Six-stroke rotary-vane internal combustion engine with hermetically sealed working space

Abstract

The invention relates to a six-stroke rotary-vane internal combustion engine with hermetically sealed working space comprising a stator with at least one inlet and at least one outlet, a respective hole for at least one spark plug, and working chambers comprising of an air-fuel intake and compression, and of expansion and exhaust of combustion products working chamber; a cylindrical rotor rigidly fastened to a shaft with combustion chambers alternating with vane grooves made in the cylindrical surface and vanes fitted in the vane grooves; side walls; front and rear bearing shields. The whole working space of the engine is bound by parts rigidly and hermetically fastened to the stator. Composite prismatic pieces are placed into end grooves on both sides of the rotor, while the ends of said composite prismatic pieces are pushed by a first spring against the adjacent vanes and one of the longer sides of the composite prismatic pieces is pushed by a second spring against the side walls.

Claims

1. A six-stroke rotary-vane internal combustion engine comprising: a stator with at least one inlet and at least one outlet, a respective hole for at least one spark plug, and working chambers of the stator; wherein the working chambers comprise of an air-fuel intake and compression working chamber, and expansion and exhaust of combustion products working chamber; a cylindrical rotor rigidly fastened to the shaft, with combustion chambers alternating with vane grooves made in the cylindrical surface of the rotor and vanes fitted in the vane grooves; side walls; front and rear bearing shields; wherein the side walls, the front and rear bearing shields are hermetically fastened to the stator; and wherein composite prismatic pieces are placed into end grooves on both sides of the rotor, while the ends of said composite prismatic pieces are pushed by a first spring against the adjacent vanes and one of the longer sides of the composite prismatic pieces is pushed by a second spring against the side walls.

2. The six-stroke rotary-vane internal combustion engine of claim 1, wherein the combustion chambers are made in the form of hemispherical recesses between the vane grooves on the cylindrical surface of the rotor.

3. The six-stroke rotary-vane internal combustion engine of claim 1, wherein the working chambers of the stator are designed as cylindrical bores with the axes parallel to the axis of the stator, evenly spaced along the inner surface of the stator.

4. The six-stroke rotary-vane internal combustion engine of claim 1, wherein each vane of said vanes comprises of separate vane plates in a free relative movement; and wherein each of said separate vane plates is made of two vane parts pulled apart by a third spring in an axial direction.

5. The six-stroke rotary-vane internal combustion engine of claim 4, wherein the number of vanes is a multiple of the number of the working chambers of the air-fuel intake and compression working chamber.

6. The six-stroke rotary-vane internal combustion engine of claim 5, wherein the working chambers of the stator are designed as cylindrical bores with the axes parallel to the axis of the stator, evenly spaced along the inner surface of the stator.

7. The six-stroke rotary-vane internal combustion engine of claim 1, wherein the number of vanes is a multiple of the number of the working chambers of the air-fuel intake and compression working chamber.

8. The six-stroke rotary-vane internal combustion engine of claim 1, wherein the at least one inlet includes two or more inlets, and the at least one outlet includes two or more outlets.

Description

(1) The invention is illustrated by drawings, where

(2) FIG. 1 shows a cross-sectional view of the engine;

(3) FIG. 2 shows axial cross-section of the engine in FIG. 1;

(4) FIG. 3 shows place I in FIG. 1;

(5) FIG. 4 shows place II in FIG. 2;

(6) FIG. 5 shows cross-section A-A in FIG. 3.

(7) The rotary-vane ICE contains a stator 1 (FIG. 1; 2) with inlet 2 and outlet 3 (FIG. 1). On the inner cylindrical surface of the stator 1 there are cylindrical bores, pairwise forming chambers 4 for intake of the air-fuel mixture and chambers 5 for expanding the combustion products (FIG. 1). Plugs 6 are screwed into the threaded holes of stator 1 (FIG. 1; 2). The side walls 7 and 8 (FIG. 2; 5) are centered and rigidly fastened to the stator 1 (FIG. 2). The front 9 and rear 10 bearing shields are centered and rigidly fastened to the stator 1 and the side walls 7 and 8 (FIG. 2). In the bearing shields 9 and 10 on the angular contact bearings a shaft 11 is mounted to which the rotor 12 is rigidly fastened (FIG. 1; 2; 3). Plates 13, 14, 15 with inserts 16 are placed in the vane grooves of the rotor 12 (FIG. 3; 5). The number of the plates is not limited, but no less than two. Inserts 16 and plates 13, 14, 15 are pushed apart by springs 17 (FIG. 5). Springs 18 (one for all plates of the vane) are inserted under the plates 13, 14, 15 (FIG. 3; 5), springs 19 (separate one for each plate) are inserted under the plates 14, 15 (FIG. 5). Semispherical recesses 21 are made in the cylindrical surface of the rotor 12 between the vane grooves (FIG. 1; 2). Spring-loaded oil removers 22 (FIG. 1; 3) are fitted in the bores made in the rotor 12. In the end grooves formed in the sides of the rotor 12 (point II, FIG. 2) composite prismatic pieces consisting of two components 23 and 24 are placed (FIG. 3; 4), the components being pushed apart by a spring 25 (FIG. 4) and pressed by a spring 26 (FIG. 4) against the side walls 7 and 8 (FIG. 2). In the upper part of the shields 9 and 10 there are openings 27 and 28 (FIG. 2). In the lower part of the bearing shields 9 and 10 there are openings 29 and 30 (FIG. 1; 2).

(8) An example of the ICE operation as designed by the inventor is given in FIG. 1 (with two intake chambers, clockwise rotation).

(9) Each of the plates 13, 14, 15 is pressed through the insert 16 against side walls 7 and 8 in a checkerboard manner. The ends of each of the components 23 and 24 of the prismatic pieces are pressed by springs 25 against the vane plates 13, 15 (or vanes, being their constituent parts), and by springs 26 against the side walls 7 and 8. All the above parts as a whole provide hermetical sealing of the side walls. Once the engine starts the springs 18, 19 press the vanes against the working surface of the stator 1. When the rotor 12 rotates, the air-fuel mixture is sucked through inlet 2 into the space in the chambers 4 of air-fuel mixture intake formed behind the advancing vanes. This air-fuel mixture upon further rotation of the rotor is compressed by the next vane within the tapered space bound by the cylindrical surfaces of stator 1 and rotor 12, and the side walls 7 and 8.

(10) At the final stage of compression the mixture is concentrated in a hemispherical recess 21 in the cylindrical surface of the rotor 12. At this point the spark plugs 6 ignite the mixture, which then is burned in an enclosed space before the front vanes following the rotation direction start extending into the opening space of the chamber 5 of combustion product expansion thus transmitting torque to the shaft 11. Following the rotation of the rotor the outlet 3 are opened behind the front vanes and exhaust from the chambers 5. The central part of cylindrical surface of the stator between the chambers 5 of combustion product expansion and exhaustion and the chambers 4 of air-fuel mixture intake and compression forces the exhaust gases out and prevents them from entering into the air-fuel mixture intake zone. Cooling lubricant is supplied through the openings 27 and 28 (oil, oil mist), cooling the working space and lubricating the wearing surfaces. Through the openings 29 and 30 the substance is exhausted for regeneration and temperature reduction. The synchronous movement of the vanes in the vane grooves of the rotor provides dynamic balance of the engine. Once a steady mode of the engine movement is reached the supply of fuel to one (or more) chambers of air-fuel intake and compression can be stopped by any known method provided that the air supply to the given chamber is still maintained. In this case, the engine continues to operate with reduced power output maintaining the same number of working strokes per one rotor rotation.