WO2004015246A1

WO2004015246A1 - Improvements in or relating to internal combustion engines

Info

Publication number: WO2004015246A1
Application number: PCT/GB2003/003517
Authority: WO
Inventors: Andrew J. Boulton
Original assignee: Individual
Current assignee: Individual
Priority date: 2002-08-12
Filing date: 2003-08-12
Publication date: 2004-02-19
Anticipated expiration: 2005-02-12
Also published as: US20060086335A1; GB0218674D0; EP1570159A1; AU2003259324A1; WO2004015246A9

Abstract

Cylinder head apparatus (100) for an internal combustion engine having a cylinder (F) and piston (M) comprises a rotating shaft (110) having a recess (112) causing periodic communication between the cylinder (F) and intake (C) and exhaust (L) passages. In other embodiments, two shafts are used, and hollow shafts with apertures are used.

Description

Improvements in or Relating to Internal Combustion Engines

This invention relates to improvements in or relating to internal combustion engines, and in particular, but not exclusively, to improvements relating to replacement apparatus for the intake and exhaust valves of internal combustion engines.

Conventional four stroke internal combustion engines involve a four stage cycle. Firstly, there is an intake of air/fuel mixture into a cylinder; known as "intake stroke". Secondly, a piston within the cylinder compresses the air/fuel mixture; known as "compression stroke" . Thirdly, the compressed air/fuel mixture is ignited in the cylinder causing combustion; known as "combustion stroke" . And lastly, the combusted gases are exhausted; known as "exhaust stroke" .

A four stroke internal combustion engine comprises an intake valve to allow an ingress of air/fuel mixture into a cylinder, and an exhaust valve, to allow an egress of exhausted gases after combustion of the air/fuel mixture.

The timing of the opening and closing of the valves is vital to an engines performance.

To allow the piston to draw-in the fuel/air mixture (or air alone in the case of a direct injection engine) , the intake valve needs to open as the piston moves from an extended position to a retracted position on the intake stroke.

The exhaust valve needs to be opened as the piston is extended in the exhaust stroke.

Both the intake and the exhaust valves each comprise a rocker arm and a valve return spring, with the rocker arm being actuated by a cam or a lobe located on a camshaft.

The valves act against the valve return springs, where the valves are fired in one direction, only then to stop at the extent of their travel, and be sent flying in the opposite direction. This happens many times a minute which wastefully drains power from the engine. This also causes noise, vibration and harshness.

As the camshaft rotates, the shape of the cam which actuates the rocker arm, determines the timing of the opening and closing of the intake and exhaust valves .

Conventional designs of cams, particularly fixed cams, will only operate optimally over a limited range of speeds .

According to one aspect of the present invention, a cylinder head assembly comprises a cylinder head having an inlet passage and an outlet passage for communication, in use, with a cylinder, and at least one rotatably mounted shaft member interposed between the inlet and outlet passages and the cylinder, the shaft member (s) having passage means to allow an ingress of air mixture from the inlet passage to the cylinder at a first desired rotational position, and to allow an egress of combusted gases from the cylinder through the outlet passage at a second desired rotational position and to prevent the air or combusted gases from entering or exiting the cylinder at a third desired rotational position.

There may be two shaft members, one cooperating with the inlet passage and one with the outlet passage.

Preferably, the shaft members are coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said shaft members.

Alternatively, the shaft members are driven independently of the crankshaft, and of each other, with means for individually controlling or adjusting the speed of rotation of said shaft members.

The shaft member or each shaft member may be substantially solid, and the passage means may comprise a recess in the shaft member or a respective recess in each of the shaft members.

Alternatively, each shaft member may be hollow; each shaft member having at least one aperture located around a portion of its circumference, wherein the inlet shaft member allows an ingress of air/fuel mixture through the inlet shaft member to enter said cylinder when the aperture in the inlet shaft is presented to the cylinder, and the outlet shaft member allows an egress of combusted gases to exit the cylinder when the aperture in the outlet shaft member is presented to the cylinder.

Preferably each shaft member is provided with an inner hollow tube member rotatably mounted within said shaft member; each inner tube member having at least one aperture located around a portion of its circumference; rotation of said inner tube member within the respective hollow shaft members providing a variable size effective aperture, which allows a variable ingress of combustion air to enter said cylinder through the effective aperture in the inlet shaft member, and allows a variable egress of combusted gases from the cylinder to exit through the effective aperture in the outlet shaft member. Preferably also, the speed of rotation of the inner and outer tube members are such that the effective aperture maximises or restricts the rate of ingress of air, or egress of exhaust gases, through the respective inner tube members.

The inner tube members may be coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said tube members. Alternatively, the tube members may be driven independently of the crankshaft, and of each other, with means for individually controlling or adjusting the speed of rotation of said tube members .

Typically, the cylinder head assembly will form part of a multi-cylinder engine with the shaft member (s) extending over a number of cylinders, the shaft member (s) having a corresponding number of passage means.

The shaft member (s) suitably have gas tight seal assemblies.

From another aspect, the invention provides a method of allowing an ingress and egress of combustion air and combusted gases from a cylinder comprising the steps of: presenting a passage means within a shaft member to an inlet passage; retracting of a piston within a cylinder to allow an induction of air from the inlet passage through said passage means into the cylinder; rotating the shaft member to prevent any leakage of air upon a compression of the air in the cylinder by the piston; combusting air/fuel mixture in the cylinder to cause said piston to retract; extending the piston in the cylinder; presenting passage means to the cylinder and an outlet passage to allow an egress of combusted gases; and repeating the above steps.

In one form of the method, the same passage means is used for induction and egress.

The passage means may be formed by an aperture in at least one hollow shaft, and the method further includes the step of varying the effective size of the aperture to restrict or maximise the amount of fluid flow through the aperture.

Embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings in which: -

Fig. 1 is a schematic front sectional view of a conventional four stroke internal combustion engine;

Figs. 2a-d are schematic front sectional views illustrating the workings of a single rotatably mounted shaft member of the present invention; Figs. 3a-d are schematic front sectional views illustrating the workings of an alternative embodiment with two rotatably mounted shaft members;

Figs. 4a and 4b are a side view and perspective side view respectively (shown schematically) of an alternative shaft member;

Fig. 5 is a schematic plan view of further alternative shaft members ;

Fig. 6 is a schematic plan view of shaft member embodiments applied to more than one cylinder;

Fig. 7 is a schematic perspective view of apparatus of a first embodiment;

Fig. 8 is a schematic perspective view of apparatus of a second embodiment; and

Fig. 9 is a schematic perspective view of apparatus of a third and fourth embodiment;

With reference to the drawings, and in particular Fig. 1, there is shown conventional apparatus of a four stroke internal combustion engine 10.

The conventional engine 10 comprises the known element of a cylinder 12 which houses a piston M which is ovably sealed therein. The piston M is attached to a crankshaft P by a connecting rod N and rod bearing 0. The crankshaft P serves to convert the up and down motion of the piston M into rotational motion; which is utilised to turn wheels of a vehicle, propellers of a vessel or aircraft.

The conventional engine 10 also comprises the known element of a cylinder head D having an intake valve assembly A and an exhaust valve assembly J which are both intermittently actuated by a camshaft I. Both valve assemblies A, J have rocker arms 14, 18 with corresponding springs 16, 20, and conventional poppet valves 22, 24.

On the intake stroke of a four stroke engine 10, the intake valve assembly A is open to allow an ingress of air/fuel mixture into the cylinder 12 via an intake port C.

Meanwhile, the exhaust valve assembly J is closed. The piston M will retract drawing the air/fuel mixture into the cylinder 12.

The piston retracts by virtue of stored energy being transferred from a flywheel (not shown) to the piston M via the crankshaft P.

It should be understood that on all "non-power strokes", namely, retraction of the piston M on the intake stroke, compression of the air/fuel mixture, and exhausting of the combusted gases, the energy required to drive the piston M is transferred from the flywheel to the connected crankshaft P .

As the piston M bottoms out it will change direction and extend within the cylinder 12. Closure of the intake valve assembly A allows for the air/fuel mixture to be compressed within the cylinder 12; referred to as "compression stroke" .

Again, the exhaust valve assembly J is closed.

When fully compressed, a spark plug extending into the cylinder 12, ignites the compressed mixture to cause combustion.

Alternatively, in a diesel engine, the heat caused by compressing the air/fuel mixture alone will result in combustion.

The resultant combustion produces an excess of gases which force the piston M to retract within the cylinder 12.

The exhaust valve assembly J is opened as the piston M bottoms out to allow an egress of the combusted gases through an exhaust port ; referred to as "exhaust stroke" .

As the piston M returns to an extended position, the exhaust valve assembly J is closed, whereas the intake valve assembly A is open to start the cycle again and allow in ingress of air/fuel mixture.

10

It will be realised that the timing of the opening and closing of the valve assemblies A, J will have a large bearing on the performance of the engine 10. If either of the valve assemblies A, J are open on the compression stroke, then the air/fuel mixture will not be fully compressed resulting in poor performance of the engine 10.

Lobes or cams 26 located on the camshaft I are designed to intermittently open and close each of the valve assemblies A, J as and when required.

It will be realised however, that (fixed) cams 26 of a particular design operate optimally for a given range of speeds only.

The rocker arms 14, 18 act against the corresponding valves 22, 24 and valve return springs 16, 20. The valves 22, 24 are fired in one direction, only then to stop at the extent of their travel, and be sent flying in the opposite direction. This happens many times a minute which wastefully drains power from the engine 10 and can cause noise, vibration and harshness.

In a first embodiment of the present invention, as illustrated in Figs. 2a-d and Fig. 7, there is provided apparatus 100 in the form of a cylinder head assembly comprising a cylinder head D adapted with a valve assembly replacement shaft member 110 rotatably mounted. The shaft member 110 is of the form of a cylindrical rod with a recess 112 removed around a portion of the circumference of the shaft member 110 and along that part of its length which is presented to (above) the cylinder 12.

It is to be understood that the shaft member 110 and recess 112 are presented facing the cylinder irrespective of the cylinder's orientation; for example, it may be a horizontal engine, in which case the recess 112 is presented adjacently facing the cylinder 12.

The shaft member 110 is rotatably mounted in the cylinder head D.

The shaft member 110 is parallel with, and is co- operatively driven by, the crankshaft P by virtue of connecting means (not shown) in the form of a belt or gearing 114.

The recess 112 serves to allow an ingress or egress of air/fuel mixture or exhaust gases to and from the cylinder 12 upon rotation of the shaft member 110.

The depth and length of the recess 112 presented to (above) the cylinder 12 can be of any design and dimensions to allow optimum ingress and/or egress of air/fuel mixture and/or combusted gases to and from the cylinder 12; for example, the recess 112 may be of uniform depth and length or may have varying PCl /ϋB ^UJ / U U 0 I

12

depths or lengths, or the recess 112 may also be of the form of a helix, etc.

In operation, as shown in Fig. 2a and Fig. 7, there is an inlet of air from an inlet manifold 116 which is coupled to a carburettor/fuel injector (not shown) to form an air/fuel mixture.

The shaft member 110 is presented such that the recess 112 faces the intake port C and the cylinder 12 to allow an ingress of air/fuel mixture.

Rotation of the crankshaft P, initially caused by a starter motor (not shown) then subsequently by the transfer of energy from the flywheel, causes contra- rotation of the shaft member 110 by virtue of contra-connecting means (not shown) being connected to the crankshaft P and gearing 114 on the shaft member 110.

Rotation of the crankshaft P will cause the piston M to retract, drawing-in the air/fuel mixture through the inlet port C, into the cylinder 12.

Meanwhile, as the piston M is retracted by virtue of the rotating crankshaft P, the recess 112 of the shaft member 110 will contra-rotate in unison.

As the piston M bottoms out, the rotating shaft member 110 and recess 112 face the intake port C and the cylinder head D. Thus preventing any ingress or ΓL I / UB UUJ / u u 0 b 1

13

leakage of air/fuel mixture on the compression stroke, as shown in Fig. 2b.

On the compression stroke, the piston M is extended to compress the air/fuel mixture as the crankshaft P and interconnected shaft member 110 similarly rotate, as shown in Fig. 2c.

The recess 112 faces the cylinder head D and the exhaust port .

A spark plug K (not shown for convenience in Figs . 2a-d) , ignites the compressed air/fuel mixture in the cylinder 12.

Alternatively, in a diesel engine, the heat caused by compressing the air/fuel mixture alone will result in combusted gases .

The resultant combustion causes the piston M to be fired to a retracted position causing the crankshaft P and shaft member 110 to rotate.

The recess 112 meanwhile, will rotate facing both the exhaust port L and cylinder 12 to allow the piston to extend exhausting the combusted gases out through the recess 112 into the exhaust port L.

Upon exhaustion of the combusted gases, rotation of the crankshaft P will cause the recess 112 to rotate and face the cylinder 12 and inlet port C to allow the cycle to begin again. As the rotation of the crankshaft P and shaft member 112 are rotating opposite to one another, this will have a balancing effect which may reduce noise and vibration of the engine 10.

To prevent any unburnt fuel being expelled with the exhaust gases, fuel injectors (not shown) may be used to control the flow of fuel into the separate branches of the inlet manifold. The fuel injectors would be closed before the recess 112 closes, such that no unburnt fuel would be exhausted by being trapped in the recess 112 as the shaft 110 rotates. Alternatively, the fuel injectors may directly inject the fuel into the cylinder 12. Hence, only air would therefore pass through the manifold, via the recess 112 into the cylinder 12, avoiding unburnt fuel being trapped in the recess 112, and being exhausted as the shaft 110 rotates.

In a second embodiment of the present invention, as shown in Figs. 3a-d and Fig. 8, there is provided apparatus 200 in the form of a cylinder head assembly comprising a cylinder head D having two valve assembly replacement shaft members, namely, an intake shaft member 210 and an exhaust shaft member 212 which are rotatably mounted.

The shaft members 210, 212 are of the form as described above with recesses 214, 216 as also described above. The shaft members 210, 212 are rotatably mounted in the cylinder head D as before.

The shaft members 210, 212 are parallel with, and are co-operatively driven by, the crankshaft P by connecting means (not shown) coupled to gearing 114.

Alternatively, the shaft may be belt driven from the crankshaft P .

The recesses 214, 216 are as described above, and serve to allow an ingress of air/fuel mixture and an egress of combusted gases respectively, into the cylinder 12 upon rotation of the crankshaft P and shaft members 210, 212.

The depth and length of the recesses 214, 216 presented to (above) the cylinder 12 can be of any design and dimensions to allow optimum ingress and egress of air/fuel mixture and combusted gases to and from the cylinder 12; for example, the recesses 214, 216 may be of uniform depth and length or may have varying depths or lengths, or they may be of the form of a helix, etc.

In operation, as shown in Fig. 3a, the intake shaft member 210 is rotated, by the crankshaft P, to face the intake port C and the cylinder 12 to allow an ingress of air/fuel mixture.

Meanwhile, the exhaust shaft member 212 faces the exhaust port and cylinder head D thus preventing air/fuel mixture to leave the cylinder 12 or air to enter therein.

As the air/fuel mixture enters the cylinder 12 from the intake port C, the crankshaft P rotates causing the piston M to retract, causing the shaft members 210, 212 and hence recesses 214, 216, to rotate in unison by virtue of them being interconnected by connecting means to the gearing 114.

As the piston M begins to extend, the recess 214 rotates to face the cylinder 12 and cylinder head D. Thus preventing any ingress or leakage of air/fuel mixture from the cylinder 12 on the compression stroke, as shown in Fig. 3b.

Meanwhile, the exhaust shaft member 212 will likewise have rotated with the recess 216 now facing the cylinder head D completely. Thus preventing an ingress of air or an egress of air/fuel mixture.

On the compression stroke, the crankshaft P rotates causing the piston to extend compressing the air/fuel mixture. The interconnected shaft members 210, 212 and recesses 214, 216 similarly rotate.

As the piston M becomes fully extended on the compression stroke, the intake recess 214 at this point completely faces the cylinder head D and is thus closed off preventing any egress of compressed air/fuel mixture, as shown in Fig. 3c. A spark plug (not shown for convenience in Figs. 3a-d) , ignites the compressed air/fuel mixture in the cylinder 12.

The resultant combustion causes the piston to be fired to a retracted position causing the crankshaft P and shaft members 210, 212 to rotate.

The intake recess 214 will rotate facing both the cylinder head D and the intake port C.

The exhaust recess 216 will rotate facing the cylinder 12 and exhaust port L to allow an egress of combusted gases, as shown in Fig. 3d.

The piston M then extends exhausting the combusted gases out through the recess 216 into the exhaust port L by virtue of the rotating crankshaft.

Meanwhile, rotation of the crankshaft P will cause the intake recess 214 to rotate and face the inlet port C and the cylinder 12 to allow the cycle to begin again.

The exhaust recess 216 will likewise rotate facing the exhaust port L and the cylinder head D, as shown in Fig. 3a. In a third embodiment of the present invention there is provided apparatus 400, as shown in Figs. 5 and 9, having apparatus 200 as previously described in the second embodiment, wherein the intake shaft member 210 and the exhaust shaft member 212 are of the form of a hollow cylindrical intake shaft member 410 and a hollow cylindrical exhaust shaft member 412.

In this way, it should be realised that the heavy intake manifold (not shown) and outlet manifold 116, can be replaced by single, less heavy and complicated manifolds 418, 420, which allow the ingress of air/fuel mixture and egress of combusted gases through the hollow shaft members 410, 412.

The shaft members 410, 412 are presented to (above) the cylinder 12 to allow an ingress of air/fuel mixture thereto through aperture 414, and an egress of exhaust gases therefrom through aperture 416.

In this third embodiment, the air/fuel mixture passes through the hollow intake shaft member 410 and exits through the aperture 414 into the cylinder 12.

After the compression and combustion strokes, the exhaust gases exit the cylinder 12 through the aperture 416 and leave via the hollow exhaust shaft member 412.

The shaft members 410, 412 are connected to the crankshaft P by connection means (not shown) coupled to gearing 114.

Alternatively, the shaft members 410, 412 may be coupled to the crankshaf P by a belt .

It is conceived that rotation of the shaft members 410, 412 although specifically described as being coupled to and controlled by the crankshaft P, may be independently and controllably adjustable.

Furthermore, both shaft members 410, 412 may be driven independently of the crankshaft P and of each other.

In a fourth embodiment of the present invention, there is provided apparatus 200 wherein the shaft members 210, 212 are of the form of hollow shaft members 300, as shown in Figs. 4a and 4b. Each shaft member 300 has an inner hollow cylindrical tube 310, rotatably mounted within an outer hollow cylindrical tube 312, also rotatably mounted.

The tubes 310, 312 have apertures 314, 316 which correspondingly serve to allow an ingress of air/fuel mixture and egress of exhaust gases to pass therethrough.

The apertures 314, 316, when appropriately aligned, form a passage 326. The area of the passage 326 is adjusted and controlled by the speed of rotation of the tubes 310, 312 relative to one another.

Rotation of the tubes 310, 312 is controlled by gears 318, 320 located around the circumference of respective cylindrical buttressed ends 322, 324 of the tubes 310, 312.

Rotation of the tubes 310, 312 may be coupled to the crankshaft P with independently controllable/ adjustable means for varying the speed of rotation of the tubes 310, 312.

Alternatively, both tubes 310, 312 may be driven independently of the crankshaft P and of each other, with controllable/ adjustable means for varying the speed of rotation of the tubes 310, 312.

It will be recognised that the tubes 310, 312 may also be belt driven or the like, independently of, or coupled to, the crankshaft P.

The speed of rotation of the inner tube 310, relative to the outer tube 312, is such that the area of the passage 326 maximises or restricts the rate of ingress or egress of air/fuel mixture or exhaust gases. In this way, the rotatable shaft members 300 offer a variable valve timing and variable valve size.

With reference to Figs. 4a and 4b, it is to be understood that both tubes 310, 312 do not move horizontally/longitudinally. The apertures 314, 316 share a common centre-line C/L, and are shown offset for illustrative purposes only.

Common to all embodiments and with regard to sealing of the various shaft members 110, 210, 212, 310, 312, 410, 412 of the present invention, these will be as tight a fit as possible cognisant of the expansion of materials of the individual, respective, components that will occur once the . engine reaches working temperature.

The shaft members 110, 210, 212, 310, 312, 410, 412 include gas tight seals (not shown) incorporated on the outside faces of bearing races (not shown) , of support bearings (not shown) , that will be spaced along the rotating shaft members 110, 210, 212, 310, 312, 410, 412 between the cylinder 12.

Gas tight paddles (not shown) are located within apertures (not shown) of the shaft members 110, 210, 212, 310, 312, 410, 412, at either side of the respective recesses and apertures 112, 214, 216, 314, 316, 414, 416, of the axis of rotation.

Springs (not shown) are located at the base of the paddles within the apertures. These serve to force the paddles outwards towards and against the inside surfaces of the cylinder head D, within which the shaft members rotate, so ensuring a gas tight seal in a similar way to the WANKEL rotary engine. Common to all embodiments, it should be realised that the shaft members 110, 210, 212, 310, 312, 410, 412 may be of the form of extended or adapted shaft members 510, 512, rotatably mounted, with a plurality of recesses or apertures 514, 516 corresponding to the number of cylinders 12, as shown in Fig. 6.

Furthermore, the recesses 112, 214, 216 and apertures 314, 316, 414, 416 of the corresponding shaft members 110, 210, 212, 310, 312, 410, 412 can be as wide as the diameter of the cylinder 12 above which they sit. This means that a far greater area will be available for an ingress of air/fuel mixture or egress of exhausted gases, than might be associated with conventional valves.

The hollow intake shaft members (310, 312,) 410, 510 may form an integral part of an inlet system (not shown), or may feed into, much simplified, single branch manifolds 418, at the respective open end of the shaft members (310, 312) , 410, 510 at an end of the cylinder head D.

The hollow exhaust shaft members (310, 312), 412, 512 may form an integral part of an exhaust system (not shown) , or may feed into, much simplified, single branch manifolds 420, at respective open ends of the shaft members (310, 312), 412, 512 at an end of the cylinder head D.

In this way, the air/fuel mixture and exhaust gases would not be required to travel via individual openings within the cylinder head D to individual, heavy, complicated, and expensive multiple branches of intake/exhaust manifolds, feeding the intake/exhaust ports C, L to each cylinder 12.

The present invention as described, has a reduced size compared to a conventional engine 10 and offers greater flexibility to the location, installation, and utilisation of internal combustion engines.

The simpler design will have favourable implications as to complexity, overall size of the engine, efficiency, noise and reliability, finance of raw materials, manufacturing, etc.

For the sake of clarity, it should be understood that fuel injectors/carburettors, and the spark plug, have been omitted from Figs. 2a-d and 3a-d but may be part of the cylinder head assembly.

The foregoing description refers to the induction of air/fuel mixture, as will be the case where a carburettor or manifold fuel injection is used. It will be appreciated that the invention may equally be applied to direct fuel injection engines, in which case the induction will be of charge air without fuel.

Modifications and improvements may be made to the above without departing from the scope of the present invention. CLAIMS

1. A cylinder head assembly comprising a cylinder head having an inlet passage and an outlet passage for communication, in use, with a cylinder, and at least one rotatably mounted shaft member interposed between the inlet and outlet passages and the cylinder, the shaft member (s) having passage means to allow an ingress of air mixture from the inlet passage to the cylinder at a first desired rotational position, and to allow an egress of combusted gases from the cylinder through the outlet passage at a second desired rotational position and to prevent the air or combusted gases from entering or exiting the cylinder at a third desired rotational position.

2. A cylinder head assembly according to claim 1, in which there are two shaft members, one cooperating with the inlet passage and one with the outlet passage.

3. A cylinder head assembly as claimed in claim 2, in which the shaft members are coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said shaft members.

4. A cylinder head assembly as claimed in claim 2, in which the shaft members are driven independently of the crankshaft, and of each other, with means for individually controlling or adjusting the speed of rotation of said shaft members.

5. A cylinder head assembly according to any preceding claim, in which the shaft member or each shaft member is substantially solid.

6. A cylinder head assembly according to claim 5, in which the passage means comprises a recess in the shaft member or a respective recess in each of the shaft members.

7. A cylinder head assembly according to claim 2, in which each shaft member is hollow; each shaft member having at least one aperture located around a portion of its circumference, wherein the inlet shaft member allows an ingress of air/fuel mixture from the inlet shaft member to enter said cylinder when the aperture in the inlet shaft is presented to the cylinder, and the outlet shaft member allows an egress of combusted gases to exit the cylinder when the aperture in the outlet shaft member is presented to the cylinder.

8. A cylinder head assembly according to claim 7, in which each shaft member is provided with an inner hollow tube member rotatably mounted within said shaft member; each inner tube member having at least one aperture located around a portion of its circumference; rotation of said inner tube member within the respective hollow shaft members providing a variable size effective aperture, which allows a variable ingress of combustion air to enter said cylinder through the effective aperture in the inlet shaft member, and allows a variable egress of combusted gases from the cylinder to exit through the effective aperture in the outlet shaft member.

9. A cylinder head assembly according to claim 8, in which the speed of rotation of the inner and outer tube members are such that the effective aperture maximises or restricts the rate of ingress of air, or egress of exhaust gases, through the respective inner tube members .

10. A cylinder head assembly as claimed in claim 8 or claim.9, in which the inner tube members are coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said tube members .

11. A cylinder head assembly as claimed in claim 8 or claim 9, in which the tube members are driven independently of the crankshaft, and of each other, with means for individually controlling or adjusting the speed of rotation of said tube members.

12. A cylinder head assembly according to any preceding claim, in which the shaft member (s) extend over a number of cylinders, the shaft member (s) having a corresponding number of passage means. 13. A cylinder head assembly according to any preceding claim, in which the shaft member (s) have gas tight seal assemblies.

14. A method of allowing an ingress and egress of combustion air and combusted gases from a cylinder comprising the steps of: presenting a passage means within a shaft member to an inlet passage; retracting of a piston within a cylinder to allow an induction of air from the inlet passage through said passage means into the cylinder; rotating the shaft member to prevent any leakage of air upon a compression of the air in the cylinder by the piston; combusting air/fuel mixture in the cylinder to cause said piston to retract; extending the piston in the cylinder; presenting passage means to the cylinder and an outlet passage to allow an egress of combusted gases; and repeating the above steps.

15. A method according to claim 14, in which the same passage means is used for induction and egress.

16. A method according to claim 14, in which the passage means is formed by an aperture in at least one hollow shaft, and the method further includes the step of varying the effective size of the aperture to restrict or maximise the amount of fluid flow through the aperture. 1/6

3/6

4/6

Fig.4b 5/6

Fig. 5

Fig. 6 6/6

CD

ForrnPCT O/101 (first sheet) (March 2001; reprint January 2003) See Notes to the rεq estform

Form PCT RCV101 (second sheet) (January 2003) See Nσles to the request form Sheet No. .. .3.

Box No. VI PRIORITY CLAIM

The priority of the following earlier appHcatfon{s) is hereby claimed:

Filing date Number Where earlier application is; of earlier application of earlier application national application:

(d y/monthfyear) country or Member regional application:* international application:

Λ"wτn regional Office receiving Office item^_{Augusl 2002}

0218674.0 United Kingdom

item (2)

item (3)

item (4)

item (5)

| | Further priority claims are indicated in Hie Supplemental Box.

The receiving Office is requested to prepare and transmit to the International Bureau a certified copy ofthe earlier application.^) (only if the earlier application was filed with the Office which for ϋie purposes of this international application is the receiving Office) identified above as:

BB all items π ta* ϋ ^ (2 D ta- P) □ -** <'*) 0 ^(5⁾ Q sϊ_ppierantal Box

* Where the earlier application is em ARIPO application, indicate at least one country party to the Paris Convention for the Protection of Industrial Property or one Member of the WoridTrade Organization for which that earlier applicators vms filed (Rule 4.ΪO(b)(ii)): . , , ,

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The following declarations are contained in Boxes Nos. VIE (i) to (v) (mark the applicable Number of check-boxes below and indicate in the right column the number of each type ofdedarati&rt) declarations

□ Box No. VIA (i) Declaration as to the identity ofthe inventor

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□ Box No. Vm (iii) Declaration as to the applicant's entitlement, as at the international filing d te^ to claim the priority o the earlier application Q Box No. VIII (ϊv) Declaration of inventorship (only for the purposes ofthe designation ofthe United States of America)

□ Box No. Vm (v) Declaration as to non-prejudicial disclosures or exceptions to lack of novelty

Form PCT/RO/jOl (third sheet) (July 2002; reprint January 2003) See Notes to the request form Sheet No.

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This international application contains: This international application is accompanied by the following Number

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Form T fROn 01 Oast sheet) (January 2003) See Notes to the request form

1 Improvements in or Relating- fco Internal Combust σn

2 Engines 3

4 This invention relates to improvemen s in or

5 relating to internal combustion engines, and in

6 particular,, but not exclusively, to improvements

7 relating to replacement apparatus for the intake and

8 exhaust valves of internal combustion engines. 9

10 Conventional four stroke internal combustion engines^'

11 involve a four stage cycle. Firstly, there is an

12 intake of air/fuel mixture into a cylinder; known as

13 ^tt ntake stroke". Secondly, a piston within the

14 cylinder compresses the ai /fuel mixture; known as

15 "compression stroke" . Thirdly, the compressed

16 air/fuel mixture is ignited in the cylinder causing

17 combustion;, known as "combustion stroke". And •

18 lastly, the combusted gases are exhausted; known as

19. "eshaust stroke" . 20

21 A four stroke internal combustion engine comprises

22 an intake valve to allow an ingress of air/fuel mixture into a cylinder, and an exhaust valve, to allow an egress of exhausted gases after combustion of the air/fuel mixture.

The timing of the opening and closing of the valves is vital to an engines performance,

To allow the piston to draw-in the fuel/air mixture (or air alone in the case of a direct injection engine) , the intake valve needs to open as the piston moves from, an extended position to a retracted position on the intake stroke, .

As the camshaft rotates, the shape of the cam which actuates the rocker arm, determines the timing of the opening and closing of the intake and exhaust valves.

According to one aspect of the present invention, a cylinder head assembly comprises a cylinder head having an inlet passage and an outlet passage for communication, in use, with a cylinder, and at least one. rotatably mounted shaft member interposed between the inlet and outlet passages and the cylinder, the shaft membe (s) having passage means to allow an ingress of air mixture from the inlet passage to the cylinder at a first desired rotational position, and to allow an egress of combusted gases from the cylinder through the outlet passage at a second desired rotational position and to prevent the air or combusted gases from entering or exiting the cylinder at a third desired rotational position.

Preferably each shaft member is provided with an inner hollow tube member rotatably mounted within said shaft member; each inner tube member having at least one aperture located around a portion of its circumference; rotation of said inner tube member within the respective hollow shaft members providing a variable size effective aperture, which allows a variable ingress of combustion air to enter said cylinder through the effective aperture in the inlet shaft member, and allows a variable egress of combusted gases from the- cylinder to exit through the effective aperture in the outlet shaft member. Preferably also, the speed of rotation of the inner and outer tube members are such that the effective aperture maximises or restricts the rate of ingress of air, or egress of exhaust gases, through the respective inner tube members.

The inner tube members may be coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said tube members. Alternatively, the tube members may be driven independently of the cranksha t , and of each other, with means for individually controlling or adjusting the speed of rotation of said tube members.

, Typically, the cylinder head assembly will form part . of a multi-cylinder engine with the shaft member (s) extending over a number of cylinders, the shaft member (s) having a corresponding number of passage means .

The shaft member (s) suitably have gas tight seal asse blies .

From another aspect, the invention provides a method of allowing an ingress and egress of combustion air - and combusted gases from a cylinder comprising the - steps of Ϊ presenting a passage means within a shaf member to an inlet passage; retracting of a piston within a cylinder to allow an induction of air from the inlet passage through said passage means into the cylinder,- rotating the shaft member to prevent any leakage of air upon a compression of the air in the cylinder by the piston; combusting air/fuel mixture in the cylinder to cause said piston to retract; extending the piston in the cylinder; presenting passage means to the cylinder and an outlet passage to allow an egress of combusted gases; and repeating the above steps.

In one form of the method, the same passage means is used for induction and egress .

Embodiments of the present invention will now be described, by way of example only, with reference to the accompanying drawings in which : -

Fig. 1 is a schematic front sectional view of a conventional- four stroke internal combustion engine;

Figs. 2a-d are schematic front sectional views illustrating the workings of a single rotatably mounted shaft member of the present invention; Figs. 3a-d are schematic front sectional views illustrating the workings of an alternative embodiment with two rotatably mounted shaft members ;

Figs. 4a and 4b are a side view and perspective side view respectively {shown schematically) of an alternative shaft member;

Fig, 5 is a schematic plan view o£ further alternative shaft members;

Fig. 7 is a schematic perspective view of apparatus αf a first embodiment;

Fig. 8 is a schematic perspective view of apparatus of a second embodiment; and

Fig. 9 is a schematic perspective view- of apparatus of a third and fourth embodiment;

The conventional engine 10 comprises the known element of a cylinder 12 which houses a piston M which is movably sealed therein. 8 The piston H is attached to a crankshaft P by a connecting rod N and rod bearing 0. The crankshaft P serves to convert the up and down motion of the piston into rotational motion,^* which is utilised to turn wheels of a vehicle, propellers of a vessel or aircraft .

The conventional engine 10 also comprises the known element of a cylinder head D having an intake valve assembly A and an exhaust valve assembly J which are both intermittently actuated by a camshaft I. Both valve assemblies A, <T have rocker arms 14, 18 with corresponding springs 15, 20, and conventional poppet valves 22, 24.

The piston K retracts by virtue of stored energy being transferred from a flywheel (not shown) to the piston M via the crankshaft P.

It should be understood that on all "non-power strokes", namely, retraction of^' the piston M on the intake stroke, compression of the air/fuel mixture, and exhausting of the combusted gases, the energy required to drive the piston M is transferred from the flywheel to the connected crankshaft P.

As the piston M bottoms out it will change direction and extend within the cylinder 12. Closure of the intake valve assembly A allows for the air/fuel mixture to be compressed within the cylinder 12; referred to as compression stroke" .

Again, the exhaust valve assembly J is closed.

The exhaust valve assembly J is opened as the piston M bottoms out to allow an egress of the combusted gases through an exhaust port L; referred to as '"exhaust stroke" .

As the piston M returns to an extended position, the exhaust valve assembly J is closed, whereas the intake valve assembly A is open to start the cycle again and allow in ingress of air/fuel mixture. 10 It will be realised that the timing of the opening and closing of the valve assemblies A, J will ^• have a large bearing on the performance of the engine 10. If either of the valve assemblies A, J are open on the compression stroke, then the air/fuel mixture ^• will not be fully compressed resulting in poor performance of the engine 10.

It will be realised however, that (fixed) cams 25 of a particular design operate optimally for a given range of speeds only.

In a first embodiment of the present invention, as illustrated in Figs. 2a-d and Fig. 7, there is provided apparatus 100 in the form of a cylinder head assembly comprising a cylinder head D adapted with a valve assembly replacement shaft member 110 rotatably mounted. 11 The shaft member 110 is of the form of a cylindrical rod with a recess 112 removed around a portion of the circumference of the shaft member 110 and along that part of its length which is presented to (above) the cylinder 12.

The shaft member 110 is rotatably mounted in the cylinder head D.

The depth and length of the recess 112 presented to (above) the cylinder 12 can be of any design and dimensions to allow optimum ingress and/or egress of air/fuel mixture and/or combusted gases to and from the cylinder 12; for example, the recess 112 may be of uniform depth and length or may have varying 12 depths or lengths, or the recess 112 may also be of the form of a helix, etc.

In operation, as shown in Fig. 2a and Fig. 7, there is an inlet of air from an inlet manifold 115 which is coupled to a carburettor/fuel injector (not shown) to form an air/fuel mixture.

The shaft member 110 is presented such that the recess 112 faces the intake port C and the cylinder 12 to allow an ingress of air/ uel mixture.

Rotation of the crankshaft P, initially caused by a starter motor (not shown) then subsequently by the transfer of energy from the flywheel, causes contra- rotation of the shaft member 110 by virtue of contr -connecting means (not shown) being connected to the crankshaf P and gearing 114 on the shaft member 110.

Meanwhile, as the piston M is retracted by virtue of the rotating crankshaft P, the recess 112 of the shaft member 110 will contra- ota e in unison.

As the piston V bottoms out, the rotating shaft member 110 and recess 112 face the intake port C and the cylinder head D. Thus preventing any ingress or 13 leakage of air/fuel mixture on the compression stroke, as shown in Fi - 2b. . On the compression stroke, the piston te is extended to compress the air/fuel mixture as the crankshaft P and interconnected shaft member 110 similarly rotate, as shown in Fig. 2c.

The recess 112 faces the cylinder head D and the exhaust port .

A spark plug K (not shown for convenience in Figs. 2a-d) , ignites the compressed air/fuel mixture in the cylinder 12.

Alternatively, in a diesel engine, the heat caused by compressing the air/fuel mixture alone will result in combusted gases.

The resultant combustion causes the piston to be fired to a retracted position causing the crankshaft P and shaft member 110 to rotate.

The recess 112 meanwhile, will rotate facing both the exhaust port and cylinder 12 to allow the piston M to extend exhausting the combusted gases out through the recess 112 -into the exhaust port L. - Upon exhaustion of the combusted gases, rotation of the crankshaft P will cause the recess 112 to rotate and face the cylinder 12 and inlet port C to allow the cycle to begin again. 14 As the rotation of the crankshaft P and shaft member 112 are rotating opposite to one another, this will have a balancing effect which may reduce noise and vibration of the engine 10.

The shaft members 210, 212 are of the form as described above with recesses 214, 216 as also described above. 15 The shaft members 210, 212 are rotatably mounted in the cylinder head D as before.

Alternatively, the shaft may be belt driven from the crankshaft P.

The recesses 214, 216 are as described above, and serve to allow an ingress αf air/fuel mixture and an egress of combusted gases respectively, into the cylinder 12 upon rotation of the crankshaft P and shaft members 210, 212.

The depth and length Of the recesses 214, 216 presented to (above) the cylinder 12 can be of any design and dimensions to allow optimum ingress and egress of air/fuel mixture and combusted gases to and from the cylinder 12; for example, the recesses 214, 215 may be of uniform depth and length or may have varying depths or lengths, or they may be of the form of a helix, etc .

In operation, as shown in Fig. 3a, the intake shaft member 210 is rotated, by the -crankshaf P, to face the intake, port C and the cylinder 12 to allow an ingress of air/ uel mixture.

Meanwhile, the exhaust shaft member 212 faces the exhaust port L and cylinder head D thus preventing 16 air/fuel mixture to leave the cylinder 12 or air to enter therein.

As the air/fuel mixture enters the cylinder 12 from the intake port C, the crankshaft P rotates causing the piston M to retract, causing the shaft members 210, 212 and hence recesses 214, 216, to rotate in unison by virtue of them being interconnected y connecting means to the gearing 11 .

On the compression stroke, the crankshaft P rotates causing the piston M to extend compressing the air/fuel mixture. The interconnected shaft members 210, 212 and recesses 214, 216 similarly rotate.

As the piston M becomes fully extended on the compression stroke, the intake recess 214 at this point completely faces the cylinder head D and is thus closed off preventing any egress of compressed air/fuel mixture, as shown in Fig. 3c. 17 A spark plug K (not show for convenience in Figs. 3a-d) , ignites the compressed air/fuel mixture in the cylinder 12.

The resultant combustion causes the piston M to be fired to a retracted position causing the crankshaft P and shaft members 210, 212 to rotate.

The exhaust recess 216 will rotate facing the cylinder 12 and exhaust port It to allow an egress of combusted gases, as shown in Fig. 3d.

The piston te then extends exhausting the combusted gases out through the recess 216 into the exhaust port I. by virtue of the rotating crankshaft.

The exhaust recess 216 will likewise rotate facing the exhaust port L and the cylinder head D, as shown in Fig. 3a. 18 In a third embodiment of the present invention there is provided apparatus 400, as shown in Figs. 5 and 9, having apparatus 200 as previously described in the second embodiment, wherein the intake shaft member 210 and the exhaust shaft member 212 are of the form of a hollow cylindrical intake shaft member 410 and a hollow cylindrical exhaust shaft member 412.

In this way, it should be realised that the heavy intake manifold (not shown) and outlet manifold 115, can be replaced by single, less heavy and complicated manifolds 418, 420, which allow the ingress of air/fuel mixture and egress of combusted gases through the hollow shaft members 410, 412.

The shaft members 410, 412 are connected to the 19 crankshaft P by connection means (not shown) coupled to gearing 114.

Alternatively, the shaft members 410, 412 may be coupled to the crankshaft P by a belt.

It is conceived that rotation of the shaft members 410, 412 although specifically described as being coupled to and controlled by the crankshaft P, may be independently and controllably adjustable,

The tubes 310, 312 have apertures 314, 316 which correspondingly serve to allow an ingress of - air/fuel mixture and egress of exhaust gases to pass ^" therethrough.

The apertures 314, 316, when appropriately aligned, form a passage 326. 20 The area of the passage 326 is adjusted and controlled by the speed of rotation of the tubes 310, 312 relative to one another.

It will be recognised that the tubes 310, 312 may also be belt driven or the like, independently of, or coupled to, the crankshaft .

The speed of rotation of the inner tube 310, relative to the outer tube 312, is such that the area of the passage 326 maximises or restricts the rate of ingress or egress of air/fuel mixture or • exhaust gases. In this way, the rotatable shaft members 300 offer a variable valve timing and variable valve size.

With reference to Figs. 4a and 4b, it is to be 21 understood that both tubes 310, 312 do not move horizontally/longitudinally. The apertures 314, 316 share a common centre-line C/L, and are shown offset for illustrative purposes only.

Common to all embodiments and with regard to sealing of the various shaft members 110, 210, 212, 310, 312, 410, 412- of the present invention, these will be as tight a fit as possible cognisant of the expansion of materials of the individual, respective, components that will occur once the engine reaches working temperature.

The shaft members 110, 210, 212, 310, 312, 410, 412 include gas tight seals (not shown) incorporated on the outside faces of bearing races (not shown) , of support bearings (not shown) , that will be spaced along the rotating shaft members 110, 210, 212, 310, 312, 410, 412 between the cylinder 12,

Gas tight paddles (not shown) are located within , apertures (not shown) of the shaft members 110, 210, 212, 310, 312, 410, 412, at either side of the respective recesses and apertures 112, 214, 216, 314, 316, 414, 416, of the axis of rotation.

Springs (not shown) are located at the base of the paddles within the apertures. These serve to force the paddles outwards towards and against -the inside surfaces of the cylinder head D, within which the shaft members rotate, so ensuring a gas tight seal in a similar way to the WANKE rotary engine. 22

Common to all embodiments, it should be realised that the shaft members 110, 210, 212, 310, 312, 410, 412 may be of the form of extended or adapted shaft members 510, 512, rotatably mounted, with a plurality of recesses or apertures 514, 516 corresponding to the number of cylinders 12, as shown in Fig. S.

Furthermore, the recesses 112, 214, 216 and apertures 314, 316, 414, 416 of the corresponding shaft members 110, 210, 212, 310, 312, 410, 412 can be as wide as the diameter of the- cylinder 12 above which they sit. This means that a far greater area will be available for an ingress of air/fuel mixture or egress of exhausted gases, than might be associated with conventional valves.

The hollow intake shaft members (310, 312,) 410, 510 may form an integral part of an inlet system (not shown) , or may eed into, much simpli ied, single branch manifolds 418, at the respective open end of the shaft members (310, 312), 410, ^' 510 at an end of the cylinder head D.

In this way, the air/fuel mixture and exhaust gases 23 would not be required to travel via individual openings within the cylinder head TJ to individual, heavy, complicated, and expensive multiple branches of intake/exhaust manifolds, feeding the intake/exhaust ports C, to each cylinder 12.

The foregoing description refers to the induction of air/fuel mixture, as will be the case where a carburettor or manifold fuel injection is used. It will be appreciated that _. he invention may equally be applied to direct fuel injection engines, in which case the induction will be of charge air without fuel, -

Modifications and improvements may be made to the above without departing from the scope of the present invention.

Claims

24

1. CLAIMS 2

3 1. A cylinder head assembly comprising a cylinder

4 head having an inlet passage and an outlet passage

5 for communication, in use, with a cylinder, and at least one rotatably mounted shaft member interposed between the inlet and outlet passages and the cylinder, the shaft member (s) having passage means to allow an ingress of ^' air mixture f om the inlet passage to the cylinder at a first desired rotational position, and to allow an egress of combusted gases from the cylinder through the outlet passage at a second desired rotational position and to prevent the air or combusted gases from entering or exiting the cylinder at a third desired rotational position.

3. A cylinder head assembly as claimed in claim 2, in which the shaft members are coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said shaft membe s .

4. A cylinder head assembly as claimed in claim 2, in which the shaft members are driven independently of the crankshaft, and of each other, with means for 25 individually controlling or adjusting the speed of rotation of said shaft members .

5.' A cylinder head assembly according to any preceding claim, in which the shaft member or each shaft member is substantially solid.

5. A cylinder head assembly according to claim 5, in which the passage means comprises a recess in the shaft member or a respective recess in each of the shaft members .

7. A cylinder head assembly according to claim 2, in which each shaft member ^' is hollow; each shaft member having at least one aperture located around a portion of its ci cumference, wherein the inlet shaft member allows an ingress of air/fuel mixture from the inlet shaft member to enter said cylinder when the aperture in the inlet shaft is presented to the cylinder, and the outlet shaft member allows an egress of combusted gases to exit the cylinder when the aperture in the outlet shaft member is presented to the cylinder.

8. A cylinder head assembly according to claim 7, in which each shaft member is provided with an inner hollow tube member rotatably mounted within said shaft member; each inner tube member having at least one aperture located around a portion of its circumference; rotation of said inner tube member within the respective hollow shaft members providing a variable size effective aperture, which allows a 26 variable ingress of combustion air to enter said cylinder through the effective aperture in the inlet shaft member, and allows a variable egress of combusted gases from the cylinder to exit through the effective aperture in the outlet shaft member.

9 - A cylinder head assembly according to claim 8 , in which the speed of rotation of the inner and outer tube members are such that the effective aperture maximises or restricts the rate of ingress of air, or egress of exhaust gases, through the respective inner tube members . .

10. A cylinder head assembly as claimed in claim 8 or claim 9, in which the inner tube members are coupled, in use, to a crankshaft with means for independently controlling or adjusting the speed of rotation of said tube members.

11. A cylinder head assembly as claimed in claim 8 or claim 9, in which the tube members are driven independently of the crankshaft, and of each other, with means for individually controlling or adjusting the speed of rotation of said tube members .

12. A cylinder head assembly according to any preceding claim, in whic -the shaft membe (s) extend over a number of cylinders, the shaft member (s) having a corresponding number of passage means . 27

1 . 13. A cylinder head assembly according to any

2 preceding claim, in which the shaft membe (s) have

3 gas tight seal assemblies . ^■ 4

5 14. A method of allowing an ingress and egress of

6 combustion air and combusted gases from a cylinder

7 comprising the steps of:

8 presenting a passage means within a shaft

9 member to an inlet passage;

10 retracting of a piston within a cylinder to

11 allow an induction of air from the inlet passage

12 through said passage means into the cylinder;

13 rotating the shaft member to prevent any

14 leakage of air upon a compression of the air in the

15 cylinder by the piston;

16 combusting air/fuel mixture in the cylinder to

17 cause said piston to retract;

18 extending the piston in the cylinder;

19 presenting passage means to the cylinder and

20 an outlet passage to allow an egress of combusted

21 gases; and

22 repeating the above steps. 23

24 15. A method according to claim 14, in which the

25 same passage means is used for induction and egress. 26

27 16. A method according to claim 14, in which^' he

28 passage means is formed by an aperture in at least

29 one hollow shaft, and the method further includes

30 the step of- varying the effective size of the

31 aperture to restrict or maximise the amount of fluid 32 flow through the aperture. 28

ABSTRACT (Fig . 2 )

Improvements in or Relating to Internal Combustion Engines