Quadroid rotary piston engine with magnetic field

Abstract

The present invention resides in an engine in which the function of a working cylinder is performed by a chamber formed by a rotating rotor with blades. The blades also rotate about their own axis within the rotor, thus causing the chamber to have a variable cross-section. The rotor and the blades divide and completely close off the chamber in such a way that, as they rotate, spaces are formed which have changing volumes. This divides the chamber into a working mixture intake zone, a compression zone, an ignition zone, an expansion (working stroke) zone and an exhaust gas outlet zone, thus forming an internal combustion engine. The rotor passes through the entire chamber and may be a disc rotor, a cylindrical rotor or a conical rotor. The blades are secured in the rotor and rotate about their own axis such that, as they pass through a narrow zone of the chamber, they retract into the rotor. For an external combustion engine, two strokes are used: an intake-expansion stroke, and an exhaust stroke. According to the same principle, the quadroid operates as a pump or as an engine supplied with a pressurized working fluid. In the gaps between the moving parts, a magnetic field keeps a portion of the gas ionized during combustion.

Description

[0001] Description

[0002] [EN] A quadrilateral rotary screw engine with a magnetic field. The engine operates on the principle of the rotor and blades creating chambers within the engine and changing their volumes during the operating cycles. The configuration of the rotor, blades, and their synchronous operation continuously closes the chamber into zones of start, compression, combustion, power stroke, and exhaust during the cycles. The rotor passes continuously through the entire chamber (or is part of it) perpendicular to the direction of rotation and can undergo a break perpendicular to the direction of rotation only at the points where the blades pass, with the minimum possible gap. This allows the blades to be separated by a significant distance from each other, and the number of blades can be reduced to one. Fixing the blade at both ends by the rotor significantly increases the latter's resistance to deformation under loads. The blades are secured in the rotor and rotate around their axis so that, when passing through a narrow zone of the chamber, they enter the rotor, adjacent to it.During the working cycle, the blades enter and exit the rotor simultaneously, with the rotor and blades interacting with the stator. To minimize leakage losses, the interaction between the parts occurs with the smallest possible clearance: thermal expansion, bearing play, gearbox play, deformation under load, manufacturing tolerances... At high flame temperatures, some of the gases, which have converted to an ionized state (plasma), can be held by a magnetic field. The rotor, depending on its angle (from 0 to 90 degrees) to the axis of rotation, can be disc, cylindrical, or conical. It can be double-sided, double-sided solid, or single-sided solid. In Fig.

[0003] 11 shows some rotor variants. The blades can be convex, concave, or closer to straight. Their shape is determined by the passage of narrow sections of the stator. Helical blades 33, 34, 36 allow the working medium to be moved not only in the direction of rotor rotation, but also perpendicularly. Thickening blade 33 towards the center increases its resistance to deformation. In the same way, blade 33 with rotor 23 can divide the chamber into several. Blade rotation around its axis in the rotor can be a multiple of 0.5 to the rotor revolutions (0.5; 1.0; 1.5...). The rotation of the rotor and blades forms a chamber with a variable cross-section. An external combustion engine also operates on the described principles.

[0004] The drawings show some variants of the invention and the operating principle.

[0005] The diagram shows:

[0006] 1. Stator.

[0007] 2. Rotor.

[0008] 3. Blade.

[0009] 4. Toroidal chamber.

[0010] 5. Gearbox.

[0011] 6. Spark plugs (injectors).

[0012] 7. Inlet window.

[0013] 8. Exhaust window.

[0014] 9. Intake-compression zone (cold zone).

[0015] 10. Working stroke-release zone (hot zone).

[0016] 11. Rotor shaft (power take-off shaft).

[0017] 12. Bearings.

[0018] 13. Sealing ring.

[0019] 14. Compression adjustment piston.

[0020] 15. Reducing the volume of the compression chamber.

[0021] 16. Reducing the volume of the working stroke chamber.

[0022] 17. Exhaust gas ventilation window.

[0023] 18. Contact wire.

[0024] 19. Combustion chamber.

[0025] 20. Magnet.

[0026] 21. Pumping channel.

[0027] 22. Steam supply channel.

[0028] Motor Fig. 1, 6

[0029] The engine has a chamber formed by a solid, double-sided disc rotor 23 and helical, concave blades 33, thickening toward the center. Each blade completes 0.5 revolutions per rotor revolution. Blade 2 exits top dead center (TDC), simultaneously closing the chamber. Rotating about its axis and the rotor's axis of rotation, the blade changes the chamber volumes. The lower portion of the blade, in zone 9, compresses the working mixture while simultaneously drawing in new mixture through inlet port 7. The upper portion of the blade, in zone 10, performs the power stroke while simultaneously releasing exhaust gases through outlet port 8. As it moves toward the ignition zone in zone 9, the blade compresses the working mixture and, due to its helical shape, moves it toward the center of the blade and, through a slit in sealing ring 13, transfers it from zone 9 to zone 10, where ignition occurs. For this motor design, it is also possible to use double-sided 26 or solid single-sided 25 disc or conical 31 rotors.

[0030] Motor Fig. 2, 5

[0031] The engine has a chamber formed by a double-sided cylindrical rotor 27 or 30 and convex blades. At TDC, the compressed working mixture in combustion chamber 19, bounded at the top by housing 1 and piston 14, on the sides by rotor 2, and below by blade 3, ignites. The rotor, rotating clockwise, closes the chamber at TDC and BDC. At this time, the blade moves from contact with the rotor to contact with the chamber walls. Gases press on the blade, performing the power stroke simultaneously with the exhaust gases from the previous cycle being released. At BDC, the blade enters the rotor and passes into the intake and compression zone, where it compresses the working mixture from the previous cycle while simultaneously drawing in new mixture. At TDC, the synchronous operation of the rotor and blade creates a combustion chamber into which the compressed working mixture is supplied, and the cycle repeats. Retracting piston 14 upward reduces compression and reduces the possibility of detonation, and vice versa.Retracting cylinder wall 15 to the left reduces the volume of the compression chamber, while retracting cylinder wall 16 to the right reduces the volume of the power chamber. This allows for a reduction in engine power without sacrificing efficiency. The rotor can be divided into several sections along the axis of rotation, as can blade 35, creating multiple engine chambers. Magnet 20 magnetizes the stator and rotor with blades. A magnetic field is generated in the gaps between the rotor, blades, and stator. During combustion, several percent of the gas is ionized. As the Lorenz forces pass through the gaps perpendicular to the magnetic field, they deflect charged particles, reducing plasma leakage through the gaps.

[0032] Motor Fig. 3

[0033] The motor has a chamber formed by a solid, single-sided cylindrical rotor 28, relative to which the blades are positioned inward. This motor differs from the previous one in that the combustion chamber is formed inside the rotor. The blade, performing compression and power stroke, interacts with the rotor on only one side. When using injectors, the inner part of the motor can rotate. A motor with rotor 29, relative to which the blades are positioned externally, will operate in a similar manner.

[0034] Fig. 4, 9

[0035] In this design, the blade rotates 0.5 times around its axis for every rotor revolution. When external pressure is applied to one of the ports, it functions as a motor. When the rotor rotates, it functions as a pump.

[0036] Fig. 7

[0037] Vacuum pump. A disc rotor (26 or 32) with a blade (35) extracts air, reducing the pressure in the chamber and channel (21). It can also function as a compressor.

[0038] Fig. 8

[0039] Internal combustion engine. Disc rotor 26 or 32 with blades twisted into a spiral 34, 36.

[0040] Fig. 10

[0041] The motor has a chamber formed by a conical rotor. As the blade passes TDC, pressurized steam (superheated water) is supplied through channel 22. As the blade exits TDC, channel 22 is interrupted by the rotor. The expanding steam performs work.

Claims

[RU] Invention formula 1. The energy conversion device consists of: a) a stator; b) a rotor with an output shaft rotating relative to the stator; c) a rotation mechanism blades around their own axis relative to the rotor; d) a plurality of blades, convex in shape in cross-section perpendicular to the axis of rotation, fixed in the rotor, rotating in orbit around the axis of rotation of the rotor and rotating relative to the rotor around its own axis; e) an annular chamber surrounding the axis of rotation with a variable cross-section formed by the working part of the blades rotating in orbit around the axis of rotation of the rotor and rotating around its own axis, in such a way that the stator walls approach the blades along the trajectory of their protruding parts during rotation, has two windows. The device is distinguished by the fact that its rotor contains an element that performs function of the wall of the annular chamber, which is part of the rotor that passes A closed annular chamber divides it into two parallel chambers and has recesses for the working portion of the rotating blades, allowing the blades to rotate around their own axis and blocking the leakage of fluid between the blade and the rotor during the working cycle. The blades emerge from different sides, with at least one blade on each side. Blades located on different sides rotate in different directions, and blades located on one orbital trajectory rotate in the same direction. The configuration of the stator, rotor, blades, and their trajectory of motion are coordinated so that they continuously divide the sections of the closed annular chamber into chambers of working cycles. Change The cross-sectional change of the annular chamber occurs due to the cyclically changing distance from the rotor to the stator wall. 2 The device according to paragraph 1 is distinguished in that the rotor does not divide the annular chamber into two parallel ones, and the blades, of which there is at least one, emerge from one side of the rotor.

3. The device according to paragraph 2 is distinguished by the fact that the rotor element is not solid and fills the interblade space along the orbital rotation trajectory of the working portion of the blade, during which the blade exits the rotor in both directions. The rotor does not function as a wall of the annular chamber, but rather functions as a valve cyclically closing the bottleneck of the annular chamber simultaneously with the exit from it. Blades. The cross-section of the annular chamber changes due to the cyclically changing distance between the stator walls. The volume of the chambers during the working cycle changes due to the distance from the narrow section of the annular chamber blocked by the rotor to the blade and the change in the cross-section of the annular chamber for at least part of the working cycle. The device according to paragraph 1 is characterized in that it is an internal combustion engine The rotor has a partition between the outer edges of the annular chamber, located on opposite sides along the blade's axis of rotation. The annular chamber also has a partition in the same location, dividing the annular chamber into intake, compression, power, and exhaust chambers. Fuel injection / ignition elements are also present. 1 of 2 PCT / IB 2024 / 000629 February 17, 2024 5. The device according to paragraph 4 is distinguished by all the features set out in paragraph 2.

6. The device according to paragraph 5 is distinguished by all the features set out in paragraph 3.

7. The device according to paragraphs 4-6 is distinguished by the absence of a bulkhead, and the closed annular chamber has at least two bottlenecks that divide it into the intake-compression, combustion chamber, and power-exhaust zones.

8. The device according to paragraphs 4-7 is distinguished by the presence of a magnetic field between the stator, rotor and blade to hold part of the ionized gas by Lorentz forces. 9 The device according to paragraphs 1-3, the engine for converting the internal energy of water into mechanical energy, has, instead of an inlet window, a nozzle for injecting into the chamber a limited amount of water having a temperature sufficient for all the water to be converted into a gaseous aggregate state during the process of expansion of the working stroke chamber and reduction of pressure.

10. The devices according to paragraphs 1-9 are distinguished by helical blades with the ability to move the fluid along the axis of their own rotation. 11 A device according to paragraphs 1-9, blades, in a section perpendicular to the axis of their own rotation, of a shape from convex to concave, with the ability to go around narrow sections of annular chambers and, together with the rotor, continuously cover them. 12 The device according to paragraphs 1-9 has an angle between the axis of rotation of the rotor and the axis of rotation of the blade around its own axis in the range from 0 to 90 degrees. 2 of 2 PCT / IB 2024 / 000629 February 17, 2024

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