 1.5mm of the periphery of centre portion 5.
• valve seats 17 require a radial depth greater than 3mm to function satisfactorily as face seals.
• at least a portion of each axial passage 21 is radially outside the inside diameter of valve seats 17, as can be seen in Fig. 1. Consequently any axial passages 21 machined directly into valve 1 using conventional manufacturing techniques would penetrate valve seats 17 against which valve sealing ring 18 is preloaded thus preventing proper sealing.
• Figs. 3 to 5 illustrate a method of manufacturing valve seats 17 and axial passages 21 that overcomes this difficulty.
• Fig. 3 shows a partial section through unfinished valve 1.
• centre portion 5 has not yet been finished machined and its outside diameter is larger than its final diameter.
• An annular groove 44 is machined in each end face of centre portion 5.
• Axial passages 21 terminating at grooves 44, may be machined through centre portion 5 before or after machining grooves 44.
• axial passages 21 are some distance from the oversized outside diameter of centre portion 5 of valve 1 which still has a machining allowance remaining on its diameter.
• the outside diameter of unfinished valve 1 is deformed inwardly at both ends of centre portion 5 such that grooves 44 become annular cavities 22 adjacent the ends of the axial passages 21 , as shown in Fig. 4.
• the ends of centre portion 5 may be deformed by rolling, swaging or any other suitable process.
• the outside diameter of centre portion 5 is then machined to final size and the ends of centre portion 5 are machined to form valve seats 17, as shown in Fig. 5.
• axial passages 21 can be machined into valve 1 radially outboard of the inner diameter of valve seats 17 whilst providing sufficient radial thickness for valve seats 17 to ensure correct functioning of the face seal.
• the radial gap between the inside diameter of valve seat 17 and its radially adjacent surface 24 forms a coolant opening to cavities 22. This gap must be sufficient to ensure the required oil flow to the axial passages 21 can pass to and from cavities 22 without excessive pressure drop.
• the diameter of the radial adjacent surface 24 determines the size of inlet port 3 and exhaust port 4, and therefore the breathing capacity of valve 1.
• the maximum allowable port diameter adjacent this surface 24 is the diameter of the radial adjacent surface 24, minus twice the minimum allowable wall thickness.
• Bearing surface 25 is the surface against which the rolling elements of bearings 8 roll and is typically designed to be no smaller in diameter than that of the radial adjacent surface 24, as this would unnecessarily reduce the size of inlet port 3 and exhaust port 4.
• the diameter of bearing surface 25 cannot be larger than the inner diameter of the valve sealing ring 18 as it must be able to be assembled over this diameter.
• the number of axial passages 21 and their distribution depends on design details of the engine and its application. Their number and distribution are determined by two considerations. Firstly, they should be positioned to maximise the heat removal from the hottest areas on the valves periphery. Secondly, they should be positioned to minimise the thermal distortion of the valve. The optimum arrangement is generally established experimentally. Certain areas of the periphery of centre portion 5 are subjected to greater heat loads than others. For example the portion of the periphery exposed to combustion sees a greater heat load than the portion of the periphery exposed to the combustion chamber during compression. Bridge 32 adjacent to exhaust trailing edge 34 is also subject to high heat load whilst the area of bridge 32 adjacent to leading inlet leading edge 33 has very little heat load.
• axial passages 21 are positioned adjacent those areas on the surface of the valve subject to high heat load. In some applications where weight is particularly important, as many axial passages as possible may be provided to minimise the valve weight. Some of these axial passages 21 may subsequently be blocked to isolate the cooling oil flows to those areas discussed above.
• Minimising the number of axial passages 21 that have cooling oil flowing through them maximises the velocity of the cooling oil flow through the axial passages 21 for a given oil flow through the valve. This higher velocity improves the ability of the oil to cool the valve surface. Distributing the axial passages 21 that carry cooling oil as described above ensures heat is more efficiently removed from those surfaces with high heat input, for a given cooling oil flow.
• Exhaust port 4 has some surfaces directly exposed to axial passages 21. These axial passages 21 are subject to heat input from both the outer surface of the valve and the inner surface of exhaust port 4 and are subject to a disproportionate heat load. In some arrangements where the heat load from the exhaust is high or the predetermined small clearance is small or a combination of both these, it is necessary to limit the heat input to common wall 23 and to axial passages 21 from exhaust port 4. This can be achieved by various methods. Walls of the exhaust port 4 can be sprayed with an insulating layer. Alternatively, a heat barrier in the form of a sheet metal baffle 30 (refer to Fig. 8) can be inserted into exhaust port 4, which provides an air gap 31 (refer to Fig. 7) between the hot exhaust gases and the walls of exhaust port 4. Small raised pads 36 may be provided on the surface of exhaust port 4 to prevent baffle 30 touching the walls of exhaust port 4 except at these pads 36.
• valve distortion can be maintained at a level which can be accommodated by a predetermined small clearance, whose size does not adversely affect the engine's performance, even under the most arduous conditions.
• Axial cooling passages 21 are limited to an area immediately radially adjacent the outside diameter of valve 1.
• This arrangement has the great advantage that it can be manufactured from a casting into which the axial cooling passages 21 are subsequently machined. Such a casting is very easy to cast due to the absence of complex internal cooling passages.
• This arrangement has the added benefit that such valves may be machined from a solid billet of material. This is particularly important in the manufacture of prototype valves where even simple casting require long lead times.
• valve 1 By placing axial passages 21 immediately radially outboard of the peripheries of inlet portion 9 and exhaust portion 16, immediately radially inboard of periphery of centre portion 5, and embedding them in the centre of the valve's outside wall, the diameter and weight of the valve 1 is minimised for any given port flow area and its stiffness maximised. By deforming the outer diameter of valve 1 during manufacture an adequate valve seat 17 may be obtained without having to increase the valve outside diameter. Finally by appropriate placement of the axial passages carrying coolant and insulation of the exhaust port a valve with minimal distortion is obtained.
• axial passages 21 are relatively expensive to machine due to their small diameter and long length. This issue is addressed by the second embodiment of the present invention shown in Fig. 6 whereby valve 1 is manufactured from several pieces welded together. Axial passages 21 are formed in the outer diameter of valve inner body 28. In this case axial passages 21 are no longer necessarily round in cross-section or axially extending. Axial passages 21 may be replaced by passages that extend between the exhaust portion and the inlet portion but follow a diagonal, curvilinear or other path. Axial passages 21 are no longer confined by manufacturing considerations to the very low aspect ratios of those valves with machined holes. However, they should maintain a low aspect ratio to ensure structural efficiency.
• Valve outer body 29 is shrunk over valve inner body 28 and welded to valve inner body 28. At a minimum, valve outer body 29 must be welded to valve inner body 28 adjacent to inlet opening 6 and exhaust opening 7 in centre portion 5, to ensure that cooling oil does not leak into inlet port 3 or exhaust port 4. Additional welding of valve outer body 29 to the valve inner body 28 in the zone between the axial cooling passages will stiffen up the completed valve.
• valve inner body 28 may for example be produced as a casting and valve outer body 29 may for example be manufactured from extruded tube.
• valve outer diameter of the valve will need to be deformed and machined in a similar fashion to the first embodiment described earlier with reference to Figs. 4 and 5, after valve outer body 29 has been attached to valve inner body 28.
• small aspect ratio for axial passages 21 , is defined as one that is less than ten to one (10:1).

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

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• 2005
  • 2005-08-31 WO PCT/AU2005/001310 patent/WO2006024085A1/en active Application Filing
  • 2005-08-31 US US11/659,693 patent/US20070277770A1/en not_active Abandoned
  • 2005-08-31 JP JP2007528518A patent/JP2008511781A/ja active Pending
  • 2005-08-31 EP EP05776137A patent/EP1789657A1/en not_active Withdrawn

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