Free Piston Engine Generator

The present invention relates to a free piston engine generator and a method of manufacturing an engine generator. In particular, the present invention relates to a free piston engine generator which has a construction arranged to optimise the efficiency of the generator and to provide good control of piston position and piston motion by the generator.

Electrical power can be generated using a linear generator coupled to a free piston engine, wherein the linear movement of the reciprocating piston through one or more electrical coils generates magnetic flux change, as disclosed in US-B-7318506, for example. As the piston moves within the cylinder past the coils it interacts with a switched magnetic flux within the stator elements to generate electrical power that can be used for useful work or stored for later use.

However, the efficiency of such an electrical power generation system is highly dependent on the thickness of the cylinder wall and the proximity of the power generation electrical elements to the piston reciprocating within the engine cylinder.

According to the present invention there is provided a free -piston engine generator comprising an engine cylinder, a piston configured to move within the cylinder, a cylinder housing having a bore for receiving the engine cylinder and a plurality of magnetisable elements arranged within the cylinder housing to be adjacent the cylinder along at least a portion of its length.

In the present invention, the particular arrangement of the cylinder housing which allows the plurality of magnetisable elements to be positioned adjacent the cylinder optimises the efficiency of the free piston engine generator and provides good control of the piston position and piston motion by the generator.

Preferably, the cylinder housing has one or more recesses that permit the plurality of magnetisable elements to be positioned adjacent the cylinder. Preferably, the magnetisable elements are positioned in direct physical contact with the cylinder. Preferably, one or more of the magnetisable elements acts as a stator in the generator. Preferably, the cylinder is secured within the cylinder housing by an adhesive which provides thermal insulation between the cylinder and cylinder housing.

Preferably, the cylinder housing comprises a plurality of elements that are assembled coaxially onto the cylinder.

Preferably, the cylinder housing includes cooling means for cooling the cylinder.

Preferably, the cylinder has a wall thickness that is less than 5% of the cylinder's internal diameter, wherein the wall thickness is typically less than about 2mm.

Preferably, the piston comprises alternating laminated magnetisable core elements and non-magnetising spacer elements. Preferably, the intake means are located at a central position along the cylinder, which simplifies the engine arrangement and makes this arrangement more compact by allowing a common intake means to supply fluid into each combustion chamber.

Furthermore, by positioning the intake means at a position removed from the exhaust valve, scavenging of burned gases can be greatly improved by the unidirectional scavenging flow provided within each combustion chamber, which in turns results in improved efficiency, reduced unburned fuel hydrocarbons and lower costs.

Preferably, the intake means comprises both an air intake means and a fuel injection means, so that fuel injection into a combustion chamber may occur during the admission of intake charge air. The intake means may also comprise a plurality of air intake means and at least one fuel injection means. Providing the air intake means and fuel injection means together in the intake means allows both these features to share a common sliding port valve, each being recessed within the void behind this sliding port valve. This results in a simpler and hence cheaper construction.

Preferably, the air intake means comprises a sliding port valve and a secondary valve such as a solenoid poppet valve, barrel valve or other valve means arranged in series with the sliding port valve. The secondary valve can allow air into the chamber at any time when the sliding port valve is uncovered by the piston, which allows good control of the expansion ratio in response to a combustion event, independently of the position of the piston within the limits defined by the opening and closing positions of the sliding port valve .

Preferably, the fuel injection means comprises two injectors arranged one on each side of the air intake secondary valve to allow fuel to be injected directly into the respective chamber independently of whether the intake secondary valve is open or closed. The injectors are, ideally, piezo-injectors, which allow for precise, low cost electronic actuation and control of the fuel injection.

Preferably, the fuel injection means is configured to inject fuel immediately prior to the closing of the slide valve to ensure that fuel injected cannot be carried to and out of the exhaust port by scavenging air intake charge before the exhaust valve is closed, reducing hydrocarbon emissions.

Preferably, ignition means are provided in each chamber to initiate combustion of the compressed air-fuel mixture. Use of spark ignition fuels and their related operating cycles inherently generate less particulate emissions than compression ignition fuels and cycles.

Preferably, an exhaust means is provided in each combustion chamber to allow for burnt gases to be exhausted from the chamber following combustion.

Preferably, the exhaust means is a solenoid poppet valve provided in each combustion chamber, with the valves being coaxial with the cylinder such that the limiting area in the exhaust flow may approach 40% of the cylinder bore section area, reducing exhaust gas back-pressure during exhaust and scavenging.

Preferably, the cylinder has a length at least ten times greater than its diameter, which provides reduced variability of compression ratio in each cycle, resulting from a low rate of change of compression ratio with piston displacement error at top dead centre.

Preferably, the piston is configured to be elongate and the engine cylinder has a bore dimensioned such that a compression ratio of between 10:1 and 16:1 can be achieved. This is higher than can be achieved in a conventional spark ignition engine due to detonation (knocking). Preferably, the engine is a 'flex-fuel' engine operating on any mixture of gasoline, anhydrous ethanol and hydrous ethanol. The compression ratio may be optimised by the engine management system according to the particular ethanol/gasoline/water blend that is used.

Also, an expansion ratio greater than twice the compression ratio is obtained. A long expansion stroke allows more of the combustion energy to be transferred into the piston, and in addition allows more time for control (i.e. to react to measured piston speed variability).

Preferably, the intake means is positioned a suitable distance from the exhaust valve to ensure that a compression ratio of between 10:1 and 16:1 can be achieved.

According to the present invention there is also provided a method of manufacturing an engine generator, comprising providing a cylinder configured to accommodate at least one piston that is free to reciprocate within the cylinder, securing the cylinder within a cylinder housing that has a bore arranged to receive and provide structural support for the cylinder and arranging a plurality of magnetisable elements adjacent the cylinder such that, when the piston moves within the cylinder, it induces magnetic flux as it passes the plurality of magnetisable elements.

Preferably, one or more recesses in the cylinder housing are provided for receiving the plurality of magnetisable elements.

Preferably, one or more sections of the cylinder housing along the length of the cylinder are removed to expose one or more sections of the cylinder wall and the plurality of magnetisable elements are arranged within the recesses such that they are in direct physical contact with the cylinder wall.

According to the present invention there is also provided a method of manufacturing an engine, comprising providing a cylinder configured to accommodate at least one piston that is free to reciprocate within the cylinder, extruding a cylinder housing that is arranged to retain and provide structural support for the cylinder, and securing the cylinder within the cylinder housing such that the cylinder wall is reinforced by the structure of the cylinder housing.

Preferably, the plurality of magnetisable elements are arranged to provide load-bearing support to the cylinder. Preferably, the magnetisable elements are arranged to provide a force against the cylinder wall, for example they may be biased against the cylinder wall, or may be pre-loaded such that they apply a force against the cylinder wall when positioned adjacent it.

Preferably, the cylinder is secured within the cylinder housing using an adhesive material on the outside of the cylinder, wherein the adhesive material provides thermal insulation between the cylinder and cylinder housing.

Preferably, the cylinder housing is provided with cooling means for cooling the cylinder.

Preferably, the interior wall of the cylinder is coated with a friction- reducing material to reduce friction between the interior wall and a piston passing along it.

Preferably, the thickness of the cylinder wall is less than 5% of the cylinder's internal diameter, wherein the thickness of the cylinder wall is typically less than about 2mm.

According to the present invention there is also provided a vehicle having a free piston engine generator, as described above.

The construction of the engine generator of the present invention provides a number of important advantages over the typical free piston engine generator construction, in which two cylinder heads are affixed to two cylinders, with a separate electrical machine assembly located axially between the cylinders.

The cylinder housing is, preferably, formed by extrusion of a ductile material, such as aluminium alloy. Advantageously, the elongated construction permits the use of extrusion manufacturing technology to form the cylinder housing, rather than casting or extensive CNC machining technology used for conventional engines. Extrusion offers a faster manufacturing cycle time and higher tolerances before machining operations than casting, reducing finished part cost. Similarly, the cylinder may be formed from extrusion or other mature, low cost tube-forming manufacturing technologies. This construction therefore reduces the overall cost of the engine's cylinder assembly.

Furthermore, the contiguous form of the cylinder housing, which remains unbroken across the mid-section of the engine, ensures that both combustion chambers are coaxially aligned with high precision and provides a continuous bearing surface for the piston to travel across. This permits the piston to move over and past a centrally disposed intake, as described herein, whilst minimising the amount of wear to the inner surface of the cylinder during the operating life of the engine generator.

Although the cylinder housing is, preferably, a single extruded element, it could, alternatively, be formed by the coaxial assembly of a stack of dissimilar extruded elements onto a common cylinder. For example, two extrusions may be placed either side of an intake means, wherein the extrusions are assembled coaxially onto the cylinder.

Ideally, the wall of the cylinder housing extrusion should be sufficiently thick and/or strong that it is load-bearing to allow a much thinner cylinder wall to provide wear and sealing surfaces than would otherwise be required. The cylinder housing, ideally, has sections of material removed along the length of the cylinder to form one or more recesses that, ideally, expose the wall of the cylinder housed within. The recesses are formed through the cylinder housing, preferably extending from the outer surface inwards, such that the recesses open outwards. A plurality of magnetisable elements can be positioned in close proximity to the cylinder by arranging them in the one or more recesses, each magnetisable element preferably fixed directly to the wall of the cylinder, which separates them from the moving magnetic circuit elements of the piston.

The cylinder wall thickness dimension is an important determinant of the efficiency of the electrical machine, and should be as small as possible for high efficiency. By providing adequate load bearing strength using the cylinder housing and magnetisable stator elements, the cylinder wall is not required to bear cylinder fluid pressures and may be made considerably thinner subject to manufacturing, assembly and wear constraints.

The inner and outer surfaces of the cylinder provide substrates for wear and thermal coatings respectively. A thermal coating can be applied to the cylinder outer surface in the form of an adhesive material to provide a secure, insulating and load bearing bond between the cylinder and cylinder housing.

Furthermore, the arrangement of securing a cylinder within the cylinder housing provides the advantage that the mating surfaces of the respective components do not need to be finished to any particular standard, other than to allow the cylinder to be fitted within the cylinder housing. A free piston engine generator according to the present invention has a number of applications. For example, it may be integrated in a series-hybrid electric vehicle power train incorporating a transient electrical power store and one or more drive motors suitable for use as an automotive power source in small passenger vehicles, wherein electrical power generated by the free piston engine is accumulated in an electrical energy storage device on board the vehicle to be delivered to the vehicle drive motors on demand.

As a power source for a small passenger vehicle, the present invention preferably runs on a two-stroke engine cycle with spark ignition, with four cylinders being arranged in a planar configuration such that the engine might be transverse mounted beneath the front or rear seats of the vehicle, offering significantly more design flexibility to the layout of the passenger and storage spaces compared to a conventional internal combustion engine.

Each cylinder includes a free piston whose movement induces electrical power in a linear generator arranged around each cylinder, and whose movement is controllable by various means including the timing of valve and ignition events, and by modulation of the power drawn from or supplied to the piston on each stroke. The movement of pistons is synchronised such that the engine is fully balanced, wherein the piston, ideally, comprises alternating magnetisable elements and non-magnetising spacer elements.

Furthermore, each cylinder is charged by means of an intake mechanism that introduces fluid into the cylinder at a position distal from each end of the cylinder. The intake mechanism includes a poppet valve and sliding port valve in series such that the timing of the intake flow events may be controlled independently of the piston positions relative to the cylinders. Exhaust gas leaves the cylinders from exhaust valve mechanisms located at the end of each cylinder.

The geometry of the cylinder and disposition of the intake and exhaust mechanisms are such that the exhaust scavenging is completed with limited mixing between intake fluid and exhaust fluid. The combustion chamber geometry offers a low surface area-to-volume ratio, and low conductivity materials are used in the piston crown and cylinder head, so that minimal heat is rejected from the engine. The cylinder and piston geometry provides an expansion ratio which is at least two times the compression ratio.

The arrangement, and number, of cylinders used is, however, dependent on the application and the engine operating cycle can also be varied for different applications, for example: spark ignition internal combustion; homogeneous charge compression ignition internal combustion; and heterogeneous charge compression ignition. Some of the features of the present invention may also be embodied with an external combustion cycle. Examples of external combustion cycle embodiments include use of the present invention as a gas expander for fluid from a gas turbine exhaust, an organic rankine cycle or a Stirling cycle. In a Stirling engine, heat from an external combustion source is supplied to the chamber containing compressed working fluid at top dead centre. After expansion, the exhaust gases are expelled to a closed cooling chamber before being readmitted to the chamber through the intake means in a closed circuit.

The fuel in various alternative embodim ents may be hydrous ethanol, anhydrous ethanol-gasoline blends, or gasoline. The invention may also be embodied as using diesel, bio-diesel, methane (CNG, LNG or biogas) or other gaseous or liquid fuels. In an external combustion embodiment a wide range of combustible fuels may be used.

Accordingly, in conjunction with an energy storage system to provide peak transient power output requirements, the present invention provides a low- cost, high efficiency power supply for small passenger vehicle automotive applications, and many other applications where low cost and high efficiency are key design considerations, for example as a static power generator for distributed power generation.

An example of the present invention will now be described, with reference to the accompanying figures, in which:

Figure 1 shows a longitudinal section through a cylinder having a piston according to an example of the present invention;

Figure 2 is a longitudinal section through the piston, showing the construction from planar elements;

Figure 3 is a perpendicular section through the piston, showing the concentric arrangement of the shaft and planar elements; Figure 4 is a sectional view of the cylinder of Figure 3 illustrating the magnetic flux in switched stator elements caused by movement of the piston according tot the present invention;

Figure 5a is a perpendicular section through a cylinder showing the linear generator stator and the magnetic circuit formed by a permeable element in the first piston;

Figure 5b is a perpendicular section of an alternative linear generator stator arrangement for two adjacent cylinders wherein the linear generator stator and the magnetic circuit are formed by a permeable element in the first piston;

Figure 6 is a partial sectional view of the cylinder illustrating its construction;

Figure 7 is a more detailed longitudinal section of the intake poppet valve, intake port valve and fuel injector arrangement during the intake charge displacement scavenging phase;

Figure 8 is a more detailed longitudinal section of the exhaust means including the exhaust poppet valve and actuator during the exhaust phase;

Figure 9 is a time-displacement plot showing the changing piston position within a cylinder during a complete engine cycle, and the timing of engine cycle events during this period;

Figure 9a is a table showing different compression ratio control means that may be employed to control the compression ratio in a typical engine cycle;

Figure 9b is a flow chart corresponding to the table in Figure 9a;

Figure 10 is a pressure-volume plot showing a typical cylinder pressure plot during a complete engine cycle;

Figure 1 1 is a schematic longitudinal section through a cylinder at top dead centre, at the end of the compression phase and around the time of spark ignition and initiation of the combustion event in the first chamber;

Figure 12 is a schematic longitudinal section through a cylinder mid way through the expansion phase of the first chamber;

Figure 13 is a schematic longitudinal section through a cylinder at the end of the expansion phase, but before the intake poppet valve has opened; Figure 14 is a schematic longitudinal section through a cylinder following the opening of the intake poppet valve to charge chamber 1 , allowing intake charge fluid pressure to equalise the lower cylinder pressure in the first chamber;

Figure 15 is a schematic longitudinal section through a cylinder following the opening of the exhaust poppet valve, and whilst the intake poppet valve remains open, scavenging the first chamber;

Figure 16 is a schematic longitudinal section through a cylinder during fuel injection into the first chamber after the intake poppet valve has closed;

Figure 17 is a schematic longitudinal section through a cylinder during lubricant injection onto the piston outer surface;

Figure 18 is a schematic longitudinal section through a cylinder whilst the exhaust poppet valve is open, and after the intake poppet valve and sliding port valve have closed such that continuing expulsion of exhaust gases from the first chamber is achieved by piston displacement;

Figure 19 is a schematic longitudinal section through a cylinder mid way through the compression phase in the first chamber;

Figure 20A and 20B shows a section of a cylinder housing of an engine generator according to the present invention both with (A) and without (B) the electrical machine attached;

Figure 20C shows a perpendicular section of a cylinder housing of an engine generator through plane X-X indicated on Figure 20A;

Figure 21 is a schematic perpendicular section of a four cylinder engine construction through the intake means including the electrical charge compressor;

Figure 22 is a schematic perpendicular section of a four cylinder engine construction through the electrical generator means; and

Figure 23 is a schematic perpendicular section of a four cylinder engine construction through the exhaust means. Figure 1 shows an example of an engine according to the present invention, comprising a hollow linear cylinder 1. A piston 2 is provided within the cylinder 1 , the piston 2 having a constant diameter that is configured to be slightly smaller than the inside diameter of the cylinder 1 , but only to the extent that the piston 2 is free to move along the length of the cylinder 1. The piston 2 is otherwise constrained in coaxial alignment with the cylinder 1 , thereby effectively partitioning the cylinder 1 into a first combustion chamber 3 and a second combustion chamber 4, each chamber having a variable volume depending on the position of the piston 2 within the cylinder 1. No part of the piston 2 extends outside the cylinder 1. Using the first chamber 3 as an example, each of the chambers 3, 4 has a variable height 3a and a fixed diameter 3b.

The cylinder 1 is, preferably, rotationally symmetric about its axis and is symmetrical about a central plane perpendicular to its axis. Although other geometric shapes could potentially be used to perform the invention, for example having square or rectangular section pistons, the arrangement having circular section pistons is preferred. The cylinder 1 has a series of apertures 1 a, 1 b provided along its length and distal from the ends, preferably in a central location. Through motion of the piston 2, the apertures 1a, 1 b form a sliding port intake valve 6a, which is arranged to operate in conjunction with an air intake 6b provided around at least a portion of the cylinder 1 , as is described in detail below.

The cylinder 1 preferably has a length at least ten times greater than its diameter to provide reduced variability of compression ratio in each cycle, as a result of a low rate of change of compression ratio with piston displacement error at top dead centre.

Figure 2 shows a piston 2 having an outer surface 2a and comprising a central shaft 2c onto which are mounted a series of cylindrical elements. These cylindrical elements may include a piston crown 2d at each end of the central shaft 2c, each piston crown 2d preferably constructed from a temperature resistant and insulating material such as ceramic. The piston crown end surface 2b is, preferably, slightly concave, reducing the surface area-to-volume ratios of the first and second chambers 3, 4 at top dead centre and thereby reducing heat losses. Of course, if the cylinder was of a different geometry then the configuration of these elements would be adapted accordingly.

The piston crown 2d includes oil control features 2e to control the degree of lubrication wetting of the cylinder 1 during operation of the engine. These features comprise a groove and an oil control ring as are commonly employed in conventional internal combustion engines.

Laminated core elements 2f are also mounted on the piston shaft 2c. Each core element 2f is constructed from laminations of a magnetically permeable material, such as iron ferrite, to reduce eddy current losses during operation of the engine.

Spacer elements 2g are also mounted on the piston shaft 2c. Each spacer element 2g ideally has low magnetic permeability and is preferably constructed from a lightweight material such as aluminium alloy and has a void 2h formed within it to further reduce its weight and hence reduce mechanical forces exerted on the engine utilising it. The spacer elements 2g are included to fix the relative position of each of the core elements 2f and also act to limit the loss of "blow-by" gases flowing out of each chamber 3, 4 through the gap between the piston wall and cylinder wall, whilst keeping the overall mass of the piston 2 assembly to a minimum.

Bearing elements 2i are also mounted on the piston shaft 2c, located at approximately 25% and 75% of the length of the piston 2 to reduce the risk of thermally-induced distortion of the axis of the piston 2 causing it to lock in the cylinder 1 or otherwise damage the cylinder 1 . Each bearing element 2i features a weight-reduction void 2j and has a diameter very slightly larger than the core elements 2f and the spacer elements 2g. The bearing elements 2i also have a profiled outer surface 2k for bearing the weight of the piston 2, and any other side loads present, whilst keeping frictional losses and wear to a minimum. The bearing element 2i are preferably constructed from a hard, wear resistant material such as ceramic or carbon and the profiled outer surface 2k may be coated in a low friction material. Alternatively, bearing elements may incorporate roller bearing features as are commonly used in sliding applications.

Similar to the piston crown, or perhaps instead of, the bearing element 2i may also include oil control features to control the degree of lubrication wetting of the cylinder 1 during operation of the engine. These features comprise a groove and an oil control ring as are commonly employed in conventional internal combustion engines. The total length of the piston is, preferably, five times its diameter and is at least sufficient to completely close the sliding port valve such that at no time does the sliding port valve allow combustion chambers 3 and 4 to communicate.

Figure 3 is a sectional view of the piston 2, showing the piston shaft 2c passing through a core element 2f. The piston shaft ends 21 are mechanically deformed or otherwise fixed to the piston crowns 2d such that the elements 2f, 2g, 2i that are mounted to the piston shaft 2c are securely retained under the action of tension maintained in the piston shaft 2c.

The alternating arrangement of core elements 2f and spacers 2g positions the core laminations 2f at the correct pitch for efficient operation as, for example, part of a linear switched reluctance generator machine comprising the moving piston 2 and a linear generator means, for example a plurality of coils spaced along the length of the cylinder within which the piston reciprocates.

Figure 4 shows an example of linear generator means 9 provided around the outside of the cylinder 1 , along at least a portion of its length, for facilitating the transfer of energy between the piston 2 and electrical output means 9e. The linear generator means 9 includes a number of coils 9a and a number of stators 9c, in the form of magnetisable elements, alternating along the length of the linear generator means 9.

The linear generator means 9 may be of a number of different electrical machine types, for example a linear switched reluctance generator. In the arrangement shown, coils 9a are switched by switching device 9b so as to induce magnetic fields within the magnetisable stators 9c and the piston core laminations 2e. The magnetisable stators 9c may be laminated or constructed from a soft magnetic composite (SMC) material, for example. In each approach the stators are constructed from electrically conducting and magnetisable elements separated by non-conducting material which reduces heat losses from magnetically induced eddy currents.

The transverse magnetic flux created in the magnetisable stators 9c and piston core laminations 2f under the action of the switched coils 9a is also indicated in Figure 4. The linear generator means 9 functions as a linear switched reluctance device, or as a linear switched flux device. Power is generated at the electrical output means 9e as the flux circuits, established in the magnetisable stators 9c and induced in the piston core laminations 2f, are cut by the motion of the piston 2. This permits a highly efficient electrical generation means without the use of permanent magnets, which may demagnetise under the high temperature conditions within an internal combustion engine, and which might otherwise add significant cost to the engine due the use of costly rare earth metals.

Additionally, a control module 9d may be employed, comprising several different control means, as described below. The different control means are provided to achieve the desired rate of transfer of energy between the piston 2 and electrical output means 9e in order to deliver the maximum electrical output whilst satisfying the desired motion characteristics of the piston 2, including compression rate and ratio, expansion rate and ratio, and piston dwell time at top dead centre of each chamber 3, 4.

A valve control means may be used to control the intake valve 6c and the exhaust valve 7b. By controlling the closure of the exhaust valve 7b, the valve control means is able to control the start of the compression phase. In a similar way, the valve control means can also be used to control exhaust gas recirculation (EGR), intake charge and compression ratio.

A compression ratio control means that is appropriate to the type of electrical machine may also be employed. For example, in the case of a switched reluctance machine, compression ratio control is partially achieved by varying the phase, frequency and current applied to the switched coils 9a . This changes the rate at which induced transverse flux is cut by the motion of the piston 2 , and therefore changes the force that is applied to the piston 2 . Accordingly, the coils 9a may be used to control the kinetic energy of the piston 2, both at the point of exhaust valve 7b closure and during the subsequent deceleration of the piston 2.

A spark ignition timing control means may then be employed to respond to any residual cycle-to-cycle variability in the compression ratio to ensure that the adverse impact of this residual variability on engine emissions and efficiency are minimised, as follows. Generally, the expected compression ratio at the end of each compression phase is the target compression ratio plus an error that is related to system variability, such as the combustion event that occurred in the opposite combustion chamber 3, 4, and the control system characteristics. The spark ignition timing control means may adjust the timing of the spark ignition event in response to the measured speed and acceleration of the approaching piston 2 to optimize the combustion event for the expected compression ratio at the end of each compression phase.

The target compression ratio will normally be a constant depending on the fuel 5a that is used. However, a compression ratio error may be derived from a +/- 20% variation of the combustion chamber height 3a . Hence if the target compression ratio is 12:1 , the actual compression ratio may be in the range 10:1 to 15:1. Advancement or retardation of the spark ignition event by the spark ignition timing control means will therefore reduce the adverse emissions and efficiency impact of this error.

Additionally, a fuel injection control means may be employed to control the timing of the injection of fuel 5a so that it is injected into a combustion chamber 3, 4 immediately prior to the sliding port valve 6a closing to reduce hydrocarbon emissions during scavenging.

Furthermore, a temperature control means may be provided, including one or more temperature sensors positioned in proximity to the coils 9a , electronic devices and other elements sensitive to high temperatures, to control the flow of cooling air in the system via the compressor 6e in response to detected temperature changes. The temperature control means may be in communication with the valve control means to limit engine power output when sustained elevated temperature readings are detected to avoid engine damage.

Further sensors that may be employed by the control module 9d preferably include an exhaust gas (Lambda) sensor and an air flow sensor to determine the amount of fuel 5a to be injected into a chamber according to the quantity of air added, for a given fuel type. Accordingly, a fuel sensor may also be employed to determine the type of fuel being used.

Figure 5a shows a perpendicular section through one of the magnetisable stator elements 9c, showing the arrangement of coils 9a and stators 9c relative to each other. An alternative embodiment is shown in Figure 5b, in which a single stator 9c and coil 9a are used to induce magnetic flux in two adjacent pistons 2. This configuration has a cost advantage compared to that shown in Figure 5a due to the reduced number of coils 9a required. Figure 6 is a sectional view of the cylinder 1 , which is preferably constructed from a material of low magnetic permeability, such as an aluminium alloy. The inner surface 1 c of the cylinder 1 has a coating 1 e of a hard, wear- resistant material such as nickel silicon-carbide, reaction bonded silicon nitride, chrome plating, or other metallic, ceramic or other chemical coating. On the outer surface 1 d, an insulator coating 1f such as zirconium oxide or other sufficiently thermally insulating ceramic is applied. It will be apparent to a skilled person that the whole cylinder has an identical construction to this sectional view of the part of the cylinder close to the cylinder end 1 g.

Figure 7 shows the intake means 6 provided around the cylinder 1 , the intake means 6 comprising apertures 6a, which are a corresponding size and align with the apertures 1a, 1 b provided in the cylinder 1 , and an air intake 6b. The apertures 6a in the intake means 6 are connected by a channel 6h in which an intake poppet valve 6c is seated. The channel 6h is of minimal volume, either having a short length, small cross sectional area or a combination of both, to minimise uncontrolled expansion losses within the channel 6h during the expansion phase.

The intake poppet valve 6c seals the channel 6h from an intake manifold 6f provided adjacent to the cylinder 1 as part of the air intake 6b. The intake poppet valve 6c is operated by a poppet valve actuator 6d, which may be an electrically operated solenoid means or other suitable electrical or mechanical means.

When the sliding port intake valve 6a and the intake poppet valve 6c are both open with respect to one of the first or second chambers 3, 4, the intake manifold 6f is in fluid communication with that chamber via the channel 6h. The intake means 6 is preferably provided with a recess 6g arranged to receive the intake poppet valve 6c when fully open to ensure that fluid can flow freely through the channel 6h.

The air intake 6b also includes an intake charge compressor 6e which may be operated electrically, mechanically, or under the action of pressure waves originating from the air intake 6b. The intake charge compressor 6e can also be operated under the action of pressure waves originating from an exhaust means 7 provided at each end of the cylinder 1 , as described below, or by a conventional exhaust turbocharger device. The intake charge compressor 6e may be a positive displacement device, centrifugal device, axial flow device, pressure wave device, or any suitable compression device. The intake charge compressor 6e elevates pressure in the intake manifold 6f such that when the air intake 6b is opened, the pressure in the intake manifold 6f is greater than the pressure in the chamber 3, 4 connected to the intake manifold 6f, thereby permitting a flow of intake charge fluid.

Fuel injection means 5 are also provided within the intake means 6, such as a solenoid injector or piezo-injector 5. Although a centrally positioned single fuel injector 5 may be adequate, there is preferably a fuel injector 5 provided either side of the intake poppet valve 6c and arranged proximate to the extremities of the sliding port valves 6a. The fuel injectors 5 are preferably recessed in the intake means 6 such that the piston 2 may pass over and past the sliding port intake valves 6a and air intake 6b without obstruction. The fuel injectors 5 are configured to inject fuel into the respective chambers 3, 4 through each of the sliding port intake valves 6a

Lubrication means 10 are also provided preferably recessed within the intake means 6 and arranged such that the piston 2 may pass over and past the intake means 6 without obstruction, whereby the piston may be lubricated.

Figure 8 shows the exhaust means 7 provided at each end of the cylinder

1. The exhaust means 7 comprises a cylinder head 7a removably attached, by screw means or similar, to the end of the cylinder 1 . Within each cylinder head 7a is located an exhaust poppet valve 7b, coaxially aligned with the axis of the cylinder 1. The exhaust poppet valve 7b is operated by an exhaust poppet valve actuator 7c, which may be an electrically operated solenoid means or other electrical or mechanical means. Accordingly, when the intake poppet valve 6c and the exhaust poppet valve 7b within the first or second chamber 3, 4, are both closed, that chamber is effectively sealed and a working fluid contained therein may be compressed or allowed to expand.

The exhaust means 7 also includes an exhaust manifold channel 7d provided within the cylinder head, into which exhaust gases may flow, under the action of a pressure differential between the adjacent first or second chamber 3, 4 and the fluid within the exhaust manifold channel 7d when the exhaust poppet valve 7b is open. The flow of the exhaust gases can be better seen in the arrangement of cylinders illustrated in Figure 20, which shows the direction of the exhaust gas flow to be substantially perpendicular to the axis of the cylinder 1.

Ignition means 8, such as a spark plug, are also provided at each end of the cylinder 1 , the ignition means 8 being located within the cylinder head 7a and, preferably, recessed such that there is no obstruction of the piston 2 during the normal operating cycle of the engine.

The, preferably, coaxial arrangement of the exhaust poppet valve 7b with the axis of the cylinder 1 allows the exhaust poppet valve 7b diameter to be much larger relative to the diameter of the chambers 3, 4 than in a conventional internal combustion engine.

Each cylinder head 7a is constructed from a hard-wearing and good insulating material, such as ceramic, to minimise heat rejection and avoid the need for separate valve seat components.

Figure 9 shows a time-displacement plot of an engine according to the present invention, illustrating the movement of the piston 2 over the course of a complete engine cycle. Although the operation of the engine is described here with reference to the first chamber 3, a skilled person will recognise that the operation and sequence of events of the second chamber 4 is exactly the same as the first chamber 3, but 180 degrees out of phase - that is to say, top dead centre for the first chamber 3 occurs at the same time as bottom dead centre for the second chamber 4.

Figure 9a is a table showing a number of different compression ratio control means that may be employed to control the compression ratio in response to changes in signals received from a number of different variables which can affect the compression ratio during an engine cycle. Figure 9b is a flow chart corresponding to Figure 9a. The compression ratio control means may comprise part of the control module 9d, discussed earlier.

Both the table and flow chart illustrate the main variables which can affect the compression ratio at the different stages (A to F) of an engine cycle, such as the one illustrated in Figure 9. These variables include: power demand from user, the fuel type being used, the compression ratio and knock status from the previous engine cycle, piston position, and the kinetic energy of a piston. The table and flow chart illustrate the different processes that take place to control the compression ratio and how the different variables affect these throughout an engine cycle and also the subsequent effect of each process, which can have an effect on more than one of the control processes throughout the engine cycle. It can be seen that in the last step of the sequence, once the expected compression ratio has been determined, optimum ignition timing is achieved by the spark ignition timing control means adjusting the timing of the spark event.

The events A to F, highlighted throughout the engine cycle, correspond to the events A to F illustrated in Figure 10, which shows a typical pressure-volume plot for a combustion chamber 3, 4 over the course of the same engine cycle. The events featured in Figures 9 to 10 are referred to in the following discussion of Figures 1 1 to 19.

Considering now a complete engine cycle, at the start of the engine cycle, the first chamber 3 contains a compressed mixture composed primarily of pre- mixed fuel and air, with a minority proportion of residual exhaust gases retained from the previous cycle. It is well known that the presence of a controlled quantity of exhaust gases is advantageous for the efficient operation of the engine, since this can reduce or eliminate the need for intake charge throttling as a means of engine power modulation, which is a significant source of losses in conventional spark ignition engines. In addition, formation of nitrous oxide pollutant gases are reduced since peak combustion temperatures and pressures are lower than in an engine without exhaust gas retention. This is a consequence of the exhaust gas fraction not contributing to the combustion reaction, and due to the high heat capacity of carbon dioxide and water in the retained gases.

Figure 1 1 shows the position of the piston relative to the cylinder 1 , defining the geometry of the first chamber 3 at top dead centre (A). This is also around the point of initiation of the combustion phase AB. The distance between the top of the piston 2b and the end of the first chamber 3 is at least half the diameter of the first chamber 3, giving a lower surface area to volume ratio compared to combustion chambers in conventional internal combustion engines, and reducing the heat losses from the first chamber 3 during combustion. The ignition means 8 are recessed within the cylinder head 7a so that in the event that the piston 2 approaches top dead centre in an uncontrolled manner there is no possibility of contact between the ignition means 8 and the piston crown 2d. Instead, compression will continue until the motion of the piston 2 is arrested by the continuing build up of pressure due to approximately adiabatic compression in the first chamber 3. With reference to Figure 10, the combustion expansion phase AB is initiated by an ignition event (A).

Figure 12 shows the position of the piston 2 relative the linear generator means 9 mid-way through the expansion phase (AB and BC). The first chamber 3 expands as the piston 2 moves under the action of the pressure differential between the first chamber 3 and the second chamber 4. The pressure in the second chamber 4 at this point is approximately equivalent to the pressure in the intake manifold 6f. The expansion of the first chamber 3 is opposed by the action of the linear generator means 9, which may be modulated in order to achieve a desired expansion rate, to meet the engine performance, efficiency and emissions objectives.

Figure 13 shows the position of the piston 2 at bottom dead centre relative to the first chamber 3. At the end of the expansion phase (C), the motion of the piston 2 is arrested under the action of the linear generator means 9 and the pressure differential between the first chamber 3 and the second chamber 4. The pressure in the second chamber 4 at this point is approximately equal to the high pressure in the first chamber 3 at its top dead centre position (A). Preferably, the expansion ratio is at least two times the compression ratio, wherein the compression ratio is in the range of 10:1 to 16:1 . This gives an improved thermal efficiency compared to conventional internal combustion engines wherein the expansion ratio is similar to the compression ratio.

Figure 14 shows the arrangement of the piston 2 and intake means 6 and the initial flow of intake gas at the time of bottom dead centre during the intake equalisation phase (CD). This arrangement can also be seen in Figure 7. At this point, the sliding port intake valve 6a is open due to the piston 2 sliding through and past the apertures 1a, 1 b provided along the inner wall 1 c of the cylinder 1 . The pressure in the first chamber 3 is lower than the pressure in the intake manifold 6f due to the over-expansion reducing fluid pressure in the first chamber 3 an d due to the intake compressor 6e elevating the pressure in the intake manifold 6e. Around this time, the intake poppet valve 6c is opened by intake poppet valve actuator 6d allowing intake charge to enter the first chamber 3 within cylinder 1 whose pressure approaches equalisation with the pressure at the intake manifold 6f. A short time after the intake poppet valve 6c opens, the exhaust poppet valve 7b is also opened allowing exhaust gases to exit the first chamber 3 under the action of the pressure differential between the first chamber 3 and the exhaust manifold channel 7d, which remains close to ambient atmospheric pressure.

Figure 15 shows the position of the piston 2 during the intake charge displacement scavenging phase (DE). Exhaust gas scavenging is achieved by the continuing displacement of exhaust gas in the first chamber 3 into the exhaust manifold channel 7d with fresh intake charge introduced at the piston end of the first chamber 3. Once the intended quantity of intake charge has been admitted to the first chamber 3 , the intake poppet valve 6c is closed and the expulsion of exhaust gas continues by the movement of the piston 2, as shown in Figure 17, explained below.

Figure 16 shows the arrangement of the piston 2 and intake means 6 at the point of fuel injection (E). Fuel 5a is introduced directly onto the approaching piston crown 2d which has the effects of rapidly vaporising fuel, cooling the piston crown 2d and minimising the losses and emissions of unburned fuel as a wet film on the inner wall 1 c of the cylinder 1 , which might otherwise vaporise in the second chamber 4 during the expansion phase.

Figure 17 shows the position of the piston 2 during lubrication (E), whereby a small quantity of lubricant is periodically introduced by the lubrication means 10 directly to the piston outer surface 2a as it passes the intake sliding port valve 6a. This arrangement minimises hydrocarbon emissions associated with lubricant wetting of the cylinder inner wall, and may also reduce the extent of dissolution of fuel in the cylinder inner wall oil film. Oil control ring features 2e are included in the piston crown 2d and/or bearing elements 2i to further reduce the extent of lubricant wall wetting in the first and second chambers 3, 4.

Figure 18 shows the position of the piston 2 during the piston displacement scavenging phase EF. The intake poppet valve 6c is closed and the expulsion of exhaust gas continues by the movement of the piston 2. The piston 2 at this time is moving towards the exhaust means 7 and reducing the volume of the first chamber 3 due to the combustion event in the second chamber 4.

As a result of the relatively larger diameter of the exhaust poppet valve, as discussed above, the limiting area in the exhaust flow past the valve stem may approach 40% of the cylinder bore section area, resulting in low exhaust back pressure losses during both the intake charge displacement scavenging phase (DE) and piston displacement scavenging phase (EF).

Figure 19 shows a longitudinal section of the position of the piston 2 relative to the cylinder 1 mid-way through the compression phase (FA). When a sufficient exhaust gas expulsion has been achieved, such that the proportion of exhaust gas in the fluid in the first chamber 3 is close to the intended level, the exhaust poppet valve 7b is closed and the compression phase (FA) begins. Compression continues at a varying rate as the piston 2 a ccelerates and decelerates under the action of the pressure differential between the first chamber 3 and the second chamber 4. The pressure in the second chamber 4 is at this point falling during the expansion phases (AB and BC) and by the action of the linear generator means 9. The linear generator force may be modulated in order to achieve the desired compression rate to meet the engine performance, efficiency and emissions objectives. The compression rate in the first chamber 3 is substantially equal to and opposite the expansion rate in chamber 4.

Figures 20A and 20B, in particular, show how the cylinder 1 is, preferably, located coaxially within a cylinder housing 1 1 , which provides structural support to the cylinder 1 and can also be arranged to provide cooling means. The cylinder housing 1 1 may be slightly shorter than the cylinder 1 and the cylinder heads 7a may be attached, by screw fixings or any other suitable means, to the cylinder housing 1 1 to maintain compression between each cylinder head 7a and the surface of each cylinder end 1 d. Figure 20C shows section of the cylinder housing 1 1 having an electrical machine 9e attached

The cylinder housing 1 1 is, preferably, formed by extrusion of a ductile material, such as aluminium alloy, and arranged to provide structural support and cooling means 12 whilst allowing the electrical power generating components 9a-9e to be integrated in close and accurately defined proximity to the moving piston 1 within the cylinder 1.

The wall of the cylinder housing 11 extrusion is, ideally, sufficiently thick and/or strong that it is load-bearing to allow a much thinner cylinder 1 wall that provides wear and sealing surfaces than would otherwise be required. As mentioned above, the generator of the present invention comprises a plurality of magnetic coils 9a arranged in the cylinder housing 1 1 , a plurality of stators, in the form of magnetisable elements 9c and the piston 2, which acts as the translator in this instance.

The cylinder housing 11 , preferably, has sections of material removed along the length of the cylinder 1 to form one or more recesses 15 that, ideally, extend through the cylinder housing 11 to expose the wall of the cylinder 1 housed within. A plurality of the, ideally, load-bearing, magnetisable elements 9c can be positioned in close proximity to the cylinder 1 by arranging them in the one or more recesses 15, each magnetisable element 9c preferably being fixed directly to the wall of the cylinder 1 , which separates them from the moving magnetic circuit elements 2f of the piston 2.

In the example shown, only one magnetisable element 9c is provided to a recess. However, it should be noted that two or more magnetisable elements 9c recesses may be positioned within a single recess 15 if desired, depending on desired performance characteristics, and that not all recesses 15 have to contain the same number of magnetisable elements 9c, if any. The inner and outer surfaces of the cylinder 1 provide substrates for wear and thermal coatings respectively. A thermal coating can be applied to the outer surface of the cylinder 2 in the form of an adhesive material, for example, to provide a secure, insulating and load bearing bond between the cylinder 1 and cylinder housing 1 1.

Figures 21 shows an exemplary engine arrangement comprising four free-piston engines configured to operate in cycles that are synchronised to create a fully balanced engine. In this configuration, the overall length of the engine generating 50kw with a thermal efficiency of around 50% is approximately 1400mm. The cylinder housing 1 1 can be attached, by screw fixings or any other suitable means, to a structural housing 13 which provides the basis for mechanical attachment of the engine to a vehicle or other device drawing electrical power from the electrical output means 9e such as is shown in Figure 2 2. An enclosure 14 provides a physical enclosure for the engine, manifolds and control systems. Interfaces are provided across the enclosure 14 for intake and exhaust flows, admission of fuel and lubricant, rejection of heat, output of electrical power and input of electrical power for start-up and control.

Figure 23 shows an end view of an arrangement in which a cylinder head 7a houses four engines, whereby exhaust gases exit an engine's combustion chamber 3, 4 via the exhaust poppet valve 7b and flow substantially perpendicular to the axes of the cylinders 1.

Advantageously, with the present invention, the narrow bore geometry of the first chamber 3, and the relative positions of the intake means 6 and exhaust means 7, which are located at opposite ends of the first chamber 3, permits a highly efficient and effective scavenging process with little mixing between the intake charge and the exhaust gases. This scheme offers several advantages compared to scavenging in conventional two stroke engines or in free piston two stroke engines.

Firstly, the expulsion of exhaust gases can be accurately controlled by the timing of the exhaust valve closure, providing variable internal exhaust gas recirculation as a means of engine power control without the need for a throttling device and the associated engine pumping losses.

Secondly, the limited mixing between the retained exhaust gas and the intake charge may improve the completeness of combustion since the combustion flame front within the fresh charge is not interrupted by pockets of non-combustible exhaust gas mixed with the combustible fuel/air mixture.

Thirdly, the introduction of fuel 5a by the fuel injector means 5 shortly before the closure of the sliding intake port valve 6a, and also the introduction of lubricant by the lubrication means 10 around this time, is unlikely to result in fuel or lubricant entrainment in the exhaust gases and cause tailpipe hydrocarbon emissions.

Furthermore, the geometry of the chambers 3, 4 is such that at top dead centre, the distance between the top of the piston 2b and the end of the chambers 3, 4 is at least half the diameter of the chamber 3, 4. The rate of change of compression ratio with piston displacement at top dead centre is therefore smaller than a conventional free piston engine of similar diameter, but in which the depth of the chamber 3, 4 is less. As a result, the impact of small variations in the depth of the first chamber 3 at top dead centre due to combustion variations in the second chamber 4, control system tolerances or other sources of variability, are considerably reduced. Engine operating cycle stability and control are considerably improved by this feature.

By arresting the motion of the piston 2 at top dead centre (A), a desired compression ratio may be achieved. A target compression ratio may be in the range 10:1 to 16:1 , and higher compression ratios will in general enable higher thermal efficiencies to be achieved. Different compression ratio targets may be set for different fuels, to take advantage of the octane number characteristics of the particular fuel or blend of fuels in use. Any combination of feedback signals from a knock-sensor, from piston motion, from exhaust gas composition, and from other engine operating characteristics may be used as input to the control module 9d in order to achieve the desired compression rate and ratio.

An additional benefit of this embodiment compared to other internal combustion engines is that noise levels are reduced due to the over-expansion cycle and which results in a low pressure differential across the exhaust valve immediately prior to opening. As a result, the shock waves propagating through the exhaust system and causing exhaust noise in a conventional internal combustion engine or free piston engine are substantially avoided.

If the present invention was incorporated into a low cost passenger vehicle having a series hybrid drive train configuration, the cost to the vehicle user as a means for automotive electrical power generation are reduced compared to existing internal combustion engine designs. This reduction in cost is a result of a number of factors, including the low cost of fuel per unit of electrical power generated due to high thermal efficiency. Other factors include the low cost of component manufacture due to the relatively small number of high tolerance dimensions required and hence the low cost of component assembly. Also, the cost of maintenance is low due to the small number of separate components and moving parts required. Furthermore, the avoidance of complex auxiliary systems and the elimination of complex force transmission pathways including highly stresses hydrodynamic plain bearings characteristic of conventional internal combustion engines and the low cost of materials for the engine, due to the reduced part count and the small number of components having functional design constraints that require the use of high cost materials such as permanent magnets or specialised alloys of aluminium or steel are all factors that help to keep the cost down.

The thermal efficiency is also improved compared to existing internal combustion engine designs. In addition to the factors already discussed, the improved efficiency is also a result of good heat exchange, transferring a proportion of the exhaust, engine and electrical generator heat losses into the intake charge, reduced frictional losses due to the elimination of cylinder wall loads during conversion of cylinder pressure load to crankshaft torque and the elimination of throttling losses due to engine power modulation being achieved by variable intake charge flow duration at full intake boost pressure and variable internal exhaust gas recirculation, and not by throttling intake air flow as is done in a conventional spark ignition engine.

In addition, tailpipe emissions (including NOx, hydrocarbon and particulate emissions) are reduced compared to other known free piston engine designs. This reduction in tailpipe emissions is a result of a number of factors, including: improved control of compression ratio in each cycle due to the elongated electrical generator geometry, which results in a high electrical control authority over piston movement during the compression stroke and therefore a lower piston displacement error at top dead centre; and variable retained exhaust gas composition of compressed charge to reduce peak combustion temperatures and pressures which determine NOx formation.