EP0947680A2 - Free-piston gas generator - Google Patents
Free-piston gas generator Download PDFInfo
- Publication number
- EP0947680A2 EP0947680A2 EP99113550A EP99113550A EP0947680A2 EP 0947680 A2 EP0947680 A2 EP 0947680A2 EP 99113550 A EP99113550 A EP 99113550A EP 99113550 A EP99113550 A EP 99113550A EP 0947680 A2 EP0947680 A2 EP 0947680A2
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- EP
- European Patent Office
- Prior art keywords
- piston
- chamber
- cylinder
- gas generator
- free
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B71/00—Free-piston engines; Engines without rotary main shaft
- F02B71/04—Adaptations of such engines for special use; Combinations of such engines with apparatus driven thereby
- F02B71/06—Free-piston combustion gas generators per se
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B71/00—Free-piston engines; Engines without rotary main shaft
- F02B71/04—Adaptations of such engines for special use; Combinations of such engines with apparatus driven thereby
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/04—Engines with variable distances between pistons at top dead-centre positions and cylinder heads
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Definitions
- the invention relates to a free-piston gas generator with at least one cylinder and a piston provided therein, the ends of which together with the cylinder define a combustion chamber, a buffer chamber and a compressor chamber respectively the compressor chamber supplying compressed air to the combustion chamber.
- Such free-piston devices may be of the diesel type and be employed, e.g., as gas generators.
- GB 2 214 569 discloses a free-piston gas generator having a combustion chamber, a compressor chamber and return chamber.
- the return chamber is defined by the gas generator cylinder and a compressor piston which is directly connected to the free-piston and the return chamber is connected to a swirl tank through a regulator and a check valve.
- the regulator provides a topping up of air in the return chamber in the event of an unintentional leakage therefrom and the return chamber is in principle a closed chamber the only moving wall of which being the portion of the compressor piston facing this chamber.
- the gas generator has a gas outlet port which is opened and closed by the piston.
- the object of the invention is to provide an exhaust gas device of the above-mentioned type which improves the possibility of regulating the gas generator as mentioned above.
- a gas generator of the type which is illustrated in the application WO 97/28362 instead of the pistons uncovering exhaust gas ports at each stroke, in the centre of the cylinder device there is provided a channel which communicates with the combustion chamber, and in which there is provided an exhaust gas valve 1 for controlling the discharge of the exhaust gas from the combustion chamber.
- the discharge of exhaust gases from the combustion chamber can be independent of an opening of outlet ports in the cylinder sections by means of the pistons.
- This exhaust gas valve 1 can be controlled, e.g., by the computer which is described in the application WO 97/28362, thereby permitting operation of the gas generator during part load.
- cylinders can hereby be obtained which are symmetrical about a transverse median plane with regard to inlet ports, as well as individual stroke lengths and heat load. Assembly and dismantling of the gas generator is simplified and thereby also the maintenance thereof.
- fig. 2 there is illustrated a gas generator with a single piston 2 which is provided in a cylinder 3 corresponding to one half of the cylinder device which is illustrated in the application WO 97/28362.
- an exhaust gas valve 4 like that described in connection with fig. 1 is installed at the combustion chamber on the end surface of the cylinder.
- a cylindrical, axially extending dowel 7 is mounted on the enlarged section 5 of the piston 2.
- the cross section of the dowel 7 is adapted to the cross section of an axially extending hole 8, which is provided in the compressor housing wall, and through which the air in the ventilation chamber 10 communicates with the ambient air.
- a further movement of the piston thus causes a progressive increase in the pressure of the enclosed air and brakes the piston's movement, preventing a collision between the piston and the cylinder end wall.
- This design requires guide devices (not shown) which prevent rotation of the piston about its longitudinal axis.
- extra air can be supplied by means of the aforementioned computer to the return or buffer chamber in order to prevent the piston from striking the buffer chamber end wall, or air can be removed from the buffer chamber in order to reduce the speed at which the piston is brought into the combustion chamber.
- Fig. 2 illustrates the arrangement of the compressor's valves which supply compressed air to the cylinder's inlet ports when the piston is moved away from the combustion chamber.
- the former valve arrangement is advantageous, since there is no need for any pressure chamber between the compressor chamber 6 and the inlet ports, and thus no hysteresis loss occurs in connection with a related accumulation of pressure energy.
- This device further permits variation of the compression ratio without such a variation influencing the inlet air compression.
- One drawback, however, is that small tolerances are required for the pistons at the outer dead centre position, i.e. at the dead centre position at which the piston is located when it is remote from the combustion chamber.
- the return or buffer chamber volume can be adjustable. This can be achieved by providing the cylinder end wall at the buffer chamber in the form of a screw (not shown) which is screwed axially into the cylinder end section.
- a motor which can rotate this cylinder end wall, thereby screwing it into or out of the cylinder, the buffer chamber volume can easily be varied.
- the motor can be controlled, e.g. by the computer which is described in the application WO 97/28362.
- the air from the compressor is passed to a compressed air container 11 from which air may be drawn, passed, e.g., to a gas turbine via a valve 12 and mixed with the exhaust gas from the gas generator.
- the filling of the combustion chamber during the suction phase can thereby be controlled.
- control can also be provided, e.g., by controlling the suction valves (not shown) in the cylinder.
- each cylinder section thereby obtains its own combustion chamber which is located at the extreme end of the cylinder section, thus enabling the cylinder sections to be of the same design as the cylinders for standard diesel motors.
- the cooling of the cylinders at the combustion chambers can thereby be improved.
- each piston In order for the gas generator to function properly, each piston must have a separate buffer chamber. For this reason a central partition 15 is provided, thus creating two separate buffer chambers 16,17.
- a gas generator is illustrated with a piston where the compressor chamber also acts as a return or buffer chamber for returning the piston towards the combustion chamber after it has reached the external dead centre position.
- regulation such as by means of the aforementioned computer and as mentioned in connection with fig. 2 must be implemented in order to ensure that the energy of the air in the compressor chamber is always sufficiently great to return the piston, thus enabling the stroke for compression of the gas in the combustion chamber (the compression stroke) to be performed.
- a generator of this kind can be provided together with and operate jointly with corresponding gas generators, the movement of the pistons being phase shifted.
- FIG. 5 As illustrated in fig. 5 four gas generators of the type which is illustrated in fig. 3 are arranged in a row on a common frame (not shown).
- the pistons of the two outer gas generators 21,22 can be operated in the same phase. These pistons are phase shifted by 180° in relation to the pistons of the two inner gas generators.
- a pipe 27 extends to a shut-off valve 28 which in turn is connected via a pipe 29 to a manifold 30 which connects pipes similar to pipe 29 to one another. Exhaust gas is passed from the exhaust gas port to the pipe 29 via a pipe 31.
- the exhaust gas is passed from the manifold 30 to a chamber 35 where the pressure fluctuations in the exhaust gas are moderated to some extent. It is passed from there to a gas turbine 32 which is arranged to drive a turbocompressor 33. During operation the turbocompressor 33 draws in ambient air, compresses it and passes it to the inlet valve of each gas generator's compressor via an intermediate cooler 34 and an air manifold 36.
- channels can extend in the respective cylinders.
- a gas generator with a single piston 51 which has a central, enlarged section which forms a compressor piston section 52. On each side thereof, the piston 51 has a working piston section 53 and 54.
- the piston 51 is provided in a cylinder device 55 comprising a central, enlarged compressor cylinder section 56. On each side thereof, the cylinder device has a working cylinder section 57 and 58 with smaller diameter.
- the piston sections 52,53,54 are arranged to be moved together axially forwards or backwards in the respective cylinder sections 56,57,58.
- the compressor piston section 52 defines two compressor chambers 61,62.
- Each compressor chamber has an inlet valve and an outlet valve 63,64 and 65,66.
- the ends of the working piston sections define combustion chambers 71,72.
- the outlet valve 65 for the right compressor chamber 62 is connected via pipes to the inlet port 75 for the left working cylinder section 57 and in addition connected via a shut-off valve 91 to the inlet of a gas turbine 95 which is fed via pipes with exhaust gas from both working cylinders.
- outlet valve 64 for the left compressor chamber 61 is connected via pipes to the inlet port 76 for the right working cylinder section 58 and in addition connected via a shut-off valve 92 to the inlet of the gas turbine 95.
- the gas turbine 95 is arranged to drive a turbocompressor 96 and, e.g., an electrical generator 97.
- the turbocompressor draws in ambient air and passes this in a compressed state to the compressor chambers' inlet valves 63,66 via an intermediate cooler 98.
- exhaust gas valves' activators 85-88 can be operated by a computer as mentioned above.
- the advantage of an exhaust gas generator according to fig. 6 is that the combustion chambers are placed at the extreme ends of the cylinder device, thus providing easy access to the adjacent cylinder sections which become very hot during running, and enabling them to thereby receive a good cooling. Moreover, the heavily loaded exhaust gas ports can be replaced by known per se valve devices which can be satisfactorily cooled in the known manner.
- the shut-off valves 91,92 can be opened for the supply of cold air to the exhaust gases from the gas generator in order thereby to reduce the temperature of the gas which is supplied to the turbine 95.
- this gas generator only has one cylinder, four gas generators, e.g., may advantageously be placed on a common frame in order to obtain an approximately dynamically balanced device as mentioned above in connection with the device which is illustrated in fig. 5.
- FIG. 7 there is illustrated a central section of a gas generator with two pistons 101,102 which are provided axially and in the same cylinder 103. Together with the cylinder 103, the ends of the pistons which are located opposite each other define a combustion chamber 104. A fuel injection nozzle 105 is provided for supplying fuel to the combustion chamber 104.
- the left piston 101 is illustrated at the inner dead centre position, i.e. in the position at which it is located when it has been inserted furthest into the combustion chamber 104, and the right piston 102 is illustrated at the outer dead centre position. It will be understood, however, that during operation the pistons are substantially located simultaneously at the inner or the outer dead centre position.
- each piston Near the end which faces the combustion chamber there is mounted on each piston a pair of sealing rings 111,112,113,114, where the sealing rings in each pair, 111,112 and 113,114 respectively are provided with a spacing which enables them to provide a seal on each side of the exhaust gas ports or the inlet air ports, considered in the axial direction when the pistons are brought into a suitable position.
- Each piston thus constitutes a shut-off valve, which is important for the regulation of output, since gas generators usually have at least two cylinders whose piston pairs can be started and stopped in turn.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
Description
- The invention relates to a free-piston gas generator with at least one cylinder and a piston provided therein, the ends of which together with the cylinder define a combustion chamber, a buffer chamber and a compressor chamber respectively the compressor chamber supplying compressed air to the combustion chamber.
- Such free-piston devices may be of the diesel type and be employed, e.g., as gas generators.
- In known diesel free-piston gas generators, during its movement the piston uncovers exhaust gas ports in the cylinder for discharging the exhaust gas from the combustion chamber. This uncovering of the exhaust gas ports which is only dependent on the piston's position, restricts the possibility of changing the compression by controlling the beginning of the compression in the combustion chamber and thereby a part load regulation of the gas generator. In practice this means that during operation the gas generator has to be run the whole time with almost nominal output.
- It is also known to provide separate return and compressor chambers, with the result that the gas generator requires a great deal of space.
- It is also known for the end section of the piston which faces the combustion chamber to be equipped with only one sealing ring. The result of this can be that the ports are not completely sealed in relation to the outlet ports.
- In known free-piston generators the volume of the return chamber is fixed in the sense that the volume is only established of that section of the gas generator's free piston which projects into the return chamber, with the result that this return chamber cannot be used for regulation of the gas generator's operation.
- In known free-piston generators, moreover, there is a risk that the free piston may come into contact with an adjacent end wall of the cylinder section and that these components can be damaged.
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GB 2 214 569 discloses a free-piston gas generator having a combustion chamber, a compressor chamber and return chamber. The return chamber is defined by the gas generator cylinder and a compressor piston which is directly connected to the free-piston and the return chamber is connected to a swirl tank through a regulator and a check valve. - The regulator provides a topping up of air in the return chamber in the event of an unintentional leakage therefrom and the return chamber is in principle a closed chamber the only moving wall of which being the portion of the compressor piston facing this chamber.
- The gas generator has a gas outlet port which is opened and closed by the piston.
- Thus the air volume of and the pressure of the air in the return chamber and the exhaust outlet timing is a function only of the position of the reciprocating piston relative to the cylinder.
- Thus important running parameters of the gas generator is a function only of the piston position. Also the return chamber does not function as a compressor chamber and must be provided with separate means for maintaining the pressure therein.
- The object of the invention is to provide an exhaust gas device of the above-mentioned type which improves the possibility of regulating the gas generator as mentioned above.
- The characteristics of the device according to the invention are presented by the characteristic features indicated in the claims.
- The invention will now be described in more detail with reference to the drawing which schematically illustrates embodiments of the device according to the invention.
- Fig. 1 is a schematic longitudinal section through a free-piston gas generator with two cylinder sections with respective pistons and with coincident longitudinal axes together with a common combustion chamber for the cylinder sections situated in neighbouring areas of the cylinder sections, this section resembling the section which is illustrated in application WO97/28362.
- Fig. 2 is a longitudinal section through a gas generator with a piston.
- Fig. 3 is a longitudinal section through a gas generator with two cylinder sections and pistons, comprising in principle two gas generators of the type which resembles that which is illustrated in fig. 2, these extending with coincident longitudinal axes and their return or buffer chambers being placed against each other.
- Fig. 4 is a longitudinal view through a gas generator with a cylinder section and a piston, with a combined buffer or return chamber and compressor device.
- Fig. 5 is a longitudinal section through four jointly operating gas generators of the type which is illustrated in fig. 4.
- Fig. 6 is a longitudinal section through a gas generator with a single piston and a cylinder device with a cylinder which has a combustion chamber at each end.
- Fig. 7 is a cross section through the section in the vicinity of a combustion chamber of a cylinder device for a gas generator, sections of the device being cut away.
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- For a more detailed description of the gas generator's design, reference should be made to the
application WO 97/28362. A method is described therein for controlling the stroke of gas generators of the above-mentioned type by means of a computer which is programmed to vary the mass or the energy of the air in the return chamber in order thereby to vary the piston's stroke movement. This computer is arranged to establish values of operating parameters of the free-piston gas generator via an array of sensors such as pressure, temperature and position sensors. Features will now be described and claimed which are based on features described in the above-mentioned application, but which for the sake of simplicity are not repeated here. It will be understood that these basic features should be considered to also be included in the present application. - In fig. 1 there is illustrated a gas generator of the type which is illustrated in the application WO 97/28362. Instead of the pistons uncovering exhaust gas ports at each stroke, in the centre of the cylinder device there is provided a channel which communicates with the combustion chamber, and in which there is provided an
exhaust gas valve 1 for controlling the discharge of the exhaust gas from the combustion chamber. Thus, the discharge of exhaust gases from the combustion chamber can be independent of an opening of outlet ports in the cylinder sections by means of the pistons. Thisexhaust gas valve 1 can be controlled, e.g., by the computer which is described in theapplication WO 97/28362, thereby permitting operation of the gas generator during part load. - Furthermore, cylinders can hereby be obtained which are symmetrical about a transverse median plane with regard to inlet ports, as well as individual stroke lengths and heat load. Assembly and dismantling of the gas generator is simplified and thereby also the maintenance thereof.
- In fig. 2 there is illustrated a gas generator with a
single piston 2 which is provided in acylinder 3 corresponding to one half of the cylinder device which is illustrated in the application WO 97/28362. In this embodiment, however, an exhaust gas valve 4 like that described in connection with fig. 1 is installed at the combustion chamber on the end surface of the cylinder. - In order to prevent a collision between the end section of the piston which faces the combustion chamber and the opposite cylinder end wall, in a
ventilation chamber 10 on the side of the compressor piston which faces away from thecompressor chamber 6, a cylindrical, axially extending dowel 7 is mounted on the enlargedsection 5 of thepiston 2. The cross section of the dowel 7 is adapted to the cross section of an axially extendinghole 8, which is provided in the compressor housing wall, and through which the air in theventilation chamber 10 communicates with the ambient air. When the piston end which projects into the combustion chamber comes too close to the opposite cylinder end wall, the dowel 7 is brought into thehole 8, thereby closing theventilation chamber 10. A further movement of the piston thus causes a progressive increase in the pressure of the enclosed air and brakes the piston's movement, preventing a collision between the piston and the cylinder end wall. This design requires guide devices (not shown) which prevent rotation of the piston about its longitudinal axis. - In order to prevent a collision between the piston and the cylinder end wall at both dead centre positions, extra air can be supplied by means of the aforementioned computer to the return or buffer chamber in order to prevent the piston from striking the buffer chamber end wall, or air can be removed from the buffer chamber in order to reduce the speed at which the piston is brought into the combustion chamber.
- If little clearance is provided between the piston and the buffer cylinder wall, a relatively high buffer chamber pressure can quickly be provided which counteracts a collision between the piston and the buffer chamber end wall.
- Fig. 2 illustrates the arrangement of the compressor's valves which supply compressed air to the cylinder's inlet ports when the piston is moved away from the combustion chamber. In contrast to the arrangement, where compressed air is supplied to the cylinder's inlet ports when the piston is moved towards the combustion chamber, the former valve arrangement is advantageous, since there is no need for any pressure chamber between the
compressor chamber 6 and the inlet ports, and thus no hysteresis loss occurs in connection with a related accumulation of pressure energy. This device further permits variation of the compression ratio without such a variation influencing the inlet air compression. One drawback, however, is that small tolerances are required for the pistons at the outer dead centre position, i.e. at the dead centre position at which the piston is located when it is remote from the combustion chamber. In order to counteract this, it can be advantageous for the return or buffer chamber volume to be adjustable. This can be achieved by providing the cylinder end wall at the buffer chamber in the form of a screw (not shown) which is screwed axially into the cylinder end section. By providing a motor which can rotate this cylinder end wall, thereby screwing it into or out of the cylinder, the buffer chamber volume can easily be varied. Thus the energy content of the buffer chamber can be controlled, especially during power control. The motor can be controlled, e.g. by the computer which is described in the application WO 97/28362. - In fig. 2 it is shown that the air from the compressor is passed to a
compressed air container 11 from which air may be drawn, passed, e.g., to a gas turbine via avalve 12 and mixed with the exhaust gas from the gas generator. The filling of the combustion chamber during the suction phase can thereby be controlled. Such control can also be provided, e.g., by controlling the suction valves (not shown) in the cylinder. - Instead of positioning the combustion and buffer chambers as shown in fig. 1, these can change places as shown in fig. 3. Each cylinder section thereby obtains its own combustion chamber which is located at the extreme end of the cylinder section, thus enabling the cylinder sections to be of the same design as the cylinders for standard diesel motors. The cooling of the cylinders at the combustion chambers can thereby be improved. In order for the gas generator to function properly, each piston must have a separate buffer chamber. For this reason a
central partition 15 is provided, thus creating twoseparate buffer chambers - In fig. 4 a gas generator is illustrated with a piston where the compressor chamber also acts as a return or buffer chamber for returning the piston towards the combustion chamber after it has reached the external dead centre position. In this arrangement, regulation such as by means of the aforementioned computer and as mentioned in connection with fig. 2 must be implemented in order to ensure that the energy of the air in the compressor chamber is always sufficiently great to return the piston, thus enabling the stroke for compression of the gas in the combustion chamber (the compression stroke) to be performed.
- Since a gas generator with only one piston is not in dynamic balance, a generator of this kind can be provided together with and operate jointly with corresponding gas generators, the movement of the pistons being phase shifted.
- As illustrated in fig. 5 four gas generators of the type which is illustrated in fig. 3 are arranged in a row on a common frame (not shown). For example, the pistons of the two
outer gas generators - From each gas generator's compressor chamber air is led via a
pipe 25 to the respective gas generators' inlet ports via acompressed air container 26. - From this container a
pipe 27 extends to a shut-offvalve 28 which in turn is connected via apipe 29 to a manifold 30 which connects pipes similar topipe 29 to one another. Exhaust gas is passed from the exhaust gas port to thepipe 29 via apipe 31. - The exhaust gas is passed from the manifold 30 to a
chamber 35 where the pressure fluctuations in the exhaust gas are moderated to some extent. It is passed from there to agas turbine 32 which is arranged to drive aturbocompressor 33. During operation theturbocompressor 33 draws in ambient air, compresses it and passes it to the inlet valve of each gas generator's compressor via anintermediate cooler 34 and anair manifold 36. - Instead of
pipes 25 from the compressor to the inlet ports, channels (not shown) can extend in the respective cylinders. - In fig. 6 there is illustrated a gas generator with a single piston 51 which has a central, enlarged section which forms a compressor piston section 52. On each side thereof, the piston 51 has a working
piston section - The piston 51 is provided in a cylinder device 55 comprising a central, enlarged compressor cylinder section 56. On each side thereof, the cylinder device has a working
cylinder section 57 and 58 with smaller diameter. - The
piston sections respective cylinder sections 56,57,58. - Together with end walls of the compressor cylinder section 56, the compressor piston section 52 defines two
compressor chambers outlet valve - Together with the end areas of the working cylinder sections, the ends of the working piston sections define
combustion chambers 71,72. - In the working
cylinder sections 57,58 there are providedair inlet ports gas outlet ports valves related activators fuel injection nozzles - The
outlet valve 65 for theright compressor chamber 62 is connected via pipes to theinlet port 75 for the left workingcylinder section 57 and in addition connected via a shut-offvalve 91 to the inlet of agas turbine 95 which is fed via pipes with exhaust gas from both working cylinders. - Moreover, the
outlet valve 64 for theleft compressor chamber 61 is connected via pipes to theinlet port 76 for the right working cylinder section 58 and in addition connected via a shut-offvalve 92 to the inlet of thegas turbine 95. - The
gas turbine 95 is arranged to drive aturbocompressor 96 and, e.g., anelectrical generator 97. The turbocompressor draws in ambient air and passes this in a compressed state to the compressor chambers'inlet valves intermediate cooler 98. - In this case too the exhaust gas valves' activators 85-88 can be operated by a computer as mentioned above.
- The advantage of an exhaust gas generator according to fig. 6 is that the combustion chambers are placed at the extreme ends of the cylinder device, thus providing easy access to the adjacent cylinder sections which become very hot during running, and enabling them to thereby receive a good cooling. Moreover, the heavily loaded exhaust gas ports can be replaced by known per se valve devices which can be satisfactorily cooled in the known manner.
- The shut-off
valves turbine 95. - Since this gas generator only has one cylinder, four gas generators, e.g., may advantageously be placed on a common frame in order to obtain an approximately dynamically balanced device as mentioned above in connection with the device which is illustrated in fig. 5.
- In fig. 7 there is illustrated a central section of a gas generator with two pistons 101,102 which are provided axially and in the
same cylinder 103. Together with thecylinder 103, the ends of the pistons which are located opposite each other define acombustion chamber 104. Afuel injection nozzle 105 is provided for supplying fuel to thecombustion chamber 104. - For example, the left piston 101 is illustrated at the inner dead centre position, i.e. in the position at which it is located when it has been inserted furthest into the
combustion chamber 104, and theright piston 102 is illustrated at the outer dead centre position. It will be understood, however, that during operation the pistons are substantially located simultaneously at the inner or the outer dead centre position. - Near the end which faces the combustion chamber there is mounted on each piston a pair of sealing rings 111,112,113,114, where the sealing rings in each pair, 111,112 and 113,114 respectively are provided with a spacing which enables them to provide a seal on each side of the exhaust gas ports or the inlet air ports, considered in the axial direction when the pistons are brought into a suitable position. Each piston thus constitutes a shut-off valve, which is important for the regulation of output, since gas generators usually have at least two cylinders whose piston pairs can be started and stopped in turn.
- It will be understood that further devices are provided, e.g. for starting of the gas generators, sensors etc. for the computers etc., even though such devices are not specifically illustrated in the figures.
Claims (5)
- Free-piston gas generator with at least one cylinder and a piston (2) provided therein, the ends of which together with the cylinder (3) define a combustion chamber (13), a buffer chamber (14) and a compressor chamber (6) respectively the compressor chamber (6) supplying compressed air to the combustion chamber,
characterized in that the gas generator comprises at least one exhaust gas valve which is aranged in a port provided in the cylinder section, which port constantly communicates with the combustion chamber and which exhaust valve is operated by an actuator, and that the cylinder portion of the buffer chamber comprises a component which is movable relative to the rest of this cylinder portion, by means of which component the volume of the buffer chamber is variable. - Free-piston gas generator according to claim 1,
characterized in that the component is a screw which can be screwed in or out of the buffer chamber. - Free-piston gas generator according to claim 1 or 2,
characterized in that the movement of the component in and out of the cylinder portion is controlled by means of a computer which is provided with information about the movement of the piston relative to the cylinder. - Free-piston gas generator according to one of the claims 1 - 3,
characterized in that the piston (2) opposite to its side defining the compresssor chamber, has a side which together with a portion of the cylinder (3) defines a ventilating chamber (10), which via a through-going axial passage (8) communicates with the ambient air when the piston (2) is in the outer dead center relative to the ventilating chamber (10), i.e. when the volume of the ventilating chamber is maximal, and that a dowel (7) protrudes axially from the piston into the ventilating chamber, which dowel (7) sealingly is introduced into the passage (8) when the piston (2) is moved a distance from the outer dead center towards the inner dead center of the ventilating chamber (10). - Free-piston gas generator according to one of the claims 1 - 4,
comprising a valve device which communicates with the buffer chamber (14) and a compressed air container, and control device for operating the valve device for introducing compressed air from a container into the buffer chamber (14) when the piston is in the outer dead center relative to the buffer chamber,
characterized in that the valve device also communicates with the ambient air, the control device via a position sensor continuously establishes the position of the free piston (2) in the cylinder section (3), and the control device is arranged to activate the valve device for connection of the buffer chamber (14) with the compressed air container or the ambient air at any posistion of the piston in order to counteract a contact of one of the free piston's (2) end sections with a thereto adjacent end section of the cylinder section.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NO960402A NO305451B1 (en) | 1996-01-30 | 1996-01-30 | Device for preventing collision between a piston and a cylinder of a free piston device |
NO960402 | 1996-01-30 | ||
EP97902766A EP0877858A1 (en) | 1996-01-30 | 1997-01-29 | An improvement in free-piston devices |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97902766A Division EP0877858A1 (en) | 1996-01-30 | 1997-01-29 | An improvement in free-piston devices |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0947680A2 true EP0947680A2 (en) | 1999-10-06 |
EP0947680A3 EP0947680A3 (en) | 1999-10-27 |
Family
ID=19898987
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97902766A Ceased EP0877858A1 (en) | 1996-01-30 | 1997-01-29 | An improvement in free-piston devices |
EP99113550A Withdrawn EP0947680A3 (en) | 1996-01-30 | 1997-01-29 | Free-piston gas generator |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97902766A Ceased EP0877858A1 (en) | 1996-01-30 | 1997-01-29 | An improvement in free-piston devices |
Country Status (4)
Country | Link |
---|---|
EP (2) | EP0877858A1 (en) |
JP (1) | JP2000504084A (en) |
NO (1) | NO305451B1 (en) |
WO (1) | WO1997028363A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103967604A (en) * | 2013-01-28 | 2014-08-06 | 安徽中鼎动力有限公司 | Free piston type engine |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6925971B1 (en) * | 2004-05-20 | 2005-08-09 | Ford Global Technologies, Llc | Exhaust gas recirculation for a free piston engine |
WO2007059565A1 (en) * | 2005-11-22 | 2007-05-31 | Peter Charles Cheeseman | Four-stroke free piston engine |
DE202006018098U1 (en) * | 2006-11-27 | 2008-04-10 | Jung, Nadine | Energy conversion system |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE536930C (en) * | 1928-04-23 | 1931-10-28 | Robert Lee Gray | Internal combustion engine with adjustable compression by adjusting a piston |
CH498290A (en) * | 1969-03-06 | 1970-10-31 | Braun Anton | Free piston engine |
GB2214569A (en) * | 1988-01-21 | 1989-09-06 | Barry John Rymer | Free-piston I.C engine |
US4876991A (en) * | 1988-12-08 | 1989-10-31 | Galitello Jr Kenneth A | Two stroke cycle engine |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4369021A (en) * | 1980-05-16 | 1983-01-18 | Heintz Richard P | Free-piston engine pump |
US4653274A (en) * | 1984-03-06 | 1987-03-31 | David Constant V | Method of controlling a free piston external combustion engine |
US5363651A (en) * | 1993-07-12 | 1994-11-15 | Knight Arthur G | Free piston internal combustion engine |
-
1996
- 1996-01-30 NO NO960402A patent/NO305451B1/en unknown
-
1997
- 1997-01-29 JP JP9527517A patent/JP2000504084A/en active Pending
- 1997-01-29 EP EP97902766A patent/EP0877858A1/en not_active Ceased
- 1997-01-29 WO PCT/NO1997/000023 patent/WO1997028363A1/en not_active Application Discontinuation
- 1997-01-29 EP EP99113550A patent/EP0947680A3/en not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE536930C (en) * | 1928-04-23 | 1931-10-28 | Robert Lee Gray | Internal combustion engine with adjustable compression by adjusting a piston |
CH498290A (en) * | 1969-03-06 | 1970-10-31 | Braun Anton | Free piston engine |
GB2214569A (en) * | 1988-01-21 | 1989-09-06 | Barry John Rymer | Free-piston I.C engine |
US4876991A (en) * | 1988-12-08 | 1989-10-31 | Galitello Jr Kenneth A | Two stroke cycle engine |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103967604A (en) * | 2013-01-28 | 2014-08-06 | 安徽中鼎动力有限公司 | Free piston type engine |
Also Published As
Publication number | Publication date |
---|---|
JP2000504084A (en) | 2000-04-04 |
NO960402D0 (en) | 1996-01-30 |
EP0947680A3 (en) | 1999-10-27 |
WO1997028363A1 (en) | 1997-08-07 |
NO960402L (en) | 1997-08-25 |
NO305451B1 (en) | 1999-05-31 |
EP0877858A1 (en) | 1998-11-18 |
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