WO2015003818A2 - Brinkmann turbines having active seals, precompression, post-expansion and wankel two-stroke function - Google Patents

Abstract

Philosophically speaking, the force-generating Brinkmann turbine assembly is a machine that goes back to the minimum number of parts currently necessary, in which the principles of universal symmetry are used fully and therefore permit turbine-like rotation. This leads automatically to immense but economical force generation in the smallest possible space. The fixed points can also be limited to THREE as the minimal centrally symmetrical requirement, in which case, in a manner of speaking, it no longer matters whether the rest of the universe rotates around the dervish or the latter rotates in the universe. Asymmetrical parts are largely eliminated as rotary bodies, especially the crankshaft as such, which is only still used for relatively slowly rotating special applications. The space remaining at the front of the Brinkmann turbine is taken up by the likewise stationary asymmetrical parts of fuel pump, oil pump and water pump, which are coupled to the front, stationary planetary gearbox, and by the air duct. The smallest possible imbalance has an effect radially at the most. The energy recuperation cycles are brought to a preliminary maximum level in the Brinkmann turbine, which is likewise attributable to the symmetrical configuration as a principle and at the same time ensures extremely quiet running of the Brinkmann turbine even at the highest rotation speeds. All this applies not only during the use of self-igniting diesel fuels, because a very large amount of compression is now available and can also be kept frictionless owing to active sealing technology, but also to the use of combinations of fuels or propellants that can be produced from electricity, which makes it possible in a manner of speaking to transport electricity as an easily stored liquid, which however has a high energy density. Insofar as the invention relates to the conventional rotary piston principle as turbines and pumps for expandable media or liquids under pressure, the improvements are likewise primarily attributable to better active sealing possibilities, but also relate to the arrangement of the inlet and outlet elements in combination with the asymmetrical symmetrical Wankel-type rotors specifically described here, and to the use of catalytic combustion by means of H2O2 in such turbines.

Description

 Brinkmann turbines with active seals, pre-compression, re-expansion and Wankelzweitaktfunktion.

The subject of the invention are dual-functional Wankelartige combustion engines with triple compression, symmetric Wankelzweitaktfunktion, triple expansion and double recharge and active seals. A second object is rotary steam turbines for direct drive or propulsion of generators in cars with H 2 O 2 or combinations thereof with others producible by electricity

Fuels. A third object are rotary steam turbines for driving

Generators in steam power plants or similar applications also pumps of the

Principle for the generation of torque with relaxable media or with liquids under pressure.

In the current state of the art in the art of Wankel engine construction, the principles of the inventor Felix Wankel from Germany are mainly applied, which were developed by him from 1930. He could build the first engine but not before 1950. Since the rotary engine (the housing and the rotor revolve around the fixed crankshaft) proved to be impractical at that time, the principle was kinematically reversed by Paschke and became a rotary engine. Companies producing this engine today include Mazda with the RX 8, VW AG, Wankel AG and Mistral. There are still problems with the gaskets that, for example, can not withstand the much higher pressures required for true diesel operations.

However, the majority of today's internal combustion engines that produce higher pressures are still working with pistons. However, the engines with pistons have a big problem in the field of kinematics. Kinematics is the branch of the theoretical

Mechanical engineering, in which mechanical movements are studied. Here, the reciprocating motion proves to be the Achilles heel of the piston engine. The masses need to be rotated twice per revolution of the crankshaft in each case

set in motion in the opposite direction. This causes tremendous tension in the connecting rods and in the piston, as well as in the

Fasteners. In addition one needs hundreds of trouble-prone parts eg ice he eae oc e as it must and in addition. The crankshaft in a piston engine is the most dreadful nightmare of a stress analyst with tensions and twists in each direction associated with constant change. The use of metals requires cooling thereof, which means that much of the engine's energy is tapped off. By

complicated shapes e.g. Motor blocks can not be used on a large scale for temperature-insulating ceramics, thus preserving the temperature problem of the reciprocating motor, ie requiring high cooling. Hard ceramics get slightly cracked during their production when they have to combine very thick and very thin areas due to the different cooling rates. A problem which does not occur with centralsymetrischen industrial ceramics.

Combustion turbines also have a very poor efficiency because they are basically open tubes with paddle wheels. For example, you fill it with gallons of fuel on one side and leave in fractions of a second

Energy as a cloud of smoke, noise and heat the turbine on the other side. In order to prevent the gases from rotating, stators have to be installed, which generate a large resistance and thus further impair the efficiency.

Steam turbines used today (Parson turbines) for generating electricity do not have high efficiency because they are also basically open pipes. They also lack a way of better sealing to turn electric generators more economically. For all axial turbines applies that stators are necessary to prevent the rotation of the driving medium to prevent, ie counter-rotating fixed paddle wheels which align the flow of the medium again axially. So these are really pointless resistances at which the used energy breaks. Both kinetic and thermal. This explains the miserable efficiency of this waste technology. In addition, the complexity to make these turbines is tremendous. This requires a lot of work and energy. These turbines are also tons heavy behemoths. Only by padding with fuel is so even a so-called "economic"

Working method with today absolutely common generation principle of electrical energy via steam generation achieved, but only because there is nothing better. But that's first and foremost why electricity is such an expensive form of energy. All of this is inextricably linked to the safe phasing out of fossil oil supplies within the shortest possible time, as according to the reputable sources of information, peak (peak) oil production already took place in 2006. So less and less is being produced, and that is why the prices are soaring and thrift is important. PROBLEMS TO BE SOLVED IN THE WANKEL PRINCIPLE:

A problem with the lack of compression, because when Wankelmotoren than

Combustion engines or be used as a combined converter of propellant energy. For example, To run an economical diesel process in Wankel engines, it would first be necessary to increase the compression and thus the temperature in the combustion chamber to more completely burn the fuel as it is injected. By higher compression is basically a better one

Use of fuel or propellant possible, but also a higher

High limit for aircraft engines, since the air pressure at high altitude is known to be strong

subsides. THE SOLUTION OF THIS PROBLEM consists in a three-stage compression, a symmetrical combustion in the Wankel symmetric housing (dual function or two-stroke function), a subsequent expansion with water as fuel and in an additional double increase of the compression by the intelligent use of the residual energy of the exhaust gases. The latter by exhaust gas charger plus a compression by a reciprocating compressor, because the higher the total compression the better.

B A problem with the seal of Wankel engines. This problem in Wankel

Engines are to be seen in connection with the lack of stability of the previous seals with simultaneously required adaptability. These seals are not strong enough in current technology to withstand the higher compression required for, for example, diesel processes. Therefore, it is necessary to find a better principle seals of Wankel engines. Traditional rotary gaskets also had a problem with the generation of chatter marks and too much friction. TO SOLVE THESE PROBLEMS, I propose active, so-controlled seals, so that an almost friction-free running with the smallest sealing gap can be realized. 1/1000 mm is easily realizable with this new sealing technology.

C A problem with the complexity of today's engines, these are not sufficiently simple in design, mainly when compression is needed. See Napier Nomad, considered the most efficient piston engine, but monstrous in its complexity. In order to solve this problem in the first place, the kinematic reversal of the entire previously practiced Wankel engine principle, ie the return to the ingenious original idea of Felix Wankel, is needed again. Namely one

fixed crankshaft and a symmetrical housing rotating around it, which is also its own flywheel to use. n. em m er omp exe rn.

reduces the Wankel principle to a sheer lack of components, by perhaps only one steam-generating propellant (H202) in one with pre-compression

Wankeldampfturbine brings to use. (This with both the kinematically restored to the original type and the Paschke modification) In the first case, there are then two moving parts, one is the rotor and the other the housing. In the latter case, the rotor and the crankshaft moves as has been practiced in recent years.

E A problem with the efficiency of conventional Parson turbines, which are miserable in this respect. The improvement of efficiency in the generation of electricity is therefore urgently needed and finally a better principle should be used. I suggest, because the Wankel principle like the Parson turbine is also a pump and it does not matter to the pump whether it's turning on its axis

To pump medium or whether a medium flows into the pump whereupon its axis rotates to use a special Wankel turbine to turn el. Generators. First of all, the axial steam entry is problematic with Parson turbines. To solve THIS PROBLEM BASIC, there are with the Wankelprinzip the

Possibility that the kinetic energy ALREADY RADIAL enters a rotary steam turbine. It saves the force deflection by 90 degrees as it is necessary for axial entry with conventional paddle wheels. This alone enormously improves efficiency. But secondly, in the Parson turbine as well as in the Wankel principle, the seals were the problem, so the new sealing technology is in

Wankeldampfturbinen also reduce energy losses on a large scale by less steam, which otherwise only heats the environment, will escape. Steam that can not escape does not have to be costly and polluting. Friction is also eliminated by the new sealing technology, and the expansion can be completely unhindered by a new rotor shape directly on a large area directly in the required direction of action. Wankel turbines and Wankeldampfturbinen can be built from very small to very large and are therefore suitable for a variety of uses where previously only

significantly more imperfect technologies were available. Above all, the wankelike asymmetrical symmetrical rotary piston will help.

The purpose of the invention is to be achieved by the following means:

1) in a first version by a gear driven compression turbine which in a first step by the decrease of a spirally shaped cross section In this case, it does not regenerate at this rapid air flow, whereupon this air is under increased pressure

Speed in a second step Pdyn = Pstat (Bernoulli pressure) is converted with a counter-rotating centrifugal impeller in three times higher pressure. The air moves thereby naturally and without artificially created resistors to the vortex principles of nature, whereby this compression process to three times the output pressure hardly any torque from the rotating motor housing per

Gear decreases and consumes.

2) in the same first version should then by a Wankel Vorrotor, which will produce a certain pressure as a Wankel compressor, this air in

Pre-compression further compressed and the 180 degrees offset current main rotor are pushed to there the compression in its subsequent

Maximize compression phase. In this double precompression combination, the pressure should first be at least ninefold. In total, the pressure should be at least 24 bar before the explosions. Furthermore, should after the

Haupttexpansionsprozeß after which expand the hot gases in a turn rotated by 180 degrees further rotating expansion chamber, by a Nachexpansion with the atomizing of water better use of energy used can be achieved by this steam generation cools the exhaust gas and the steam drives the Nachrotor, which in turn supports all

Compression phases, but still provides an additional benefit. This also because of an exhaust gas charge with a voluminous faster vapor-exhaust gas mixture produced by the water misting after the second

Expansion phase, the compression of fresh air with exhaust chargers should be further increased, whereupon on the housing from the outside and from the inside further air pressure generated by a compressor and this increased pressure of fresh air in both the central combustion process for blowing out the combustion chamber and in the Nachrotor should be returned to manage the water misting there. This is for the time being a maximum concept for energy recycling and thus maximum energy use would be achieved.

3) In the same first embodiment, the purpose of the invention is thus to be achieved by the fuel injection under high pressure from the inside via cams on the crankshaft. This should then, for example, diesel fuel in the

Compression phase of the main rotor can be injected and ignited via such cams on the crankshaft, whereupon the pressure of the explosion will rise enormously and the main rotor is to move in its direction of rotation. After this first

Expansion of the hot gases should be at least three quarters of these gases over a , , , -. This may also be controlled by cams or crankshaft segments which are eccentrically located on the crankshaft. There should then be the possibility, this hot, so still high-energy gas, which also with

SCAVENGING (aeration) can be heated to 1000 degrees with the introduction of air and water under high pressure, ie in the form of a mist during a second containment phase to a second expansion by steam generation before the hot gases leave the main engine part with the rotors , The same applies to other fuels or propellants such as methane or hydrogen also in

Combination with H202. But it is essential that when overflowing certain

Cam positions on the crankshaft certain high-pressure injections are triggered and thereby complicated and vulnerable valve outer controls would be eliminated as in normal engines. The real Wankeldiesel with two-stroke function would thus be completely without great effort selbststeuernd but also with high-performance electronic valves and Druckpufferspeicherungen shapable and where necessary, supplemented by additional valves and membranes.

4) In the same first version it should be possible to seal the rotor perfectly, namely by the generation of electricity in the rotors and with an electronics which the distance of the seals between the rotors in their three corners, as well as on the sides and the motor housing first measures an accuracy of one thousandth of a millimeter and then stops. This electronics should also be able to determine exactly the gradual position of the respective rotor on the crankshaft with indicators. By means of this sealing technology of the fully balanced running engine, one will be able to use the engine for dozens of years under the highest loads without wearing much material, e.g. also with the use of ceramics, both heat-conducting and non-heat-conducting. It should also be possible by the availability of electrical energy in the rotor other functions such as the measurement of fuel quantities both electronically and mechanically or fuels are thermally prepared (for example, heavy oil should be heated). Injections could also be precisely timed. This is achieved by simply turning the rotors with the release of openings or channels on the crankshaft as well as electronically.

5) In the same first embodiment, the simplification of the construction of the motor is possible because it will no longer be necessary to build hundreds of UNSYMETRIC moving parts, which can take place by the possibility of kinematic reversal of the previously known Wankel movement principle. Namely by a fixed crankshaft, which also the internal cooling of the engine (important

Fuels, as well as cooling and lubricants for reducing friction in the engine via the rotors allows.

6) In the same first version by cooling the fully symmetrical motor housing on the outside with axially, spirally or radially shaped cooling plates as

Components of the housing. The predominant engine mass will also act as their own flywheel mass, when doing the crankshaft fixed as a crank shaft stands still. Not only fuels, coolants and lubricants can be supplied via this central tube, but ultimately exhaust gases can be discharged as well

7) In the same first version by the construction of, for example, a Wankel Diesel engine, with a minimum of the use of fuel using

Steam generation from the heat of exhaust gases with water as a further blowing agent (substance), so as to achieve a minimization of size and weight but a maximum of power development and dynamics, with water or mixtures with other liquids first as a coolant and then as to be heated propellant can be evaporated. Above all, however, new fuel combinations are to be used especially those which can be generated from electricity such as hydrogen, methane and H 2 O 2. These fuels are ideal for use in the new Wankel-type engines. It can be used to build very small, powerful, efficient and fast-rotating engines with turbine-like speeds. But it is the same

Possibility of building huge Wankel heavy oil engines for flying ships heavier than air.

8) In a second version, the use of the propellant H202 is intended to cause the

Reduction of the total technical effort is made possible by

only this ELECTRIC CREATIVE "fuel" in the respective

Compression phase of the engine through a catalyst through (cold combustion) is sprayed. These motors can also be equipped with active seals and a more efficient rotor principle, namely asymmetric symmetrical rotors. The exhaust gas then consists of oxygen and distilled water.

9) In a third execution by the construction of very large Wankel Steam Turbines on the rotary piston principle but with active gaskets to generate electricity, thus giving a better efficiency than through

ParsonTurbinen gets, which by its axial steam introduction and extreme

Gasket losses are severely impaired in their efficiency. At the same time, the more effective rotor principle will help, namely that of asymmetrical symmetrical rotors. The principle can also be used for other media such as compressed air for motors and pumps. Detailed description of the figures

In order to make the subject matter of the invention easier to understand, the modalities of the preferred embodiment are shown schematically below and assume a character demonstrative example, wherein the reference numbers always refer to the same or corresponding elements in which the movements of rotors in stationary housings with Steps of 120 degrees counterclockwise take place. If the housings and rotors rotate on fixed crank shafts, the movements of these housings and the rotors are to be seen in the ratio of 3: 2 clockwise as they are connected by gears in inverse proportion, as usual in Wankel engines.

Fig. 1 is an isometric view of the main part of a Brinkmann turbine with a fixed cam crank shaft (0) mounted in the base plate (1). In this base plate (1) is also a passage for air (2) which connects to the clockwise rotating housing end face of the supercharger housing (3) and with the suction openings (4) serves as an air inlet. By the pre-rotor (5) on the cam crank shaft (0) and around its fixed eccentric (6) with the

Turning clockwise, this air is first sucked in and then compressed. The conduit with valve (7) serves to push the precompressed air under pressure into the main rotor housing (8), which is firmly connected to the supercharger housing (3). The main rotor (9) then goes down into its own compression phase with subsequent explosion of the mixture of highly compressed air and the now injected under high pressure fuel. Since the eccentric (10) of the main rotor offset by 180 degrees on the cam crank shaft (0) is attached, this compression and explosion thus takes place below and the expansion of the hot gases continues in a clockwise direction until the hot gases through the valve located above ( 11) in the room of his

Compensating after-rotor (12) out, but which is at least 2 times longer than the main rotor (9), then to atomize water or mixtures of other substances with water under high pressure by means of compressed air. Nozzle nebulizers (compressor nebulizers) are based on an air flow and the Venturi principle for atomizing the liquid. Due to the subsequent expansion of the mist with the then about 1000 degrees hot exhaust gases is the Nachrotor

whereupon the generated steam-exhaust mixture moves on to the last one

Rotation chamber, so the post-rotation housing (13) via the valves (14) leaves. G. As it is, the front wall of the supercharger housing (3) houses the control rods (15) for the valve control (16) of the intake valves (4), which are controlled via the eccentric (17). In the same way, the slide valves (7) for the transfer of the

Controlled pre-compressed air to the main rotor housing (8), as well as the valves (11) for the transfer of the hot exhaust gases from the main rotor housing to the Nachrotor- housing and the valves (14) for the exit of the steam-mixed exhaust gas.

Fig. 3 is a side view of a cam crank shaft (0) for a Brinkmann turbine in which the cams (18) are for both high pressure fuel injection and high pressure injection of propellants (water or mixtures thereof). At the same time, these fluids have cooling and lubricating functions, and ultimately serve as evaporation agents to optimally utilize the energy of the fuel. The grooves (19) for passing the liquids (water, mixtures thereof, oil for cooling circuits, fuels, propellant) are located on the eccentrics (6, 10, 20) of the cam crank shaft (0). Also visible is the passage for air (2)

Fig. 4 is a front view of the main rotor (9) which rotates about the cam crank shaft (0) on its eccentric (10). He sweeps over the cam (18), each with a ball bearing (21) which is mounted on a slide (22) and in the main rotor (9) which is designed there as a guide, can move to the outside and inside. The slider has at the other end a small piston (23) attached, which moves in the cylinder (24) to the outside and inside, while the fuel is under high pressure, which in turn by one or more nozzles in the

highly compressed air of the respective combustion chamber is sprayed. Laterally there is a pressure accumulator with membrane (25) which store excess fuel under pressure and by an electronic valve timing in terms of time and volume, the fuel supply can accurately meter. (Fuel supply and discharge as well as controls to the three high pressure pumps are not shown.) The Z-combustion chamber mold (26) advantageously distributes the force vectors of the explosions in the direction of the desired direction of travel, mainly at the beginning of the respective explosion, since these vectors are always perpendicular to surfaces. These

Combustion chamber shape is embedded as an asymmetrical recess in the normal Wankelrotorform (27), which may be following the original walls of this or following the Z-shape sealed on the side walls. The return springs (28) (not shown) are in u dm zw sc en en ruc produ s em (24) attached.

Fig. 5 is a front view of the post rotor (12) which rotates about the cam crank shaft (0) on its eccentric (20). It passes over several parallel cams (18), each with a ball bearing (21) which are mounted on slides (22) and in the secondary rotor (12) which is designed there as a guide, can move to the outside and inside. The propellant is there either water, compressed air and or

Mixtures of these with other substances. The movements of the pistons of the slide of the ball bearings and springs are the same as described under Fig. 4. However, the post-rotor design may include multiple sets of three injector pumps since the post-rotor (12) is much longer than the main rotor (9) and because it will only accept expanded exhaust gas and provide for post-expansion by steam generation for better fuel economy. However, the post-expansion is amply sufficient to operate all the compression phases and thus to achieve a much greater overall efficiency. For the realization of this is in

Nachrotor (12) and the Z-combustion chamber shape (26) formed much sharper than in the main rotor (9) to namely supply a maximum of hot exhaust gases of the post-expansion. Any excess exhaust gases are still controlled directly via the valves (14), or drained via an overpressure valve. (This valve is not shown)

Fig. 6 In this isometric view of a Brinkmann turbine it is visible how the at least still 500 degrees hot exhaust gas vapor mixture from the valves (14) via lines (not shown) between the post-rotor housing (13) in the

Replace turbo compressor supercharger housing (29), and (via lines not shown) the co-rotating turbochargers (30) are supplied. These loaders (30) produce compressed fresh air streams which are immediately input to the two compressors (31) for further compression. This then highly compressed fresh air is immediately made available again in a further cycle the main rotor (9) for blowing out the exhaust gases from the local expansion phase. In this case, the exhaust gas is pushed into the compression space of the Nachrotors, which has a much larger volume, because it is longer and its asymmetrical contour is more pronounced. Thereupon, water is atomized from the interior of the rotor into this space, which evaporates immediately. Of course, by the steam enrichment, of course, the exhaust gas flow for the turbines (30) is much more voluminous so faster and the following he cdnem he em ruc sa. s to e so a further cycle of energy return and thus better

Contributes to energy use. Since the turbocharger co-rotates compressor combination, an energy recirculation entry can be made directly via the outside of the cam crank shaft (0) rotating housing, wherein the blowing of the respective expansion space of the main rotor (9) via the valves (11) from the main rotor (9) to Nachrotor ( 12) takes place and the introduction of the required compressed air via the outside rotating housing of the main rotor (9) takes place directly with the respective nozzle (32). Another

Compressed air is transferred through the housing to a groove with a hole in it

Cam crank shaft (0) shortly before the "crankshaft part" of the same order in the

corresponding groove of the eccentric Nachrotors can be tapped again as air pressure. Namely, with this increased pressure by more

To generate compression of the post-rotor compressed air by cam actuated pistons in cylinders for nebulization (not shown)

Fig. 7 is an isometric view of a set in front of the Brinkmann turbine

Gear transmission with a gear (33) which is mounted on the rotating housing of the Brinkmann turbine and drives the gears (34). These gears (34) run on axles (35) through the base plate (1) (not shown here) and carry on the other side of the gears (36), which in turn an impeller (37)

Centrifugal compression of air and the opposite intake funnel for air (38) drive (gears not shown). Of the gears 36, a ring gear (39) is also driven, from which torque can be removed. Thus, in front of the air inlets (4) of the pre-rotation housing (3), which is connected to an air passage (2) through the base plate (1) (not shown here), a compression turbine consisting of the parts (37) and (38 ) which by means of gear drive on its axis (40) rotate in opposite directions and the air for the first time

precompress and already under pressure through the air supply (2) in the rotating Vorverdichtergehäuse (3) with its intake ports (4) initiate.

Fig. 8 is a front view with magnets (41) on its eccentric, but

Sensors / Activators (42) Electronics (43) and coils (44) with indicator rings for power generation in the rotors. This combination is capable of generating electricity and using piezoceramic first measure the distance to the housing wall and then set the distance to a thousandth of a millimeter gap width with great speed, as well as using the indicator rings (45) to make accurate statements about the circular position. This information is in the electronics (43) to a It is possible to maintain the gap between the seal and the wall

Fig. 9 is an isometric view of the rotary turbocompressor compressor

Housing (29) which for the provision of the exhaust air of the respective

Expansion spaces of the main rotor housing (8) and for the compressed air supply of Nachrotors (12) is responsible for nebulization of the water. Therein are the

Exhaust valves (14) visible from which the exhaust-steam mixture flows into the rotating around the center of the Brinkmann turbine turbocharger (30). These generate a highly compressed fresh air stream which serves to blow out the expansion chambers of the main rotor housing (8) and which is generated in the cylinders of the compressor (31) by its rotating double-acting pistons on rotating connecting rods which rotate about the cam crankshaft (0) in this part resembles a normal crankshaft, though the part of course stands still. After this "crankshaft part" of the cam crank shaft (0) goes back into its central arch form around which rotates the entire Brinkmann turbine housing in the last central part of the

Cam crank shaft (0) which can also be used mechanically as a stationary fixed point, the exhaust gases can be introduced circularly (not shown), since this last part of the cam crank shaft (0) practically only a Steady albeit extremely stable and accurate executed central pipe is. The pistons of the downstream double-acting 2-cylinder compressor move in a completely circular manner around its crank shaft, whereby only the housing rotates, so practically no imbalance arises.

Fig. 10 is an isometric general view and concurrent overview of the Brinkmann turbine showing that this closed combustion process with multiple energy recirculation is an extremely useful way of generating torque because from the front to the rear 3 compression processes 3

Expansionsprozeße and again two compression processes combined and recombined with each other for the time being maximum heat-pressure feedback a Wankelzweitakt process under highest at the time so to achieve compaction to realize which should not be easily overtaken in its efficiency, especially a tremendous torque in the smallest space, even with the use of

Water instead of fuel, is developed. This is mainly because of the not so quickly limited rotational ability of the arrangement by their inherent symmetry, which thereby also acts as their own flywheel. G. orn er he to ur amp he runs a catalyst, wherein the thus produced about 500 degrees hot steam under pressure in a Wankel housing according to the principle of the rotary piston engine first Left Bottom enters to emerge on the right lower side and thereby the rotor continues to turn. Again, the SZ-form of the wankelähnlichen rotor is the

Increasing the overall efficiency because the pressure as the basic fact of physics always works perpendicular to a wall with a corresponding resulting vector component. Which, of course, has to be done taking into account the adequate direction of rotation of the rotor, since this is now asymmetrically symmetrical.

Fig. 12 is a front view of a Wankel steam turbine (46) where H2O2 passes over a catalyst, with the approximately 500 degree hot steam produced thereby under pressure into a Wankel housing according to the principle of the rotary piston engine by a reversing associated with rotor motion Now enters from the right top to exit on the left upper side and the rotor back to the starting position, so then then continuously rotate completely, because the process of

Reversal automatically with closure of other inflows and outflows.

Fig. 13 is a front view of a Wankel turbine (47) where steam or other releasable gas or fluid under pressure enters the lower left to exit to the right, continuing to rotate the rotor. Again, the SZ shape of the wankel-like rotor will increase the overall efficiency, because the pressure as a fundamental fact of physics always acts perpendicular to a wall with a corresponding resulting vector fraction. Which, of course, has to be done taking into account the adequate direction of rotation of the rotor, since this is now asymmetrically symmetrical.

Fig. 14 is a front view of the Wankel turbine (47) where steam or other relaxable gas or fluid under pressure enters from the right and exits the left as soon as the rotor has arrived in its home position before frictional engagement on the other side is, so now by a simple with the

Rotor position coupled reversal of the steam or another relaxable gas or a liquid under pressure from the other side and turn the rotor back to the starting position, so let continuously rotate completely, because the process of reversal repeats automatically.

Claims

 claims

After describing the exact nature of the function, I explain my invention as a novelty and therefore I make the following

Claims for:

1) main rotors (9) which rotate in Wankelartigen turbines, for

Combustion of fuels suitable and which with coils (44) for

Power generation via magnets (41) on eccentric cam crank shafts (0), with indicators (45), pumps (21, 22, 23, 24, 25), and with electronics (43) for measuring and regulating, with sensors (42) and actuators (42) are equipped for active seal on the basis of piezoceramic. Characterized by the fact that they pressurized from a crankshaft or a cam crank shaft (0) by internal pumps (21,22,23,24,25) fuel at an exactly adjustable time by cams (18), the pressure stored, the fuels can be injected into the compression and combustion area and self-ignited, for example, to achieve the possibility of good injection of diesel or heavy oil, and also fuel oil can be heated, but also by the fact that ideal combinations of electrically producible fuels such as H 2 O 2, methane and Hydrogen and LPG can be used. As further characterized by the fact that the main rotors (9) are sealed almost without friction on all sides towards the housing with highly stable piezoceramic measuring and controlled seals (42) to a thousandth of a millimeter gap, the feedable lubricating and cooling Fabric combination for circulating lubrication and cooling of mechanical parts, electronics, magnets, sensors and actuators, and also by the

Cam crank shafts (0) from or from the crankshaft ago, so from

Engine interiors, interact with these inflows and outflows of fluids, as well as with mechanical pressure and magnetic field energy for power generation. 2) Pre-rotors (5) of the same rotational dimensions as the main rotors (9) which rotate in Wankel-type turbines, but the pre-rotors (5) are generally longer than the main rotors (9), characterized in that they increase the pressure in main rotors (9) for a process of auto-ignition injection, thus causing a higher compression to the complete combustion of fuels such as gasoline, diesel, kerosene and heavy oil, the more economical use of LPG electrically generated fuels such as hydrogen, methane and hydrogen peroxide thus allow H202 in high concentration, the use of by and through

Exhaust gas generated steam, as well as catalysing, lubricating, evaporating and cooling agents as necessary, allow. They may also be equipped with self-standing seals as described above, provided that they have the necessary equipment such as e.g.

have internal power supply.

3) post-rotors (12) which rotate in Wankelartigen turbines and which are equipped with the same. Mechanical and electrical functions as described in claim 2, ie with coils (44) for

Power generation, electronics (43) for regulation, indicators (45), sensors and actuators (42) for active sealing and internal pumps

(21,22,23,24,25) etc. are equipped. Characterized by the fact that through them afterburning by compressed air and thus oxygen supply via the cam crank shaft (0), the misting of propellants in their the

Main rotor (9) opposite compression range can be made possible at a precisely adjustable time to the post-expansion of already hot exhaust gases together with these means for Scavanging and

To operate steam generation. Also characterized by the possibility of adding combined lubricating lubricants for circulation lubrication, which will provide internal lubrication of the mechanical parts and cooling of the electronics as well as the magnets. The post-rotors are further characterized by the fact that they also catalizing substances in the Injectors for liquids may have, which the

Steam generation in H202 Use with oxygen scavenging also possible in combination with other fuels that can be generated by electricity such as hydrogen or methane.

4) Symmetric double-function housing (for Wankelzweitaktfunktion with blowing out the exhaust gases and the reloading of new combustion air) even with a reduction in the relative movements between the rotors and housings, characterized by the completely symmetrical structure of the Wankelgehäuses it alternately past the air inlet (2)

Intake ports (4) of the symmetrical internal valve controls to the symmetrical outlets, which are also controlled symmetrically and are connected to the integrated symmetrical exhaust gas energy recovery, the two co-rotating exhaust gas turbines and also two rotary pistons on rotating connecting rods acting in two rotating cylinders, comprising and abovementioned rotary blowing out of the expansion phases of the

Allow main rotor (9) and Scavanging the exhaust gases and the supply of compressed air in the cam crank shaft (O) via one and the same rotating housing. Also characterized by the multiple possibility of supplying liquids from the cam crank shaft (0) in the

Housing walls (), which can be used for liquid cooling of the housing outer wall or for additional fuel or propellant via the housing, as well as its symmetry because of the possibility of such housing can put into extreme rotation.

5) Symmetrical asymmetric wankelartige rotors, which an asymmetric combustion and expansion space form while still maintained and

to realize a balanced central symmetry, characterized by the

Optimization of the useful vector areas which act positively in the desired direction of rotation. Characterized by the fact that the pre-rotors practically unchanged, possibly still slightly excessive Wankel rotor forms for the maximum compression, the main rotors (9) but already the asymmetric depressions in the original

Wankelform have been completely or asymmetrically to the

Align force vectors better in the direction of movement. Further characterized by the fact that in post-rotors and expansion and

Pressure fluid rotors assume an asymmetric dimples or completely asymmetrical configurations of an extreme shape, in order for the expanded gases from the main rotor (9) or other expansion

To provide maximum volume in the beneficial desired direction of action for receiving combustion gases for post-expansion or expansion generally. Ultimately characterized by the fact that these openings, lines and valves are released or covered by the further rotation of the rotors and or by internal eccentric valves or external electronic control the implementation and introduction of gases and media together with the rotation of the housing can be precisely timed and ideal for drives and vice versa pumps.

6) Wankel-type turbines are surrounded outside the housing with cooling fins radially or axially and spirally aligned, characterized in that they cool the housing by means of air and at the same time increase in its strength. Also characterized by the fact that carbon or other fibers can be applied or wound around these casings with special adhesives to further increase the stability of the casings for truly extreme speeds.

7) H2O2 Wankeldampf turbines (46), which can be constructed both with rotating housings on swiveled or fixed cam crank shafts (0) as well as with locked housings and crankshafts rotating therein, characterized by a pattern of simplicity of engine function characterized by Introduction of the H202 via the cam crank shaft (0) or via the housing depending on the application. Further characterized by rotors or housings, which for the catalytic cold combustion of H2O2 have built-in catalysts in the nozzles of the fuel injection, the rotors may also be formed with asymmetric-symmetrical recesses in the original Wankel rotor shape or completely asymmetrical-symmetrical and have active seals to a good efficiency of the drive or the process of electrical generation to obtain.

8) Wankel turbines (47) with alternatively usable inlet and outlet openings, characterized by the use of relaxable media such as.

Steam as propellant or of pressurized liquids and by the reciprocal introduction of the media to use in the electricity production to drive generators on a large scale or as other drives or pumps as the rotors also with asymmetric-symmetrical Profiles are equipped and have active seals to obtain a good efficiency of the process of electrical generation or other drive.

9) cam crank shafts (0) for Wankelartige turbines characterized by the possibility of on and Aus-eitbarkeit of fuel lubricants and coolants mounted on eccentrics wankelartigen rotors or to be able to initiate such substances directly in centrally rotating Wankelartige housing. Also characterized by the asymmetrical parts are eccentrics and cams which can perform a number of control functions and positioning under pressure via linkages and slides. Ultimately characterized by the fact that they can be derived via exhaust gas via holes via piezoelectric seals and behind an additional stable fixed point for suspension of the unit is created.

10) compressor combinations characterized both by the use of a vortex-shaped inlet funnel (38), the flow velocity and the medium air in rotation in combination with an opposite conventional compression impeller (37) generates the centrifugal force compression from the higher rotating flow velocity, as well as the combined use of conventional

Exhaust gas turbines (30) in a rotating housing together with a rotating double-acting piston compressor (31).

11) seals according to the described active principle of measuring and setting on a piezoelectric base (proportional current when pressure is applied to the ceramic, or extension of the ceramic upon initiation of a current) for all conceivable sealing problems of counter-rotating parts by piezoceramics to set a minimum gap and To minimize losses of trapped media as well as friction between the parts via an electronic circuit.