ENERGY CONVERTER

Abstract: An energy converter comprising a free piston engine with a cylinder (2), a piston (3), a body connected to the piston such as an armature (11) of a linear electric generator (10). The energy converter comprises a spring device (15), via which the armature (11) is springingly connected to the housing (1), and which is arranged to permit an oscillation of the armature (11) in the piston's (3) direction of movement with a natural frequency fe relative to the stator (12).

Description: Energy converter The invention relates to an energy converter comprising a free piston engine with a cylinder, a piston, a body connected to the piston and an elastic device, which is arranged to exert a force in the cylinder's longitudinal direction against the body and a corresponding reaction force against the cylinder, From US 5 002 020 there is known an energy converter of the above- mentioned type with an oscillating magnet. In this publication devices are also described for controlling the engine, and suitable devices of this kind can also be used for controlling the engine according to the description below. In order to create an oscillation with a fixed frequency, the engine of the known energy converter comprises a separate frequency control device, thus increasing the complexity of the device. This also results in an increase in the price and maintenance costs of the device in addition to the risk of failure during operation. Furthermore, from GB 2 206 931 it is known that a piston of a vacuum pump can be caused to oscillate when a magnet, hereinafter called an armature, of a linear electromotor, is operated by the electric field from a winding, hereinafter called a stator, which is fed with electric current from a public electricity network. In order to adapt the electromotor to different frequencies of the feeding current, the armature is connected to a chamber whose opening via which the chamber communicates with the ambient air, can be varied in such a manner that the oscillation frequency can be varied. The device illustrated here is not a generator, and the armature/piston assembly is not arranged for continued oscillation during an "idling condition" of the pump and the influence of the armature by a force, e.g. at intervals corresponding to a certain number of periods, in order to compensate for any amplitude reduction. The object of the invention is to provide an energy converter of the aforementioned known type which is encumbered to a lesser degree by the above-mentioned disadvantages. Moreover, it is an object of the invention to provide an energy converter which adapts to a free piston engine to a linear electric generator in such a manner that an exceptionally high degree of efficiency is obtained. Characterising features of the device according to the invention will be presented 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. Figs. 1 - 5 illustrate a longitudinal section through five respective embodiments of an energy converter according to the invention. Figs. 6 - 8 illustrate a section through a combustion chamber of a device according to the invention during the introduction of a first fuel, introduction of a second fuel and a detonation of the fuels respectively, portions of the device being cut away. Fig. 9 illustrates a longitudinal section through a sixth embodiment of a device according to the invention, where explosive charges and helical springs are employed to move an armature of the device. Fig. 10 illustrates a longitudinal section through a seventh embodiment of a device according to the invention, where four pairs of uniformly polarised magnets are employed for moving the armature. The terms right and left should be understood to refer to the direction towards the right and left edges respectively of the drawing as it is viewed by the reader, Components which have the same function in the different embodiments in figures 1 - 5 have been given the same reference numerals with the addition of one or more apostrophes. As can be seen in fig. 1, which illustrates the simplest embodiment, in a cylinder 2 of a housing 1 there is mounted a piston 3 which is arranged to be moved backwards and forwards in the cylinder 2. The cylinder 2 and the piston 3 are preferably components of an internal combustion engine with a combustion chamber 4 which is defined by the cylinder portion 2 and the piston 3. In the usual manner the engine may comprise components such as an inlet valve for admitting a combustion gas into the cylinder, and an outlet valve for releasing exhaust gas, sensors for establishing values of movement parameters for the piston, where these values can be supplied to a computer for control of the engine, etc., the components not being illustrated in the figures, A piston rod 5 is rigidly connected via one of its ends with the piston 3 and rigidly connected via its other end with a movable part, hereinafter called an armature 11, of a linear electric generator 10. Near the armature 11, a stator 12 of the generator 10 is attached to the housing 1, it being understood that the armature 11 may be mounted in bearings (not shown) which support the armature 11, permitting a preferably linear movement of the armature 11 backwards and forwards relative to the stator 12, thereby inducing an electric current in the stator 12. This current can be conducted away from the stator 12 via suitable wires (not shown). On the opposite side of the armature 11, between the armature 11 and the housing 1 there is mounted an elastic device comprising an elastic element such as a spring 15. When the piston rod 5 is not exerting any force against the armature 11, the spring attempts to bring the armature 11 to a neutral location N considered in the armature's direction of movement and in relation to the stator 12, When the armature is continuously at rest, it is therefore situated in this location N which is indicated by a dot-and-dash line in fig. 1 , If, e.g., a combustible gas is introduced to the combustion chamber 4 via valves, whereupon the valves are closed and the gas ignited, an increase in the temperature and pressure of the gas in the combustion chamber is obtained. A force is thereby exerted towards the right on the piston 3, which force is transferred via the piston rod 5 to the armature 11, and the piston and the armature are moved towards the right, thereby inducing an electric current in the stator 12. At the same time the spring 15 is compressed and the tension gradually increased, with the result that it exerts a corresponding increasing spring force which is directed towards the left, A reaction force is hereby also exerted by the stator 12 towards the left on the armature 11. After a ventilation of the combustion chamber by opening the valves and the combustion gases no longer exert any compressive force on the piston 3 and the armature 11 has reached its outer dead point, the spring 15 causes an acceleration of the armature 11 to the left, whereupon a current is again induced in the stator 12, while at the same time the piston 3 is moved into the cylinder 2. After the armature 11 has hereby passed the neutral location N, the spring force is reversed, the spring 15 then being extended. If the valves remain open and substantially only the spring influences the piston's and the armature's movement, the armature is caused to oscillate about the neutral location N. During this oscillation, with every movement of the armature 11 past the stator 12, a current is induced therein and the stator's amplitude is gradually reduced. When the armature's amplitude has been reduced to such an extent that it falls below a predetermined minimum value, the combustion gas in the combustion chamber 4 can be caused to combust once again, with the result that a force is again exerted on the armature 11 in order to increase its amplitude to a desired value. If there is only a need for a little current from the converter, there may be no need to implement combustion in the combustion chamber 4 for every oscillation of the armature 11. The above-mentioned oscillation has a frequency corresponding to a natural frequency f c for the oscillation device which is formed from the spring 15, the armature 11, the piston 3 and the piston rod 5, and this frequency f e is dependent on the rigidity of the spring 15 and the total inert mass of the objects which are oscillating. With this energy converter, therefore, it is a very simple matter to obtain an electric current with a fixed frequency corresponding to the natural frequency Fig. 2 illustrates a second embodiment of an energy converter according to the invention. In this case a wall or flange 20 is provided between the piston 3" and the armature 11", and between the armature 11" and this flange 20 there is mounted a spring 21. On the opposite side of the armature 11" between it and the housing 1" there is mounted a spring 15". The armature 11", the piston 3" and the springs 15" and 21 here form the oscillating device. Fig. 3 illustrates a third embodiment of an energy converter according to the invention. Instead of the piston rod 5'" being rigidly connected to the armature IT", it is provided with a contact plate 25, a spring 26 being provided between the contact plate 25 and the armature 11'". The force created by the piston 3'" in this case is therefore transferred to the armature 11'" via the spring 26. The armature 11'", the piston 3'" and the springs 26 and 15'" here form the oscillating device. Fig. 4 illustrates a fourth embodiment of an energy converter according to the invention. On the side of the housing 1"" facing away from the cylinder 2"", there is provided a second cylinder 27 with a second piston 28 which is connected to a second piston rod 29. Between the armature 11"" and the cylinders 2"" and 27 respectively there are provided transverse walls 30, 31. Between these walls 30, 31 and the armature 1 i"" there are provided respective springs 32, 33, which are supported on the walls and the armature. The pistons 3"" and 28 are rigidly connected to the armature 11"" via piston rods 5"" and 35 respectively. According to requirements, therefore, a force can be exerted on the armature 11"" from either only one piston or both pistons. Fig. 5 illustrates a fifth embodiment of an energy converter according to the invention. The difference between the energy converters illustrated in fig. 4 and fig, 5 is that the two springs 36, 37 of the energy converter according to fig. 5 are mounted between the armature 11'"" and flanges 38, 39 at the ends of the piston rods facing the armature. The pistons 3"'" and 40 thus influence the armature 11'"" via the springs. The oscillating device comprises the springs 36, 37, the piston rods and the pistons 3'"" and 40. Where the pistons are connected to the armature via one or two springs, the pistons can be secured relative to the housing, e.g., by abutting against a portion of the respective cylinder tops when the oscillating device is oscillating freely, and for example compressed combustion gas can be brought into the combustion chamber and ignited when a movement of the pistons is required. If the armature is supported by the piston (fig. 1) and only one piston is provided, the connection between the piston rod and the piston must be rigid. If the armature has a separate guide or control, the piston rod may be connected to the piston via a piston bolt. Even though in figs. 4 and 5 two cylinders and pistons are illustrated which are mounted on each side of the armature, it will be understood that they may be mounted on the same side of the armature. Furthermore, more than two cylinders and pistons may be provided depending on requirements. It is illustrated above that the energy which is supplied to the converter can be converted to electrical energy if the relatively small amount of energy is discounted which is consumed in overcoming the friction between the movable and the stationary components. It will be appreciated, however, that an energy converter of the above-mentioned type can be used as a gas generator for production of an energy-rich exhaust gas, whose energy can be exploited by a further energy conversion. For example a gas generator according to figs. 2 - 5 can be very easily controlled, since any combustion and thereby exhaust gas production can take place, e.g. every time the piston is located at its upper dead point, or a whole number of piston oscillations can be performed between each time a combustion occurs in the combustion chamber. Furthermore, it is stated in the above that the elastic device is composed of springs, but it will be understood that any device can be employed which provides a return force which attempts to bring the body back to the neutral location N when the body is moved away from it. For example, the stator and the armature may comprise two pairs of interacting magnets with the same polarity, where between them is produced a force, which attempts to move the magnets away from each other, and which is a function of the inverse value of the distance between the magnets. One pair may attempt to move the armature to the left and the other pair may attempt to move the armature to the right. Such magnets are particularly advantageous if the oscillation frequency of the armature and the piston is high, as will be apparent below. In addition to a friction between the stationary and movable components, a resistance to the armature's movement will be exerted by the generator's stator. By introducing combustion gas into the combustion chamber and producing a combustion process therein corresponding to the combustion process in traditional internal combustion engines, the rate of combustion will be a maximum of approximately 10 m/s. A corresponding slow increase is thereby obtained in the pressure of the gas in the combustion chamber and the force exerted thereby on the piston. A relatively small proportion of the energy contained in the combustion gases is hereby also converted to kinetic energy by the piston, since a correspondingly large proportion is converted to heat which is taken away from the engine. In an internal combustion engine of this type, the pressure of the combustion gases and the corresponding force exerted on the piston are maintained during a relatively long period of time, and if the energy in the combustion gases has to be transferred completely to the piston, the piston must move in the same direction during the power transfer, i.e. in the direction corresponding to an increase in the combustion chamber's volume, viz. away from the combustion chamber. It will be appreciated that if a natural frequency of the piston/aπnature/spring device is chosen which is too high, and after a few oscillations of this device there is a need to compensate for a reduction in the oscillation amplitude by implementing a combustion in the combustion chamber, the situation may arise that during the combustion the device is moved towards the combustion chamber and against the force exerted by the combustion gases on the piston, which may cause the piston and the armature to be braked instead of accelerated. The interval, hereinafter called the transfer interval, during which the force from the combustion gases can be transferred, and which is a function of the natural oscillation frequency of the armature, must therefore be sufficiently great, i.e. the natural frequency must be relatively low. For linear generators with an oscillating armature/stator device and a stator, the efficiency, i.e. the proportion of the electrical energy which is converted in the generator, in relation to the armature's kinetic energy, is a function of the oscillation frequency. In order to obtain a high oscillation frequency with an energy converter according to the invention, the natural frequency of the piston/armarure/spring device, hereinafter called the armature frequency, consequently must be high. With a high armature frequency there is a need for a rapid transfer of the energy of the fuel to the armature since the transfer interval is small. According to the invention, therefore, instead of the above-mentioned, relatively slow combustion of the fuel, a detonation or explosion of the fuel in the combustion chamber may be chosen. A very rapid combustion of the fuel and a very large output are thereby obtained. For example, by exploding a dynamite cartridge with a diameter of 10 mm, an output of 4 GW is obtained. A device will be described below for utilising this output in connection with a linear generator as indicated above. Figs. 6 - 8 illustrate a schematic longitudinal section through an embodiment of a combustion chamber 50 of a free piston engine of the above-mentioned type. The combustion chamber 50 is defined by a cylinder 56 comprising a side wall 52 which is circular in cross section and an end wall 54, and a piston 58, which is axially movable towards or away from the cylinder 56, i.e. to the right or to the left in figs. 6 - 8. The piston 58 is connected to an armature of the generator (not shown), as mentioned above. In the cylinder 56 there is provided a first aperture 60. In the aperture there is provided in the cylinder 56 a valve seat 62 for a valve 64, which can be moved in the direction of a double arrow A, towards or away from the valve seat 62 in the known per se manner. The valve 64 may be arranged for very rapid movement by means of a device of a suitable type, e.g. a solenoid 66. Alternatively, the valve may be moved by means of the piston via a device, e.g. a mechanism. In the cylinder 56 there is further provided a second aperture 70, wherein there is arranged a nozzle 72. It will be understood, however, that instead of a valve 64 and a nozzle 72, either a valve or a nozzle may be provided in both apertures 60, 70. A first, gaseous fuel ingredient may be introduced into the combustion chamber 50 via the valve 64, and a second fuel ingredient may be introduced via the nozzle 72. A right-hand end portion 76 of the piston 58 which is in the form of a circular, axially extending peripheral flange, has a short, radial internal cylinder surface 78, and radially inside this cylinder surface 78 the piston 58 may have a radially and plane surface 84. The side wall 52 is trumpet-shaped and its left-hand end portion 80 is arranged to come into sealing abutment against the cylinder surface 78 when the piston 58 is located in a position wherein it has been moved a maximum distance to the right, as illustrated in fig. 6, By moving the piston 58 a short distance to the left, away from the position illustrated in figs. 6 - 8, a small opening is formed between the piston 58 and the cylinder 56, thus enabling combusted material to be removed from the combustion chamber 50, e.g. in a manner which will be described more fully in connection with fig. 9. If a combustion requires to be performed in the combustion chamber when the piston is in sealing abutment against the cylinder's left-hand end portion 80, the first step is to open the valve 64. A fixed amount of the first fuel ingredient is then introduced into the combustion chamber 50 via an opening between the valve 64 and its seat 62, as indicated by curved arrows in fig. 6. As illustrated in fig. 7, the valve 64 is then closed and a fixed amount of the second fuel ingredient is introduced into the combustion chamber 50 via the nozzle 72. The fuel ingredients may be of a type which, when mixed, instantly initiate a powerful chemical reaction, with the result that a detonation or explosion then immediately occurs in the combustion chamber, as illustrated in fig. 8. The pressure front obtained during the detonation or explosion may typically move at a speed of up to 9 km s towards the piston 58. On account of the curved shape of the cylinder's side wall 52, the pressure front acquires a shape which is approximately parallel to the flat surface 84. It will be appreciated that the shape of the wall may be different from that which is illustrated schematically here. All portions of the pressure front therefore strike the piston simultaneously and the pressure front's energy is transferred to the piston in the course of a very short time. It will be understood that the time taken for the transfer of heat energy from the combusted material in the combustion chamber to its surroundings is very short and that a loss of heat energy from the combustion chamber will be very slight. Since the piston's movement is transferred directly to the armature, i.e. without the piston's linear movement being converted to a rotary motion via additional components of the device, a very slight energy loss is obtained due to friction between components moving relative to one another. In fig. 9 it is illustrated that instead of the above-mentioned two fuel ingredients, explosive charges of, e.g. a solid explosive may be introduced sequentially into the combustion chamber. As illustrated in this figure, a combustion chamber 100 is defined by a cylinder 102 and a piston 104, which are substantially similar in form to those illustrated in figs. 6 - 8. The only essential difference is that in the cylinder 102, or more precisely its rear wall 106, there is provided a cylindrical, axially extending chamber 108, which communicates with the combustion chamber 100 via a narrowed portion 110, thus forming a contact shoulder 112 facing to the right in fig. 9. On the outside of the cylinder 102 there is arranged a substantially axially movable push body 114, whose left-hand end portion together with an adjacent area of the piston 104 and the cylinder 102 define a pressure compartment 116. The right-hand end portion of the push body 114 is arranged to abut against a sliding piece 132 which is arranged to slide axially in a guide tube or holder 120 which is securely connected to the cylinder 102. The sliding piece 132 is influenced by a spring device 122, which attempts to move the sliding piece 132 and thereby the push body 114 to the left in fig. 9 relative to the guide tube 120. In the axial extension of the cylinder 102, near the sliding piece 132, there is provided an ignition piece 134. In the sliding piece 132 there is provided a groove 136, which is open to the ignition piece 134, and the ignition piece 134 has a pin 138 which is arranged to project into the groove 136, and which is slightly shorter than the groove 136, considered in the axial direction. In the lower portion of the guide tube 120, e.g., there is provided an aperture 124 and to the guide tube 120 there is attached near the opening a magazine 126, which extends radially away from the guide tube 120. The cylinder chamber 108 is arranged to receive an explosive body 128 whose shape is adapted to the cylinder chamber 108, the explosive body's position in the axial direction being determined by the abutment of its left-hand end portion against the contact shoulder 112. The magazine 126 is arranged to receive a series of explosive bodies 130, these being stacked in the magazine 126 beside one another, whereby they are forced by a pushing device (not shown) in the direction towards the aperture 124. In a known manner, the explosive body's explosive and possibly the above-mentioned explosive ingredients may contain the oxygen required for an explosion of the explosive material. Furthermore, the arrangement of the piston 104, the generator's armature and the springs which attempt to move them in order to create an oscillation are substantially of the type illustrated in fig. 3. A successive firing and shifting of explosive bodies in the cylinder chamber 108 will now be described in more detail, on the assumption that an explosive body 128 is initially located in the cylinder chamber 108 and a series of explosive bodies 130 are stacked in the magazine 126. It is further assumed that the piston 104, the sliding piece 132 and the ignition piece 134 are initially located in the position illustrated in fig. 9. The explosive body 128 which is located in the cylinder chamber 108 may be caused to explode, e.g., by means of electrical energy, which is supplied to the explosive body via an electrical ignition circuit (not shown), or, e.g., by the ignition piece 134 being gripped via a hoop 140, moved slightly to the right against the force exerted by the spring 122 and released, whereupon the ignition piece 134 is moved in the opposite direction on account of the spring 122 and the kinetic energy, which is released by the ignition piece's impact against the explosive body 128, causes an explosion thereof. Due to the detonation pressure front, which is created after the explosion and which influences the piston 104, the piston 104 is moved very rapidly to the left in fig. 9, thereby receiving a very large amount of kinetic energy. Since the piston is moved away from the cylinder, an opening is formed between the cylinder and the piston via which explosion residue in the cylinder chamber 108 under great pressure can flow into the pressure compartment 116, where it puts pressure on the push body 114 for a short period, thus causing it and thereby the sliding piece 132 to be moved to the right, whereby the spring 122 is compressed and constricted. When the left-hand end of the sliding piece's groove 136 comes into abutment against the pin 138, the ignition piece 134, which hitherto has been in abutment against the cylinder chamber's right-hand end, is also carried along. When the sliding piece 132 and the ignition piece 134 have been moved so far axially that they no longer cover the aperture 124 in the guide tube 120, the explosive body 130 which is located nearest the guide tube 120 is pushed into it via the aperture 124. On account of the increased force of the spring 122, however, the sliding piece 132 and the ignition piece 134 will be reversed and moved to the left approximately at the moment when the explosive body is axially aligned with the cylinder chamber 108, whereupon the explosive body 130 is pushed into the cylinder chamber 108. During this process the piston 104 has also been reversed and moved back to renewed abutment against the cylinder on account of the springs influencing the piston and the armature. The ignition piece's pin 138 is hereby located in the right-hand portion of the groove. When the left-hand end of the explosive body 130 comes into abutment against the contact shoulder 112, the explosive body 130 is stopped while the ignition piece 134 is pressed with great force against the explosive body's right-hand end portion. The explosive body 130 in the cylinder chamber 108 is thereby caused to explode and the above- mentioned process is repeated. In a second embodiment of the invention whereby an explosive body located in the cylinder chamber 108 can be caused to explode according to other criteria determined by the piston's movement parameters, sensors (not shown) may be provided for measuring these movement parameters, such as the piston's axial position, amplitude, etc. These sensors (not shown) may for example be arranged to transmit signals to a computer (not shown) which calculates the values of the parameters, and which, e.g., is arranged to transmit an electrical firing signal to the cylinder chamber 108 via a suitable ignition circuit (not shown) for ignition of the explosive body which may momentarily be located in the cylinder chamber 108. When there is a need for a supply of energy to the piston/armature device, e.g, on account of an excessive reduction in its amplitude, at a time which has been determined by the computer on the basis of the signals received from the sensors, an ignition signal is supplied to the explosive body 128 which is located in the cylinder chamber 108, with the result that the explosive body 128 explodes. A new explosive charge is then brought into the cylinder chamber 108 and caused to explode in the above-described manner after the next oscillation period or a multiple of periods. In fig. 10 a further embodiment of an energy converter according to the invention is illustrated, where the springs, which influence the piston and the armature, and which are illustrated in fig. 9, have been replaced by four pairs of interacting magnets 150 and 152 respectively with the same polarity. By this means enormous forces can be created which can cause a reversal of the movement of the piston/armature device during its oscillation, thus preventing any collision between stationary and moving components. Instead of arranging separate explosive bodies in a magazine, the explosive bodies may be arranged on a belt which is driven by means of a suitable device, e.g. like that used for operating a machine gun.

Claims: PATENT CLAIMS 1. An energy converter comprising a free piston engine with at least one cylinder (2,2"",27), a piston (3 S 3",3'",3" ,, ,3 , "",28,40) mounted in the cylinder, a body (11, 11", 11'", 11"") connected to the piston and an elastic device (15,21, 15",26,15"',32,33, 36,37) which is arranged to exert a force in the cylinder's (2,2"") longitudinal direction against the body (11, H", 11'" 5 11"") and a corresponding reaction force against the cylinder (2,2""), characterized in that the elastic device (15,21, 15",26,15"',32,33,36,37) is arranged to either hold the body (11,11", 11"', 11"") constantly at rest in a neutral position (N) relative to the cylinder (2,2"") or to cause an oscillation of the body (11,11 ",11 '",11"") about the neutral position (N) with a natural frequency f e . 2. An energy converter according to claim 1, characterized in that it comprises an electric linear generator (10) with a stator (12) which is stationary relative to the cylinder (2,2""), and a part movable relative to the stator (12), hereinafter called an armature, which constitutes the body (11, 11 ",11"', 11""), and which is connected to the piston. 3. An energy converter according to claim 2, characterized in that the elastic device comprises an elastic element, e.g. a spring (15), and the piston (3) is rigidly connected to the armature (11). 4. An energy converter according to claim 2, characterized in that the elastic device comprises two elastic elements, such as springs (21,15 ",26, 15"', 32, 33, 36, 37) or magnets (150,152) with the same polarisation, which are mounted on each side of the armature (l l",i r", i r , l l' M "), considered in the cylinder's longitudinal direction. 5. An energy converter according to claim 4, characterized in that the piston (3,3",3'",3"") is either rigidly connected to the armature (11"") or connected to the armature (11'") via one of the springs (21,15",26, 15'" ) 32,33,36,37). 6. An energy converter according to claim 4, characterized in that the engine comprises two pistons (3"",28;3'"",40), which is arranged to move the armature in either direction, and which are either rigidly connected to the armature (I V") or each connected to the armature (11'"") via respective springs (36,37). 7. An energy converter according to one of the preceding claims, characterized in that the engine is connected to a consumer of the engine's exhaust gas energy. 8. An energy converter according to one of the preceding claims, characterized in that it is arranged to be operated by a fuel (128, 130) which creates a detonation in the cylinder (56,102). 9. An energy converter according to claim 8, characterized in that the energy converter comprises a device for successive introduction of the fuel at intervals into the cylinder. 10. An energy converter according to claim 8 or 9, characterized in that the fuel is explosive bodies (128, 130). 11. An energy converter according to claim 10, characterized in that the cylinder and a surface (84) of the piston define a combustion chamber (50), and that the portion of the cylinder's walls (52,54) which faces the piston surface (84) has a shape which, on detonation of the fuel, creates a pressure wave front which is parallel to the piston surface (84). 12. An energy converter according to claim 11, characterized in that the cylinder's walls (52,54) are widened in the direction away from the end which defines the combustion chamber.

Inventors: SAGOV MAGOMET S, SAGOV, MAGOMET, S.
Applicants: CLAVIS TECHNOLOGY AS, SAGOV MAGOMET S, SAGOV, MAGOMET, S.
Application year: 2001
Main classification: H05B
IPC codes: F02B71, H02K7