RU2812232C2 - Wind gas turbine engine - Google Patents

Abstract

FIELD: engines.

SUBSTANCE: engine adapted to produce thrust or designed to produce torque contains a combustion chamber, the combustion chamber generates an exhaust gas flow to push the rotor blades related to the rotor in the rotor housing, the exhaust gas flow rotates the rotor, shaft and fan, which generates a rotating force and generates air flow. The rotor housing has the first wall, the second wall and a third wall that direct the flow of exhaust gas until the exhaust gas flow reaches a housing gap in the second wall and the exhaust gas flow moves outward from the rotor housing, wherein the first wall has another clearance of the housing to allow air flow through to cool the rotor, and this cooling process adds torque to the engine. The engine contains an optional wind turbine assembly. An air compressor is driven either by an electric motor or driven by other means. This wind gas turbine engine has comparatively fewer parts than the prior art turbine engine, which require makes the wind gas turbine engine cheaper to manufacture and therefore does not very expensive materials or expensive parts, since the wind gas turbine engine blades of the wind gas turbine engine are not always exposed to hot exhaust gases during operating time of the wind gas turbine engine, since in the design of the wind gas turbine engine according to the present invention, the rotor blades of the gas turbine engine are heated during the power stage, and during the operating cycle of the engine during the cooling stage, said rotor blades of the wind gas turbine engine are cooled by fast moving air from the fan.

EFFECT: invention makes the wind gas turbine engine cheaper to manufacture and therefore does not very expensive materials or expensive parts.

20 cl, 65 dwg

Description

FIELD OF TECHNOLOGY TO WHICH THE INVENTION RELATES

The present invention relates to an engine called a wind gas turbine engine.

DESCRIPTION OF THE BACKGROUND OF THE ART

The wind turbine engine of the present invention is considered an improvement on the engine disclosed in U.S. Patent No. 2,608,058 to L. J. Geeraert, an improvement on the engine disclosed in U.S. Patent No. 4,807,440 issued to Ahmed Salem, and an improvement on the engine disclosed in U.S. Patent No. 6,298,821 B1 , issued in the name of Alexander Alexandrovich Bolonkin; These three prior art U.S. patents cited above do not mention large fan airflow or usable airflow from the fan housing assembly and fan assembly for cooling turbine rotor blades, so making the above prior art engines without proper blade cooling rotor may lead to engine failure if the engine is running for a long period of time. The wind turbine engine of the present invention is further an improvement over the prior art turbojet engine because the prior art turbojet engine does not use air or wind directly from the fan to cool the turbine rotor and to cool the turbine rotor blades of the prior art engine. Also not disclosed are prior art engines where wind, or usable air flow, or large fan air flow from a fan provides additional push to the turbine rotor to rotate, which provides more force to rotate the engine turbine rotor shaft. Gas turbine engines of the prior art do not include a wind turbine, but one engine configuration of the present invention includes a wind turbine assembly.

SUMMARY OF THE INVENTION

The prior art turbine engine for a jet aircraft, turbine-powered aircraft, land vehicle, water vehicle, amphibious vehicle, drive shaft turbine, jetpack, auxiliary power unit, and engine for other power generating systems is much more complex or has more moving parts and therefore the prior art engine is much more expensive and has more problems associated with multiple moving parts, and the prior art turbine engine is additionally somewhat problematic because the rotor blades are constantly exposed to hot exhaust gases during turbine operation. a prior art turbine engine that requires a complex and energy-intensive cooling system, requires expensive materials, and requires frequent maintenance of said prior art turbine engine, which likely increases the maintenance costs of the prior art turbine engine.

The inventor has discovered that the disadvantages of the prior art engine can be overcome by disclosing a simple engine according to the present invention, which can be called a wind gas turbine engine, this wind gas turbine engine has comparatively fewer parts than the prior art turbine engine, which makes the wind gas turbine engine cheaper to manufacture and whereby very expensive materials or expensive parts are not required, since the blades of the wind gas turbine engine, the rotor blades of the wind gas turbine engine are not always exposed to hot exhaust gases during operation of the wind gas turbine engine, since in the design of the wind gas turbine engine according to the present invention, the rotor blades of the gas turbine engine are heated during the power stage, and During the engine operating cycle, during the cooling stage, said wind turbine engine rotor blades are cooled by fast moving air from the fan as said first fan air flow or usable air flow passes through a gap in the first wall and a gap in the second wall of the rotor housing of the wind gas turbine engine for cooling blades, and this process of cooling the rotor blades of the wind gas turbine engine generates additional power for the wind gas turbine engine according to the present invention, because in the wind gas turbine engine according to the present invention, the air flow or fast moving wind generated by the fan and generated by the parts related to the fan also pushes the rotor blades of the wind gas turbine engine , which provides additional force to rotate the rotor of the wind gas turbine engine. The wind gas turbine engine has at least one combustion chamber where an exhaust gas flow is generated, the exhaust gas flow is directed to the rotor blades of the wind gas turbine engine and, because said rotor blades of the wind gas turbine engine are adjacent to the exhaust gas conduit opening at some point during rotation of the wind gas turbine engine rotor and since said rotor blades of the wind gas turbine engine are located between the walls of the rotor housing of the wind gas turbine engine, the exhaust gas flow pushes the rotor blades of the wind gas turbine engine and rotates the rotor of the wind gas turbine engine, and also rotates the main shaft of the wind gas turbine engine of the wind gas turbine engine when generating power, the pressure of the exhaust gas flow pushes the rotor blades of the wind gas turbine engine nogo engine and rotates the rotor of the wind turbine engine and also rotates the attached main shaft of the wind turbine engine, which is an operation that generates power to do work. The flow of exhaust gas that pushes the rotor blades of a wind turbine engine ends up in the mixture flow pipe. A wind turbine engine according to the present invention in another configuration comprises an optional wind turbine assembly having a wind turbine rotor, said wind turbine rotor is attached to a main shaft of the wind turbine engine, said wind turbine is housed in a housing system of the engine, and said wind turbine is rotated by exhaust gases and further rotated by air flow from a fan and fan housing assembly, exhaust gas flow and air flow into the wind turbine are directed by the fourth guide vanes. Some of the fourth guide vanes may be attached to the second wall of the wind turbine engine casing such that the cooling air flow is substantially unaffected by the exhaust gas flow. For a wind turbine engine to operate properly, the air pressure generated by the engine fan in the torque generating engine must be higher than the pressure of the mixture of usable air flow and exhaust gas flow in the mixture flow line, whereas in the thrust generating engine the air pressure generated by the first fan must be higher than the pressure of the mixture of air and exhaust gas flow in the mixture flow pipe, the pressure of the mixture of air and exhaust gas in the mixture flow pipe can be reduced by increasing the mixture flow pipe, and this can also be done by reducing the outer casing or reducing the air flow duct of the first fan to increase the air pressure passing into the rotor casing of the wind turbine engine.

The wind gas turbine engine of the present invention either has an air cooling system or has both an air cooling system and a liquid cooling system, the air cooling system being adapted for aviation purposes or adapted to another model of wind gas turbine engine, since a wind gas turbine engine with an air cooling system is likely to be is a lighter weight engine, but an air-cooled and liquid-cooled wind turbine engine is likely to be suited for power generation applications or for applications where the wind gas turbine engine must operate in a relatively hot environment or where a liquid cooling medium for the wind gas turbine engine is required for heating purposes , which is likely to be a requirement in a land-based wind turbine engine system, or an amphibious wind turbine engine system vehicle, or an aquatic wind turbine engine system-operated vehicle.

A wind gas turbine engine is a simple rotary engine having a starting system that rotates the main shaft of the wind gas turbine engine and activates the air compression system, and also rotates the wind gas turbine engine fan, the air compression system, which contains the compressor fan, is designed to deliver more air to the combustion chamber, The air compression system supplies air to cool the combustion chamber and supplies air to burn the air-fuel mixture in the combustion chamber, and when the air-fuel mixture is ignited, the gas pressure in the combustion chamber increases and the pressure in the exhaust gas pipe also increases, which also increases the pressure in the area where the rotor of the wind gas turbine engine is located so that the gas pressure pushes the rotor blades of the wind gas turbine engine and rotates the rotor of the wind gas turbine engine, and also rotates the main shaft of the wind gas turbine engine, which produces torque for the engine according to the present invention, the rotation of the main shaft of the wind gas turbine engine also rotates the fan of the wind gas turbine engine, so that the fan creates air pressure for use of the engine, and further said air pressure from the fan helps rotate the rotor of the wind gas turbine engine and in the process cools the rotor of the wind gas turbine engine and cools other parts of the wind gas turbine engine.

In the present invention, the wind turbine engine may have only one shaft or several shafts, which are called the drive shaft means, but in the specification of the present invention are called the main shaft of the wind turbine engine, since the main shaft of the wind turbine engine is attached to the rotor of the wind turbine engine, the specification refers to the fan shaft engine, since the engine fan shaft is attached to the engine fan, and the specification refers to the first fan shaft as it is attached to the first fan, although the wind turbine engine in the present invention may have only one shaft. The air compression system as shown in the present invention can be replaced by another air compression system. Changing the air compression system or changing other elements of the engine according to the present invention does not invalidate the claims. Replacing a bearing with bearings of a different configuration does not invalidate the claims. Moving other parts, or replacing some parts with a different configuration, or eliminating some parts of the engine according to the present invention does not invalidate the claimed claims. The patent specification contains information that can be used to guide the proper design of a wind gas turbine engine, partial or complete information about the assembly of a wind gas turbine engine, and new information as evidence of novelty, usefulness, and new ways of mechanically operating the engine. The information disclosed herein explains and shows one or more options that allow partial or complete adaptation of how to build a wind turbine engine.

DIGITAL INDICATION OF WIND GAS TURBINE ENGINE PARTS ON GRAPHIC MATERIALS AND SCHEMATIC IMAGES

Wind gas turbine engine - 1.00, first axis of rotation - 1.10, first plane - 1.11, second plane - 1.12, fourth plane - 1.14, fifth plane - 1.15, sixth plane - 1.16, first engine housing - 1.17, second engine housing - 1.18, third housing engine - 1.19, usable air flow - 1.20, air passages - 1.21, air pipe assemblies - 1.25, air hoses assemblies - 1.27, air convergence zone - 1.29, shaft play sensor - 1.30, first part - 1.31, second part - 1.32, space for turbo air - 1.40, first space - 1.41, second space - 1.42, third space - 1.43, air gap - 1.44, belt - 1.52, bracket - 1.54, radius - 1.70, bushing - 1.80, gear - 1.90, outer casing - 2.00, engine fan housing - 2.11, engine fan - 2.12, engine fan containment - 2.13, engine fan shaft - 2.14, engine fan hub - 2.15, engine fan blades - 2.18, air pressure sensor - 2.19, shell of the central part - 2.20, section of the fourth guide blade - 2.21, fourth line - 2.22, fourth leading edge - 2.23, fourth trailing edge - 2.24, fourth corner - 2.25, fourth root part - 2.26, fourth section - 2.27, wind gas turbine engine rotor housing - 2.30, fourth guide vanes - 2.40, wall - 2.41, body clearances - 2.42, exhaust gas pipeline opening - 2.43, first wall - 2.44, second wall - 2.45, third wall - 2.46, first guide vane - 2.50, first guide section blades - 2.51, first line - 2.52, first leading edge - 2.53, first trailing edge - 2.54, first corner - 2.55, first root - 2.56, first section - 2.57, engine casing - 2.70, heat sink - 2.90, coolant hoses in Assembly - 2.91, Liquid Cooling Pump - 2.92, Liquid Cooling Passages - 2.93, Liquid Cooling Spaces - 2.94, Coolant Pipes Assemblies - 2.95, Internal Air Compression System - 3.00, Internal Air Compression Fan - 3.10, Internal Compression Fan Hub air - 3.11, fan blades of the internal air compression system - 3.12, fan housing of the internal air compression system - 3.20, shaft of the internal air compression system - 3.21, protective shell of the internal air compression system - 3.22, first fixed blades assembly of the internal air compression system - 3.23 , the second stationary blade assembly of the internal air compression system - 3.24, the blade assembly mounted on the shaft of the internal air compression system - 3.25, the sliding joint - 3.30, the small groove - 3.40, the compressed air receiving means - 3.50, the starting air tube - 3.55, auxiliary air compressor - 3.60, first auxiliary air compressor housing - 3.61, auxiliary air compressor guide vanes - 3.62, auxiliary air compressor fan - 3.63, auxiliary air compressor fan guard - 3.64, first auxiliary air compressor fixed blade assembly - 3.65, second auxiliary air compressor fixed blade assemblies - 3.66, auxiliary air compressor shaft mounted blade assemblies - 3.67, auxiliary air compressor shaft - 3.68, second auxiliary air compressor housing - 3.69, air filtration system - 3.71, air filtration element - 3.72, housing air filtration element - 3.73, booster air compressor - 3.80, dust cover - 3.81, first stationary vanes in the booster air compressor assembly - 3.85, second stationary vanes in the booster air compressor assembly - 3.86, mounted on the shaft of the booster air compressor vanes in assembly - 3.87, first booster air compressor housing - 3.88, second booster air compressor housing - 3.89, booster air compressor shaft - 3.90, combustion chamber - 4.00, combustion chamber housing - 4.10, combustion chamber - 4.11, swirl blades - 4.12, lining - 4.13, corrugated connection - 4.15, small through spaces - 4.16, combustion chamber seal - 4.17, exhaust gas pipeline - 4.20, exhaust gas pipeline body - 4.25, fuel delivery means - 4.30, fuel tank - 4.40, fuel pump - 4.45 , fuel lines assemblies - 4.47, air-fuel mixture igniter - 4.50, exhaust gas flow - 4.70, idler pulley - 4.81, first pulley - 4.82, belt tension maintaining system - 4.83, turbine guide vanes - 4.90, first fan - 5.00, housing first fan - 5.02, first fan containment - 5.03, first fan shaft - 5.04, first fan hub - 5.05, first fan blades - 5.06, first fan nose - 5.07, air duct - 5.15, first fan air flow - 5.20, main frame - 5.30, body oil bypass - 5.40, fins - 5.50, bearing holder - 5.55, lock - 5.56, key - 5.60, o-ring - 5.65, hydraulic pump - 5.70, pylon - 5.80, structural guide vanes - 5.90, clamp - 6.00, wind gas turbine engine rotor - 6.10, wind gas turbine engine rotor hub - 6.20, hub groove for oil ring - 6.26, radial oil ring oil channel - 6.27, inner periphery of hub groove for oil ring - 6.29, exhaust gas compression ring - 6.30, center of radial oil passage of exhaust gas compression ring - 6.31, inner periphery of exhaust gas compression ring - 6.32, radial oil passage of exhaust gas compression ring - 6.33, spring of exhaust gas compression ring - 6.34, protrusion of compression ring for exhaust gas compression ring - 6.35, exhaust gas compression ring thermal expansion gap - 6.36, exhaust gas compression ring spring protrusion - 6.37, exhaust gas compression ring outer periphery - 6.38, exhaust gas compression ring spring pusher leg - 6.39, hub groove exhaust gas compression ring - 6.40, inner periphery of the hub groove for the exhaust gas compression ring - 6.45, radial center of the exhaust gas compression ring - 6.48, wind gas turbine engine main shaft - 6.50, wind gas turbine engine rotor blades - 6.60, second section - 6.61, second line - 6.63, second root - 6.64, second edge - 6.65, second leading edge - 6.66, second trailing edge - 6.67, second corner - 6.69, oil lines assemblies - 6.70, oil ring radial oil channel center - 6.75, oil ring radial center - 6.77, oil ring - 6.80, coil spring - 6.81, oil seal - 6.82, oil ring spring - 6.83, oil ring projection - 6.84, oil ring outer periphery - 6.85, oil ring thermal expansion gap - 6.86, inner oil ring periphery - 6.87, oil ring spring protrusion - 6.88, oil ring spring pusher leg - 6.89, compressed air space - 6.90, oil hoses assembly - 6.95, oil pump assembly - 7.00, oil pump - 7.10, screen - 7.20, Oil Line - 7.30, Alternator - 7.40, Electrical Generator - 7.50, Mount - 7.55, Starter - 7.60, A/C Compressor - 7.70, Flywheel Housing - 7.80, Flywheel - 7.90, Transmission - 8.00, Rotor wind turbine - 8.10, wind turbine rotor hub - 8.20, wind turbine rotor blade - 8.30, sixth section - 8.31, sixth leading edge - 8.32, sixth trailing edge - 8.33, sixth line - 8.34, sixth corner - 8.35, sixth root part - 8.36, sixth edge 8.37, block containing oil - 8.50, through opening - 8.60, first electric motor - 8.80, second electric motor - 8.90, bearing assembly - 9.00, bearings - 9.10, gaskets - 9.11, ball bearings - 9.15, tapered roller bearings - 9.16, cylindrical roller bearings - 9.17, pipeline for mixture flow - 9.20, exhaust gas manifold - 9.25, fastenings - 9.30, pipeline for air flow of the first fan - 9.50, plain bearing - 9.60, bearing housing assembly - 9.70, first cooling fan - 9.80, second cooling fan - 9.90, first location - 111, second location - 222, first end - 666, side view - 777, second end - 888, third location - 999, first guide vane length - 100, rotor blade length wind gas turbine engine - 200, length of the fourth guide blades - 400, length of the wind turbine rotor blade - 600.

DESCRIPTION OF GRAPHIC MATERIALS AND TECHNICAL CHARACTERISTICS OF THE INVENTION

In fig. 1 illustrates a view of a first end of a wind turbine engine having an air-cooled system and adapted to generate thrust. In fig. 2 illustrates a side view of the wind turbine engine shown in FIG. 1. In FIG. 3 illustrates a section 1-1' of the wind gas turbine engine shown in FIG. 1 and shows the internal air compression system. In fig. 4 shows section 2-2' of FIG. 2. In FIG. 5 illustrates an alternative cross-section 2-2' of the wind turbine engine shown in FIG. 2. In FIG. 6 illustrates a view of a first end 666 of a torque generating wind turbine engine having an air cooling system and having an external air compression system. In fig. 7 illustrates a view of the second end 888 of the wind turbine engine shown in FIG. 8, and a view of the second end of the wind turbine engine shown in FIG. 6. In FIG. 8 illustrates a view of the third location 999 of the wind turbine engine shown in FIG. 6. In FIG. 9 illustrates a 4-4' sectional view of the wind gas turbine engine shown in FIG. 8. In FIG. 10 illustrates a section 3-3' of FIG. 6. In FIG. 11 illustrates a first end view of yet another torque generating wind turbine engine having an external air compression system and a liquid cooled system supplemented by an air cooling system. In fig. 12 illustrates a view of the second end 888 of the wind turbine engine shown in FIG. 13, and a view of the second end of the wind turbine engine shown in FIG. 11. In FIG. 13 illustrates a view of the third location 999 of the wind turbine engine shown in FIG. 11. In FIG. 14 illustrates a section 6-6' of FIG. 13. In FIG. 15 illustrates a 5-5' sectional view of the wind turbine engine shown in FIG. 11. In FIG. 16 illustrates a view of a first end 666 of a wind turbine engine having an external air compression system and having an air-cooled torque generating system. In fig. 17 illustrates a view of the second end 888 of the wind turbine engine shown in FIG. 18, and a view of the second end of the wind turbine engine shown in FIG. 16. In FIG. 18 illustrates a view of the third location 999 of the wind turbine engine shown in FIG. 16. In FIG. 19 illustrates a section 8-8' of FIG. 18. In FIG. 20 shows a section 7-7' of FIG. 16. In FIG. 21 illustrates an air-cooled wind turbine engine having a typical belt arrangement with the booster air compressor driven by a second electric motor. In fig. 22 illustrates an air-cooled wind turbine engine having a typical belt arrangement, showing that a booster air compressor is driven by a second electric motor, and wherein a booster air compressor is driven by a first electric motor. In fig. 23 illustrates an air-cooled and a liquid-cooled wind turbine engine having a typical belt arrangement, with the booster air compressor being driven by a second electric motor. In fig. 24 illustrates an air-cooled and a liquid-cooled wind turbine engine having a typical belt arrangement, showing that a booster air compressor is driven by a second electric motor, and wherein a booster air compressor is driven by a first electric motor. electric motor. In fig. 25 shows a section 9-9' of FIG. 6 typical auxiliary air compressor. In fig. 26 illustrates a section 10-10' of FIG. 6 typical booster air compressor. In fig. 27 illustrates an enlarged view for better understanding of a typical gas compression ring for an engine according to the present invention for generating torque. In fig. 28 illustrates an enlarged view of the first location 111 in FIG. 27 for a better understanding of a typical gas compression ring and a typical gas compression ring spring for an engine according to the present invention for producing torque, wherein the rotor hub of a wind turbine engine is not shown to show in more detail the details of the gas compression ring and the gas compression ring spring. . In fig. 29 is a schematic view of a first guide vane, walls, housing clearances, fourth guide vanes and a rotor of a wind gas turbine engine of a wind gas turbine engine according to the present invention. In fig. 30 is an enlarged view for better understanding of a typical engine oil ring of the present invention for generating torque. In fig. 31 illustrates an enlarged view of the second location 222 of FIG. 30 for a better understanding of a typical oil ring and a typical oil ring spring of a torque generating engine according to the present invention, wherein the rotor hub of a wind turbine engine is not shown to show the details of the oil ring and the oil ring spring in more detail. In fig. 32 shows a known bearing holder with a lock. In fig. 33 is a schematic view of an exhaust pipe casing attached to a third wall of a rotor casing of a wind gas turbine engine, and the rotor casing of a wind gas turbine engine is composed of a first motor casing having a first wall, a second motor casing having a second wall, and a third motor casing having a third wall. In fig. 34 is a schematic view of an exhaust pipe housing attached to a third wall of a wind gas turbine engine rotor housing, and the first wind gas turbine engine rotor housing piece includes a first wall and a third wall, and the second wind gas turbine engine rotor housing piece includes a second wall. In fig. 35 is a schematic view of an exhaust pipe housing attached to a first wall of a wind turbine engine rotor housing, and the first wind turbine engine rotor housing portion has a first wall and has a third wall, while the wind turbine engine rotor housing portion includes a second wall. In fig. 36 is a schematic diagram of an exhaust pipe housing attached to a second wall of a wind gas turbine engine rotor housing, and a first wind turbine engine rotor housing piece has a first wall, and a second wind gas turbine engine rotor housing piece has a second wall and has a third wall. In fig. 37 is a schematic view of an exhaust pipe housing attached to a third wall of a wind gas turbine engine rotor housing and attached to a second wall of a wind gas turbine engine rotor housing, and the first wind gas turbine engine rotor housing piece has a first wall, and the second wind gas turbine engine rotor housing piece has a second wall and has a third wall. In fig. 38 is a schematic view of an exhaust pipe housing attached to a first wall of a wind gas turbine engine rotor housing and attached to a third wall of a wind gas turbine engine rotor housing, and the first part of the wind gas turbine rotor housing has a first wall and has a third wall, while the second part has a second wall. In fig. Figure 39 shows a view of the rotor of a wind gas turbine engine. In fig. 40 is a section view viewed along line 1-1' of FIG. 39 rotor blades of a wind gas turbine engine when cut along a radial arc. In fig. 41 is an illustration of the first guide vane. In fig. 42 is a cross-sectional view of the first guide vane along line 2-2' of FIG. 41 when cutting along a radial arc. In fig. Figure 43 shows a wind turbine rotor blade cut along a radial arc. In fig. 44 is a sectional view along line 3-3' of FIG. 43 wind turbine rotor blades when cut along a radial arc. In fig. 45 shows yet another configuration of a bearing means assembled with a cylindrical roller bearing, a sleeve and tapered roller bearings according to the present invention, which can be used for a wind turbine engine according to the present invention. In fig. 46 shows yet another configuration of a bearing assembly with ball bearings, a sleeve and a cylindrical roller bearing according to the present invention, which can be used for a wind turbine engine according to the present invention. In fig. 47 shows the transmission and second cooling fan in an air-cooled wind turbine engine. In fig. 48 shows a wind turbine engine having both air cooling and liquid cooling, which includes a transmission and a second cooling fan. In fig. 49 is a schematic representation of a typical compressed air flow according to the present invention when using an internal air compression system. In fig. 50 is a schematic representation of another exemplary compressed air flow according to the present invention in an internal air compression system like a jet engine. In fig. 51 is a schematic diagram of a typical oil flow according to the present invention. In fig. 52 is a schematic diagram of a typical fuel flow according to the present invention. In fig. 53 is a schematic diagram of another exemplary compressed air flow of an outdoor air compression system according to the present invention. In fig. 54 is a schematic diagram of a typical compressed air flow according to the present invention when using an auxiliary air compressor and a booster air compressor. In fig. 55 is a schematic representation of a typical liquid cooling flow according to the present invention. In fig. 56 shows a schematic illustration of a system for extracting air from an auxiliary air compressor or an internal air compression system into air passages in the second wall of the rotor housing of a wind turbine engine. In fig. 57 shows a schematic representation of a system for extracting air from a booster air compressor into the air passages in the second wall of the rotor housing of a wind gas turbine engine. In fig. 58 is an illustration of a fourth guide vane. In fig. 59 shows a section through the fourth guide vane along line 4-4' of FIG. 58 when cutting along a radial arc. In fig. 60 is a detailed and enlarged schematic view of the expansion gap of an exhaust gas compression ring according to the present invention. In fig. 61 is a detailed and enlarged schematic view of an oil ring expansion gap according to the present invention. In fig. 62 is an illustration or schematic representation of an optional oil conduit located adjacent to a wind turbine engine main shaft in a wind turbine engine rotor hub that is not parallel to the axis of rotation of the wind turbine engine rotor shaft such that oil circulates to provide more efficient cooling of the wind turbine engine rotor. In fig. 63 is an illustration or schematic representation of an alternative coil spring for oil rings. In fig. 64 is a schematic view of an engine according to the present invention having three main bodies, which include a first body with a first wall, a second body with a second wall and a third body with a third wall in an air-cooled engine according to the present invention, and shows that the bearings used are ball bearings. FIG. 65 is a schematic view of an engine according to the present invention having three main bodies, which include a first motor body having a first wall, a second motor body having a second wall, and a third motor body having a third wall, in a liquid-cooled engine according to the present invention. , and the bearings used are shown to be tapered roller bearings.

With reference to FIG. 1, fig. 2, fig. 3, fig. 4 and fig. 5 and any of the applicable graphics from FIG. 29 according to FIG. 65, inclusive, which are used for cross-reference, shows the first disclosure of the wind gas turbine engine invention set forth in specifications from specification number 1 to specification number 3, inclusive, as follows.

1. A wind gas turbine engine 1.00 having an air cooling system, wherein said wind gas turbine engine 1.00 comprises an engine housing system, an air pressure sensor 2.19, a shaft play sensor 1.30, structural guide vanes 5.90, a first fan assembly having a first fan 5.00, an internal compression system 3.00 air or several internal air compression systems 3.00, at least one combustion chamber 4.00 having a combustion chamber housing 4.10, at least one compressed air delivery system, at least one compressed air receiving means 3.50, at least one fuel system, electrical a system having at least one air-fuel mixture ignition system with at least one air-fuel mixture ignition means 4.50, at least one exhaust gas pipeline housing 4.25, at least one wind gas turbine engine rotor assembly, a lubrication system, a drive means shaft, wind turbine engine accessories, several bearing assemblies 9.00, several known exhaust gas seal means, several known oil seal means, 5.50 fins, 1.90 gears, 5.07 first fan nose, mounting system with 9.30 fasteners, pipes for air assemblies 1.25, air hoses assemblies 1.27, wind gas turbine engine components and a drive system or several drive systems for operating said wind gas turbine engine components; said components of the wind gas turbine engine comprise one or more of the following: a first fan 5.00, an air pressure sensor 2.19, a shaft play sensor 1.30, a known starting system, which is either in the form of an electric starter, or a combined unit with starting capability and power generating capability, or any suitable starter, internal air compression system or several internal air compression systems, fuel pump 4.45, oil pump 7.10; said fuel system comprises a fuel tank 4.40, a fuel pump 4.45, a fuel line assembly 4.47, a fuel flow control means and has at least one fuel delivery means 4.30; said air cooling system comprises air passages 1.21 and air pipe assemblies 1.25, said air pipe assemblies 1.25 and air hoses assemblies 1.27 are interchangeable; said fuel delivery means 4.30 has a means of communication with the fuel system, said fuel delivery means 4.30 being either a single injector or an optional multi-injector system; said lubrication system contains at least one known oil pump assembly 7.00, several oil lines 7.30, oil lines assemblies 6.70, oil hoses assemblies 6.95 and lubrication system accessories, said oil pump assembly 7.00 includes an oil pump 7.10, The specified 6.70 oil line assemblies and the specified 6.95 oil hose assemblies are interchangeable; said wind gas turbine engine rotor assembly contains a wind gas turbine engine rotor 6.10 and a wind gas turbine engine main shaft 6.50, said wind gas turbine engine main shaft 6.50 has a first rotation axis 1.10, during operation of said wind gas turbine engine 1.00 said wind gas turbine engine rotor 6.10 and said main shaft 6.50 of a wind gas turbine engine rotates on said first axis 1.10 of rotation of said main shaft 6.50 of the wind gas turbine engine; said exhaust gas conduit housing 4.25 includes an exhaust gas conduit 4.20 and fins 5.50, said internal air compression system 3.00 is an air pump that generates air pressure for cooling the air seal means and air for the combustion process of the air-fuel mixture; said internal air compression system 3.00 comprises an air conduit 5.15 and a compressed air space 6.90, said air conduit 5.15 has means for communication with said compressed air receiving means 3.50 and said compressed air space 6.90, and said compressed air space 6.90 has means communicating with said compressed air receiving means 3.50, said air-fuel mixture ignition means 4.50 is attached to said exhaust gas conduit housing 4.25, or attached to said combustion chamber housing 4.10, or attached at another suitable location;

wherein the engine housing system is either adapted for an engine configuration with a large bypass air flow, or adapted for an engine configuration with a small bypass air flow, said engine housing system comprising an outer housing 2.00, an engine casing 2.70, a central part shell 2.20, a space 1.40 for turbocharged air , at least one air gap 1.44, a second space 1.42, a third space 1.43, at least one wind turbine engine rotor housing 2.30, multiple bearing assembly housings 9.70, fourth guide vanes 2.40 and a mixture flow conduit 9.20; said outer casing 2.00 includes a first fan housing assembly and a main frame 5.30, said main frame 5.30 includes a pylon 5.80 and a first fan air flow conduit 9.50; a first fan assembly, which is complemented by a housing of the first fan assembly, generates a first fan air flow 5.20 during operation of said wind gas turbine engine 1.00, said first fan air flow 5.20 being adapted to cool hot parts of said wind gas turbine engine 1.00; said center section shell 2.20 is attached to the main frame 5.30 by means of structural guide vanes 5.90, said main frame 5.30 and said structural guide vanes 5.90 also direct the first fan air flow 5.20 to the second end 888 of said wind turbine engine 1.00, said center section shell 2.20 is attached to the main frame 5.30 with the help of structural guide vanes 5.90, the specified shell 2.20 of the central part contains fins 5.50 for radiating heat, the specified structural guide vanes 5.90 ensure smooth movement of the specified air flow 5.20 of the first fan into the second end 888 of the specified wind gas turbine engine 1.00; said turbocharged air space 1.40 is designed to ensure proper movement of said first fan air flow 5.20 into the second end 888 of said wind gas turbine engine 1.00, while said wind gas turbine engine rotor housing 2.30 and said third space 1.43 allow a portion of said first fan air flow 5.20 to pass, said third space 1.43 located in the pipeline 9.20 for mixture flow, said engine casing 2.70 provides access for repair of certain parts of the wind gas turbine engine 1.00;

wherein the bearing assembly 9.00 comprises bearings 9.10 and accessories for the bearing assembly, said bearing assembly 9.00 prevents too much axial movement and prevents too much radial movement of the shaft in relation to the housing 9.70 of the bearing assembly, said bearings 9.10 are shaped ball bearings 9.15, tapered roller bearings 9.16, cylindrical roller bearings 9.17, plain bearings 9.60 and other suitable form of bearings 9.10, the specified accessories for the bearing assembly contain: gaskets 9.11, keys 5.60, bushing 1.80, o-rings 5.65, bearing holders 5.55 , castle 5.56 and oil seals 6.82; said bearing holders 5.55 and said bearing housing 9.70 assembly support the position of said bearings 9.10, said bearing holder 5.55 prevents said bearings from moving out of place, said bearing holder 5.55 is in the form of eyelet and threaded fasteners, said bearing holder 5.55 operates in conjunction with a lock 5.56, the specified spacers 9.11 are designed to transfer axial load from the shaft to the specified bearings 9.10, or the specified spacers 9.11 transfer the axial load from the specified bearing 9.10 to another bearing 9.10, or the specified spacers 9.11 are intended to transfer the axial load from the specified bushing 1.80 to the specified bearings 9.10 , while the bearing holders 5.55 are designed to transfer axial load from said bearings 9.10 to said housing 9.70 of the bearing assembly, said sleeve 1.80 allows for easy removal or separation of the bearing assembly from the shaft and allows for easy removal of said wind turbine engine main shaft 6.50 from said bearing assembly means by performing several processes that result in a slip-out procedure, said bushing 1.80 also allows for less damage by said bearing assembly 9.00 when inserting said main shaft 6.50 of a wind turbine engine, or less damage by said bearing assembly 9.00 when inserting another the shaft of the specified wind gas turbine engine 1.00 during the assembly process with slipping inward; said bushing 1.80 shall be secured to said wind turbine engine main shaft 6.50 such that said bushing 1.80 rotates with said wind turbine engine main shaft 6.50 and the proper position of said bushing 1.80 is maintained in relation to said bearings 9.10 and in relation to said wind turbine main shaft 6.50 new engine, and said sleeve 1.80 shall be secured to another shaft associated with said wind turbine engine 1.00 such that said sleeve 1.80 rotates with said other shaft associated with said wind turbine engine 1.00 and the proper position of said sleeve 1.80 is maintained with respect to said bearings 9.10 and in relation to said other shaft;

wherein the first fan assembly has a first fan 5.00, a first fan shaft 5.04 and a first fan nose 5.07, said first fan 5.00 is attached to a first fan shaft 5.04, said first fan 5.00 has a first fan hub 5.05, said first fan hub 5.05 contains several blades 5.06 of a first fan, said nose section 5.07 of a first fan is attached to said hub 5.05 of a first fan, said multiple blades 5.06 of a first fan are attached to said hub 5.05 of a first fan, said hub 5.05 of a first fan is attached to said shaft 5.04 of a first fan, said shaft 5.04 of a first fan the fan is supported to rotate by means of a bearing assembly 9.00;

wherein the housing of the first fan assembly comprises a housing 5.02 of the first fan, a protective shell 5.03 of the first fan and turbine guide vanes 4.90, said turbine guide vanes 4.90 contain an oil pipeline 7.30 for injecting the injection oil and outputting the return oil for the bearing means assembly 9.00, according to at least one of said bearing means assemblies 9.00 is located adjacent to the first fan assembly, said oil conduit 7.30 of said first fan housing 5.02 constitutes oil spaces along said turbine guide vanes 4.90, said oil conduit 7.30, oil lines assemblies 6.70 and oil hose assemblies 6.95 carry oil to and from said bearing assembly 9.00 in said first fan housing 5.02, said oil line 7.30, said oil hoses assemblies 6.95 and said oil lines assemblies 6.70 are in communication with lubrication system;

wherein the first fan assembly and the first fan assembly, during operation of the wind gas turbine engine 1.00, generates a first fan air flow 5.20 for thrust and cooling of said wind gas turbine engine 1.00, said first fan air flow 5.20 cools the following: combustion chamber housing 4.10, rotor housing 2.30 wind gas turbine engine, shell 2.20 of the central part, pipeline 9.20 for the flow of the mixture and other hot parts of the specified wind gas turbine engine 1.00 that require cooling; said first fan air stream 5.20 is used for thrust when said first fan air stream 5.20 moves at high speed from the second end 888 of said wind gas turbine engine 1.00, said first fan air stream 5.20 also cools the rotor parts of the wind gas turbine engine assembly and cools other parts of the said wind gas turbine engine engine 1.00 when a portion of said first fan air flow 5.20 passes through the turbocharged air space 1.40, the second space 1.42 and the third space 1.43 of said wind turbine engine 1.00;

wherein the lubrication system has means of communication with several bearing means assemblies 9.00, said lubrication system supplies oil for cooling and lubrication of said several bearing means assemblies 9.00, said lubrication system contains at least one oil pump assembly 7.00, oil lines assemblies 6.70, oil hose assemblies 6.95 and lubrication system accessories, said lubrication system accessories contain an oil cooler and an oil containing block 8.50, parts that support the housing 9.70 of the bearing means assembly of the first fan housing 5.02, contain turbine guide vanes 4.90 specified turbine guide vanes 4.90 act as an oil cooler;

wherein the internal air compression system 3.00 contains a fan 3.10 of the internal air compression system, a housing 3.20 of the fan of the internal air compression system, a protective shell 3.22 of the fan of the internal air compression system, a shaft 3.21 of the internal air compression system, the first fixed blade assembly 3.23 of the internal air compression system, second stationary blade assembly 3.24 of the internal air compression system, space 6.90 for compressed air, pipeline 5.15 for air and blade assembly 3.25 mounted on the shaft of the internal air compression system; said internal air compression system fan 3.10 includes an internal air compression system fan hub 3.11 and an internal air compression system fan blade 3.12, said internal air compression system 3.00 supplies compressed air to one or more of the following: a combustion chamber 4.00 for burning the air-fuel mixture, in combustion chamber housing 4.10 for cooling purposes and into wind gas turbine engine 1.00 for additional cooling of hot parts of said wind gas turbine engine 1.00, said internal air compression system comprises a known air bleed system;

wherein the combustion chamber 4.00 is configured to generate an exhaust gas flow 4.70 during operation of the wind gas turbine engine 1.00, said exhaust gas flow 4.70 is the result of combustion of a fuel-air mixture, said combustion chamber 4.00 comprises one or more of the following: a combustion chamber housing 4.10, a combustion chamber 4.11 , twisting blades 4.12, lining 4.13 and seal 4.17 of the combustion chamber; said exhaust gas flow 4.70 passes through the exhaust gas conduit housing 4.25 through the exhaust gas conduit 4.20, said combustion chamber housing 4.10 is cooled by one or more of the following: cooling by compressed air, cooling by the air flow of the first fan, or cooling by another air flow; said combustion chamber 4.00 has means of communication with fuel delivery means 4.30, one or more air-fuel mixture ignition means 4.50 and an air compression system; said combustion chamber housing 4.10 includes means of attachment to the main frame 5.30 or means of attachment to other parts of the wind turbine engine 1.00 to prevent stress and vibration of said combustion chamber housing 4.10 caused by the air flow 5.20 of the first fan, said main frame 5.30 allowing access to said chamber 4.00 combustion chamber for replacing parts, said combustion chamber housing 4.10 includes fins 5.50 for radiating heat and includes a starting air tube 3.55, said starting air tube 3.55 has a means of communication with another source of compressed air;

wherein the rotor of the wind gas turbine engine assembly contains a rotor 6.10 of the wind gas turbine engine and the main shaft 6.50 of the wind gas turbine engine, said rotor 6.10 of the wind gas turbine engine contains a hub 6.20 of the rotor of the wind gas turbine engine, said hub 6.20 of the rotor of the wind gas turbine engine has several blades 6.60 rotor ora wind gas turbine engine, specified multiple 6.60 rotor blades wind gas turbine engine are attached to said wind gas turbine engine rotor hub 6.20, said wind gas turbine engine rotor blades 6.60 are protrusions from said wind gas turbine engine rotor hub 6.20, said wind gas turbine engine rotor blades 6.60 are made of a different material compared to the rotor hub 6.20 wind turbine engine, or said blades 6.60 of the wind gas turbine engine rotor is made of the same material as the specified wind gas turbine engine rotor hub 6.20; said wind gas turbine engine rotor blades 6.60 extend outward from said wind gas turbine engine rotor hub 6.20, said multiple wind gas turbine engine rotor blades 6.60 are spaced substantially equal distances along said wind gas turbine engine rotor hub 6.20; during operation of the specified wind gas turbine engine 1.00, the specified blades 6.60 of the wind gas turbine engine rotor, the specified rotor 6.10 of the wind gas turbine engine and the specified main shaft 6.50 of the wind gas turbine engine are driven into rotation on the first axis 1.10 of rotation of the specified main shaft 6.50 of the wind gas turbine engine by the exhaust flow 4.70 gas from the combustion chamber 4.00, and additionally, said rotor blades 6.60 of the wind gas turbine engine, said rotor 6.10 of the wind gas turbine engine, and said main shaft 6.50 of the wind gas turbine engine are driven into rotation on said first axis 1.10 of rotation of said main shaft 6.50 of the wind gas turbine engine by part of the air flow 5.20 of the first fan from the casing of the first fan assembly and the first fan assembled;

wherein the means in the form of a drive shaft is a system in which the shaft 5.04 of the first fan, the shaft 3.21 of the internal air compression system and the main shaft 6.50 of the wind gas turbine engine are a single continuous shaft, or the shaft 5.04 of the first fan, the shaft 3.21 of the internal air compression system and the main the wind gas turbine engine shaft 6.50 are separate shafts, with said first fan shaft 5.04, said internal air compression system shaft 3.21 and said wind gas turbine engine main shaft 6.50 being in communication with each other;

wherein the mixture flow line 9.20 directs a mixture of a portion of the first fan air flow 5.20 and the exhaust gas flow 4.70 for thrust;

wherein the bearing assembly housing 9.70 supports one bearing 9.10 or supports multiple bearings 9.10, said bearing assembly housing 9.70 includes a housing oil bypass passage 5.40, said housing oil bypass passage 5.40 ensures proper circulation of oil in the bearing assembly housing 9.70 in assembly, said bearing housing assembly 9.70 and said bearings 9.10 include a corresponding groove for a key 5.60, said key 5.60 preventing said bearings 9.10 from damaging said bearing housing assembly 9.70;

wherein the exhaust gas flow 4.70 from the combustion chamber 4.00 moves into the space of the wind gas turbine engine rotor housing 2.30, and the movement of the specified exhaust gas flow 4.70 in the wind gas turbine engine rotor housing 2.30 pushes the wind gas turbine engine rotor blades 6.60 and rotates the wind gas turbine engine rotor 6.10, the main shaft 6.50 wind gas turbine engine, shaft 3.21 of the internal air compression system, shaft 5.04 of the first fan and first fan 5.00; said main shaft 6.50 of the wind gas turbine engine has means of communication with the shaft 3.21 of the internal air compression system, and said main shaft 6.50 of the wind gas turbine engine has means of communication with the shaft 5.04 of the first fan;

wherein the rotor housing 2.30 of the wind gas turbine engine is adapted to allow installation of the required parts of the wind gas turbine engine 1.00 into the specified housing 2.30 of the rotor of the wind gas turbine engine, which provides for the possibility of installing the rotor assembly of the wind gas turbine engine, said housing 2.30 of the rotor of the wind gas turbine engine allows rotation of the main shaft 6.50 of the wind gas turbine engine and wind gas turbine engine rotor 6.10, said wind gas turbine engine rotor housing 2.30 has walls 2.41, at least two housing clearances 2.42, at least one exhaust gas pipeline opening 2.43, ribs 5.50 and a wind gas turbine engine rotor assembly space, said walls 2.41 containing the first wall 2.44, second wall 2.45 and third wall 2.46; said housing gap 2.42 in said second wall 2.45, which is wider than said housing gap 2.42 in said first wall 2.44, is configured so that the exhaust gas flow 4.70 moves from said wind gas turbine engine rotor housing 2.30 through said housing gap 2.42 in said second wall 2.45 ; the specified housing 2.30 of the rotor of the wind gas turbine engine is made with air passages 1.21, a number of the specified air passages 1.21 are used to cool the specified walls 2.41 of the specified housing 2.30 of the rotor of the wind gas turbine engine, the specified space of the rotor of the wind gas turbine engine assembly contains a second space 1.42, the specified second space 1.42 provides the possibility of rotation of the specified rotor 6.10 of a wind gas turbine engine; the exhaust gas pipeline 4.20 is in communication with a portion of the second space 1.42 of the specified wind gas turbine engine rotor housing 2.30, the specified exhaust gas pipeline housing 4.25 is directly or indirectly attached to the specified wind gas turbine engine rotor housing 2.30, or is attached to any of the specified first wall 2.44, specified second wall 2.45, said third wall 2.46, or attached to any suitable combination of said first wall 2.44, said second wall 2.45 and said third wall 2.46 so as to allow said exhaust gas flow 4.70 to move into a portion of said second space 1.42 of said rotor housing 2.30 wind gas turbine engine; said exhaust gas conduit opening 2.43 on said third wall 2.46 shall be adjacent to said first wall 2.44 and adjacent to said second wall 2.45, at one point or more points of said wind gas turbine engine rotor housing 2.30, said first wall 2.44, said second wall 2.45 and said third wall 2.46 are adjacent to each other; said wind gas turbine engine rotor housing 2.30 has the required distance from said wind gas turbine engine rotor 6.10; according to the design and during operation of said wind gas turbine engine 1.00, said wind gas turbine engine rotor housing 2.30 provides said exhaust gas flow 4.70 from the combustion chamber 4.00 into said wind gas turbine engine rotor housing 2.30, said exhaust gas flow 4.70 passes through said exhaust gas conduit 4.20 and passes on. into said portion of said second space 1.42 of said wind gas turbine engine rotor housing 2.30, and said exhaust gas flow 4.70, which is directed by said walls 2.41 of said wind gas turbine engine rotor housing 2.30, pushes said wind gas turbine engine rotor blades 6.60, thereby rotating said wind gas turbine rotor 6.10 new engine on a first rotation axis 1.10 of said wind gas turbine engine main shaft 6.50, and operation generates energy for said wind gas turbine engine 1.00, said energy rotating said wind gas turbine engine main shaft 6.50 and a first fan 5.05 that moves a large volume of air for thrust; said walls 2.41 and said wind turbine engine rotor blades 6.60 prevent the majority of said exhaust gas flow 4.70 from escaping into the mixture flow conduit 9.20 until said exhaust gas flow 4.70 reaches one of said housing gaps 2.42 in said second housing wall 2.45 2.30 of a wind gas turbine engine rotor, and said exhaust gas stream 4.70 exits said wind gas turbine engine rotor housing 2.30 through said housing gaps 2.42 in said second wall 2.45, and said exhaust gas stream 4.70 ultimately ends up in said mixture flow conduit 9.20; said housing gap 2.42 in said first wall and said housing gap 2.42 in said second wall 2.44 of said wind gas turbine engine rotor housing 2.30 further provide the ability to move a portion of said first fan air flow 5.20 into and out of said wind gas turbine engine rotor housing 2.30 and from said rotor housing 2.30 wind gas turbine engine further allows said portion of said first fan air flow 5.20 to flow from said first fan housing assembly between said wind gas turbine engine rotor blades 6.60 to cool said wind gas turbine engine rotor blades 6.60 of said wind gas turbine engine rotor 6.10, and in the process of cooling said rotor blades 6.60 of a wind gas turbine engine, said portion of the first fan air flow 5.20 which moves as wind ultimately adds a rotating force to said wind gas turbine engine rotor 6.10 to rotate, and therefore, during operation of said wind gas turbine engine 1.00, said portion of the first fan air flow 5.20 adds more torque to the specified wind gas turbine engine 1.00; guide vanes direct said portion of said first fan air flow 5.20 to cool said wind gas turbine engine rotor blades 6.60, said wind gas turbine engine rotor housing 2.30 contains air passages 1.21 to provide said portion of the first fan air flow 5.20 and contains air passages 1.21 for cooling with air from the exhaust system air of said walls 2.41 of said wind gas turbine engine rotor housing 2.30, said wind gas turbine engine rotor housing 2.30 contains at least one pipeline 5.15 for air and fins 5.50.

2. A wind-gas turbine engine 1.00 according to the first disclosure, wherein the combustion chamber 4.00 comprises a lining 4.13, said lining 4.13 has a corrugated connection 4.15, said corrugated connection 4.15 contains small through spaces 4.16 that allow compressed air to pass through said corrugated connection 4.15, said compressed air passing through said small through spaces 4.16 cools said lining 4.13, and said small through spaces 4.16 further direct cooling air to said lining 4.13.

3. A wind turbine engine 1.00 according to the first disclosure, wherein parts adjacent to the main shaft 6.50 of the wind turbine engine, the first fan shaft 5.04 and the internal air compression system shaft 3.21 have a means of communication with a shaft play sensor 1.30, said shaft play sensor 1.30 monitors excessive play of the said shaft play sensor 1.30. wind turbine engine main shaft 6.50, said first fan shaft 5.04, and said internal air compression system shaft 3.21 to alert maintenance personnel of impending failure so that shutdown of the wind turbine engine is accomplished before significant damage occurs.

With reference to FIG. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, fig. 20, fig. 21, fig. 22, fig. 23, fig. 24, fig. 25, fig. 26 and any of the applicable graphics from FIG. 27 according to FIG. 65 inclusive, which are used for cross-reference, shows a second disclosure of a wind turbine engine set out in specification number 4 as follows.

4. A wind gas turbine engine 1.00 having an air cooling system or having both an air cooling system and a liquid cooling system, said air cooling system comprising fins 5.50, air pipe assemblies 1.25 and air passages 1.21, said liquid cooling system comprising a heat sink 2.90, 2.92 liquid cooling pump, 2.93 liquid cooling passages, liquid cooling medium, 2.94 liquid cooling spaces and liquid cooling accessories, specified liquid cooling accessories contain 2.91 coolant hose assemblies and 2.95 coolant pipe assemblies, specified coolant hose assemblies 2.91 and the specified coolant pipe assemblies 2.95 are interchangeable, the specified wind gas turbine engine 1.00 contains an engine housing system, an air pressure sensor 2.19, an engine fan assembly having an engine fan 2.12 and an engine fan shaft 2.14, an air filtration system 3.71 or several filtration systems 3.71 air, an air compression system or several air compression systems, at least one combustion chamber 4.00, at least one means for delivering compressed air, at least one means 3.50 for receiving compressed air, a fuel system, an electrical system having an ignition system for the air-fuel mixture with at least one means 4.50 for igniting the air-fuel mixture, at least one exhaust gas pipeline housing 4.25 having an exhaust gas pipeline 4.20, at least one wind gas turbine engine rotor assembly, a lubrication system, a means in the form of a drive shaft, accessories for the wind gas turbine engine, several bearing assemblies 9.00, first space 1.41, second space 1.42, third space 1.43, several exhaust gas seal means, several oil seal means that contain several oil seals 6.82, bearing holders 5.55, keys 5.60, sealing ring 5.65, clamps 6.00, belt 1.52, brackets 1.54, belt tension maintaining system 4.83, air pipe assemblies 1.25, air hoses assemblies 1.27, gears 1.90, wind turbine assembly, which contains the wind turbine rotor 8.10, wind gas turbine engine components and drive a system or several drive systems for operating said components of a wind gas turbine engine, said components of a wind gas turbine engine comprise one or more of the following: an electrical generating system or multiple electrical generating systems, an air pressure sensor 2.19, a starting system, a liquid cooling pump 2.92, an air compression system that contains one or more external air compression systems, an air conditioning system having an air conditioning system compressor 7.70, a transmission 8.00, a first cooling fan 9.80 or a second cooling fan 9.90, or an electrically controlled fan, a hydraulic pump 5.70, at least one idler pulley 4.81, at least one first pulley 4.82, an oil pump 7.10, at least one first electric motor 8.80, at least one second electric motor 8.90, a wind turbine rotor 8.10 and other accessories for the wind gas turbine engine; said fuel system comprises a fuel tank 4.40, a fuel pump 4.45, fuel lines assemblies 4.47, a fuel flow control means and at least one fuel delivery means 4.30, said compressed air delivery means contains air pipe assemblies 1.25 and air hoses assemblies 1.27, at least one of said air pipe assemblies 1.25 has means of communication with compressed air receiving means 3.50, said air pipe assemblies 1.25 and said air hoses assemblies 1.27 are interchangeable; said bearing assembly 9.00 comprises bearings 9.10, said bearings 9.10 are in the form of ball bearings 9.15, tapered roller bearings 9.16, cylindrical roller bearings 9.17, plain bearings 9.60 and other suitable form of bearings 9.10; said external air compression system supplies compressed air to said combustion chamber 4.00, said external air compression system is in the form of an auxiliary air compression system and a booster air compression system, said auxiliary air compression system has an auxiliary air compressor 3.60, and said booster air compression system has booster air compressor 3.80, said auxiliary air compression system is belt driven or driven by said first electric motor 8.80, and said booster air compression system is belt driven or driven by said second electric motor 8.90, said auxiliary air compression system has a means of communication with an air filtration system 3.71, said booster air compression system compresses air from said auxiliary air compression system; said combustion chamber 4.00 includes a combustion chamber housing 4.10, said combustion chamber housing 4.10 contains an air conduit 5.15, said combustion chamber 4.00 generates an exhaust gas stream 4.70 when the air-fuel mixture is ignited, said engine housing system has means of communication with said air filtration system 3.71, said air filtration system 3.71 contains at least one air filtration element 3.72, at least one air filtration housing 3.73 and accessories for the air filtration system, said wind gas turbine engine rotor assembly contains at least one wind gas turbine engine rotor 6.10 and a wind gas turbine main shaft 6.50 engine, said wind gas turbine engine rotor 6.10 comprises a wind gas turbine engine rotor hub 6.20 having several wind gas turbine engine rotor blades 6.60, several hub grooves 6.40 for a compression ring for exhaust gas and several hub grooves 6.26 for an oil ring, said hub groove 6.40 for compression exhaust ring wherein said oil ring hub groove 6.26 is adapted for oil sealing means, said wind turbine engine main shaft 6.50 and engine fan shaft 2.14 have communication means, said wind turbine engine main shaft 6.50 has a first axis 1.10 rotation, during operation of the specified wind gas turbine engine 1.00, the specified rotor 6.10 of the wind gas turbine engine and the specified main shaft 6.50 of the wind gas turbine engine rotate on the specified first axis 1.10 of rotation of the specified main shaft 6.50 of the wind gas turbine engine; said electric generating system contains an alternating current generator 7.40 and contains an electric generator 7.50, said electric generator 7.50 has supports 7.55, said starting system contains a starter 7.60, said lubrication system contains at least one oil pump assembly 7.00, oil lines assemblies 6.70, hoses for 6.95 oil assemblies and lubrication system accessories, said lubrication system accessories comprise an 8.50 block containing oil and at least one oil cooler, said 6.70 oil line assemblies and 6.95 oil hoses assemblies are interchangeable, said lubrication system also contains an oil pump 7.10, a known bypass valve, a mesh 7.20 and an oil pipeline 7.30, said oil pipeline 7.30 having means of communication with the specified lubrication system; said first cooling fan 9.80 or said second cooling fan 9.90 is a system mounted on the main shaft 6.50 of a wind gas turbine engine, said power generating system and said starting system are made as one unit or separate units, said starter 7.60 includes a flywheel 7.90 and includes a flywheel housing 7.80 ; said air compression system is an air pump that supplies air to provide one or more of the following: engine cooling and air for combustion of the air-fuel mixture in said combustion chamber 4.00, said air-fuel mixture igniter means 4.50 attached to said combustion chamber housing 4.10, or attached to said exhaust gas conduit housing 4.25, or attached at another suitable location, said fuel delivery means 4.30 has means for communicating with the fuel system, said fuel delivery means 4.30 being a single injector or a multi-injector system; said engine housing system is adapted for a low bypass air flow engine configuration, said low bypass air flow engine configuration includes a zero bypass air flow engine configuration, said engine housing system comprises an engine fan housing assembly, a center section shell 2.20, first guide vanes 2.50, at least one wind gas turbine engine rotor housing 2.30, fourth guide vanes 2.40, multiple bearing assembly housings 9.70, a mixture flow pipeline 9.20, an exhaust gas manifold 9.25 and a mounting system with fasteners 9.30, said engine housing system consisting of the first part 1.31 and a second part 1.32 or consists of a first motor housing 1.17, a second motor housing 1.18 and a third motor housing 1.19, said motor fan housing assembly comprises a motor fan housing 2.11 and an engine fan protective shell 2.13, said motor fan protective shell 2.13 is attached to said engine fan housing 2.11, said bearing assembly housing 9.70 includes a housing oil bypass 5.40, said engine fan assembly includes an engine fan 2.12, said engine fan 2.12 has an engine fan hub 2.15 and engine fan blades 2.18, said rotor housing 2.30 wind gas turbine engine makes it possible to install said wind gas turbine engine rotor assembly, said wind gas turbine engine rotor housing 2.30 has walls 2.41, at least one exhaust gas pipeline hole 2.43 and housing clearances 2.42, said walls 2.41 contain a first wall 2.44, a second wall 2.45 and a third wall 2.46; said air compression system contains a known air bleed system, said air bleed system and said air compression system have means of communication with air passages 1.21 in said second wall 2.45, said exhaust gas pipeline opening 2.43 on said third wall 2.46 must be adjacent to said first wall 2.44 and adjacent to said second wall 2.45, at one point or more points of said wind gas turbine engine rotor housing 2.30, said first wall 2.44, said second wall 2.45 and said third wall 2.46 are adjacent to each other, said exhaust gas pipeline housing 4.25 is directly or indirectly attached to said wind turbine engine rotor housing 2.30, or attached to any of said first wall 2.44, or said second wall 2.45, or said third wall 2.46, or attached to any suitable combination of said first wall 2.44, said second wall 2.45, and said third wall 2.46 so that it is possible to move said exhaust gas flow 4.70 into a portion of said second space 1.42 of said wind gas turbine engine rotor housing 2.30, said means in the form of a drive shaft comprising said wind gas turbine engine main shaft 6.50 and said engine fan shaft, during operation of said wind gas turbine engine 1.00, together with the complementary work of the fuel system, air compression system and fuel mixture ignition system, said combustion chamber 4.00 creates a high pressure exhaust gas flow 4.70, said exhaust gas flow 4.70 passes through said exhaust gas pipeline 4.20 and is directed by said walls 2.41 of said housing 2.30 wind gas turbine engine rotor, pushes said wind gas turbine engine rotor blades 6.60 and rotates said wind gas turbine engine rotor main shaft 6.50, which generates energy; said exhaust gas flow 4.70 exits through said housing gap 2.42 in said second wall 2.45 of said wind turbine engine rotor housing 2.30, and said exhaust gas flow 4.70, which is directed by the fourth guide vanes 2.40, drives said wind turbine rotor 8.10, and said exhaust gas flow 4.70 gas moves into the pipeline 9.20 for the flow of the mixture and out into the specified manifold 9.25 for the exhaust gas; rotation of said wind turbine engine main shaft 6.50 rotates said engine fan 2.12, and said engine fan motor fan assembly together with the engine fan housing assembly generates a usable air flow 1.20, said first guide vanes 2.50 direct said usable air flow 1.20, and said usable air flow 1.20 passes through said housing gap 2.42 in said first wall 2.44 of said wind turbine engine rotor housing 2.30 to push said wind turbine engine rotor blades 6.60, and said wind turbine engine rotor 6.10 rotates on said first axis of rotation 1.10 of said shaft 6.50 of a wind gas turbine engine rotor, and this process adds torque to said wind gas turbine engine 1.00, and this process also cools said wind gas turbine engine rotor 6.10 and cools other parts of said wind gas turbine engine 1.00, said usable air flow 1.20 exits through said housing gap 2.42 in said the second wall 2.45 of said wind gas turbine engine rotor housing 2.30 and drives said wind turbine rotor 8.10, and said usable air flow 1.20 passes into said mixture flow line 9.20 and into said exhaust gas manifold 9.25.

With reference to FIG. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, fig. 16, fig. 17, fig. 18, fig. 19, fig. 20, fig. 21, fig. 22, fig. 23, fig. 24, fig. 25, fig. 26 and any of the applicable graphics from FIG. 27 according to FIG. 65 inclusive, which are used for cross-reference, shows a third disclosure of a wind turbine engine set forth in specifications No. 5 to Specification No. 15 as follows.

5. A wind gas turbine engine 1.00 having an air cooling system or having both an air cooling system and a liquid cooling system, said air cooling system comprising fins 5.50, air pipe assemblies 1.25 and air passages 1.21, said liquid cooling system comprising a heat sink 2.90, liquid cooling pump 2.92, liquid cooling passages 2.93, liquid cooling medium, liquid cooling spaces 2.94 and liquid cooling accessories, said liquid cooling accessories include coolant hose assemblies 2.91 and coolant pipe assemblies 2.95, said wind turbine engine 1.00 contains housing engine system, air pressure sensor 2.19, engine fan assembly having an engine fan 2.12, an air filtration system 3.71 or several air filtration systems 3.71, an air compression system or several air compression systems, at least one combustion chamber 4.00, at least one compressed air delivery means, at least one compressed air receiving means 3.50, a fuel system, an electrical system having an air-fuel mixture ignition system with at least one air-fuel mixture ignition means 4.50, at least one exhaust gas pipeline housing 4.25 having a pipeline 4.20 for exhaust gas, at least one wind-gas turbine engine rotor assembly, lubrication system, drive shaft means, wind-gas turbine engine accessories, several bearing assemblies 9.00, first space 1.41, second space 1.42, third space 1.43, several means exhaust gas seal, several oil seals, 6.00 clamp, 1.52 belt, 1.54 bracket, 4.83 belt tension system, mounting system having 9.30 fasteners, 1.25 air pipe assemblies, 1.27 air hoses, 1.90 gears , a wind turbine assembly having a wind turbine rotor 8.10, wind gas turbine engine components and a drive system or several drive systems for operating said wind gas turbine engine components; These wind gas turbine engine components comprise one or more of the following: an electrical generating system or multiple electrical generating systems, an air pressure sensor 2.19, a starting system, a liquid cooling pump 2.92, an air compression system that contains one or more external air compression systems, an air conditioning system having air conditioning compressor 7.70, transmission 8.00, first cooling fan 9.80 or second cooling fan 9.90, hydraulic pump 5.70, at least one idler pulley 4.81, at least one first pulley 4.82, oil pump 7.10, at least one first electric motor 8.80, at least one second electric motor 8.90, a wind turbine rotor 8.10, an electrically controlled fan and other accessories for a wind gas turbine engine; said fuel system comprises: a fuel tank 4.40, a fuel pump 4.45, fuel line assemblies 4.47, a fuel flow control means and at least one fuel delivery means 4.30, said oil seal means comprises a plurality of oil seals 6.82, said external air compression system is made in the form of an auxiliary air compression system and a booster air compression system, said auxiliary air compression system is belt driven or driven by said first electric motor 8.80, and said air compression booster system is belt driven or driven by operating by said second electric motor 8.90, said auxiliary air compression system having means of communication with an air filtration system 3.71, said booster air compression system compressing air from said auxiliary air compression system; said combustion chamber 4.00 includes a combustion chamber housing 4.10, said engine housing system has means for communication with an air filtration system 3.71, said air filtration system 3.71 contains at least one air filtration element 3.72, at least one air filtration housing 3.73, and accessories for the system air filtration; said wind gas turbine engine rotor assembly contains a wind gas turbine engine rotor 6.10 and a wind gas turbine engine main shaft 6.50, said wind gas turbine engine main shaft 6.50 has a first rotation axis 1.10, during operation of said wind gas turbine engine 1.00 said wind gas turbine engine rotor 6.10 and said main shaft 6.50 of a wind gas turbine engine rotates on said first axis 1.10 of rotation of said main shaft 6.50 of the wind gas turbine engine; said electric generating system contains an alternating current generator 7.40 and contains an electric generator 7.50, said electric generator 7.50 has supports 7.55, said starting system contains a starter 7.60, said lubrication system contains at least one oil pump assembly 7.00, oil lines assemblies 6.70, hoses for an oil assembly 6.95 and lubrication system accessories, said lubrication system accessories comprise a block 8.50 containing oil and at least one oil cooler, said lubrication system comprises an oil pump assembly 7.00 having an oil pump 7.10, a known bypass valve, a screen 7.20 and an oil line 7.30, said starter 7.60 includes a flywheel 7.90 and includes a flywheel housing 7.80; said air compression system is an air pump that supplies air to provide one or more of the following: engine cooling, sealing means for air and air for combustion of the air-fuel mixture in said combustion chamber 4.00, said air-fuel mixture ignition means 4.50 is attached to said housing 4.10 combustion chamber, or attached to said exhaust gas conduit housing 4.25, or attached at another suitable location; said air cooling system comprises air passages 1.21 and air spaces as a means for cooling parts of said wind gas turbine engine 1.00; said fuel delivery means 4.30 has a means of communication with the fuel system, said fuel delivery means 4.30 is a single-injector system or a multi-injector system; said compressed air delivery means comprises air pipe assemblies 1.25 and air hoses assemblies 1.27, said air pipe assemblies 1.25 and said air hoses assemblies 1.27 are interchangeable;

wherein the engine housing system is adapted to a low bypass air flow engine configuration, said low bypass air flow engine configuration includes a zero bypass air flow engine configuration, said engine housing system consists of either a first part 1.31 and a second part 1.32, or a first engine housing 1.17, second engine housing 1.18 and third engine housing 1.19, said engine housing system comprises an engine fan housing assembly, a central part shell 2.20, first guide vanes 2.50, at least one wind gas turbine engine rotor housing 2.30, several bearing means housings 9.70 assembled, fourth guide vanes 2.40, wind-gas turbine engine support means, pipeline 9.20 for mixture flow and manifold 9.25 for exhaust gas; During operation of the wind gas turbine engine, said engine fan housing assembly and engine fan assembly generate a usable air flow 1.20 for air cooling of hot parts of said wind gas turbine engine 1.00 and for additional torque for said wind gas turbine engine 1.00, said first guide vanes 2.50 direct said usable air flow 1.20; said wind gas turbine engine rotor housing 2.30 contains a second space 1.42, said second space 1.42 is located in said wind gas turbine engine rotor housing 2.30 of said engine body system, said first guide vanes 2.50, said first space 1.41, said wind gas turbine engine rotor housing 2.30, said fourth guide vanes 2.40 and said third space 1.43 provide said usable air flow 1.20 from said engine fan housing assembly and engine fan assembly into said mixture flow conduit 9.20 and ultimately into said exhaust gas manifold 9.25; said first space 1.41 has a space between said wind gas turbine engine rotor housing 2.30 and said first guide vanes 2.50, said engine housing system has means of communication with said air filtration system 3.71, said air filtration system 3.71 contains at least one air filtration element 3.72, according to at least one air filtration element housing 3.73 and air filtration accessories, said air filtration housing allows proper installation of a second cooling fan 9.90, said engine fan housing assembly comprises an engine fan housing 2.11 and an engine fan containment 2.13, said fan containment 2.13 the engine is attached to the specified engine fan housing 2.11;

wherein the engine fan assembly has an engine fan 2.12, said engine fan 2.12 includes an engine fan hub 2.15 and an engine fan shaft 2.14, said engine fan hub 2.15 contains a plurality of engine fan blades 2.18, said multiple engine fan blades 2.18 are attached to said fan hub 2.15 engine, the specified engine fan hub 2.15 is attached to the specified engine fan shaft 2.14, during operation and during downtime of the specified wind gas turbine engine 1.00, the first guide vanes 2.50, the bearing means housing 9.70 assembly and the bearing means assembly 9.00 maintain the rotational stability of the engine fan shaft 2.14 , while the first guide vanes 2.50, the fourth guide vanes 2.40, the bearing means housing 9.70 and the bearing means assembly 9.00 support the rotational stability of the main shaft 6.50 of the wind turbine engine, said first guide vanes 2.50 and said fourth guide vanes 2.40 are adapted to include oil line 7.30 for said bearing means assembly 9.00, said oil line 7.30, which includes a return oil line and an injection oil line, being oil spaces along said first guide vanes 2.50, oil spaces along said fourth guide vanes 2.40 and oil spaces along other parts of said wind turbine engine 1.00, said oil line 7.30 is supplemented by oil line assemblies 6.70 and oil hose assemblies 6.95 which carry oil to and from said bearing assembly 9.00, said oil lines in The 6.70 oil hose assembly and the 6.95 oil hose assembly are interchangeable, the 7.30 oil line assembly, the 6.70 oil line assembly and the 6.95 oil hose assembly are in communication with the lubrication system;

wherein the combustion chamber 4.00 is designed to generate an exhaust gas flow 4.70 during operation of the wind gas turbine engine 1.00, said exhaust gas flow 4.70 is known as a result of the movement of gases when the air-fuel mixture is burned, said combustion chamber 4.00 includes a combustion chamber housing 4.10, a combustion chamber 4.11, The swirl blades 4.12, the combustion chamber liner 4.13 and the combustion chamber seal 4.17, the said combustion chamber liner 4.13 and the said combustion chamber seal 4.17 are a known aviation-related system adapted for the wind gas turbine engine 1.00, said exhaust gas flow 4.70 passes through the exhaust gas line 4.20, said housing The combustion chamber 4.10 includes an air conduit 5.15, said combustion chamber housing 4.10 is cooled by one or more of the following: liquid cooling, compressed air cooling, cooling with a usable air stream 1.20, or cooling with another air stream; said combustion chamber 4.00 has means of communication with fuel delivery means 4.30, one or more air-fuel mixture ignition means 4.50 and an air compression system;

wherein the air compression system is an external compression system, said external air compression system has an auxiliary air compression system, which contains a booster air compression system, said external air compression system has a known air bleed system, in a means of delivering compressed air to the combustion chamber 4.00 from the external air compression system uses one or more of an air pipe assembly 1.25 and an air hose assembly 1.27 or with other suitable means;

wherein the rotor of the wind gas turbine engine assembly contains a rotor 6.10 of the wind gas turbine engine and the main shaft 6.50 of the wind gas turbine engine, said rotor 6.10 of the wind gas turbine engine has a hub 6.20 of the rotor of the wind gas turbine engine, said hub 6.20 of the rotor of the wind gas turbine engine contains several blades 6.60 rotors ora of a wind gas turbine engine, several grooves 6.40 hubs under an exhaust gas compression ring and several hub oil ring grooves 6.26, said hub exhaust gas compression ring groove 6.40 has an inner periphery 6.45 of a hub exhaust gas compression ring groove, said hub oil ring groove 6.26 has an inner periphery 6.29 of a hub groove under the oil ring, said hub exhaust gas compression ring groove 6.40 is adapted to the exhaust gas sealing means, while said hub oil ring groove 6.26 is adapted to the oil sealing means; said multiple wind turbine engine rotor blades 6.60 are attached to said wind gas turbine engine rotor hub 6.20, said wind gas turbine engine rotor hub 6.20 is attached to the wind gas turbine engine main shaft 6.50, said wind gas turbine engine rotor blades 6.60 extend outward from said hub 6.20 wind turbine engine rotor, indicated 6.60 rotor blades wind gas turbine engine are protrusions from said wind gas turbine engine rotor hub 6.20, said wind gas turbine engine rotor blades 6.60 have any other suitable known shape, said wind gas turbine engine rotor blades 6.60 are made of a different material compared to the wind gas turbine engine rotor hub 6.20, or said blades 6.60 rotor wind gas turbine engine are made of the same material as said wind gas turbine engine rotor hub 6.20, said multiple wind gas turbine engine rotor blades 6.60 are spaced at substantially equal distances along said wind gas turbine engine rotor hub 6.20; at least one wind gas turbine engine rotor blade 6.60 of said plurality of wind gas turbine engine rotor blades 6.60 comprises a second edge 6.65, a second root portion 6.64, a second leading edge 6.66 and a second trailing edge 6.67, wherein during operation of said wind gas turbine engine 1.00 said rotor blades 6.60 wind gas turbine engine, the specified rotor 6.10 of the wind gas turbine engine and the specified main shaft 6.50 of the wind gas turbine engine are driven into rotation on the specified first axis 1.10 of rotation of the specified main shaft 6.50 of the wind gas turbine engine by the flow 4.70 of exhaust gas from the combustion chamber 4.00, and additionally the specified blades 6.60 of the wind gas turbine engine nitrogen turbine engine, specified rotor 6.10 of the wind gas turbine engine and said main shaft 6.50 of the wind gas turbine engine are driven to rotate on said first axis 1.10 of rotation of said main shaft 6.50 of the wind gas turbine engine by a usable air flow 1.20 from the engine fan housing assembly and the engine fan assembly;

wherein the rotor housing 2.30 of the wind gas turbine engine provides the ability to install the required parts of the wind gas turbine engine 1.00 into the specified housing 2.30 of the rotor of the wind gas turbine engine, the specified required parts contain the rotor of the wind gas turbine engine assembly, the specified housing 2.30 of the rotor of the wind gas turbine engine provides the possibility of rotating the main shaft 6.50 of the wind gas turbine engine and the rotor 6.10 wind gas turbine engine, said wind gas turbine engine rotor housing 2.30 has walls 2.41, at least two housing clearances 2.42, at least one exhaust gas pipeline opening 2.43 and a wind gas turbine engine rotor assembly space, said wind gas turbine engine rotor assembly space contains a second space 1.42 , said second space 1.42 specifically allows said wind gas turbine engine rotor 6.10 to rotate, the exhaust gas conduit housing 4.25 is attached to said wind gas turbine engine rotor housing 2.30 so as to allow said exhaust gas flow 4.70 to move into a portion of said second space 1.42 in said housing 2.30 rotor of a wind gas turbine engine, said walls 2.41 contain a first wall 2.44, a second wall 2.45 and a third wall 2.46; said exhaust gas conduit housing 4.25 is directly or indirectly attached to said wind turbine engine rotor housing 2.30, or attached to any of said first wall 2.44, said second wall 2.45, said third wall 2.46, or attached to any suitable combination of said first wall 2.44, said second wall 2.45 and said third wall 2.46 so as to allow said exhaust gas flow 4.70 to move into a portion of said second space 1.42 of said wind gas turbine engine rotor housing 2.30, said housing gap 2.42 in the second wall 2.45, which is wider than the housing gap 2.42 in the first wall 2.44 is designed such that said exhaust gas flow 4.70 passes through said housing gap 2.42 in the second wall 2.45, said exhaust gas conduit opening 2.43 on said third wall 2.46 must be adjacent to said first wall 2.44 and adjacent to said second wall 2.45, at one point or more points of the specified housing 2.30 of the rotor of the wind gas turbine engine, the specified first wall 2.44, the specified second wall 2.45 and the specified third wall 2.46 are adjacent to each other, the specified housing 2.30 of the rotor of the wind gas turbine engine is made with air passages 1.21, some of the specified air passages 1.21 in said second wall 2.45 have a means of communication with the air bleed system, a number of said air passages 1.21 are used to cool said second wall 2.45 of said wind gas turbine engine rotor housing 2.30 or are used to cool another wind gas turbine engine rotor housing, said wind gas turbine engine rotor housing 2.30 has a significant distance from the specified rotor 6.10 of the wind gas turbine engine; according to the design and during operation of said wind gas turbine engine 1.00, the combustion chamber 4.00 generates an exhaust gas stream 4.70, said exhaust gas stream 4.70 passes through the exhaust gas pipeline 4.20, said wind gas turbine engine rotor housing 2.30 allows said exhaust gas stream 4.70 to push the wind gas turbine rotor blades 6.60 binary engine and rotates said wind gas turbine engine rotor 6.10, and also rotates the wind gas turbine engine main shaft 6.50, which is an operation that produces torque to perform work on said wind gas turbine engine 1.00, said wind gas turbine engine rotor housing 2.30 further provides a usable air flow 1.20 from the engine fan housing assembly through the specified gaps 2.42 of the housing in the specified first wall 2.44 and in the specified second wall 2.45 of the specified housing 2.30 of the rotor of the wind gas turbine engine for cooling the specified blades 6.60 of the rotor of the wind gas turbine engine of the specified rotor 6.10 of the wind gas turbine engine and the cooling process of the specified blades 6.60 of the wind turbine engine zoturbine engine , said usable air stream 1.20, which moves like wind, further pushes said wind turbine engine rotor 6.10 to rotate and therefore adds more torque to said wind gas turbine engine 1.00, said usable air stream 1.20 exits said wind turbine engine rotor housing 2.30. of the engine through said second wall 2.45, and said usable air stream 1.20 drives the wind turbine rotor 8.10, and said usable air stream 1.20 enters said mixture flow line 9.20 and exits outward into an exhaust gas manifold 9.25; said wind gas turbine engine rotor housing 2.30 also ensures the movement of said exhaust gas flow 4.70 from said wind gas turbine engine rotor housing 2.30, said walls 2.41 of said wind gas turbine engine rotor housing 2.30 direct said exhaust gas flow 4.70 to said wind gas turbine engine rotor blades 6.60, and said ny flow 4.70 exhaust gas pushes the specified blades 6.60 of the wind gas turbine engine rotor, and rotates the specified wind gas turbine engine rotor 6.10, and additionally rotates the specified main shaft 6.50 of the wind gas turbine engine on the first axis 1.10 of rotation of the specified main shaft 6.50 of the wind gas turbine engine rotor; said walls 2.41 and said rotor blades 6.60 of a wind gas turbine engine prevent the majority of said exhaust gas flow 4.70 from escaping into the mixture flow conduit 9.20 until said exhaust gas flow 4.70 reaches said housing clearance 2.42 in said second wall 2.45 of said rotor housing 2.30 wind gas turbine engine, and said exhaust gas flow 4.70 exits said wind gas turbine engine rotor housing 2.30 through said housing gap 2.42 in said second wall 2.45, and said exhaust gas flow 4.70 drives said wind turbine rotor 8.10, and said exhaust gas flow 4.70 ends up in the specified pipeline 9.20 for the flow of the mixture and goes out into the manifold 9.25 for the exhaust gas; oil line 7.30 represents oil spaces along the first guide vanes 2.50 and fourth guide vanes 2.40 or another oil line 7.30 in said wind gas turbine engine rotor housing 2.30, said oil line 7.30 is supplemented by oil lines assemblies 6.70 and oil hoses assemblies 6.95 or other suitable means which carries oil into and out of said bearing means assembly 9.00;

wherein the exhaust gas flow 4.70 from the combustion chamber 4.00 moves into the space of the wind gas turbine engine rotor housing 2.30, said exhaust gas flow 4.70 also moves between at least two wind gas turbine engine rotor blades 6.60 of the wind gas turbine engine rotor 6.10, moving said exhaust gas flow 4.70 in said housing 2.30 of the wind gas turbine engine rotor of the specified engine frame system rotates the specified wind gas turbine engine rotor 6.10 and rotates the main shaft 6.50 of the wind gas turbine engine;

wherein the usable air flow 1.20 when moving pushes the wind gas turbine engine rotor blades 6.60 and rotates the wind gas turbine engine rotor 6.10 on the first axis 1.10 of rotation of the wind gas turbine engine main shaft 6.50, which adds torque to the wind gas turbine engine 1.00, said usable air flow 1.20 also supports an acceptable operating temperature of said wind gas turbine engine rotor 6.10 and further helps maintain an acceptable operating temperature of said wind gas turbine engine 1.00;

wherein the lubrication system has a means of communication with the bearing means assembled 9.00, the specified lubrication system supplies oil for cooling and lubrication of several bearing means assembled 9.00, the specified lubrication system has a means of communication with the specified bearing means assembled 9.00 of an external air compression system, the specified lubrication the system contains at least one oil pump assembly 7.00 and accessories for the lubrication system, said accessories for the lubrication system contain a block 8.50 containing oil, oil lines assemblies 6.70 and contain an oil cooler, the first guide vanes 2.50 are used as an oil cooler, said oil pump in assembly 7.00 contains oil pump 7.10;

wherein the bearing means assembly 9.00 is supported by a housing 9.70 of the bearing means assembly, said bearing means assembly contains bearings 9.10 and accessories for the bearing means assembly, said bearings 9.10 are in the form of ball bearings 9.15, tapered roller bearings 9.16, cylindrical roller bearings 9.17, bearings 9.60 sliding and other suitable form of bearings 9.10, said bearing means assembly 9.00 prevents too much axial movement and prevents too much radial movement of the shaft in relation to the housing 9.70 of the bearing means assembly; the specified accessories for the bearing assembly include gaskets 9.11, bushing 1.80, keys 5.60, O-ring 5.65, bearing holders 5.55 and oil seals 6.82; said bearing holder 5.55 and said bearing housing 9.70 assembly support the proper position of bearing 9.10, said bearing holder 5.55 is known to prevent said bearings from moving out of place, said bearing holder 5.55 is in the form of eyelet and threaded fasteners, said bearing holder 5.55 works in conjunction with the lock 5.56, the specified spacers 9.11 are designed to transfer the axial load from the shaft to the specified bearing 9.10, or the specified spacers transfer the axial load from the specified bearing 9.10 to another bearing 9.10, the specified spacer is intended to transfer the axial load from the specified bushing 1.80 to the specified bearings 9.10, while said bearing holder 5.55 is designed to transfer axial load from said bearings 9.10 to said bearing assembly housing 9.70, said sleeve 1.80 allows for easy removal or separation of the wind turbine engine main shaft 6.50 from said bearing assembly 9.00 by sliding outwards, said bushing 1.80 also allows for less damage to be caused by said bearing assembly 9.00 when inserting said main shaft 6.50 of a wind gas turbine engine during the assembly process by sliding inwards, said bushing 1.80 has a key or gear and is held on bearings 9.10 in the wind gas turbine engine rotor housing 2.30, said bushing 1.80 has an inner diameter that preferably matches the shape of a gear that fits a specially designed wind turbine engine main shaft 6.50 with a matching gear shape such that said hub 1.80 and the wind turbine engine main shaft 6.50 are assembled together and rotate together during operation of said wind turbine engine 1.00, said bushing 1.80 allows for less complex insertion of said wind gas turbine engine main shaft 6.50 into said bearing assembly 9.00 in said wind gas turbine engine rotor housing 2.30, or said bushing 1.80 allows for less complex removal of said wind gas turbine engine main shaft 6.50 from said bearing assembly 9.00 in said wind gas turbine engine rotor housing 2.30, said bushing 1.80 prevents axial movement of said wind gas turbine engine main shaft 6.50 or another wind gas turbine engine shaft 1.00, and said bearings 9.10 and mountings prevent axial movement of said bushing 1.80, similar to Bushing 1.80 is adapted for the bearing assembly 9.00 air compression system, said bearing means assembly 9.00 has means of communication with the lubrication system, said bearing means assembly 9.00 during operation of said wind gas turbine engine 1.00 or during idle periods maintains rotation of one or more of the following: engine fan shaft 2.14 main shaft 6.50 wind gas turbine engine, auxiliary air compressor shaft 3.68 and booster air compressor shaft 3.90, said bushing 1.80 shall be secured to said wind gas turbine engine main shaft 6.50 such that said bushing 1.80 rotates with said wind gas turbine engine main shaft 6.50 and proper the position of the specified bushing 1.80 was maintained in relation to the specified bearings 9.10 and in relation to the specified main shaft 6.50 of the wind gas turbine engine, or the specified bushing 1.80 must be fixed on another shaft related to the specified wind gas turbine engine 1.00, or fixed on the shaft 3.68 of the auxiliary compressor, or fixed on the shaft 3.90 of the booster compressor so, such that said bushing 1.80 rotates with said other shaft, or rotates with said auxiliary compressor shaft 3.68, or rotates with said booster compressor shaft 3.90, and the proper position of said bushing 1.80 is maintained with respect to said bearings 9.10 and with respect to said other shaft, or with respect to said auxiliary compressor shaft 3.68, or said booster compressor shaft 3.90;

wherein the bearing means assembly housing 9.70 supports one bearing 9.10 or supports multiple bearings 9.10, said bearing means housing 9.70 assembly includes a housing oil bypass passage 5.40, said housing oil bypass channel 5.40 is a groove along said bearing means housing 9.70 in assembly, said housing oil bypass 5.40 ensures proper circulation of oil within the bearing assembly housing 9.70, said bearing assembly housing 9.70 and said bearings 9.10 include a corresponding groove for a key 5.60, said key 5.60 prevents said bearings 9.10 from damaging said housing 9.70 bearing assembly;

wherein the means in the form of a drive shaft is a system in which the engine fan shaft 2.14 and the main shaft 6.50 of the wind gas turbine engine are a single continuous shaft, or the specified engine fan shaft 2.14 and the specified main shaft 6.50 of the wind gas turbine engine are separate shafts, but the specified shaft 2.14 of the engine fan and the specified main shaft 6.50 of the wind gas turbine engine are in communication with each other;

wherein the liquid cooling system has a configuration known to the engine, said accessories for the liquid cooling system include an electrically controlled fan or a wind turbine engine shaft mounted fan, liquid cooling passages 2.93, coolant hoses assemblies 2.91, coolant pipe assemblies 2.95 and liquid spaces 2.94 cooling, said liquid cooling passages 2.93 and liquid cooling spaces 2.94 are located in the following places: walls 2.41 of the wind gas turbine engine rotor housing 2.30, combustion chamber housing 4.10 and exhaust gas pipeline housing 4.25; said liquid cooling passages 2.93, said coolant hose assemblies 2.91, said coolant pipe assemblies 2.95 and said liquid cooling spaces 2.94 are in communication with said liquid cooling pump 2.92, said coolant hose assemblies 2.91 and said coolant pipe assemblies 2.95 are interchangeable, said liquid cooling passages 2.93 and said liquid cooling spaces 2.94 are used for cooling other parts of the wind turbine engine 1.00 using a liquid cooling system, said liquid cooling passages 2.93 and said liquid cooling spaces 2.94 are configured so that liquid cooling medium can flow into and leak out, said liquid coolant is plain water or water mixed with other substances that contain chemicals such as antifreeze.

6. A wind and gas turbine engine 1.00 according to the third disclosure, wherein the engine housing system comprises at least one wind turbine rotor assembly, said engine housing system is adapted to said wind turbine rotor assembly, said wind turbine rotor assembly comprises at least one wind turbine rotor 8.10, said wind turbine rotor 8.10 has a wind turbine rotor hub 8.20, said wind turbine rotor hub 8.20 contains multiple wind turbine rotor blades 8.30, each of the wind turbine rotor blades 8.30 has a sixth root portion 8.36, a sixth edge 8.37, a sixth section 8.31, a sixth leading edge 8.32, sixth trailing edge 8.33 and a substantially straight sixth line 8.34, said wind turbine rotor blades 8.30 are attached to said wind turbine rotor hub 8.20, said wind turbine rotor hub 8.20 is attached to a wind turbine engine main shaft 6.50, during operation of said wind turbine engine 1.00 usable 1.20 air flow from the housing the engine fan assembly and the engine fan assembly pushes said wind turbine rotor blades 8.30, further said wind turbine rotor blades 8.30 displaces an exhaust gas flow 4.70 that has passed through the wind turbine engine rotor housing 2.30, said exhaust gas flow 4.70 that initially emanates from the combustion chamber 4.00 , проходит через трубопровод 4.20 для выхлопного газа корпуса 4.25 трубопровода для выхлопного газа, и указанный поток 4.70 выхлопного газа перемещается в указанный корпус 2.30 ротора ветрогазотурбинного двигателя и в окрестности указанного ротора 8.10 ветротурбины, чтобы толкать указанные лопасти 8.30 ротора ветротурбины для вращения указанного ротора 8.10 ветротурбины on the first axis 1.10 of rotation of said main shaft 6.50 of the wind gas turbine engine, and the process generates additional torque for said wind turbine engine 1.00, the fourth guide vanes 2.40 direct said usable air flow 1.20 and said exhaust gas flow 4.70 into said wind turbine rotor 8.10, said blades 8.30 of the wind turbine rotor when cut along a radial arc 1.70 creates the specified sixth section 8.31, the specified radial arc 1.70 has a center that essentially lies on the specified first axis 1.10 of rotation of the specified main shaft 6.50 of the wind gas turbine engine or lies about the specified first axis 1.10 of rotation of the specified main shaft 6.50 of a wind turbine engine, said sixth section 8.31 lies between twenty and eighty percent of the wind turbine rotor blade length 600, said wind turbine rotor blade length 600 is the distance between the sixth root portion 8.36 and the sixth edge 8.37, said distance is measured along the sixteenth line, said sixteenth line is approximately perpendicular said first rotation axis 1.10, said sixteenth line intersects said sixth root portion 8.36 and intersects said sixth edge 8.37, when a substantially straight sixth line 8.34 connects the sixth leading edge 8.32 and the sixth trailing edge 8.33 of said sixth section 8.31, said sixth line 8.34 forms a sixth angle 8.35 with sixth plane 1.16, said sixth plane 1.16 substantially lies along said first axis 1.10 of rotation of said wind turbine engine main shaft 6.50 and intersects said sixth line 8.34, said sixth angle 8.35 measured perpendicularly from said sixth plane 1.16 is in the range of approximately from zero degrees to forty degrees from the specified sixth plane 1.16.

7. A wind turbine engine 1.00 according to the third disclosure, wherein each of the wind turbine engine rotor blades 6.60 comprises a second root portion 6.64, a second edge 6.65, a second leading edge 6.66, a second trailing edge 6.67, a second blade length 200, a substantially straight second line 6.63, and second section 6.61, said second section 6.61 is created by cutting said wind gas turbine engine rotor blade 6.60 along a radial arc 1.70, said radial arc 1.70 cuts said wind gas turbine engine rotor blade 6.60 between twenty and eighty percent of the length 200 of the wind gas turbine engine rotor blade, indicated second blade length 200 is the distance between the second root portion 6.64 and the second edge 6.65, said distance measured along a twelfth line, said twelfth line is approximately perpendicular to the first axis of rotation 1.10, said twelfth line intersects said second root portion 6.64 and intersects said second edge 6.65, in a fully assembled wind turbine engine 1.00, said radial arc 1.70 has a center that substantially lies on said first rotation axis 1.10 of the wind turbine engine main shaft 6.50 or lies about said first rotation axis 1.10 of the wind turbine engine main shaft 6.50 when said substantially straight second line 6.63 connects the second leading edge 6.66 and said second trailing edge 6.67 of said second section 6.61, said substantially straight second line 6.63 forms a second angle 6.69 with a second plane 1.12, said second plane 1.12 substantially lies along said first axis 1.10 of rotation of said wind gas turbine engine main shaft 6.50 and intersects said second line 6.63, said second angle 6.69, measured perpendicularly from said second plane 1.12, is in the range of approximately zero degrees to forty degrees from said second plane 1.12.

8. A wind gas turbine engine 1.00 according to the third disclosure, wherein the wind gas turbine engine assembly includes a plurality of exhaust gas seal means, the exhaust gas seal means operates in conjunction with the wind gas turbine engine rotor housing 2.30, the plurality of exhaust gas seal means comprises several grooves 6.40 of the hub for the compression ring for exhaust gas and several compression rings for the exhaust gas assembly, the specified groove 6.40 of the hub for the compression ring for the exhaust gas and the specified several compression rings for the exhaust gas assembly are located in the hub 6.20 of the rotor of the wind gas turbine engine, each of the specified hub grooves 6.40 for an exhaust gas compression ring are adapted for an exhaust gas compression ring assembly, said exhaust gas compression ring assembly comprises an exhaust gas compression ring 6.30 and at least one exhaust gas compression ring spring 6.34, said compression ring The exhaust gas compression ring 6.30 has at least one exhaust gas compression ring protrusion 6.35, an exhaust gas compression ring outer periphery 6.38, an exhaust gas compression ring inner periphery 6.32, an exhaust gas compression ring thermal expansion gap 6.36, a sliding joint 3.30, radial an exhaust gas compression ring center 6.48 and an exhaust gas compression ring oil radial passage 6.33, said exhaust gas compression ring oil radial passage 6.33 has a radial exhaust gas compression ring oil passage center 6.31, said compression ring thermal expansion gap 6.36 for the exhaust gas has an oil seal element, said exhaust gas sealing means prevents oil contamination due to exhaust gas pressure in the bearing assembly 9.00 of said wind turbine engine 1.00, said exhaust gas compression ring thermal expansion gap 6.36 is preferably located adjacent to said by the exhaust gas compression ring lip 6.35 or at a distance from the exhaust gas compression ring lip 6.35 for simplicity, the specified exhaust gas compression ring thermal expansion gap 6.36 is intended to retain any residual oil to lubricate the significant stroke of the said exhaust gas compression ring 6.30 at the specified wind gas turbine engine rotor housing 2.30, said exhaust gas compression ring thermal expansion gap 6.36 is in communication with said wind gas turbine engine rotor housing 2.30, said exhaust gas compression ring projection 6.35 extends from the outer periphery 6.38 of the exhaust gas compression ring, said compression ring projection 6.35 the exhaust gas ring has a designated space in said hub groove 6.40 for the exhaust gas compression ring such that the exhaust gas compression ring 6.30 rotates with said wind gas turbine engine rotor hub 6.20 of wind gas turbine engine rotor 6.10 during operation of said wind gas turbine engine 1.00, lowest point said inner periphery of the exhaust gas compression ring and an adjacent section of said inner periphery 6.32 of the exhaust gas compression ring shall be adjacent to the oil line 7.30 in said wind turbine engine rotor housing 2.30 when said wind turbine engine 1.00 is seated in a horizontal position so that oil flows outward , said exhaust gas compression ring inner periphery 6.32 is further required to be substantially in contact with the exhaust gas compression ring hub inner periphery 6.45 of said exhaust gas compression ring hub groove 6.40, said exhaust gas compression ring spring 6.34 includes a protrusion 6.37 exhaust gas compression ring spring that fits into the exhaust gas compression ring hub groove 6.40 designed for said exhaust gas compression ring spring protrusion 6.37, said exhaust gas compression ring spring protrusion 6.37 allows rotation of the exhaust gas compression ring spring 6.34 exhaust gas with said wind gas turbine engine rotor 6.10, said exhaust gas compression ring spring 6.34 is designed to press exhaust gas compression ring 6.30 against said wind gas turbine engine rotor housing 2.30, said exhaust gas compression ring 6.30 includes a radial oil passage 6.33 of an exhaust gas compression ring for more efficient lubrication of the stroke of said exhaust gas compression ring 6.30, said radial exhaust gas compression ring oil passage 6.33 has a center of a radial exhaust gas compression ring oil passage 6.31, said radial compression ring oil passage 6.33 is equidistant from said exhaust gas compression ring radial center 6.48 of said exhaust gas compression ring 6.30, in a fully assembled wind turbine engine 1.00, said exhaust gas compression ring oil radial center 6.31 6.31 and said exhaust gas compression ring radial center 6.48 substantially lie about the first rotation axis 1.10 of the main shaft 6.50 of the wind gas turbine engine, said radial exhaust gas compression ring oil passage 6.33 is in communication with said wind gas turbine engine rotor housing 2.30, and said radial exhaust gas compression ring oil passage 6.33 is in communication with said exhaust gas compression ring expansion gap 6.36, said exhaust gas compression ring spring 6.34 comprises exhaust gas compression ring spring pusher legs 6.39 and coil springs 6.81.

9. A wind gas turbine engine 1.00 according to the third disclosure, wherein the wind gas turbine engine rotor assembly includes a plurality of oil seal means, said oil seal means operates in conjunction with a wind gas turbine engine rotor housing 2.30, said oil seal means has a plurality of oil rings 6.80 and a plurality of grooves. 6.26 of the hub for the oil ring, located in the hub 6.20 of the rotor of the wind gas turbine engine, each of the specified grooves 6.26 of the hub for the oil ring of the hub is adapted for an oil ring assembly, the specified oil ring assembly has at least one oil ring 6.80 and at least one spring 6.83 of an oil ring, said oil ring 6.80 has at least one oil ring projection 6.84, an outer oil ring periphery 6.85, an oil ring thermal expansion gap 6.86, a sliding joint 3.30, an oil ring radial center 6.77, and an oil ring inner periphery 6.87, said oil ring projection 6.84. The oil ring is placed in a predetermined space for the oil ring protrusion 6.84 in said hub groove 6.26 under the oil ring of said wind gas turbine engine rotor hub 6.20 so that said oil ring 6.80 rotates with said wind gas turbine engine rotor hub 6.20 and wind gas turbine engine rotor 6.10 during operation of said wind gas turbine. turbine engine 1.00, said oil ring shoulder 6.84 is located on the outer periphery 6.85 of the oil ring, said oil ring thermal expansion gap 6.86 is located adjacent to said oil ring shoulder 6.84 or at a distance from the oil ring shoulder 6.84 for simplicity, said oil ring thermal expansion gap 6.86 is located at communication with the wind gas turbine engine rotor housing 2.30, said inner periphery 6.87 of the oil ring must additionally be substantially in contact with the inner periphery 6.29 of the hub oil ring groove of said hub oil ring groove 6.26, said inner periphery 6.87 of the oil ring is in communication with the lubrication system , said oil ring spring 6.83 includes an oil ring spring protrusion 6.88 that fits into a hub oil ring groove 6.26 for said oil ring spring protrusion 6.88, said oil ring spring 6.83 includes an oil ring spring pusher leg 6.89 and a coil spring 6.81, said oil ring spring 6.83. oil ring is designed to press said oil ring 6.80 against said wind turbine engine rotor housing 2.30, said oil ring 6.80 includes a small oil through groove 3.40 to provide a small amount of oil for lubrication and cooling to exhaust gas compression ring 6.30, said a small groove 3.40 is located adjacent to an oil ring thermal expansion gap 6.86, said oil ring 6.80 includes an oil ring oil radial passage 6.27 to more effectively lubricate the stroke of said oil ring 6.80, said oil ring radial oil passage 6.27 has a radial oil passage center 6.75 of the oil ring, said oil ring oil radial passage 6.27 is equidistant from said oil ring radial center 6.77 of said oil ring 6.80, in the fully assembled wind gas turbine engine 1.00, said oil ring radial oil passage center 6.75 and the oil ring radial center 6.77 lie about the first axis 1.10 rotation of the main shaft 6.50 of the wind gas turbine engine, the specified radial channel 6.27 for the oil ring oil is in communication with the specified housing 2.30 of the rotor of the wind gas turbine engine, and the specified radial channel 6.27 for the oil ring oil is in communication with the specified thermal expansion gap 6.86 of the oil ring, the specified spring 6.83 The oil ring contains legs 6.89 of the oil spring pusher, protrusion 6.88 of the oil ring spring and coil springs 6.81.

10. A wind gas turbine engine 1.00 according to the third disclosure, wherein the rotor housing 2.30 of the wind gas turbine engine has at least two main parts, which contain a first part 1.31 and a second part 1.32, said first part 1.31 and said second part 1.32 are separable from each other and capable of being attached to each other to enable installation of the wind gas turbine engine rotor assembly into said wind gas turbine engine rotor housing 2.30, between the first part 1.31 and the second part 1.32 there is a spacer ring or other suitable parts sealing material, said two main parts with a liquid cooling system have known through-holes that pass through the spacer ring for liquid cooling passage 2.93.

11. The wind gas turbine engine 1.00 according to the third disclosure, wherein the auxiliary air compression system has an auxiliary air compressor 3.60, said auxiliary air compressor 3.60 includes an auxiliary air compressor housing, an auxiliary air compressor fan 3.63, an auxiliary air compressor fan containment shell 3.64, first stationary blades in auxiliary air compressor assembly 3.65, second stationary auxiliary air compressor blade assemblies 3.66, auxiliary air compressor shaft mounted blade assemblies 3.67, auxiliary air compressor shaft 3.68 and multiple bearing means assemblies 9.00, said auxiliary air compressor 3.60 having means of communication with the system 3.71 air filtration, said air filtration system 3.71 comprises at least one filtration element housing 3.73 having a filtration element 3.72, said auxiliary air compressor housing comprises a first auxiliary air compressor housing 3.61, a second auxiliary air compressor housing 3.69, auxiliary air compressor guide vanes 3.62 , a plurality of oil lines 7.30, an air convergence area 1.29, and an air line 5.15, said first auxiliary air compressor stationary blade assemblies 3.65 and second auxiliary air compressor stationary blade assemblies 3.66 are partially inserted between said auxiliary air compressor shaft-mounted blade assemblies. 3.67, and said second stationary auxiliary air compressor vane assemblies 3.66 prevent movement of said first stationary auxiliary air compressor vane assemblies 3.65, said first stationary auxiliary air compressor vane assemblies 3.65 are attached or keyed to said first auxiliary air compressor housing 3.61, said a second auxiliary air compressor housing 3.69 is attached to said first auxiliary air compressor housing 3.61, said auxiliary air compression system has a booster air compression system, said booster air compression system compresses air from said auxiliary air compressor 3.60, said booster air compression system includes a booster air compressor 3.80, said booster air compressor 3.80 comprises a booster air compressor housing, a first booster air compressor stationary vane assembly 3.85, a second booster air compressor stationary vane assembly 3.86, a booster air compressor shaft mounted vane assembly 3.87, a booster air compressor shaft 3.90, and a plurality of bearing means assemblies 9.00, said booster air compressor housing comprising a first booster air compressor housing 3.88, a second booster air compressor housing 3.89, an oil conduit 7.30, an air convergence area 1.29, a dust cover 3.81, and a plurality of air conduits 5.15; said air convergence zone 1.29, said air conduit 5.15, air pipe assembly 1.25 and compressed air receiving means 3.50 have means of communication with combustion chamber 4.00, said second booster air compressor housing 3.89 is attached to said first booster air compressor housing 3.88, said first fixed booster air compressor vane assemblies 3.85 and second fixed booster air compressor vane assemblies 3.86 are partially inserted between said booster air compressor shaft mounted vane assemblies 3.87, and said second fixed booster air compressor vane assemblies 3.86 prevent movement of said first fixed vanes. booster air compressor blade assemblies 3.85, when said first stationary booster air compressor blade assemblies 3.85 are attached or keyed to said first booster air compressor housing 3.88, said auxiliary air compression system is belt actuated or actuated by the first electric motor 8.80, and said booster air compression system is driven by a belt or driven by a second electric motor 8.90.

12. A wind turbine engine 1.00 according to the third disclosure, wherein at least one of the fourth guide vanes 2.40 has a fourth root portion 2.26, a fourth section 2.27, a fourth leading edge 2.23, a fourth trailing edge 2.24, a length 400 of the fourth guide vanes, a substantially straight fourth line 2.22 and section 2.21 of the fourth guide vane, said section 2.21 of the fourth guide vane is created by cutting said fourth guide vane 2.40 along a radial arc 1.70, said radial arc 1.70 cuts the fourth guide vanes 2.40 between twenty percent and eighty percent of the length 400 of the fourth guide vanes, said the radial arc 1.70 has a center that lies about the first axis 1.10 of rotation of the main shaft 6.50 of the wind turbine engine, said length 400 of the first guide vane is the distance between the fourth root portion 2.26 and the fourth section 2.27, said distance measured along the fourteenth line, said fourth line is approximately perpendicular of the first axis of rotation 1.10, said fourteenth line intersects said fourth root portion 2.26 and intersects said fourth section 2.27 when said substantially straight fourth line 2.22 connects said fourth leading edge 2.23 and said fourth trailing edge 2.24 of said fourth guide vane section 2.21, said fourth line 2.22 forms a fourth angle 2.25 with a fourth plane 1.14, said fourth plane 1.14 substantially lies along said first axis 1.10 of rotation of said wind turbine engine main shaft 6.50 and intersects said fourth line 2.22, said fourth angle 2.25 measured perpendicularly from said fourth plane 1.14, is in the range of approximately zero degrees to sixty degrees from said fourth plane 1.14.

13. A wind turbine engine 1.00 according to the third disclosure, wherein each of the first guide vanes 2.50 has a first root portion 2.56, a first portion 2.57, a first leading edge 2.53, a first trailing edge 2.54, a length of 100 first guide vanes, a substantially straight first line 2.52, and section 2.51 of the first guide vane, said section 2.51 of the first guide vane is created by cutting said first guide vane 2.50 along a radial arc 1.70, said radial arc 1.70 cuts the first guide vanes 2.50 between twenty percent and eighty percent of the length of 100 first guide vanes, said radial arc 1.70 has a center that lies about the first axis 1.10 of rotation of the main shaft 6.50 of the wind turbine engine, said length 100 of the first guide vane is the distance between the first root portion 2.56 and the first section 2.57, said distance measured along an eleventh line, said eleventh line approximately perpendicular to said first axis 1.10 of rotation, said eleventh line intersects said first root portion 2.56 and intersects said first portion 2.57, said first guide vane section 2.51 has a first leading edge 2.53, a first trailing edge 2.54, and a substantially straight first line 2.52, when said substantially straight first line 2.52 connects said first leading edge 2.53 and said first trailing edge 2.54 of said first guide vane section 2.51, said first line 2.52 forms a first angle 2.55 with a first plane 1.11, said first plane 1.11 substantially lies along said first axis 1.10 of rotation of said main shaft 6.50 wind turbine engine and intersects said first line 2.52, said first angle 2.55, measured perpendicularly from said first plane 1.11, is in the range of approximately zero degrees to sixty degrees from said first plane 1.11.

2 said second leading edge 6.66 and said second trailing edge 6.67 are connected to the second edge 6.65 in a curved or other suitable manner, further a second space 1.42 of the engine housing system in the wind gas turbine engine rotor housing 2.30 for said wind gas turbine engine rotor 6.10 is adapted to the shape of said wind gas turbine engine rotor 6.10, to maintain an acceptable distance between said wind turbine engine rotor 6.10 and said wind turbine engine rotor housing 2.30.

15. A wind gas turbine engine 1.00 according to the third disclosure, wherein the wind gas turbine engine rotor housing 2.30 comprises three main sections, said three main sections being a first engine housing 1.17 that includes a first wall 2.44, a second engine housing 1.18 that includes a second wall 2.45, and a third engine housing 1.19, which contains a third wall 2.46; said third motor housing 1.19 is mounted between said first motor housing 1.17 and said second motor housing 1.18, said first motor housing 1.17, said second motor housing 1.18 and said third motor housing 1.19 are separable from each other and capable of being attached to each other to ensure the possibility of installing the wind gas turbine engine rotor assembly into the specified housing 2.30 of the wind gas turbine engine rotor.

Claims (44)

1. A wind-gas turbine engine that uses air cooling, containing: a wind gas turbine engine housing having a first end and a second end; a wind gas turbine engine rotor having a plurality of wind gas turbine engine rotor blades supported within a wind gas turbine engine housing such that the wind gas turbine engine rotor is rotatable about a rotor axis; wherein a rotor space is formed in the housing of the wind gas turbine engine, in which the rotor of the wind gas turbine engine is supported with the possibility of rotation around the rotor axis, wherein the rotor space has a first wall and a second wall at axially opposite ends of the rotor space and a third wall extending axially between the first wall and the second wall; wherein the housing of the wind gas turbine engine contains a first housing gap communicating with the rotor of the wind gas turbine engine in the rotor space through the first wall, and a second housing gap communicating with the rotor of the wind gas turbine engine in the rotor space through the second wall; an air compressor driven by rotating the rotor of the wind turbine engine to generate a flow of compressed air; a combustion chamber receiving fuel from the fuel system and receiving a flow of compressed air from the air compressor, the combustion chamber adapted to burn fuel from the fuel system with the flow of compressed air from the air compressor to generate an exhaust gas flow; wherein the combustion chamber comprises an exhaust duct adapted to direct a flow of exhaust gas from the combustion chamber into a rotor space, wherein the exhaust duct is separate from the first housing gap and the second housing gap in the wind gas turbine engine housing, and wherein the exhaust duct is directed into the rotor space in a circumferential manner relative to the rotor wind gas turbine engine; a mixture flow conduit at a second end of the wind gas turbine engine housing, the mixture flow conduit being in communication with the rotor space through a second wall of the rotor space, whereby the mixture flow conduit is adapted to receive an exhaust gas stream discharged from the wind gas turbine engine rotor rotating within the wind gas turbine engine housing engine; a cooling fan at a first end of the wind gas turbine engine housing, wherein the cooling fan is driven to rotate by rotating the wind turbine engine rotor, whereby the cooling fan generates a flow of cooling fan air in a longitudinal direction of the wind gas turbine engine housing; wherein the cooling fan is in communication with the first housing gap in the first wall such that at least a portion of the cooling fan air flow is directed through the rotor space from the first housing gap in the first wall to the second housing gap in the second wall, whereby (i) the flow the cooling fan air partially causes the rotor of the wind gas turbine engine to rotate around the rotor axis and (ii) cools the rotor blades of the wind gas turbine engine; wherein a second housing gap in the second wall communicates with the mixture flow conduit, whereby the mixture flow conduit receives said at least a portion of the air flow of the cooling fan together with the exhaust gas flow discharged from the wind gas turbine engine rotor rotating within the wind gas turbine engine housing. 2. The wind gas turbine engine according to claim 1, characterized in that the second housing gap has a larger size than the first housing gap, due to which the second housing gap receives the exhaust gas flow through itself from the rotor space into the pipeline for the mixture flow. 3. Wind gas turbine engine according to claim 1, characterized in that the first wall and the second wall of the rotor space are parallel to each other. 4. The wind gas turbine engine according to claim 1, characterized in that the cooling fan is located inside the fan housing forming a fan channel surrounding the wind gas turbine engine housing, and the second part of the cooling fan air flow generated by the cooling fan is directed externally around the wind gas turbine engine housing from the first end of the wind gas turbine engine housing into the second end of the wind gas turbine engine housing, whereby the second part of the cooling fan air flow generated by the cooling fan cools the wind gas turbine engine housing and leaves the wind gas turbine engine housing at the second end of the wind gas turbine engine housing to generate thrust. 5. The wind gas turbine engine according to claim 4, characterized in that the air compressor contains air compressor fan blades rotating inside the air compressor housing coaxially with the rotor of the wind gas turbine engine, while the cooling fan fan duct additionally surrounds the air compressor housing so that the air flow of the cooling fan , generated by the cooling fan, is directed from the outside around the air compressor housing. 6. The wind gas turbine engine according to claim 1, characterized in that the cooling fan contains engine fan blades rotating inside the engine fan protective shell, wherein the engine fan protective shell is connected to the wind gas turbine engine housing so that the cooling fan air flow generated by the cooling fan is directed into the rotor of a wind gas turbine engine separately from the exhaust gas flow from the combustion chamber. 7. The wind gas turbine engine according to claim 1, characterized in that the air compressor contains air compressor fan blades rotating inside the air compressor housing installed outside the wind gas turbine engine housing, wherein the air compressor is mechanically connected to the rotor of the wind gas turbine engine so that the rotation of the air compressor fan blades mechanically driven by rotation of the rotor of a wind gas turbine engine. 8. The wind gas turbine engine according to claim 7, characterized in that it further comprises a booster compressor connected downstream of an air compressor installed outside the wind gas turbine engine housing so that the air compressor and the booster compressor jointly generate the specified flow of compressed air directed into the combustion chamber in two stages. 9. Wind gas turbine engine according to claim 1, characterized in that the air compressor is driven by an electric motor. 10. The wind gas turbine engine according to claim 1, characterized in that it further comprises an air pressure sensor in communication with a space in the wind gas turbine engine housing that receives the cooling fan air flow from the cooling fan at a location upstream of the wind gas turbine engine rotor. 11. The wind gas turbine engine according to claim 1, characterized in that it further comprises a wind turbine rotor supported inside the wind gas turbine engine housing to rotate coaxially with said rotor axis, wherein the wind turbine rotor is located downstream of the wind gas turbine engine rotor, due to which the wind turbine rotor is driven said at least a portion of the cooling fan air flow and said exhaust gas flow. 12. The wind gas turbine engine according to claim 1, characterized in that each rotor blade of the wind gas turbine engine is characterized by: the length determined between the root part and the edge of the blade along the radial axis lying perpendicular to the specified axis of the rotor; And a straight line connecting the leading edge and trailing edge of the blade, lying at an angle of zero to forty degrees from the reference plane occupied by said rotor axis and said radial axis of the blade. 13. Wind gas turbine engine according to claim 1, characterized in that it additionally contains: a bearing assembly, rotatably supporting the rotor of a wind gas turbine engine relative to the housing of the wind gas turbine engine; an oil passage that supplies oil to the bearing assembly; And Exhaust gas sealing means to prevent contamination of the bearing assembly oil by the exhaust gas flow. 14. Wind gas turbine engine according to claim 1, characterized in that it additionally contains: a bearing assembly, rotatably supporting the rotor of a wind gas turbine engine relative to the housing of the wind gas turbine engine; an oil passage that supplies oil to the bearing assembly; And an oil-tight seal assembly containing: (i) a plurality of hub oil ring grooves located in the rotor hub of the wind turbine engine, (ii) a plurality of oil rings respectively disposed in the hub oil ring grooves, (iii) an oil ring spring associated with each oil ring for pressing said oil ring rings to said rotor housing of the wind turbine engine; and (iv) an oil ring projection on the outer periphery of each oil ring. 15. The wind gas turbine engine according to claim 1, characterized in that the wind gas turbine engine housing contains liquid cooling passages formed in the wind gas turbine engine housing to receive liquid coolant circulating through the wind gas turbine engine housing, whereby the wind gas turbine engine uses liquid cooling in addition to air flow cooling fan. 16. The wind gas turbine engine according to claim 15, characterized in that the housing of the wind gas turbine engine contains a first part and a second part connected to each other by a spacer ring located between them, and liquid cooling passages communicate between the first part and the second part to ensure communication of the liquid coolant between a first part and a second part of the wind gas turbine engine housing, wherein the spacer ring contains through holes aligned with liquid cooling passages communicating between the first part and the second part. 17. The wind gas turbine engine according to claim 11, characterized in that the wind gas turbine engine housing further comprises a plurality of guide vanes supported in communication with the exhaust gas flow between the wind gas turbine engine rotor and the wind turbine rotor, with each guide vane characterized by: the length determined between the root part and the edge of the guide vane along a radial axis lying perpendicular to the specified axis of the rotor; And a straight line connecting the leading edge and trailing edge of the guide vane, lying at an angle of zero to sixty degrees from a reference plane occupied by said rotor axis and said radial axis of the guide vane. 18. The wind gas turbine engine according to claim 6, characterized in that the wind gas turbine engine housing further comprises a plurality of guide vanes supported in communication with the air flow of the cooling fan between the cooling fan and the rotor of the wind gas turbine engine, wherein each guide vane is characterized by: the length determined between the root part and the edge of the guide vane along a radial axis lying perpendicular to the specified axis of the rotor; And a straight line connecting the leading edge and trailing edge of the guide vane, lying at an angle of zero to sixty degrees from a reference plane occupied by said rotor axis and said radial axis of the guide vane. 19. The wind gas turbine engine according to claim 1, characterized in that the rotor blades of the wind gas turbine engine and the first wall, the second wall and the third wall prevent the majority of said exhaust gas flow from escaping into the mixture flow conduit until said exhaust gas flow is circumferentially displaced the rotor of the wind gas turbine engine from the exhaust pipe of the combustion chamber to the second gap of the housing in the second wall. 20. The wind gas turbine engine according to claim 1, characterized in that the housing of the wind gas turbine engine contains a first housing part, which contains a first wall, a second housing part, which contains a second wall, and a third housing part, which contains a third wall, wherein the third housing part is installed between the first housing piece and the second housing piece such that the first housing piece, the second housing piece and the third housing piece are separable from each other, allowing the wind turbine engine rotor to be mounted into the wind gas turbine engine housing.