SK286927B6 - Rotation nose annular engine with internal combustion - Google Patents

Abstract

The rotary nasal annular engine with internal combustion operates 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 (4.1), (4.2) in the shape of a torus, inside of which the rotor (1) is rotating with at least one nose (1.2). The rotor (2) contains on its outer circumference surface (2.9), slots (2.7, 2.8) preferably for the transition of the nose (1.2).; During the nose's (1.2) transition through the slot (2.7), of the rotor (2) the compressed medium (7) is transferred through the storage system (2.5) of the rotor (2) through its intake opening (2.4) of the rotor (2) and through the outgoing opening (2.6) of the rotor (2) into the engine's combustion chamber (4.2). In the case of air or oxygen, the fuel mixture explosion as well as expansion is initiated as it is the rotation of the rotor (1).

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 mainly in the increased consumption of fuel and lubricating oils of the Wankel engine.

Efforts to improve the parameters of the Wankel's rotary piston are the object of a number of solutions that can be incorporated into the state of the art, but none of them represented a fundamental conceptual change.

SUMMARY OF THE INVENTION

The rotary nasal ring motor with internal combustion solves the above mentioned problems mainly by containing two (preferably three or more) rotating elements stored in the block, but also by means of preparing the fuel mixture, its transport, expansion, utilization of released energy in the combustion space, their exhaust outside the engine. The internal combustion rotary nasal ring motor is equivalent to a four-cylinder four-cylinder four-stroke engine whose mechanism consists of up to 35 movable engine base parts (crankshaft, flywheel, 4 connecting rods, 4 piston pins, 4 pistons and 4 piston ring sets, camshaft, 4-piston shafts) , 8 valve springs + spring retaining elements, 4 intake valves, 4 exhaust valves, not counting the camshaft drive mechanism (belts, toothed belt, pulleys), compared to two

(Preferably three or more) movable base parts in a rotary nasal ring motor with internal combustion.

The internal combustion engine rotary nose ring does not include crankshaft, camshaft, valves, pistons, connecting rods, hoists, rocker arms, valves and manifolds, eccentric rotating elements (crankshaft, Wankel engine rotor). The essence of the rotary nasal ring internal combustion engine is that it has only two (preferably three or more) base rotating components - rotors, as compared to 35 movable base parts of an adequate four-cylinder piston engine. The rotors of the rotary internal combustion engine are mounted in a block and processes such as fuel preparation, ignition 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 characteristic of internal combustion engine operation.

These processes are initiated and carried out using at least one pair of the first rotor and the second rotor (preferably two or more second rotors) and using a block in which the rotors are mounted and rotate to each other synchronously and maintain a partial structural 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 enclosing 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 torque shape. The first rotor is preferably cylindrical-plate-shaped 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 (preferably several second rotors). The second rotor (preferably a plurality of second rotors) may be of an annular shape with at least two design modifications as slits on its inner periphery. The first rotor comprises an axis-rotating shaft output for transmitting the drive of the driven system. The second rotor (preferably two or more second rotors) has e.g. a circumferential gear transmission is synchronously connected therewith to the first rotor that drives it. During rotation, there is preferably a tight and leak-free contact of the rotors with each other and between the rotors and the block. The contact sections themselves, as well as the constructional modifications of both the rotors and the block, create conditions in the chamber space for carrying out events characteristic of internal combustion engines.

In the further description of these events, the principles of the events of the rotary nasal ring motor with internal combustion are identical to those of the rotary nasal engine with internal combustion, registered at the Industrial Property Office of the Slovak Republic, under no. file PP 5068-2006 of 08/08/2006.

By suitably positioning the second rotor (preferably a plurality of second rotors) and the block and through the apertures therein, as well as the rotation of the first rotor, suction of the medium (air, oxygen or fuel mixture) into the working chamber is ensured. The aspirated medium is rotated in front of the nose by rotation of the first rotor and compressed, and at the contact area of the second rotor (preferably two or more second rotors) is moved through the transition system in the second rotor (preferably more second rotors) into the working chamber beyond the nose of the first rotor. Fuel is injected into the compressed air or oxygen in the process chamber (the fuel mixture can be preferably compressed by rotation of the second rotor - preferably two or more second rotors) 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 defining the second rotor (preferably two or more second rotors) and the block and through the apertures therein and further defining the second rotor (preferably two or more second rotors) 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.

The rotary nose ring motor with internal combustion which is the subject of the protection reveals differences, but in particular advantages over the piston engine: substantial simplification and reduction of the internal combustion engine design, reduction of engine production costs, high reliability and reliability resulting therefrom reduced repair and maintenance costs, further reduced fuel consumption, increased power, significantly less mechanical losses, higher overall (effective) efficiency compared to piston engines, mainly due to better mechanical efficiency, there is no oscillation when rotating the rotary engine motor, ie vibrations are not transmitted to the frame eg. vehicles, resulting in less noise, less stress on roasting elements, maximum combustion pressure in the rotary engine working chamber is probably 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 combustion chamber, lower emission of CO and unburnt hydrocarbons (HC), there is no torsional oscillation in the engine, only the output shaft is subjected to torsion, furthermore perfect engine balancing, the engine could work at substantially higher speeds than piston engines or even Wankel engine (higher speed - higher power), when application eg. in sports cars, it is assumed that the motor may be due to the excellent balance to operate at speeds in the order of about 20 000 min ^-1, the rotary engine can be designed as positive or as a diesel engine, it is suitable to use other conventional as well as alternative fuels , it may have a natural suction, or it may be supercharged, the rotors also serve as flywheels. Expansion at the engine generates directly torque on the shaft, unlike the piston mo

Crank mechanism ov6, where the resulting piston force is transmitted from the piston through the piston pin bearings, the connecting rod and the connecting rod bearing to the crankshaft, whereby mechanical transmission is incurred and several components are loaded. The rotary internal combustion engine uses an extremely efficient space that occupies approximately one-third the height and one-third of the equivalent four-cylinder piston engine at the same effective power, with the same dimensions assuming performance several times higher, 70% of the power weight of the piston diesel engine, the maximum piston speed compared to the piston engine is assumed to be more than 8% lower. Mounting a rotary nasal ring motor could be about 35% less time than mounting an equivalent four-cylinder piston engine.

Compared to the Wankel engine, the benefits are particularly apparent: in Wankel engines, there are complications with corner seals that do not occur in the rotary nasal ring motor, the surface area to work chamber volume ratio is significantly smaller than that of the Wankel slot combustion chamber. also the emissions of CO and unburnt hydrocarbons (HC) generated at the combustion chamber walls in the rotary nasal ring engine will be lower than those of the Wankel engine and comparable to the values of the piston engines; top lubrication, but it is assumed lower lubricant consumption than the Wankel engine.

The rotary internal combustion engine uses an even more efficient space than the rotary internal combustion engine, occupies twice the power of the rotary internal combustion engine and is equivalent to a four-cylinder four-stroke piston engine in the engine processes.

The working pair (preferably three or more) of the rotary internal combustion engine rotary nasal ring motor together with the block as one set can be placed on the same shaft-shaft simultaneously with other preferably similar sets, which is an advantage over the internal combustion internal combustion engine. are the axes of both off-rotor rotors.

BRIEF DESCRIPTION OF THE DRAWINGS

The principle of a rotary nasal ring motor with internal combustion and a method for preparing the combustion mixture, igniting it and utilizing the energy released to use the above method is 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. 1-13, the working sequence of the rotary nasal internal combustion engine with two noses on the rotor 1 is shown in a longitudinal section through the rotor 1 and a cross section through the rotor 2, and the principle of preparing the combustion mixture, igniting it and utilizing the released energy is explained.

In FIG. no. 14 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 rotary internal combustion engine with two noses on the rotor 1, as an example of half the rotation speed of the rotor 2 compared to the rotation of the rotor 1.

In FIG. no. 15 shows a longitudinal section through the rotor 1 and a transverse section through the rotors 2 and 9, the state of FIG. no. 1 of the operating sequence of a rotary nasal twin-ring internal combustion engine on a rotor 1.

In FIG. no. 16 shows a longitudinal section through the rotor 1 and a transverse 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.

Single images 1-13:

Fig. 1 and 2 show the suction of the medium behind the nose 1.3 of the rotor 1 into the working chamber 4.1 through the first section 3.2 of the suction channel in block 3, the second section 2.2 in the second rotor 2 and the compression of the medium in front of the nose 1.2 of the first rotor 1 in the working chamber 4.1; 1.3 of the first rotor 1 from the working chamber 4.2 through the first section 2.3 of the exhaust port in the second rotor 2 and the second section 3.2 in the block 3 and the expansion behind the nose 1.2 in the working chamber 4.2.

Fig. 3 shows the termination of the suction of the medium and the filling with this medium of the chamber 4.1 and the transfer of the medium through the nose 1.2 of the rotor 1 to the storage system 2.5 in the rotor 2 through the opening 2.4;

Fig. 4 and 5 illustrate the passage of the nose 1.2 of the first rotor 1 through a suitably shaped cutout 2.7 on the second rotor 2 and the passage of the nose 1.3 of the first rotor 1 through a suitably shaped cutout 2.8 on the second rotor 2 of the working chamber 4.2 behind the nose 1.2 of the rotor 1 and the rotor 2 and the exhaust gas from the chamber 4.2 upstream of the nose 1.3 through the first section 2.3 of the exhaust channel in the second rotor 2 and the second section 3.2 in the block 3; of the rotor 1 and suck the media behind the nose 1.3 of the rotor 1 into the working chamber 4.1, through the first section 3.2 of the suction channel in block 3, the second section 2.2 in the second rotor 2.

SK 286927 Β6

Fig. 6 shows the fuel injection behind the nose 1.2 in the working chamber 4.2 (if the medium has not been enriched with fuel at the entry through the inlet ports 3.2 of block 3) and the exhaust of the flue gas from the chamber 4.2 in front of the nose 1.3; 1 and suction of the medium behind the nose 1.3 of the rotor 1 into the working chamber 4.1.

Fig. 7 shows the ignition of the medium behind the nose 1.2 of the rotor 1 in the working chamber 4.2 and the exhaust of the flue gases from the chamber 4.2 before the nose 1.3, the compression of the medium in the working chamber 4.1 before the nose 1.2 of the first rotor 1;

Fig. 8 shows gas expansion - conversion from thermal energy to mechanical in chamber 4.2 and exhaust gas from chamber 4.2 in front of nose 1.3, further compressing the medium in the working chamber 4.1 in front of nose 1.2 of the first rotor 1 and sucking the medium behind nose 1.3 of rotor 1 into the working chamber 4.1.

Fig. 9 shows the expansion of the gases in the chamber 4.2 and the termination of the exhaust gas from the chamber 4.2 in front of the nose

1.3, further moving the medium from the working chamber 4.1 through the rotor 1.2 nose 1.2 to the storage system 2.5 in the rotor 2 through the opening 2.4 and terminating the suction of the medium behind the rotor 1.3 nose 1.3 into the working chamber 4.1.

Fig. 10,11 show the passage of the nose 1.2 of the first rotor 1 through a suitably shaped cutout 2.7 on the second rotor 2 and the passage of the nose 1.3 of the first rotor 1 through a suitably shaped cutout 2.8 on the second rotor 2 media in the working chamber 4.1 in front of the nose 1.2 of the first rotor 1, further moving the pressurized medium from the reservoir 2.5 in the rotor 2 through the opening 2.6 into the defined area of the working chamber 4.2 behind the nose 1.2 of the rotor 1;

1.3

Fig. 12 shows the suction of the medium behind the nose 1.3 of the rotor 1 into the working chamber 4.1 and the compression of the medium in the working chamber 4.1 before the nose 1.2 of the first rotor 1, the exhaust gas from the chamber 4.2 in front of the nose 1.3 and fuel injection after the nose 1.2 in the working chamber 4.2. fuel already enriched at entry through intake openings 3.2 of block 3).

Fig. 13 shows the suction of the medium behind the nose 1.3 of the rotor 1 into the working chamber 4.1 and the compression of the medium in the working chamber 4.1 before the nose 1.2 of the first rotor 1;

DETAILED DESCRIPTION OF THE INVENTION

The rotary internal combustion internal combustion engine is original in its construction in that it comprises only two (preferably more) rotating elements - rotors 1 and 2 (preferably other second rotors 9) housed in block 3, but also in processes typical of internal combustion engine operation.

Rotary nasal ring motor with internal combustion works on the same principle as rotary nasal motor with internal combustion, registered at the Industrial Property Office of the Slovak Republic, under no. file PP 5068-2006 of 08/08/2006.

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 (preferably another second rotor 9) and using a block 3 in which the first rotor 1 and the second rotor 2 (preferably another rotor 9) are mounted; rotate. The rotors 1 and 2 (preferably another rotor 9) rotate synchronously with each other and continuously maintain a partial structural and functional contact that is between the rotors 1 and 2 (preferably another rotor 9) and the block 3 sealing and leaking. The rotational axes of the rotors 1 and 2 (preferably another rotor 9) are preferably parallel, or suitably deflected from the parallel direction. The second rotor 2 (preferably another rotor 9) of preferably annular shape, passes through the working chamber 4.1, (4.2) and divides it in at least two places, compared to the rotary internal combustion internal combustion engine, where the second rotor 2 passes through the working chamber 4.1, (4.2) and divides it in one place. The second rotor 2 (preferably a plurality of second rotors 9) has e.g. circumferentially a toothed transmission 2.10 is synchronously interconnected by the transmission mechanism 8 with the first rotor 1 which drives it.

The first rotor 1 and the second rotor 2 (preferably another rotor 9) are continuously complementary in design and function. Block 3, in addition to the function of the enclosure delimiting the space in which the first rotor 1 and the second rotor 2 (preferably another rotor 9) are located, continuously defines, together with the rotors 1 and 2 (preferably another rotor 9), sealed or unsealed parts of the working chamber 4.1 ). The working chamber 4.1, (4.2) preferably has a torque shape and is delimited by the inner wall 3.1 of the block 3 and the peripheral wall 1.9 of the first rotor 1 as well as the rotating second rotor 2 (preferably another rotor 9). Advantageously, the first rotor 1 is cylindrical-plate-shaped, with at least one nose 1, 2, 3, on its circumference 1.9, which rotates in the working chamber 4.1, (4.2). The second rotor 2 (preferably another rotor 9) is preferably of annular shape, with slits 2.7, 2.8 (preferably with slots 9.7, 9.8 of the other rotor 9), on the inner periphery 2.11 of the second rotor 2 (preferably on the periphery 9.11 of the other rotor 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 has a gear 2.10 on the outer circumference (preferably a gear 9.10 on the other rotor 9) and is synchronously connected therewith by the gear mechanism 8 to the rotary output shaft 1. of the first rotor 1. The contact area of the first rotor 1 and the second rotor 2 the rotor 9) is provided with at least two cut-outs

2.7, 2.8 (preferably with cutouts 9.7, 9.8) on its inner circumference 2.11 (preferably on circumference 9.11 on the rotor 9) and at least one nose - nose 1.2, (1.3), whose circumference 1.8 follows the volume of the working chamber 4.1, (4.2), and this nose 1.2. (1.3) is located on the circumference 1.9 of the first rotor 1. The slots 2.7, 2.8 (preferably the slots 9.7, 9.8) on the inner circumference 2.11 (preferably on the circumference 9.11 on the next rotor 9) are provided with such constructional design as to allow sealing and leaking 1.2, (1.3) by these cutouts 2.7,

2.8 of rotor 2 (preferably by cutouts 9.7,9.8 of rotor 9). A suitable position of the second rotor 2 with the opening 2.2 in it (preferably the opening 9.2 on the next rotor 9) opposite the block 3 with the opening 3.2 in it, further defining the second rotor 2 (preferably another rotor 9) and the rotation of the first rotor 1 ensures suction medium 7 (air or oxygen or fuel mixture) into the working chamber 4.1, behind the nose 1.3. The aspirated medium is compressed by rotating the first rotor 1 and delimiting the second rotor 2 (preferably another rotor 9) in the working chamber 4.1 in front of the nose 1.2. 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 (preferably another transition system 9.4, 9.5, 9.6 of the rotor 9), its inlet port 2.4 (preferably another inlet port 9.4 on the rotor 9) and the outlet port 2.6 (preferably another outlet port 9.6 on the rotor 9) ), located in the second rotor 2 (preferably on the next rotor 9) into 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 rotor 9). Here, the medium 7 (air or oxygen, or fuel mixture) by rotating the second rotor 2 (preferably another rotor 9) and its suitable shape can still be compressed (when only air or oxygen is moved, fuel injection 5.1 is initiated) and fuel mixture explodes. 7 in the working chamber 4.2, either by compressing the mixture itself and spontaneously igniting, or by igniting with a spark 5.2. Explosion and expansion and pressure exerted on the nose 1.2 of the rotor 1 initiates rotation of the first rotor 1. Subsequently, the rotation of the first rotor 1 and the mutually suitable position of the second rotor 2 (preferably another rotor 9) with aperture 2.3 therein (preferably aperture 9.3 of further rotor 9) ) against block 3 with an opening

3.3 therein, further defined by the second rotor 2, provides exhaust gas 6 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 (preferably another slot 9.8) of the second rotor 2 (preferably another rotor 9) and the suction is initiated again.

Industrial usability

The rotary internal combustion engine has the prerequisites for use in today's classic piston combustion engines, both static and dynamic, such as small, medium-sized engines, in automobiles, airplanes and large ones, from high-speed to low-speed. The internal combustion rotary nose ring motor can 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. When converting chemical energy to mechanical, the rotary internal combustion engine is rotary in motion, is not in a linear motion, has no pivoting motion, thus neither a return phase nor eccentric rotations. The number of moving parts is extremely low - 2 to 3, which implies low failure rate and thus high reliability. The working pair (preferably triple or more) of the rotors together with the block can be combined simultaneously in several combinations, as described in essence of the technical solution and in the protection claims.

Claims (4)

PATENT CLAIMS An internal combustion rotary nose ring motor, characterized in that it comprises a block (3) in which a structural, functionally synchronized combination of at least one first rotor (1) with at least one second rotor (2), preferably another rotor, is arranged. (9), in mutual partial contact which is continuous and sealing and leaking, wherein - the axis of rotation of the first rotor (1) and the axis of rotation of the second rotor (2), preferably the other rotor (9), are parallel or offsets; (1) comprises a rotary output (1.1) - identical to the axis of rotation of the first rotor (1) for coupling by the transmission mechanism (8) to the driven system (2.1) - advantageous to the axis of rotation of the second rotor (2), preferably another rotor (9); - 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), preferably by circumference (9.9) and cut-outs (9.7), (9.8) of another rotor (9), - circumference (1.9) of the first rotor (1), contact surface (1.8) of at least one nose (1.2) the first rotor (1), the inner wall (3.1) of the block (3) defining a chamber (4.1), (4.2), the inner periphery of the second rotor (2), preferably another rotor (9), preferably in the shape of torus; 2.11) of the second rotor (2), preferably of another circumference (9.11) of the rotor (9), is provided with at least one contact section which extends or at least delimits the chamber space (4.1), (4.2) and is provided with cut-outs (2.7), (2.8), preferably by slits (9.7), (9.8) of the second second rotor (9) and this perimeter (2.11) of the second rotor (2), preferably the perimeter (9.11) of the second second rotor (9), 2866 the cut-outs (2.7), (2.8), the second rotor (2), preferably the cut-outs (9.7), (9.8) of the other rotor (9), in coordination with the first rotor (1) and the block (3) - the first rotor (1), the contact portions of the circuit (2.11) of the second rotor (2), preferably the contact portions of the circuit (9.11) of the other rotor (9), and the inner rotor (1); the wall (3.1) of the block (3) delimit the chamber parts (4.1), (4.2), - it is equipped with a fuel injection system (5.1) or a fuel mixture preparation (7) and its transport to the chamber part (4.2) of the working space - the block (3) is equipped with at least one first section of the intake duct - an opening (3.2) in the block (3), which is connected to a corresponding starting system with the intake of medium (7) (fuel mixture, air or oxygen); 1), preferably another rotor (9) is provided with a second section of the suction channel o a second rotor (2), preferably a further suction channel with an opening (9.2) in the rotor (9), which is connected to the chamber space (4.1), wherein the first section (3.2) and the chamber space (4.1) are mutually interconnected by a second section of the suction channel (2.2) of the second rotor (2), preferably by another second section of the suction channel (9.2) of the other rotor (9), and by rotation of the second rotor (2), preferably another rotor (9) only during suction of the medium ) (fuel mixture, air or oxygen), - 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), preferably another transition system (9.4), (9.5) (9.6) in a further contact cut (9.7) of the rotor (9), consisting of a reservoir (2.5) of the second rotor (2), preferably another reservoir (9.5) of the rotor (9), with an inlet (2.4) of the second rotor (2) preferably by a further inlet (9.4) of the rotor (9) from the chamber (4.1) and with an outlet (2.6) of the second rotor (9). 2), preferably a further outlet (9.6) of the rotor (9), into the chamber (4.2) for the medium (7) - fuel mixture, air or oxygen, - the block (3) is equipped with at least one second section with an opening ( 3.3) an outlet duct which is connected to a corresponding flue gas outlet (6) and the second rotor (2) is provided with a first section (2.3), preferably another first section (9.3) of another rotor (9), which is connected to 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), preferably with another opening of the outlet channel (9.3) of the other rotor (9) the first rotor (1) and the second rotor (2), preferably another rotor (9), are adapted for synchronized rotation in the same direction. An internal combustion rotary nose ring motor according to claim 1, characterized in that one basic engine operating assembly has a first rotor (1) and a second rotor (2), preferably another rotor (9), wherein - on the same axis - further assemblies are located at the same time in the shaft, all of these assemblies of rotors (1), (2) preferably other rotors (9) being synchronously interconnected. 3. A method of operating a rotary nasal internal combustion engine, wherein the intake and compression, ignition and utilization of the released energy is performed - expansion and exhaust of exhaust gases in a rotary internal combustion internal combustion engine according to claims 1 and 2, characterized in that sequence of constructional and related parametric and functional combinations in time intervals is carried out continuously initiating and running at least one process sequence or two or more process sequences simultaneously, which processes are characteristic mainly for the operation of the internal combustion engine and are initiated and performed in sealed or unsealed chamber spaces (4.1), (4.2), these being continuously delimited from the chamber space, in which: - the suction of the medium (7) as a fuel mixture, air or oxygen, through the first section of the suction channel - the opening (3.2) in the block (3) ), and the second section of the intake duct through the opening (2.2) in the second rotor (2), preferably by another section of the suction channel through the opening (9.2) of the rotor (9), into the chamber (4.1), - compressing the suction medium (7) as fuel mixture, air or oxygen, compressed medium (7) as a fuel mixture, air or oxygen from the chamber (4.1), through the transition system, its inlet (2.4) of the rotor (2), preferably another inlet (9.4) of the rotor (9), reservoir (2.5) - rotor (2), preferably another rotor magazine (9.5) and outlet (2.6), rotor (2), preferably another rotor outlet (9.6), into the chamber (4.2), - initiating an explosion and subsequent expansion, transfer of the flue gas (6) from the chamber (4.2), through the outlet section, its first section (2.3) of the rotor (2), preferably another inlet (9.3) of the rotor (9), another section (3.3) of the block ( 3) into the exhaust. A method of operating a rotary nasal ring motor with internal combustion, wherein the suction and compression, ignition thereof and utilization of released energy - expansion and exhaust of exhaust gases in the rotary nasal internal combustion engine according to claim 3 are carried out, characterized in that the second rotor (2) ), preferably another rotor (9), preferably of an annular shape, passes through the working chamber (4.1), (4.2) and divides it in at least two places, - the second rotor (2), preferably another rotor (9), preferably has a rotary output the circumferential gear transmission (2.10) of the rotor (2), preferably the circumferential gear transmission (9.10) of the other rotor (9), is synchronously interconnected therewith by the transmission mechanism (8) with the first rotor (1) which drives it.