SIX-STROKE ROTARY-VANE INTERNAL COMBUSTION ENGINE

Abstract

This invention refers to the engine-building area; in particular, to internal combustion engines with rotating parts, more specifically to a rotary-vane internal combustion engine (ICE), which can be used on water, air and land transport vehicles.

The rotary-vane ICE featuring the inlet and outlet ports and ignition plug holes with air-fuel intake and compression chambers alternating with the combustion product expansion and removal chambers, the cylindrical rotor attached to the shaft with longitudinal grooves with blades and combustion chambers arranged on the cylindrical surface of the rotor, the side walls, the front and rear end shields, in this case the side walls are arranged in the form of cylindrical borings with the axes being parallel to the stator axis and spaced evenly all over its internal surface, each blade consists of separate plates with possible mutual displacement, in this case each blade plate is made of two parts being pulled apart by a spring in axial direction and the number of blades is equal to the number of air-fuel mixture intake chambers The result to be achieved in this invention consists in simplifying the ICE design with rotary parts and in increasing its reliability and adaptability to streamlined manufacture, preventing the unburned fractions of air-fuel mixture from being emitted into atmosphere as well as ensuring that the engine can be switched over to economic run.

Claims

1. A six-stroke rotary-vane internal combustion engine comprising a stator with inlet and outlet ports, holes for spark plugs and the working chambers of the fence and the compression fuel-air mixture, alternating with working chamber expansion and removing of the combustion products; is rigidly fixed to a cylindrical rotor shaft 16 with longitudinal grooves in which vanes are placed, with combustion chambers made on its cylindrical surface between the grooves; side walls, front and rear bearing shields, characterized in that the side walls of all working chambers of the engine are formed by rotating rotor parts, and the combustion chambers are formed as hemispherical recesses on the cylindrical surface of the rotor between its longitudinal grooves, and the working stator chambers are designed as cylindrical bores with axes parallel to the axis of the stator, evenly spaced along the inner surface of the stator, each blade consists of several plates in a freely relative movement, each plate made of two parts move apart in the axial direction by a spring, and the number of blades is a multiple of the number of the chambers of the fence and the compression fuel-air mixture.

2. The engine of claim 1, characterized in that the engine is transferred to an economical mode of operation by stopping the supply of fuel to a part of the chambers of the fence and the compression fuel-air mixture while maintaining the supply to said air chambers.

Description

[0014] The essence of this invention is explained by drawings, where FIG. 1 illustrates the engine in cross-sectional view;

[0015] FIG. 2 illustrates cross-section A-A from FIG. 1;

[0016] FIG. 3 illustrates point I from FIG. 1 (some parts are not shown for clarity);

[0017] FIG. 4 illustrates point II from FIG. 2;

[0018] FIG. 5 illustrates cross-section B-B from 3.

[0019] The rotary-vane ICE has stator 1 (FIG. 1; 2) with inlet 2 and outlet 3 ports (FIG. 1). Along the cylindrical surface of stator 1 there are cylindrical bores forming air-fuel intake mixture chamber 4 and combustion product expansion chambers 5 (FIG. 1). Within the edge grooves of stator 1 enveloping the working surfaces of stator 1 there are strip (for example) end seals 6 pressed by springs 7 against the internal wall of the groove and by springs 8 through intermediate parts 9 (FIG. 2; 3; 4) against side walls 10 and 11 (FIG. 2; 4; 5). Plugs 12 are screwed into the threaded holes of stator 1 (FIG. 1; 2). The front 13 and rear 14 end shields are centered and rigidly attached to stator 1 (FIG. 2). Shaft 15 with rigidly fixed cylindrical rotor 16 with side walls 10 and 11 is fitted in the end shields on the radial-thrust bearings (FIG. 1; 2). There are plates 17, 18, 19, 20 with spacers 21 fitted in the longitudinal grooves of rotor 16 (FIG. 3; 5). The quantity of plates may be random, but no less than two. Spacers 21 and plates 17, 18, 19, 20 come loose by springs 22 (FIG. 5). Semispherical recesses 23 are made over the cylindrical surface of rotor 16 between the longitudinal grooves (FIG. 1; 2). Spring-loaded oil removers 24 are fitted in the bores made in stator 1 along the longitudinal grooves (FIG. 1;2). Holes 25, 26 as well as holes 27 and 28 (in an arbitrary way) are made in the lower side of shields 13 and 14 (FIG. 1; 2). Shaft 15 has hole 29 extended to the edge (FIG. 2).

[0020] Let us review the ICE operation according to the invention by an example given in the drawings (with two intake chambers, clockwise rotation, FIG. 1).

[0021] Prior to starting the the air is supplied under pressure P.sub.1 with periodic oil injection (an oil-air system) through holes 27 and 28 in shields 13 and 14, which passing through the radial-thrust bearings lubricates and cools the latter and then gets into the space between the end shields and the rotating parts of rotor 16, where it is to be removed for recycling through holes 25 and 26 in the lower side of the shields. Simultaneously, the air under pressure P.sub.2 (an oil-air system) is supplied through hole 29 in shaft 15 to the grooves of rotor 16 to plates 17, 18, 19, 20 located in grooves (hereinafter to be referred as a combination of blades), this air draws apart the blades in radial direction, providing a labyrinth-groove seal within the blade-stator pair and lubricating them at the same time. Each blade plate is pressed by spring 22 through spacer 21 against side walls 10 and 11 in a checkerboard manner, thus preventing the inter-chamber leaks of air-fuel mixture and exhaust gases. Strip end surfaces seals 6 prevent the leakage of air-fuel mixture and its combustions beyond the operating zone of the engine. During rotation of rotor 16, the air-fuel mixture is sucked into the space of air-fuel mixture intake chambers 4 through inlet holes 2, this air-fuel mixture then during further rotation is compressed by the next blade within the tapered space limited by the cylindrical surfaces of stator 1, rotor 16 and side walls 10 and 11. At the final stage of compression the mixture is concentrated in semispherical recess 23 on the cylindrical surface of rotor 16. At this moment plugs 12 ignite the mixture, which then burns within the closed spherical space before the front moving blade starts extending into the open space of combustion product expansion chamber 5 thus giving torque to shaft 15. During further rotation outlet ports 3 open up after the upstream blades and exhaust gases are removed from chambers 5. The central cylindrical surface of the stator between combustion product expansion and exhaust gas chambers 5 and air-fuel mixture intake and compression chambers 4 prevents the exhaust gases from entering into the air-fuel mixture intake zone. The synchrony of the combustion process within the symmetrically located chambers makes it possible to relief the bearing supports from radial forces. The synchronous movement of the blades within the rotor grooves provides dynamic balance of the engine. Once the steady motion mode (cruise speed) is reached the air-fuel mixture can be halted by any known method provided that the supply is maintained to the given air chamber. In this case, the engine continues to operate with reduces power output with the same number of working strokes maintained per one rotor revolution.

[0022] Thus, the invention makes it possible to implement the six-stroke cycle of rotary-vane ICE featuring significant advantages. Thus, allowing the side walls of all the working chambers rotate jointly with the rotor and blades and fitting seals within the rotor-blade and blade-stator pairs in a multi-row fashion makes it possible to enhance the engine's operating space tightness and reduce friction losses. A regular oil injection into the air flow allows lubricating the friction surfaces and stator and blade contact pattern as well as lubricating the rotor shaft bearings and cooling down the engine parts. The multiple-point combustion prevent one-sided heating of the engine parts and the synchronous movement of blades in radial direction allows smooth vibration free operation of the engine The engine's operating strokes (in an example considered the dual operating stroke occurs in every 36 of the shaft rotation), thus providing smooth torque. The fuel combustion in constant volume within the spherical chamber makes it possible to utilize the chemical energy of fuel as much as possible. The possibility described by this invention to stop fuel supply to a number of the air-fuel mixture intake chamber with air supply maintained provides the most efficient engine performance. Making the working surfaces flat and cylindrical ensures a high degree of adaptability to streamlined manufacture of the engine.