SK286429B6 - Rotation nose engine with internal combustion - Google Patents

Abstract

The rotary nasal engine with internal combustion works on the principle of a pair of the first rotor (1) and the second rotor (2) as well as with usage of a block (3), where the rotors are placed and rotate synchronously. The block (3), together with the circumference surface (1.9), nose (1.2, 1.3) of the rotor (1 ) and the rotor (2), determinates the engine's combustion chamber (4) in the shape of a torus, inside of which at least one nose (1.2) of the rotor (1) rotates. The rotor (2) has at least one contact part (2.9) with slots (2.7, 2.8) for the transition of the nose (1.2) on its outer circumference surface. By covering the opening (2.2) with the opening (3.2) and by rotation of the nose (1.2, 1.3) of the rotor (1), the intake of the medium into the engine's combustion chamber (4.1) takes place, in the combustion chamber, the determination of the rotor (2) and rotation of the rotor (1) the medium is transferred and compressed. During the nose's (1.2) transition through the slot (2.7), the compressed medium is transferred through the storage system (2.5), through its intake opening (2.4) and through the outgoing opening (2.6) into the engine's combustion chamber (4.2). In case of air or oxygen, the fuel mixture explosion as well as expansion is initiated as is the rotation of the rotor (1). By the rotation of the rotor (1) and by the rotor (2) determination, the exhaust emissions are transferred inside the engine's combustion chamber (4.2), further, by covering the opening (2.3) with the opening (3.3), by the rotor 2 determination, and by rotation of the rotor (1), the exhaust emissions are transferred out of the engine's combustion chamber (4.2). Consequently, the nose (1.3) of the rotor (1) moves through the slot (2.8), and the intake begins repeatedly.

Description

Technical field

The invention relates to internal combustion internal combustion engines and is directed to a conceptual change in the provision and performance of the operation of the piston internal combustion engine.

BACKGROUND OF THE INVENTION

Piston engines and compression ignition engines, as a type of internal combustion engine, are thermal engines that convert the energy of the fuel released by the explosion and combustion into mechanical energy. In this process, the driving medium is the direct conversion of chemical energy into mechanical and thermal combustion. The conversion is accomplished by a sequence of processes consisting in the preparation and transport of fuel, fuel mixture or air, its compression, initiation of ignition, expansion of combustion products, followed by the use of part of the generated energy to drive mechanisms and exhaust. This sequence of events is named as the working cycle of the petrol and diesel engines. Working cycle is ensured by positive-ignition and compression-ignition internal combustion engines, which operate using various design principles. Generally known types of spark ignition and compression ignition engines with static action of combustion products are linear piston engines. Of these engines e.g. the four-stroke gasoline engine operates in four phases, namely in the first stage the suction of the fuel mixture, which is a mixture of air and gasoline, in the second stage of its compression, in the third stage the compressed fuel mixture explodes by electric spark; The gasoline four-stroke direct injection engine also operates in four phases, namely air intake in the first phase, air compression in the second phase, followed by fuel injection, in the third phase the compressed fuel mixture explodes with an electric spark and expands and exhausts in the fourth phase combustion products. In the case of a diesel internal combustion engine, the compressed air is compressed to an explosive temperature, which at the end of the compression is enriched with diesel by injecting it into the combustion chamber of the cylinder, causing an explosion by the auto-ignition of the fuel mixture.

The energy conversion pressure to the piston ensures the transmission of the linear movement of the piston through the connecting rod and, in conjunction with the eccentric mounted crankshaft, transforms the linear movement into a rotary movement. In general, other movable elements are required for the operation of the cylindrical engine: the camshaft, the valves and the camshaft manifolds.

A more progressive concept of securing and executing events in the operation of the piston internal combustion engine is represented by a circular piston engine (Wankel engine). Its efficiency compared to compression ignition and petrol engines is increased due to the use of only a minimum number of rotating components and the absence of components performing sliding reciprocating motion. Its principle is that the process of preparing, igniting the fuel and utilizing the generated thermal energy generated by the fuel explosion is carried out using a circular piston having the shape of a triangular spherical prism. The circular triangular piston and the eccentric shaft rotate around their axes, but at the same time the piston moves along the orbit of the center of the shaft eccentric, that is, the movement of the piston is eccentric. The housing has an epitrochoid-shaped cylindrical surface inside. The side walls of the piston are constantly pressed against the walls of the housing. The ring piston is sealed with metal sealing strips and the piston is equipped with rounded strips. The type of engine, the shape of the combustion chamber and the top lubrication manifest themselves in particular in the increased fuel and lubricating oil consumption of the Wankel engine.

The aim of improving the parameters of the Wankel's rotary piston is the goal of a number of solutions that can be incorporated into the state of the art, but neither has been a fundamental change.

SUMMARY OF THE INVENTION

The rotary internal combustion internal combustion engine solves the above mentioned problems mainly by containing only two rotating elements stored in the block, but also by means of preparation of the fuel mixture, its transport, expansion, utilization of released energy in the combustion space, transport of exhaust gases and their exhaust outside the engine. Rotary internal combustion internal combustion engine is equivalent to a piston multi-cylinder four-stroke engine, whose mechanism consists eg. for two cylinders of up to 18 movable engine base parts (1 crankshaft, 1 camshaft, 2 pistons, 2 connecting rods, 4 hoists, 4 rocker arms, 4 valves), as opposed to the two movable base parts of the rotary internal combustion engine.

Rotary internal combustion internal combustion engine does not contain crankshaft, camshaft valves, pistons, connecting rods, hoists, rocker arms, valves and piping to them, eccentric rotating elements (crankshaft, Wankel engine rotor). The essence of the rotary nasal internal combustion engine is that it has only two basic rotating components - two rotors, compared to the 18 movable base parts of an adequate piston engine. The rotors of the rotary internal combustion internal combustion engine are stored in a block and processes such as fuel preparation, initiation of the combustion of the medium, conversion and utilization of energy and exhaust are effected by a sequence of structural and related parametric and functional combinations of processes typical of the internal combustion engine.

These processes are initiated and carried out using at least one pair of the first rotor and the second rotor, and using a block in which the rotors are mounted and rotated synchronously to one another and maintain a partial design and functional contact that is continuous, sealing and leaking. The rotational axes of the rotors are off-sides, preferably perpendicular or not perpendicular to each other. The rotors are continuously complemented structurally and functionally. The block, in addition to the function of the enclosure delimiting the space in which the rotors are housed, continuously defines, together with the rotors, the sealed or unsealed portions of the working chamber, which preferably has a torus shape. The first rotor is of cylindrical shape with at least one projection-nose on its peripheral wall, which moves in a working chamber which is bounded by the inner wall of the block and the peripheral surface of the first rotor as well as the rotating second rotor. The second rotor is cylindrical-plate-shaped with at least two structural modifications with cut-outs on its outer periphery. The first rotor comprises an axis-rotating shaft output for transmitting the drive of the driven system. The second rotor also has a rotary output shaft and is synchronously coupled to and driven by the first rotor. During rotation, there is preferably a tight and leaking contact of the rotors between and between the rotors and the block. The contact sections themselves, as well as the structural modifications of both the rotors and the block, create conditions in the chamber space for carrying out the events characteristic of internal combustion engines. A suitable position of the second rotor and the block and through the openings therein as well as the rotation of the first rotor ensures the suction of the medium (air, oxygen or fuel mixture) into the working chamber. The aspirated medium is rotated in front of the nose by rotation of the first rotor and compressed and, at the contact area, passed through the transition system in the second rotor to the working chamber behind the nose. Fuel is injected into the compressed air or oxygen in the process chamber (the fuel mixture can preferably be compressed by rotation of the second rotor) and ignition of the fuel mixture is initiated. The explosion expands and initiates rotation of the first rotor. Subsequently, by rotating the first rotor and delimiting the second rotor, the flue gas in the working chamber is moved in front of the contact area of the second cut-out of the second rotor. By suitably positioning the second rotor and the block and through the apertures therein, as well as defining the second rotor and rotating the first rotor, exhaust gas is provided. Subsequently, the nose of the first rotor passes through the contact area using a recess on the second rotor and suction begins again.

For the rotary internal combustion engine, which is the subject of protection, there are obvious differences, but especially advantages over the piston engine, namely: substantial simplification and reduction of the design of internal combustion engines, reduction of engine production costs, high reliability and reliability, resulting reduction repair and maintenance costs, further reduced fuel consumption, increased power, significantly less mechanical losses, higher overall (effective) efficiency compared to reciprocating engines, mainly due to better mechanical efficiency, there is no oscillation when rotating the rotary engine than with reciprocating piston engine thus vibrations are not transmitted to the frame e.g. resulting in less noise, less spring load, maximum combustion pressure in the rotary engine working chamber is likely to be more than 30% lower than the equivalent piston engine considered, lower short-term mechanical load on rotor nose and chamber, lower maximum temperature assumed in the combustion chamber, there is no torsional vibration at the engine, only the output shaft is subjected to torsion, further perfect engine balancing, the engine could work at significantly higher revolutions than piston engines or even Wankel engine (higher revs - higher power), application e.g. in sports cars, it is assumed that the engine can be operated at approximately 20,000 rpm for excellent balance. ' ¹ , the rotary engine may be designed as a spark ignition or compression ignition engine, suitable for use with other conventional as well as alternative fuels, naturally aspirated or supercharged, the rotors also acting as flywheels. Expansion of the engine generates direct torque on the shaft, unlike piston engines with a crank mechanism, where the resulting piston force is transmitted from the piston through the piston pin, connecting rod and connecting rod bearing to the crankshaft, causing mechanical losses and loads during this transmission. there are several components. The rotary internal combustion engine uses an extremely efficient space that occupies approximately one-third the piston engine at the same effective power, with the same dimensions assuming performance several times higher, another advantage is that it will reach about 70% of power weight Piston compression ignition engine, the maximum piston speed compared to the piston engine is assumed to be more than 8% lower.

Compared to the Wankel engine, the advantages are particularly apparent: Wankel engines have complications with corner seals that do not occur in the OM engine, the surface area to work chamber volume ratio is significantly smaller than that of the Wankel engine through the slot combustion chamber. CO and unburnt hydrocarbon (HC) emissions from the combustion chamber walls of the OM engine will be lower than those of the Wankel engine and comparable to those of piston engines, it is consistently proposed to use top lubrication but less lubricant consumption is expected than the Wankel engine.

The working pair of rotors together with the block can be combined in several combinations at the same time, eg. on three off-axis axes, each of which has one first rotor of system I and one second rotor of another system II, the first rotor of which is located on another axis, etc., or as a combination of one second rotor with more than one first rotor located around the periphery of the second rotor.

BRIEF DESCRIPTION OF THE DRAWINGS

The principle of a rotary nasal internal combustion engine and a method of preparing the combustion mixture, igniting it and utilizing the energy released to utilize the method are shown schematically in the figures. Since the solution to be protected creates preconditions for a number of variants of a particular construction application and its nature can be expressed only by depiction of several states, the individual figures should be understood only as illustrative to explain the essence of the invention.

In FIG. no. 1-10 shows a longitudinal section through the rotor 1 and a transverse section through the rotor 2, the working sequence of the rotary nasal internal combustion engine with two noses on the rotor 1 and explains the principle of the method of preparation of the combustion mixture, its ignition and utilization of released energy.

In FIG. no. 11 is a cross-sectional view of the rotor 1 and a longitudinal section through the rotor 2 identical to FIG. no. 1 of the operating sequence of a two-nose rotary internal combustion engine on a rotor.

In FIG. no. 12 is a longitudinal section through the rotor 1 and a transverse section through the rotor 2, the state of FIG. no. 1 of the operating sequence of a single nose rotary internal combustion engine on a rotor 1.

In FIG. no. 13 is a longitudinal section through the rotor 1 and a cross section through the rotor 2, the state of FIG. no. 1 of a four-nose rotary internal combustion internal combustion engine operating on a rotor 1.

In FIG. no. 14 is a cross-sectional view of the rotors 1 and a longitudinal section through the rotor 2, the state of FIG. no. 1 of the operating sequence of a rotary nasal internal combustion engine with two noses on the rotor 1, when with the rotor 2 the workpieces form more than one rotor 1 - a total of 12 rotors 1.

In FIG. no. 15 is a perspective view of a complex of more than one pair of rotors 1 and 2 of a rotary internal combustion internal combustion engine, preferably mutually interconnected on three off-axis axes, each having one first rotor of assembly I and one second rotor of another assembly II. whose first rotor is located on a further axis, etc.

Single images 1-10:

Fig. 1 and 2 show the suction of the medium behind the nose of the rotor 1 into the working chamber 4.1 through the first section 3.2 of the suction channel in the block 3, the second section 2.2 in the second rotor 2 1.2 of the first rotor 1 in the working chamber 4.1.

Fig. Figures 3 and 4 show the termination of the suction of the medium and the transfer of the medium behind the nose 1.3 of the first rotor 1 in the chamber 4.1, the transfer of the flue gases in the chamber 4.2 and the compression of the media in front of the nose 1.2 of the first rotor 1 as well as the passage of the nose 1.2 of the first rotor 1 through a suitably shaped slot 2.7 on the second rotor 2.

Fig. 5 shows the movement of the sucked medium behind the nose 1.3 in the chamber 4.1 and the flue gas in the chamber 4.2 and the movement of the pressurized medium from the reservoir 2.5 in the rotor 2 through the opening 2.6 into the space behind the nose 1.2 of the rotor 1 and the rotor

Second

Fig. 6 shows the displacement of the suction medium behind the nose 1.3 in the chamber 4.1 and the flue gas in the chamber 4.2 and the fuel injection (if the medium has not been enriched with fuel already at the inlet through the suction ports 3.2 of block 3).

Fig. 7 shows the transfer of the suction medium behind the nose 1.3 in the chamber 4.1 and the flue gas in the chamber 4.2 and the ignition of the medium behind the nose 1.2 of the rotor 1.

Fig. 8 and 9 show the transfer of the sucked medium behind the nose 1.3 in the chamber 4.1 and the flue gases and their extrusion in front of the nose 1.2 of the rotor 1 in the chamber 4.2 through the openings 2.3 and 3.3 and gas expansion - conversion from thermal energy to mechanical in chamber 4.2.

Fig. 10 shows the transfer of the suction medium behind the nose 1.3 in the chamber 4.1 and the flue gases in the chamber 4.2 as well as the passage of the nose 1.3 of the first rotor 1 through a suitably shaped slot 2.8 on the rotor 2 and then suction begins again.

DETAILED DESCRIPTION OF THE INVENTION

The rotary internal combustion internal combustion engine is original in its construction in that it contains only two rotating elements - rotors 1 and 2 housed in block 3, but also in processes characteristic of the operation of the internal combustion engine.

The rotary internal combustion internal combustion engine operates on the principle of at least one pair of the first rotor 1 and the second rotor 2 and using a block 3 in which the first rotor 1 and the second rotor 2 are mounted and rotated. The rotors 1 and 2 rotate synchronously to one another and continuously maintain a partial structural and functional contact that is sealing and leaking between the rotors 1 and 2 and the block 3. The axes of rotation of the rotors 1 and 2 are off-sides, preferably perpendicular to one another or suitably offset from the perpendicular direction. The first rotor 1 and the second rotor 2 are continuously constructed structurally and functionally. The block 3, in addition to the function of the enclosure enclosing the space in which the first rotor 1 and the second rotor 2 are housed, continuously defines, together with the rotors 1 and 2, the sealed or unsealed portions of the working chamber 4.1, (4.2, etc.). The working chamber 4.1, (4.2, etc.) preferably has a torus shape and is delimited by the inner wall 3.1 of the block 3 and the circumferential 1.9 of the first rotor 1 as well as the rotating second rotor 2. It is preferred that the first rotor 1 is cylindrical at least one projection through the nose 1.2, 1.3, etc., on its circumference 1.9, which rotates in the working chamber 4.1, (4.2, etc.). The second rotor 2 is cylindrical-plate-shaped, with cutouts 2.7, 2.8, etc., at its periphery 2.9. The first rotor 1 comprises a rotary output shaft 1.1 on a pivot axis for transmitting the drive to the driven system. The second rotor 2 is synchronously connected to the first rotor 1 by a rotary output - shaft 2.1 on the axis of rotation. The contact area of the first rotor 1 and the second rotor 2 is provided with at least two cut-outs 2.7, 2.8, etc. on its perimeter 2.9 and at least one nose 1.2 (1.3, etc.) whose perimeter 1.8 follows the volume of the working chamber 4.1, (4.2 etc.), and this nose 1.2, (1.3, etc.) is located on the first rotor 1.9 1. Cutouts 2.7, 2.8 etc. are fitted with such designations as to permit the sealing and leaking passage of the nose 1.2, (1.3, etc.) through these cutouts 2.7, 2.8, etc. A suitable position of the second rotor 2 with the opening 2.2 therein, against the block 3 with the opening 3.2 therein, further by defining the second rotor 2 as well as the rotation of the first rotor 1 ensures suction of medium 7 (air or oxygen or fuel mixture) into the working chamber 4.1, for nose 1.3. The aspirated medium is moved by the rotation of the first rotor 1 and delimited by the second rotor 2 in the working chamber 4.1 to the contact area of both rotors, while at the same time delimiting the second rotor 2 and in front of the nose 1.2 the medium is compressed. The compressed medium is moved from the nose 1.2 of the first rotor 1 of the working chamber 4.1 through the transition system 2.4, 2.5, 2.6, its inlet opening 2.4 and the outlet opening 2.6 present in the second rotor 2 to the working chamber 4.2, beyond the nose 1.2 of the first rotor 1 after the nose 1.2 of the first rotor 1 passes through the contact area of the first cutout 2.7 of the second rotor 2. Here, the medium can still advantageously be compressed by rotating the second rotor 2 and its suitable shape (when only air or oxygen is moved) the explosion of the fuel mixture in the working chamber 4.2 either by the compression of the mixture itself by self-ignition or by ignition of a spark 5.2. Explosion and expansion initiates rotation of the first rotor 1. Subsequently, by rotating the first rotor 1 and delimiting the expensive rotor 2, the flue gas is moved in front of the contact area of both rotors 1 and 2 to an expensive slot 2.8 of the second rotor 2. therein, against the block 3 with the opening 3.3 therein, further by defining the expensive rotor 2 as well as the rotation of the first rotor 1, the flue gas 6 is discharged from the working chamber 4.2. Subsequently, the nose 1.3 of the first rotor 1 is moved through the contact area of the second slot 2.8 of the second rotor 2 and the suction is initiated again.

Industrial usability

The rotary internal combustion internal combustion engine has the potential to be used where conventional piston combustion engines are used today, both static and dynamic, from small engines to aircraft engines to large ones, from high-speed to low-speed. The rotary nasal engine can be designed as a spark ignition or compression ignition engine, is also suitable for use with other conventional but also alternative fuels, has a natural suction, or can be supercharged. When converting chemical energy to mechanical, the OM motor is in a rotary motion, it is not in a linear motion, it has no oscillating motion, thus neither the return phase nor the eccentric rotations. The working pair of rotors together with the block can be combined simultaneously in several combinations, as described in the essence of the invention and in the claims.

Claims (11)

PATENT CLAIMS Rotary internal combustion internal combustion engine, characterized in that it consists of a block (3) in which a structural, functionally synchronized combination of at least one first rotor (1) with at least one second rotor (2) is arranged in partial contact with one another. is continuous and sealing and leaking, whereby - the axis of rotation of the first rotor (1) and the axis of rotation of the second rotor (2) are extruded, preferably mutually perpendicular to each other, or preferably offset from the perpendicular direction, - the first rotor (1) comprises a rotary output (1.1) - identical to the axis of rotation of the first rotor (1) for connection to the driven system (2.1) - identical to the axis of rotation of the second rotor (2), - the perimeter (1.9) of the first rotor (1) is provided with at least one nose (1.2), with a contact surface (1.8) adapted for sealing and leaking contact with the inner wall (3.1) of the block (3), perimeter (2.9) and cutouts ( 2.7, 2.8) of the second rotor (2), - the periphery (1.9) of the first rotor (1), the contact surface (1.8) of the nose (1.2) of the first rotor (1), the inner wall (3.1) of the block (3) defining a chamber (4.1, 4.2), preferably torus-shaped the circumference (2.9) of the second rotor (2) is provided with at least one contact section which extends into or at least delimits the chamber space (4.1, 4.2) and is provided with slots (2.7, 2.8) and this circumference (2.9) as well as the cut-outs (2.7, 2.8), in coordination with the first rotor (1) and the block (3), create conditions in the chamber space (4.1, 4.2) for carrying out events characteristic of internal combustion engines, - the first rotor (1), the peripheral contact portion (2.9) of the second rotor (2) and the inner wall (3.1) of the block (3) continuously define the chamber portions (4.1,4.2), - it is equipped with a fuel injection system (5.1) or, as appropriate, for preparing the fuel mixture and transporting it to the chamber section (4.2) of the working space, - the block (3) is equipped with at least one first section of the suction channel - an opening (3.2) in the block (3), which is connected to a corresponding starting system with suction of the medium (7) (fuel mixture, air or oxygen); ) is provided with a second section of the suction channel (2.2) in the second rotor (2), which is connected to the chamber (4.1), the first section (3.2) and the chamber (4.1) being interconnected by a second section of the suction channel (2.2) of the second the rotor (2) by rotating the second rotor (2) only during the intake of fuel mixture, air or oxygen (7), - at least one contact cut-out (2.7) of the second rotor (2) is provided with a transition system (2.4), (2.5), (2.6), consisting of a reservoir (2.5) with an inlet (2.4) from the chamber (4.1) and an outlet ( 2.6) into the chamber (4.2) for fuel mixture, air or oxygen, - the block (3) is provided with at least one second section with an outlet channel opening (3.3) which is connected to a corresponding flue gas outlet (6) and each second rotor (2) is provided with a first outlet channel section (2.3) which adjoins the chamber space (4.2), wherein the first section with the opening (3.3) and the chamber space (4.2) are interconnected by a second section with the opening of the outlet channel (2.3) of the second rotor (2) by rotation of the second rotor (2) only during exhaust gas (6); - the first rotor (1) and the second rotor (2) are adapted for synchronized rotation in the same direction. Rotary internal combustion internal combustion engine according to claim (characterized in that one basic engine operating set has two rotors (1 and 2), wherein a synchronized combination comprising one second rotor (2) with more than one first rotor is preferred. a rotor (1), wherein the first rotors (1) are arranged around the periphery of the second rotor (2), each forming a separate working set with the second rotor (2) and its working cycle angle offset by an angle relative to the minor first rotor (1) its location on the second rotor (2). Rotary internal combustion internal combustion engine according to claim 1, characterized in that one basic engine operating assembly has a first rotor (1) and a second rotor (2), wherein: - preferably at least two second rotors (2) are arranged perpendicular or not perpendicular to the plane of rotation of the rotor (1), - all these rotor assemblies are synchronously connected. Rotary internal combustion internal combustion engine according to claim 1, characterized in that one engine base assembly has a first rotor (1) and a second rotor (2), further, at the rotary output (1.1) of the first rotor (1) of the working assembly (1). I.) a second rotor (2) of the working system (II) is mounted next to this first rotor (1), further, the first rotor (1) of the working system (II) is mounted on another mutually advantageously mutually preferably non-perpendicular rotary output, opposite the rotary output a second rotor (2) of another working system (III) is mounted on this rotary output (1.1), the first rotor 1 of which is mounted on a mutually advantageously mutually preferably not perpendicular rotary output (2.1) of the second rotor (2) from the work system (I), where multiple off-axis axial-rotary outputs form more work systems, synchronously interconnected. A method of preparing a medium for an engine, wherein the suction and compression is carried out, ignited and utilized energy released - flue gas expansion and exhaust in a rotary internal combustion internal combustion engine according to claims 1 to 4, characterized in that using a continuous sequence of their associated parametric and functional combinations in time intervals, a continuous initiation and run of one process sequence, or at least two process sequences at a time, are carried out, which processes are mainly characteristic of internal combustion engine operation and initiate and take place in sealed or unsealed chamber spaces (4.1, 4.2). , ..), which are continuously defined from the chamber space, in which: - suction of fuel mixture, air or oxygen, - transfer of the fuel mixture, air or oxygen, before compression, - compression of the fuel mixture, air or oxygen, - transfer of the compressed fuel mixture, air or oxygen from the chamber (4.1), through the transition system, its inlet port 2.4, container 2.5, and the outlet port 2.6, to the chamber (4.2), - expansion, - transfer of flue gas after expansion before exhaust, - exhaust. Method for preparing a medium according to claim 5, characterized in that when the first rotor (1) is cylindrical with at least one nose (1.2) on the circumference and the second rotor (2) is cylindrical, its circumference (2.9) temporarily transversely splits the working chamber (4.1, 4.2, etc.) and temporarily directs the supply of fuel, air or oxygen to the working chamber (4.1) and temporarily stores and moves fuel, air or oxygen outside the chamber (4.1) through the transition system (2.4, 2.5, 2.6). ) into the chamber (4.2) and temporarily directs the flue gas outlet (6). Method according to claims 5 to 6, characterized in that the process of preparing the fuel mixture and the process of initiating the release of its energy is a continuous sequence of events and these are carried out in the following order: mixing fuel with air or oxygen which takes place outside the engine compartment bounded by the block (3), further sucking the fuel mixture into the partially sealed part of the chamber (4.1), then transporting and compressing the mixture in the sealed part of the chamber (4.1) and then: - is either forced through the inlet opening (2.4) into the storage volume (2.5) provided with the transition system (2.4, 2.5, 2.6) of the second rotor (2), which is first closed by the storage system (2.5) by rotation of the second rotor (2); by using the wall of the block (3) and thereafter the nose (1.2) using the cutout (2.7) on the second rotor (2) is moved through the cutout (2.7) and together with the perimeter (2.9) of the second rotor (2) form a transverse barrier 4.2), then by rotating the second rotor (2) the storage system (2.5) is opened and the fuel mixture is moved through the outlet (2.6) into the combustion chamber of the chamber (4.2), further initiating its energy release process or increasing its pressure rotating the second rotor (2) and then initiating the energy release process of the fuel mixture; or - is either displaced using the transition system (2.4, 2.5, 2.6) of the second rotor (2) as a connecting channel to the combustion part of the chamber (4.2) of the first first rotor (1), from at least one pair of first rotors (1) along the circumference of the second rotor (2) opposite the direction of rotation of the second rotor (2) and then initiating the energy release process or increasing the fuel mixture pressure by rotating the second rotor (2) and subsequently initiating the energy release process. Method according to claims 5 to 7, characterized in that the process of preparing the fuel mixture and the process of initiating the release of its energy is a continuous sequence of events in which air or oxygen is first drawn into the partially sealed part of the chamber (4.1). the fuel mixture component is transported and compressed in the sealed part of the chamber (4.1), as follows: - either pushed through the inlet (2.4) into the storage volume (2.5) provided with the transition system (2.4, 2.5, 2.6) of the second rotor (2), which is first closed by the rotation of the second rotor (2) with by using the wall of the block (3) and thereafter the nose (1.2) using the cutout (2.7) on the second rotor (2) is moved through the cutout (2.7) and together with the perimeter (2.9) of the second rotor (2) form a transverse barrier 4.2), then by rotation of the second rotor (2) the storage system (2.5) is opened, whereby air or oxygen is moved through the outlet (2.6) into the combustion chamber of the chamber (4.2) and then either enriched with the fuel component and subsequently initiating the energy release process or increase its pressure by rotation of the second rotor (2), and at the same time or thereafter enrich the fuel component, and subsequently initiate the energy release process of the fuel mixture, or - is either displaced by means of a transition system (2.4, 2.5, 2.6) of the second rotor (2) as a connecting channel to the combustion part of the chamber (4.2) of the first first rotor (1), from at least one pair of first rotors (1) along the circumference of the second rotor (2) opposed to the direction of rotation of the second rotor (2) and then initiating the energy release process or increasing the fuel mixture pressure by rotating the second rotor (2) and subsequently initiating the energy release process. Method according to claims 5 to 8, characterized in that the process of preparing the fuel mixture and the process of initiating the release of its energy is a continuous sequence of events in which air or oxygen is first sucked into the partially sealed part of the chamber (4.1), this component of the fuel mixture is transported and compressed in the sealed part of the chamber (4.1), as follows: - is either forced through the inlet opening (2.4) into the storage volume (2.5) provided with the transition system (2.4, 2.5, 2.6) of the second rotor (2), which storage volume (2.5) is first closed by rotation of the second rotor (2) the block (3) and for this purpose the nose (1.2) is moved through the cutout (2.7) using the cutout (2.7) on the second rotor (2) and together with the perimeter (2.9) of the second rotor (2) form a transverse barrier in the chamber (4.2) ), then the storage system (2.5) is opened by rotation of the second rotor (2), whereby air or oxygen is moved through the outlet (2.6) into the combustion chamber of the chamber (4.2) and then enriched with the fuel component and increased (2) and then initiate the fuel release process, or - either move using the transition system (2.4, 2.5, 2.6) of the second rotor (2) as the connection channel to the combustion section of the chamber (4.2) of the first first rotor (1) ), of at least one pair of first rotors (1) arranged preferably evenly around the periphery of the second rotor (2) opposed to the direction of rotation of the second rotor (2) and then enriched with the fuel component and increasing the fuel mixture pressure by rotating the second rotor (2); its energy. Method according to Claims 5 to 9, characterized in that at least one action is carried out within the rotation of the first rotor (1) with more than one nose (1.2, 1.3, etc.). Method according to Claims 5 to 10, characterized in that at least one action is carried out by rotating the first rotor (1) with one nose (1.2) by two turns.