RU2021137817A - WIND AND GAS TURBINE ENGINE - Google Patents

Claims (40)

1. A wind turbine engine having an air cooling system, said wind turbine engine comprises an engine housing system, an air pressure sensor, a shaft backlash sensor, structural guide vanes, a first fan assembly having a first fan, an internal air compression system or several internal air compression systems, at least one combustion chamber having a combustion chamber body, at least one compressed air delivery system, at least one compressed air receiving means, at least one fuel system, an electrical system having at least one air-fuel mixture ignition system with at least one air-fuel mixture ignition means, at least one exhaust gas pipeline housing, at least one wind turbine rotor assembly, a lubrication system, a drive shaft means, wind turbine accessories, several bearing assemblies, several known exhaust gas sealing means, several known oil sealing means, fins, gears, first fan nose, fastening system with fasteners, air tube assemblies, air hose assemblies, wind turbine components and a drive system or several drive systems for the operation of these components of the wind turbine engine; said wind turbine components comprise one or more of the following: a first fan, an air pressure sensor, a shaft play sensor, a known starting system which is in the form of either an electric starter, or a combination unit with starting capability and electrical generating capability, or any suitable starter, an internal system air compression or multiple internal air compression systems, fuel pump and oil pump; said fuel system comprises a fuel tank, a fuel pump, fuel lines assemblies, a fuel flow control means, and has at least one fuel delivery means; said air cooling system comprises air passages and air tube assemblies, said air tube assemblies and air hose assemblies are interchangeable; said fuel delivery means having means of communication with the fuel system, said fuel delivery means being a single injector or a multi-injector system; said lubrication system comprises at least one known oil pump assembly, several oil lines, oil lines assemblies, oil hose assemblies, and lubrication system accessories, said oil pump assembly comprises an oil pump, said oil lines assemblies, and specified oil hose assemblies are interchangeable; Said wind turbine engine rotor assembly comprises a wind turbine engine rotor and a main wind turbine engine shaft, said wind turbine engine main shaft has a first axis of rotation, during operation of said wind turbine engine, said wind turbine engine rotor and said wind turbine main shaft rotate on said first axis of rotation of said main wind turbine shaft; said exhaust gas line body comprises an exhaust gas line and ribs; said internal air compression system is an air pump that pressurizes air for: cooling, sealing means for air and air for the air-fuel combustion process; said internal air compression system comprises an air conduit and a compressed air space, said air conduit has means of communication with said compressed air space, said air conduit and said compressed air space have means of communication with said compressed air receiving means; said air-fuel mixture igniter is attached to said exhaust gas line housing, or attached to said combustion chamber housing, or attached at another suitable location; wherein the engine casing 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 casing system comprises an outer casing, an engine casing, a central part shell, a space for turbocharged air, at least one air gap, a second space, a third space, at least one wind turbine rotor housing, a plurality of bearing means assemblies, fourth guide vanes, and a mixture flow conduit; the specified outer case contains the first fan housing assembly and the main frame, the specified main frame contains a pylon and a pipeline for the air flow of the first fan; a first fan assembly, which is complemented by a first fan assembly housing, generates a first fan airflow during operation of said wind turbine, said first fan airflow adapted to cool hot parts of said wind turbine; said central part shell is attached to the main frame by means of structural guide vanes, said main frame and said structural guide vanes also direct the airflow of the first fan to the second end of said wind turbine engine, said central part shell contains ribs for heat radiation, said structural guide vanes provide smooth movement of the specified air flow of the first fan in the second end of the specified wind turbine engine; said turbocharged air space is designed to ensure proper movement of said first fan air flow to the second end of said wind turbine, while said wind turbine rotor housing and said third space allow a portion of said first fan air flow to pass, said third space located in the conduit for the flow of the mixture, the specified engine casing provides access for the repair of some parts of the specified wind turbine engine; wherein the bearing means assembly comprises bearings and accessories for the bearing means assembly, said bearing assembly prevents too much axial movement and prevents too much radial movement of the shaft in relation to the housing of the bearing means assembly, said bearings are in the form of ball bearings, tapered roller bearings , cylindrical roller bearings, plain bearings and other suitable form of bearings, the specified accessories for the complete bearing means include: gaskets, keys, bushing, o-rings, bearing holders, lock and oil seals; said bearing holders and said bearing means housing assembly support the position of said bearings, said bearing holder prevents said bearings from moving out of place, said bearing holder is in the form of eye and threaded fasteners, said bearing holder works in conjunction with a lock, said spacers are designed to carry axial load from the shaft to the specified bearings, or the specified spacers transfer the axial load from the specified bearing to another bearing, or the specified spacers are designed to transfer the axial load from the specified bushing to the specified bearings, while the bearing holders are designed to transfer the axial load from the specified bearings to the specified housing of the bearing means assembly, said bushing allows easy removal or separation of the bearing assembly from the shaft and provides for the simple removal of said wind turbine main shaft from said bearing means assembly by performing several processes that lead to an outward slipping procedure, said bushing also makes it possible to obtain less damage by said bearing assembly when inserting said wind turbine main shaft, or less damage by said bearing assembly when inserting another shaft of said wind turbine during an inward slip assembly process; said bushing shall be secured to said wind turbine main shaft so that said bushing rotates with said wind turbine main shaft and said bushing is properly positioned with respect to said bearings and with respect to said wind turbine main shaft, and said bushing shall be secured to another shaft related to the specified wind turbine engine, so that the specified sleeve rotates with the specified other shaft related to the specified wind turbine engine, and the proper position of the specified sleeve is maintained in relation to the specified bearings and in relation to the specified other shaft; wherein the first fan assembly has the first fan, the shaft of the first fan and the nose of the first fan, the specified first fan is attached to the shaft of the first fan, the specified first fan has a hub of the first fan, the specified hub of the first fan contains several blades of the first fan, the specified nose of the first a fan is attached to said first fan hub, said plurality of first fan blades are attached to said first fan hub, said first fan hub is attached to said first fan shaft, said first fan shaft is supported to rotate by the bearing means assembly; wherein the housing of the first fan assembly comprises the housing of the first fan, the protective shell of the first fan and the guide vanes of the turbine, said guide vanes of the turbine contain an oil pipeline for input of the pumped oil and output of the return oil for the bearing assembly, at least one of the specified bearing means assembly is adjacent to the first fan assembly, said oil piping of said first fan housing is oil spaces along said turbine guide vanes, said oil piping, oil lines assemblies and oil hose assemblies carry oil to said bearing the means assembly to and from said first fan housing, said oil conduit, said oil hose assemblies, and said oil lines assemblies are in communication with the lubrication system; wherein the first fan assembly and the housing of the first fan assembly, during operation of the wind turbine engine, generate an air flow of the first fan for traction and for cooling the said wind turbine engine, said first fan air flow cools the following: the combustion chamber housing, the wind turbine rotor housing, the central shell parts, mixture flow piping and other hot parts of said wind turbine that require cooling, said first fan air flow is used for draft when said first fan air flow moves at high speed from the second end of said wind turbine, said first fan air flow also cools parts of the wind turbine rotor assembly and cools other parts of said wind turbine when a portion of said first fan air flow passes through the turbocharged air space, the second space, and the third space of said wind turbine; while the lubrication system has a means of communication with several bearing assembly, the specified lubrication system supplies oil for cooling and lubrication of the specified several bearing assembly, the specified lubrication system contains at least one oil pump assembly, oil lines assemblies, hoses for oil assemblies and accessories for the lubrication system, said accessories for the lubrication system comprise an oil cooler and an oil containing block, the parts that support the bearing means housing assembly of the first fan casing contain turbine guide vanes, said turbine guide vanes function as an oil cooler; wherein the internal air compression system comprises a fan of the internal air compression system, a fan housing of the internal air compression system, a protective shell of the fan of the internal air compression system, a shaft of the internal air compression system, the first stationary blades in the assembly of the internal air compression system, the second fixed blades in the assembly of the internal air compression systems, compressed air space, air pipeline and blade assemblies mounted on the shaft of the internal air compression system; Said internal air compression system fan comprises an internal air compression system fan hub and internal air compression system fan blades, said internal air compression system supplies compressed air to one or more of the following: into a combustion chamber to burn an air-fuel mixture, into a combustion chamber housing to cooling and into the wind turbine engine for additional cooling of the hot parts of the specified wind turbine engine, the specified internal air compression system contains a known air bleed system; wherein the combustion chamber is designed to generate an exhaust gas flow during operation of the wind turbine engine, said exhaust gas flow is the result of combustion of an air-fuel mixture, said combustion chamber comprises one or more of the following: a combustion chamber housing, a combustion chamber, swirling vanes, a lining, and a seal combustion chambers; said exhaust gas flow passes through the exhaust gas line housing through the exhaust gas pipeline, said combustion chamber body being cooled by one or more of compressed air cooling, first fan airflow cooling, or another airflow cooling; said combustion chamber having means of communication with a fuel delivery means, one or more air-fuel mixture ignition means, and an air compression system; said combustion chamber housing comprises means for attaching to the main frame or means for attaching to other parts of the wind turbine engine to prevent stress and vibration of said combustion chamber housing caused by the air flow of the first fan, said main frame allows access to said combustion chamber for replacement of parts, said housing the combustion chamber contains ribs for heat radiation and contains a tube for starting air, the specified tube for starting air has a means of communication with another source of compressed air; wherein the wind turbine engine rotor assembly comprises a wind turbine engine rotor and the main wind turbine engine shaft, said wind turbine engine rotor contains a wind turbine engine rotor hub, said wind turbine engine rotor hub has several wind turbine engine rotor blades, said several wind turbine engine rotor blades are attached to said rotor hub wind turbine engine, said wind turbine rotor blades are protrusions from said wind turbine rotor hub, said wind turbine rotor blades are made of a different material compared to the wind turbine rotor hub, or said wind turbine rotor blades are made of the same material as said rotor hub of a wind turbine engine; said wind turbine rotor blades extending outwardly from said wind turbine rotor hub, said plurality of wind turbine rotor blades spaced substantially equally along said wind turbine rotor hub; during operation of said wind turbine engine, said wind turbine engine rotor blades, said wind turbine engine rotor, and said wind turbine engine main shaft are rotated on the first rotation axis of said wind turbine engine main shaft by the exhaust gas flow from the combustion chamber, and additionally, said wind turbine engine rotor blades, the rotor of the wind turbine and said main shaft of the wind turbine are driven on said first axis of rotation of said main shaft of the wind turbine by part of the air flow of the first fan from the first fan assembly and the first fan assembly; wherein the drive shaft means is a system in which the shaft of the first fan, the shaft of the internal air compression system and the main shaft of the wind turbine engine are a single continuous shaft, or the shaft of the first fan, the shaft of the internal air compression system and the main shaft of the wind turbine engine are separate shafts, wherein said first fan shaft, said internal air compression system shaft, and said wind turbine main shaft are in communication with each other; wherein the mixture flow conduit directs a mixture of a portion of the air flow of the first fan and the exhaust gas flow for thrust; wherein the bearing means assembly supports one bearing or supports multiple bearings, said bearing means assembly contains a housing oil bypass, said housing oil bypass provides proper oil circulation in the bearing means assembly, said bearing means housing in assembly and said bearings contain a corresponding keyway, said key prevents said bearings from damaging said housing of the bearing means assembly; in this case, the exhaust gas flow from the combustion chamber moves into the space of the wind turbine engine rotor housing, and the movement of the specified exhaust gas flow into the specified wind turbine engine rotor housing pushes the wind turbine engine rotor blades and rotates the wind turbine engine rotor, the main shaft of the wind turbine engine, the shaft of the internal air compression system, a first fan shaft and a first fan; said main shaft of the wind turbine has means of communication with the shaft of the internal air compression system, and said main shaft of the wind turbine has means of communication with the shaft of the first fan; at the same time, the rotor housing of the wind turbine engine is adapted to enable installation of the required parts of the wind turbine engine in the specified casing of the rotor of the wind turbine engine, which provides for the possibility of installing the rotor of the wind turbine engine assembly, the specified housing of the rotor of the wind turbine engine provides the possibility of rotation of the main shaft of the wind turbine engine and the rotor of the wind turbine engine, said wind turbine rotor housing has walls, at least two housing gaps, at least one exhaust gas piping opening, wind turbine rotor assembly fins and space, said walls comprising a first wall, a second wall, and a third wall; said housing gap in said second wall, which is wider than said housing gap in said first wall, is configured such that the exhaust gas flow moves from said wind turbine rotor housing through said housing gap in said second wall; said wind turbine rotor housing is provided with air passages, a number of said air passages are used to cool said walls of said wind turbine rotor housing, said wind turbine rotor assembly space contains a second space, said second space enables said wind turbine rotor to rotate; the exhaust gas piping is in communication with a portion of the second space of said wind turbine rotor housing, said exhaust gas piping housing is directly or indirectly attached to said wind turbine rotor housing, or attached to any of said first wall, said second wall, said third wall or attached to any suitable combination of said first wall, said second wall, and said third wall so as to allow said exhaust gas flow to move into a portion of said second space of said wind turbine rotor housing; said exhaust gas conduit opening on said third wall must be adjacent to said first wall and adjacent to said second wall, at one point or more points of said wind turbine rotor housing said first wall, said second wall and said third wall are adjacent to each other friend; said wind turbine rotor housing has a required distance from said wind turbine rotor; according to the design and during operation of said wind turbine engine, said wind turbine rotor housing provides said exhaust gas flow from the combustion chamber to said wind turbine rotor housing, said exhaust gas flow passes through said exhaust gas pipeline and passes further into the specified part of the specified second space of the specified of the wind turbine rotor housing, and said exhaust gas flow, which guides said walls of said wind turbine rotor housing, pushes said wind turbine rotor blades, thereby rotating said wind turbine rotor on the first axis of rotation of said wind turbine main shaft, and the work generates energy for said wind turbine, said energy drives said wind turbine main shaft and a first fan that moves a large amount of air for thrust; said walls and said wind turbine rotor blades prevent most of said exhaust gas flow from entering the mixture flow conduit until said exhaust gas flow reaches one of said housing gaps in said second wall of said wind turbine rotor housing, and said flow exhaust gas exits said wind turbine rotor housing through said housing gaps in said second wall, and said exhaust gas flow ultimately ends up in said mixture flow conduit, said housing gap in said first wall, and said housing gap in said second wall of said the wind turbine rotor housings further enable a portion of said first fan air flow to move into and out of said wind turbine rotor housing; said wind turbine rotor housing additionally ensures flow of said portion of said first fan air flow from said first fan housing assembly between said wind turbine rotor blades to cool said wind turbine rotor blades of said wind turbine rotor, and in the process of cooling said wind turbine rotor blades said the portion of the airflow of the first fan that moves as the wind eventually adds rotational force to said wind turbine rotor to rotate, and therefore, during said wind turbine operation, said portion of the airflow of the first fan adds more torque to said wind turbine, guides the blades direct said portion of said first fan airflow to cool said wind turbine rotor blades; said wind turbine engine rotor housing contains air passages to provide cooling by said part of the air flow of the first fan of said walls of said wind gas turbine rotor housing, said wind turbine engine rotor housing contains air passages that provide air cooling from the air extraction system of said walls of said wind gas turbine rotor housing, the specified housing of the rotor of the wind turbine engine contains at least one pipeline for air and fins. 2. The wind turbine engine according to claim 1, characterized in that the combustion chamber comprises a lining, said lining has a corrugated joint, said corrugated joint contains small through spaces that allow compressed air to pass through said corrugated joint, said compressed air passing through said small through spaces, cools said cladding, and said small through spaces additionally direct cooling air to said cladding. 3. Wind turbine engine according to claim 1, characterized in that the parts adjacent to the main shaft of the wind turbine engine, the shaft of the first fan and the shaft of the internal air compression system, have a means of communication with the shaft play sensor, said shaft play sensor monitors the excessive play of the specified main shaft the wind turbine, said first fan shaft, and said shaft of the internal air compression system to alert maintenance personnel of an impending failure so that shutdown of the wind turbine occurs before significant damage occurs. 4. Wind turbine engine having an air cooling system or having both an air cooling system and a liquid cooling system, said air cooling system includes fins, air tube assemblies and air passages, said liquid cooling system includes a heat sink, liquid cooling pump, passages liquid cooling, liquid coolant, liquid cooling spaces and liquid cooling accessories, said liquid cooling accessories include refrigerant hose assemblies and refrigerant pipe assemblies, indicated refrigerant hose assemblies and indicated refrigerant pipe assemblies are interchangeable, Said wind turbine engine comprises an engine housing system, an air pressure sensor, an engine fan assembly having an engine fan and an engine fan shaft, an air filtration system or several air filtration systems, an air compression system or several air compression systems, at least one combustion chamber, at least one compressed air delivery means, at least one compressed air receiving means, a fuel system, an electrical system having an air-fuel mixture ignition system with at least one air-fuel mixture ignition means, at least one exhaust gas pipeline housing having exhaust gas piping, at least one wind turbine rotor assembly, lubrication system, drive shaft means, wind turbine accessories, several bearing assemblies, first space, second space, third space, multiple airtight seal means for exhaust gas, several oil seals that contain several oil seals, bearing holders, keys, o-ring, clips, belt, shackles, belt tension maintenance system, air tube assemblies, air hose assemblies, gears, wind turbine assembly , which contains a wind turbine rotor, components of a wind turbine engine and a drive system or several drive systems for operating said components of a wind turbine engine, said components of a wind turbine engine contain one or more of the following: an electric generating system or several electric generating systems, an air pressure sensor, a starting system, a liquid pump cooling, an air compression system that includes one or more external air compression systems, an air conditioning system having an air conditioning compressor, a transmission, a first cooling fan or a second cooling fan or an electrically controlled fan, a hydraulic pump, at least one idler pulley , at least one first pulley, an oil pump, at least one first electric motor, at least one second electric motor, a wind turbine rotor and other accessories for a wind turbine engine, said fuel system includes a fuel tank, a fuel pump, fuel lines assemblies , a fuel flow control means and at least one fuel delivery means, said compressed air delivery means comprises air pipes assemblies and air hoses assemblies, at least one of said air pipes assemblies has means for communicating with compressed air receiving means said air tube assembly and said air hose assembly are interchangeable, said bearing assembly comprises bearings, said bearings are in the form of ball bearings, tapered roller bearings, cylindrical roller bearings, plain bearings and other suitable bearing shapes; said external air compression system supplies compressed air to said combustion chamber, said external air compression system is in the form of an auxiliary air compression system and an air booster system, said auxiliary air compression system has an auxiliary air compressor, and said booster air compression system has an air booster compressor, said auxiliary air compression system is belt driven or driven by said first electric motor, and said booster air compression system is belt driven or driven by said second electric motor, said auxiliary system the air compression system has means of communication with the air filtration system, said booster air compression system compresses air from said auxiliary air compression system; said combustion chamber comprises a combustion chamber housing, said combustion chamber housing comprises an air duct, said combustion chamber generates an exhaust gas flow when an air-fuel mixture is ignited, said engine housing system has means of communication with said air filtration system, said air filtration system comprises at least at least one air filtration element, at least one air filtration housing and accessories for the air filtration system, said wind turbine rotor assembly comprises at least one wind turbine rotor and the wind turbine main shaft, said wind turbine rotor comprises a wind turbine rotor hub, having a plurality of wind turbine rotor blades, a plurality of exhaust gas compression ring hub grooves and a plurality of oil ring hub grooves, said exhaust gas compression ring hub groove is adapted for an exhaust gas tight sealing means, while said hub oil ring groove adapted for sealing means for oil, the specified main shaft of the wind turbine engine and the shaft of the fan of the engine have a means of communication, the specified main shaft of the wind turbine engine has a first axis of rotation, during operation of the specified wind turbine engine, the specified rotor of the wind turbine engine and the specified main shaft of the wind turbine engine rotate on the specified first the axis of rotation of the specified main shaft of the wind turbine engine, the specified power generating system contains an alternator and contains an electric generator, the specified electric generator has supports, the specified starting system contains a starter; said lubrication system comprises at least one oil pump assembly, oil lines assemblies, oil hose assemblies and lubrication system accessories, said lubrication system accessories comprise an oil containing unit and at least one oil cooler, said oil lines assembly and oil hose assemblies are interchangeable, said lubrication system also includes an oil pump, a known bypass valve, a screen and an oil pipeline, said oil pipeline has means of communication with said lubrication system; said first cooling fan or said second cooling fan is a system mounted on the main shaft of the wind turbine engine, said power generation system and said starting system are made as one unit or separate units, said starter includes a flywheel and includes a flywheel housing; said air compression system is an air pump that supplies air to provide one or more of the following: engine cooling and air to burn the air-fuel mixture in said combustion chamber; said air-fuel mixture igniter is attached to said combustion chamber body, or is attached to said exhaust pipe body, or is attached in another suitable location, said fuel delivery means is in communication with the fuel system, said fuel delivery means is a single injector or a multi-injector system; said engine case system is adapted for a low bypass airflow engine configuration, said low bypass airflow engine configuration includes an engine configuration with zero bypass airflow, said engine casing system comprises an engine fan housing assembly, a central portion shell, first guide vanes, at least one rotor housing of a wind turbine engine, fourth guide vanes, several housings of bearing means assemblies, a mixture flow pipeline, an exhaust gas manifold and a fastening system with fasteners, said engine housing system consists of a first part and a second part or consists of a first of the motor housing, the second motor housing and the third motor housing, said motor fan housing assembly comprises a motor fan housing and a motor fan protective shell, said motor fan protective shell is attached to said motor fan housing, said bearing housing assembly contains an oil bypass channel housing, said engine fan assembly comprises an engine fan, said engine fan has an engine fan hub and engine fan blades, said wind turbine engine rotor casing allows installation of said wind turbine engine rotor assembly, said wind turbine engine rotor casing has walls, at least one the opening of the pipeline for the exhaust gas and the clearances of the housing, these walls contain the first wall, the second wall and the third wall; said air compression system comprises a known air bleed system, said air bleed system and said air compression system have means of communication with air passages in said second wall, said exhaust gas line opening on said third wall must be adjacent to said first wall and adjacent to said second wall, at one point or more points of said wind turbine rotor housing, said first wall, said second wall, and said third wall are adjacent to each other, said exhaust gas duct housing is directly or indirectly attached to said wind turbine rotor housing, or attached to any of said first wall, or said second wall, or said third wall, or attached to any suitable combination of said first wall, said second wall, and said third wall so as to allow said exhaust gas flow to move into a portion of said second space said wind turbine rotor housing, said means in the form of a drive shaft comprises said wind turbine main shaft and said engine fan shaft, during operation of said wind turbine engine, together with the complementary operation of the fuel system, air compression system and air-fuel mixture ignition system, said combustion chamber creates a high exhaust gas flow pressure, said exhaust gas flow passes through said exhaust gas pipeline and is guided by said walls of said wind turbine rotor housing, pushes said wind turbine rotor blades, and rotates said wind turbine rotor main shaft that generates power and said exhaust gas flow exits through said housing gap in said second wall of said wind turbine rotor housing, said exhaust gas flow, which is guided by the fourth guide vanes, drives said wind turbine rotor, and said exhaust gas flow moves into the mixture flow conduit and out into said manifold for of exhaust gas, rotation of said main shaft of the wind turbine rotates said motor fan, and said motor fan of the motor fan assembly together with the motor fan housing assembly generates a usable air flow, said first guide vanes direct said usable air flow, and said usable air flow passes through said housing gap in said first wall of said wind turbine rotor housing to push said wind turbine rotor blades, and said wind turbine rotor rotates on said first axis of rotation of said wind turbine rotor shaft, and this process adds torque moment to said wind turbine engine, and this process also cools said wind turbine rotor and cools other parts of said wind turbine engine, said usable air flow exits through said housing gap in said second wall of said wind turbine rotor housing and drives said wind turbine rotor, and said usable air flow passes into said mixture flow conduit and exits into said exhaust manifold. 5. A wind turbine having an air cooling system or having both an air cooling system and a liquid cooling system, said air cooling system comprising fins, air tube assemblies and air passages, said liquid cooling system comprising a heat sink, liquid cooling pump, passages liquid cooling, liquid coolant, liquid cooling spaces and liquid cooling accessories, said liquid cooling accessories include refrigerant hose assemblies and refrigerant pipes assemblies, specified wind turbine includes motor case system, air pressure sensor, motor fan assembly having an engine fan, an air filtration system or multiple air filtration systems, an air compression system or multiple air compression systems, at least one combustion chamber, at least one compressed air delivery means, at least one compressed air receiving means, a fuel system , an electrical system having an air-fuel mixture ignition system with at least one air-fuel mixture ignition means, at least one exhaust gas pipeline housing having an exhaust gas pipeline, at least one wind turbine rotor assembly, a lubrication system, a means for drive shaft, wind turbine accessories, several bearing assemblies, first space, second space, third space, several exhaust gas tight seals, several oil seals, clips, belt, shackles, belt tension maintenance system, mounting a system having fixtures, air tube assemblies, air hose assemblies, gears, a wind turbine assembly having a wind turbine rotor, wind turbine engine components, and a drive system or multiple drive systems for operating said wind turbine engine components; Said wind turbine engine components comprise one or more of the following: an electrical generating system or multiple electrical generating systems, an air pressure sensor, a starting system, a liquid cooling pump, an air compression system that includes one or more external air compression systems, an air conditioning system having a system compressor air conditioning, transmission, first cooling fan or second cooling fan, hydraulic pump, at least one idler pulley, at least one first pulley, oil pump, at least one first electric motor, at least one second electric motor, rotor wind turbines, an electrically controlled fan and other accessories for a wind turbine engine, said fuel system includes: a fuel tank, a fuel pump, fuel lines assemblies, a fuel flow control means and at least one fuel delivery means, said oil seal means contains several oil seals, said external air compression system is in the form of an auxiliary air compression system and an air compression booster system, said auxiliary air compression system is driven by a belt or driven by said first electric motor, and said booster air compression system is driven by by means of a belt or driven by said second electric motor, said auxiliary air compression system has means of communication with the air filtration system, said air compression booster system compresses air from said auxiliary air compression system; said combustion chamber comprises a combustion chamber housing, said engine housing system has communication means with an air filtration system, said air filtration system comprises at least one air filtration element, at least one air filtration housing, and accessories for the air filtration system; Said wind turbine engine rotor assembly comprises a wind turbine engine rotor and a main wind turbine engine shaft, said wind turbine engine main shaft has a first axis of rotation, during operation of said wind turbine engine, said wind turbine engine rotor and said wind turbine main shaft rotate on said first axis of rotation of said main shaft wind turbine engine, the specified power generating system contains an alternator and contains an electric generator, the specified electric generator has supports, the specified starting system contains a starter; said lubrication system comprises at least one oil pump assembly, oil lines assemblies, oil hose assemblies and lubrication system accessories, said lubrication system accessories comprise an oil containing unit and at least one oil cooler, said lubrication system contains an oil pump assembly having an oil pump, a known bypass valve, a grid and a pipeline for oil; said first cooling fan or said second cooling fan is a wind turbine main shaft mounted system, said starter includes a flywheel and includes a flywheel housing; 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 burning the air-fuel mixture in said combustion chamber, said air-fuel mixture igniter is attached to said combustion chamber body, or attached to said exhaust pipe body, or attached at another suitable location; said air cooling system comprises air passages and air spaces as means for cooling parts of said wind turbine engine; said fuel delivery means having means of communication with the fuel system, said fuel delivery means being a single injector system or a multi injector system; said compressed air delivery means comprises air pipes assemblies and air hose assemblies, said air pipes assemblies and said air hose assemblies are interchangeable; wherein the engine casing system is adapted for an engine configuration with a low bypass air flow, said engine configuration with a small bypass air flow includes an engine configuration with zero bypass air flow, said engine casing system consists of a first part and a second part, or consists of a first engine casing, of the second motor housing and the third motor housing, said motor housing system comprises: an engine fan housing assembly, a central part shell, first guide vanes, at least one wind turbine rotor housing, several bearing housings assemblies, fourth guide vanes, support means wind turbine, the mixture flow piping, and the exhaust manifold, during operation of the wind turbine, said engine fan housing assembly and engine fan assembly generate a usable airflow for air cooling of hot parts of said wind turbine and for additional torque for said a wind turbine engine, said first guide vanes guide said usable air flow; said wind turbine rotor housing comprises a second space, said second space is located in said wind turbine rotor housing of said engine housing system, said first guide vanes, said first space, said wind turbine rotor housing, said fourth guide vanes and said third space provide said usable for using air flow from said engine fan housing assembly and engine fan assembly to said mixture flow conduit and ultimately to said exhaust manifold; said first space has a space between said wind turbine rotor housing and said first guide vanes, said motor housing system has communication means with said air filtration system, said air filtration system comprises at least one air filtration element, at least one filtration element housing air and air filtration accessories, said air filtration case allows the second cooling fan to be properly installed, said motor fan case assembly comprises an motor fan case and an engine fan guard, said motor fan guard is attached to said motor fan case; wherein the engine fan assembly has an engine fan, said engine fan includes an engine fan hub and an engine fan shaft, said engine fan hub includes multiple engine fan blades, said multiple engine fan blades are attached to said engine fan hub, said engine fan hub is attached to said motor fan shaft, during operation and during idle periods of said wind turbine engine, the first guide vanes, the bearing means assembly and the bearing means assembly maintain the rotational stability of the motor fan shaft, while the first guide vanes, the fourth guide vanes, the bearing means housing in assembly and bearing means assembly maintain rotational stability of the wind turbine main shaft, said first guide vanes and said fourth guide vanes are adapted to include an oil conduit for said bearing assembly, said oil conduit which includes a return oil conduit, and piping for injected oil, represents oil spaces along said first guide vanes, oil spaces along said fourth guide vanes, and oil spaces along other parts of said wind turbine engine, said oil piping is supplemented with oil lines assemblies and oil hose assemblies which carry oil into and out of said bearing means assembly, said oil lines assemblies and said oil hose assemblies are interchangeable, said oil line, said oil lines assemblies and said oil hose assemblies are in communication with lubrication system; wherein the combustion chamber is designed to generate an exhaust gas flow during operation of a wind turbine engine, said exhaust gas flow is known as a result of the movement of gases when an air-fuel mixture is burned, said combustion chamber comprises a combustion chamber housing, a combustion chamber, swirling vanes, lining and sealing of the chamber combustion chamber, said lining and said combustion chamber seal is a known aviation system adapted for a wind turbine engine, said exhaust gas flow passes through an exhaust gas pipeline, said combustion chamber housing contains an air pipeline, said combustion chamber housing is cooled by one or more of liquid cooled, compressed air cooled, usable air flow cooled, or other air flow cooled, said combustion chamber having means of communication with a fuel delivery means, one or more air-fuel mixture ignition means, and an air compression system; wherein the air compression system is an external compression system, said external compression system has an auxiliary air compression system that contains a booster air compression system, said external air compression system has a known air bleed system, in the means of delivering compressed air to the combustion chamber from the external system air compression using one or more of the air pipe assembly and air hose assemblies or other suitable means; wherein the wind turbine engine rotor assembly comprises a wind turbine engine rotor and the main shaft of the wind gas turbine engine, said wind turbine engine rotor has a wind turbine engine rotor hub, said wind turbine engine rotor hub comprises several wind turbine engine rotor blades, several hub grooves for the exhaust gas compression ring, and several said hub groove for the exhaust gas compression ring has an inner periphery of the hub groove for the exhaust gas compression ring, said hub groove for the oil ring has an inner periphery of the hub groove for the oil ring, said hub groove for the exhaust gas compression ring gas is adapted for an exhaust gas tight sealing means, while said oil ring groove of the hub is adapted for an oil sealing means; said multiple wind turbine rotor blades are attached to said wind turbine rotor hub, said wind turbine rotor hub is attached to the wind turbine main shaft, said wind turbine rotor blades extend outward from said wind turbine rotor hub, said wind turbine rotor blades are protrusions from said wind turbine rotor hubs, said wind turbine rotor blades are of any other suitable known shape, said wind turbine rotor blades are made of a different material than the wind turbine rotor hub, or said wind turbine rotor blades are made of the same material as said hub of the rotor of the wind turbine engine, said several blades of the rotor of the wind turbine engine are spaced substantially at equal distance along the specified hub of the rotor of the wind turbine engine, at least one blade of the rotor of the wind turbine engine of the said several blades of the rotor of the wind turbine engine contains a second edge, a second root part, a second leading edge and a second trailing edge, wherein during operation of said wind turbine engine, said wind turbine rotor blades, said wind turbine rotor, and said main shaft of the wind turbine engine are rotated on said first axis of rotation of said main shaft of the wind turbine engine by the exhaust gas flow from the combustion chamber, and additionally said wind turbine rotor blades, said wind turbine rotor, and said wind turbine main shaft are driven on said first axis of rotation of said wind turbine main shaft by a usable airflow from the engine fan housing assembly and the engine fan assembly; at the same time, the rotor housing of the wind gas turbine engine provides the ability to install the required parts of the wind gas turbine engine in the specified housing 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 of the rotor of the wind gas turbine engine provides the possibility of rotation of the main shaft of the wind gas turbine engine and the rotor of the wind gas turbine engine, the specified rotor housing wind turbine engine has walls, at least two housing gaps, at least one exhaust gas pipeline opening and a wind turbine rotor assembly space, said wind turbine rotor assembly space contains a second space, said second space specifically enables rotation of said wind turbine rotor engine, the exhaust gas pipeline housing is attached to the specified wind turbine rotor housing so that it is possible to move the specified exhaust gas flow to the part of the specified second space in the specified wind turbine rotor housing, the specified walls contain the first wall, the second wall and the third wall, the specified housing the exhaust gas conduit is directly or indirectly attached to said wind turbine rotor housing, or attached to any of said first wall, said second wall, said third wall, or attached to any suitable combination of said first wall, said second wall, and said third wall so , which makes it possible to move the specified exhaust gas flow into the part of the specified second space of the specified housing of the rotor of the wind turbine engine, the specified housing gap in the second wall, which is wider than the housing gap in the first wall, is made so that the specified exhaust gas flow passes through the specified housing gap in the second wall, said exhaust gas conduit opening on said third wall must be adjacent to said first wall and adjacent to said second wall, at one point or more points of said wind turbine rotor housing said first wall, said second wall and said third wall are adjacent to each other, said wind turbine rotor housing is provided with air passages, some of said air passages in said second wall have means of communication with the air extraction system, a number of said air passages are used to cool said second wall of said wind turbine rotor housing or are used for cooling another wind turbine rotor housing, said wind turbine rotor housing has a significant distance from said wind turbine rotor, according to the design and during operation of said wind turbine engine, the combustion chamber generates an exhaust gas flow, said exhaust gas flow passes through the exhaust gas pipeline indicated the rotor housing of the wind turbine engine allows said exhaust gas flow to push the rotor blades of the wind turbine engine and rotates the specified rotor of the wind turbine engine, and also rotates the main shaft of the wind turbine engine, which is an operation that generates a torque to perform work by the specified wind turbine engine, the specified rotor casing of the wind turbine The motor further provides for the flow of usable air flow from the motor fan housing assembly through said housing gaps in said first wall and in said second wall of said wind turbine rotor housing to cool said wind turbine rotor blades of said wind turbine rotor and a process for cooling said rotor blades wind turbine, said usable air flow that moves as wind further pushes said wind turbine rotor to rotate and therefore adds more torque to said wind turbine, said usable air flow exits said wind turbine rotor housing through the gap housing in said second wall and drives said wind turbine rotor, and said usable airflow passes into the mixture flow conduit and exits to the exhaust manifold, said wind turbine rotor housing also moves said exhaust gas flow out of said housing of the wind turbine rotor, said walls of said wind turbine rotor casing direct said exhaust gas flow to said wind turbine rotor blades, and said exhaust gas flow pushes said wind turbine rotor blades, and rotates said wind turbine rotor, and additionally rotates said wind turbine main shaft on the first axis of rotation of said main shaft of the wind turbine rotor, said walls and said wind turbine rotor blades prevent most of said exhaust gas flow from escaping into the mixture flow conduit until said exhaust gas flow reaches said housing gap in said second wall said wind turbine rotor housing, and said exhaust gas flow exits said wind turbine rotor housing through said housing gap in said second wall, and said exhaust gas flow drives said wind turbine rotor, and said exhaust gas flow enters said flow conduit mixture and exits to the exhaust manifold; oil conduit is oil spaces along the first guide vanes and fourth guide vanes or other oil conduit in said wind turbine rotor housing, said oil conduit is supplemented with oil lines assemblies and oil hose assemblies or other suitable means that carries oil into and out of said bearing means assembly; at the same time, the exhaust gas flow from the combustion chamber moves into the space of the rotor housing of the wind gas turbine engine, the specified exhaust gas flow also moves between at least two rotor blades of the wind turbine engine of the wind turbine engine rotor, the movement of the specified exhaust gas flow in the specified rotor housing of the wind gas turbine engine of the specified engine housing system rotates said rotor of the wind turbine engine and rotates the main shaft of the wind turbine engine; wherein the usable air flow pushes the wind turbine rotor blades and rotates the wind turbine rotor on the first axis of rotation of the wind turbine main shaft, which adds torque to the wind turbine, said usable air flow also maintains an acceptable operating temperature of said wind turbine rotor and further helps to maintain an acceptable operating temperature of said wind turbine engine; while the lubrication system has a means of communication with the bearing means assembly, the specified lubrication system supplies oil for cooling and lubrication of several bearing assemblies, the specified lubrication system has a means of communication with the specified bearing means assembly of the external air compression system, the specified lubrication system contains at least one oil pump assembly and accessories for the lubrication system, said accessories for the lubrication system contain a block containing oil, oil lines assemblies and contain an oil cooler, the first guide vanes are used as an oil cooler, said oil pump assembly contains an oil pump; wherein the bearing means assembly is supported by the housing of the bearing means assembly, said bearing means assembly comprises bearings and accessories for the bearing means assembly, said bearings may be in the form of ball bearings, tapered roller bearings, cylindrical roller bearings, plain bearings and other suitable bearing shape said bearing means assembly prevents too much axial movement and prevents too much radial movement of the shaft in relation to the housing of the bearing means assembly; said bearing means assembly accessories include: gaskets, bushing, keys, o-ring, bearing holders and oil seals, said bearing holder and said bearing means assembly support proper bearing position, said bearing holder is known to prevent movement of said bearings in place, said bearing holder is in the form of eyelet and threaded mounts, said bearing holder works in conjunction with a lock, said spacers are designed to transfer axial load from a shaft to said bearing, or said spacers transfer an axial load from said bearing to another bearing, specified the spacer is designed to transfer axial load from said bushing to said bearings, while said bearing holder is designed to transfer axial load from said bearings to said bearing means housing assembly, said bushing allows easy removal or separation of the wind turbine main shaft from said bearing means in outward slip assembly, said bushing also allows for less damage by said bearing assembly when inserting said wind turbine main shaft during inward slip assembly, said bushing has a key or gear and is held in bearings in the wind turbine rotor housing, said bushing has inner diameter, which preferably matches the shape of the gear, which is suitable for the specially designed main shaft of the wind turbine with the same gear shape, so that the specified sleeve and the main shaft of the wind turbine are assembled together and rotate together during the operation of the specified wind turbine, the specified sleeve provides the ability to less complex inserting said main wind turbine shaft into said bearing assembly in said wind turbine rotor housing, or said bushing enables said wind turbine main shaft to be more easily removed from said bearing assembly in said wind turbine rotor casing, said bushing prevents axial movement said wind turbine main shaft or other wind turbine shaft, and said bearings and fasteners prevent said bushing from axial movement, such bushing being adapted to the bearing means assembly of the air compression system; said bearing assembly has a means of communication with a lubrication system, said bearing assembly during operation of said wind turbine engine or during downtime maintains the rotation of one or more of the following: engine fan shaft, wind turbine main shaft, auxiliary air compressor shaft, and shaft booster air compressor, said bushing shall be secured to said wind turbine main shaft so that said bushing rotates with said wind turbine main shaft and said bushing is maintained in proper position with respect to said bearings and with respect to said wind turbine main shaft, or said bushing shall be mounted on another shaft related to the specified wind turbine, or mounted on the shaft of the auxiliary compressor, or mounted on the shaft of the booster compressor so that the specified sleeve rotates with the specified other shaft, or rotates with the specified shaft of the auxiliary compressor, or rotates with the specified shaft of the booster compressor, and the proper position of said bushing was maintained with respect to said bearings and in relation to said other shaft, or in relation to said auxiliary compressor shaft, or in relation to said booster compressor shaft; wherein the bearing housing assembly supports one bearing or supports multiple bearings, said bearing housing assembly comprises a housing oil bypass, said housing oil bypass is a groove along said bearing housing assembly, said oil bypass the housing ensures proper circulation of oil in the bearing housing assembly, said bearing housing assembly and said bearings contain a corresponding keyway, said key prevents said bearings from damaging said bearing housing assembly; wherein the drive shaft means is a system in which the engine fan shaft and the wind turbine main shaft are a single continuous shaft, or said engine fan shaft and said wind turbine main shaft are separate shafts, but said engine fan shaft and said the main shaft of the wind turbine engine are in communication with each other; wherein the liquid cooling system is of a configuration known to the engine, said liquid cooling system accessories include an electrically controlled fan or wind turbine shaft mounted fan, liquid cooling passages, coolant hose assemblies, coolant pipe assemblies and liquid cooling spaces, said passages liquid cooling and liquid cooling spaces are located at the following locations: wind turbine rotor housing walls, combustion chamber housing and exhaust gas piping housing, indicated liquid cooling passages, indicated refrigerant hose assemblies, refrigerant pipe assemblies, and indicated liquid cooling spaces are located in communication with said liquid cooling pump, said coolant hose assemblies and coolant pipe assemblies are interchangeable, said liquid cooling passages and said liquid cooling spaces are used to cool other parts of the wind turbine with a liquid cooling system, said liquid cooling passages and said liquid cooling spaces are configured such that liquid coolant can flow in and out, said liquid coolant is plain water or water mixed with other substances that contain chemicals such as antifreeze. 6. The wind turbine engine according to claim 5, characterized in that the engine casing system comprises at least one wind turbine rotor assembly, said engine casing system is adapted for said wind turbine rotor assembly, said wind turbine rotor assembly comprises at least one wind turbine rotor , said wind turbine rotor has a wind turbine rotor hub, said wind turbine rotor hub comprises several wind turbine rotor blades, each of the wind turbine rotor blades has a sixth root portion, a sixth edge, a sixth section, a sixth leading edge, a sixth trailing edge, and a substantially straight sixth line as indicated the wind turbine rotor blades are attached to said wind turbine rotor hub, said wind turbine rotor hub is attached to the main shaft of the wind turbine engine, during operation of said wind turbine engine, a usable air flow from the engine fan housing assembly and the engine fan assembly pushes said wind turbine rotor blades, additionally said wind turbine rotor blades move an exhaust gas flow that has passed through the wind turbine rotor housing, said exhaust gas flow that initially originates from the combustion chamber passes through the exhaust gas conduit of the exhaust gas conduit housing, and said exhaust gas flow moves into said housing wind turbine rotor and in the vicinity of said wind turbine rotor to push said wind turbine rotor blades to rotate said wind turbine rotor on the first axis of rotation of said wind turbine main shaft, and this process generates additional torque for said wind turbine rotor, the fourth guide vanes guide said suitable for use, the air flow and the specified exhaust gas flow into the specified wind turbine rotor, the specified wind turbine rotor blades, when cut along a radial arc, create the specified sixth section, the specified radial arc has a center that essentially lies on the specified first axis of rotation of the specified main shaft of the wind turbine engine or lies about of said first axis of rotation of said main shaft of the wind turbine, said sixth section lies between twenty and eighty percent of the length of the wind turbine rotor blade, said length of the wind turbine rotor blade is the distance between the sixth root portion and the sixth edge, said distance is measured along the sixteenth line, said sixteenth line approximately perpendicular to said first axis of rotation, said sixteenth line intersects a sixth root portion and intersects said sixth edge, when a substantially straight sixth line connects a sixth leading edge and a sixth trailing edge of said sixth section, said sixth line forms a sixth angle with a sixth plane, said sixth the plane essentially lies along the specified first axis of rotation of the specified main shaft of the wind turbine engine and intersects the specified sixth line, the specified sixth angle, measured perpendicularly from the specified sixth plane, is in the range from approximately zero degrees to forty degrees from the specified sixth plane. 7. Wind turbine engine according to claim 5, characterized in that each of the rotor blades of the wind turbine engine contains a second root part, a second edge, a second leading edge, a second trailing edge, a second blade length, a substantially straight second line and a second section, the second the section is created by cutting said wind turbine rotor blade along a radial arc, said radial arc cuts said wind turbine rotor blade between twenty and eighty percent of the length of the wind turbine rotor blade, said second blade length is the distance between the second root portion and the second edge, the specified distance measured along a twelfth line, said twelfth line is approximately perpendicular to a first axis of rotation, said twelfth line intersects said second root portion and intersects said second edge, in a fully assembled wind turbine said radial arc has a center that substantially lies on said first axis of rotation of the main shaft wind turbine engine or lies near the specified first axis of rotation of the main shaft of the wind turbine engine, when the specified essentially straight second line connects the second leading edge and the specified second trailing edge of the specified second section, the specified essentially straight second line forms a second angle with the second plane, the specified second plane essentially lies along the specified first axis of rotation of the specified main shaft of the wind turbine and intersects the specified second line, the specified second angle, measured perpendicularly from the specified second plane, is in the range from approximately zero degrees to forty degrees from the specified second plane. 8. Wind turbine engine according to Claim. 5, characterized in that the wind turbine rotor assembly contains several exhaust gas tight sealing means, said exhaust gas tight sealing means works in conjunction with the wind turbine rotor housing, said several exhaust gas tight sealing means contain a plurality of exhaust gas compression ring hub grooves and a plurality of exhaust gas compression ring assemblies, said exhaust gas compression ring hub groove and said multiple exhaust gas compression ring assembly are located in a wind turbine rotor hub, each of said hub grooves for exhaust gas compression ring adapted for exhaust gas compression ring assembly, said exhaust gas compression ring assembly includes exhaust gas compression ring and at least one exhaust gas compression ring spring, said exhaust gas compression ring has at least one exhaust gas compression ring protrusion, an exhaust gas compression ring outer periphery, an exhaust gas compression ring inner periphery, an exhaust gas compression ring thermal expansion gap, a sliding joint, an exhaust gas compression ring radial center, and a radial oil passage exhaust gas compression ring, said exhaust gas compression ring radial oil passage has center of exhaust gas compression ring radial oil passage, said exhaust gas compression ring thermal expansion gap has oil seal element, said exhaust air tight seal means prevents oil contamination due to exhaust gas pressure in the bearing means assembly of said wind turbine engine, said exhaust gas compression ring thermal expansion gap is preferably located adjacent to said exhaust gas compression ring protrusion or spaced away from said exhaust gas compression ring protrusion for simplicity, said exhaust gas compression ring thermal expansion gap is designed to contain any residual oil to lubricate the essential travel of said exhaust gas compression ring on said wind turbine rotor housing, said exhaust gas compression ring thermal expansion gap is in communication with said wind turbine rotor housing , said exhaust gas compression ring protrusion extends from the outer periphery of the exhaust gas compression ring, said exhaust gas compression ring protrusion has a designated space in said exhaust gas compression ring groove in the hub so that the exhaust gas compression ring rotates with said hub of the wind turbine rotor of the wind turbine rotor during operation of said wind turbine, the lowest point of said exhaust gas compression ring inner periphery and the adjacent section of said exhaust gas compression ring inner periphery shall be adjacent to the oil conduit in said wind turbine rotor housing when said wind turbine is mounted in a horizontal position so that oil flows out, said inner periphery of the exhaust gas compression ring further must substantially be in contact with the inner periphery of the exhaust gas compression ring hub groove of said exhaust gas compression ring hub groove, indicated The exhaust gas compression ring spring comprises a protrusion of the exhaust gas compression ring spring, which fits into the groove of the exhaust gas compression ring hub designed for said protrusion of the exhaust gas compression ring spring, said protrusion of the exhaust gas compression ring allows rotation of the exhaust gas compression ring spring. exhaust gas rings with said wind turbine rotor, said exhaust gas compression ring spring is designed to press the exhaust gas compression ring against said wind turbine rotor housing, said exhaust gas compression ring comprises a radial passage for oil of the exhaust gas compression ring gas to more effectively lubricate the stroke of said exhaust gas compression ring, said radial exhaust gas compression ring oil passage has a center of the exhaust gas compression ring radial oil passage, said exhaust gas compression ring radial oil passage is equidistant from said radial center exhaust gas compression ring of said exhaust gas compression ring, in a fully assembled wind turbine engine, said center of the radial oil passage of the exhaust gas compression ring and said radial center of the exhaust gas compression ring substantially lie about the first axis of rotation of the main shaft of the wind turbine, indicated said exhaust gas compression ring radial oil passage is in communication with said wind turbine rotor housing, and said exhaust gas compression ring radial oil passage is in communication with said exhaust gas compression ring expansion gap, said exhaust gas compression ring spring contains pusher legs, exhaust gas compression ring springs and coil springs. 9. Wind turbine engine according to claim 5, characterized in that the wind turbine rotor assembly contains several oil sealing means, said oil sealing means works in conjunction with the wind turbine rotor housing, said oil sealing means has several oil rings and several grooves hubs under the oil ring, located in the rotor hub of the wind turbine engine, each of the specified grooves of the hub under the oil ring of the hub is adapted for the oil ring assembly, the specified oil ring assembly has at least one oil ring and at least one oil ring spring, specified the oil ring has at least one oil ring protrusion, an oil ring outer periphery, an oil ring thermal expansion gap, a sliding joint, an oil ring radial center, and an oil ring inner periphery, said oil ring protrusion is placed in a predetermined space for the oil ring protrusion in said groove hubs under the oil ring of said wind turbine rotor hub so that said oil ring rotates with said wind turbine rotor hub of the wind turbine rotor during operation of said wind turbine engine, said oil ring protrusion is located on said outer periphery of the oil ring, said oil ring thermal expansion gap located adjacent to said oil ring protrusion or spaced from said oil ring protrusion for simplicity, said oil ring thermal expansion gap is in communication with the wind turbine rotor housing, said inner periphery of the oil ring further must substantially be in contact with the inner periphery of the hub groove under oil ring of said oil ring groove of the hub, said oil ring inner periphery is in communication with the lubrication system, said oil ring spring contains an oil ring spring protrusion that fits into the oil ring groove of the hub for said oil ring spring protrusion, said oil ring spring which contains an oil ring spring follower leg and a coil spring, said oil ring spring is designed to press said oil ring against said wind turbine rotor housing, said oil ring contains a small oil through groove to provide a small amount of oil for lubrication and for exhaust gas compression ring, said small groove is located adjacent to the thermal expansion gap of the oil ring, said oil ring contains a radial oil ring oil passage to more effectively lubricate the stroke of said oil ring, said radial oil ring oil passage has the center of the radial passage for oil ring oil, said radial oil ring channel is equidistant from said oil ring radial center of said oil ring, in a fully assembled wind turbine engine, said center of oil ring radial channel and said oil ring radial center lie about the first axis of rotation of the wind turbine main shaft , said radial oil ring channel is in communication with said wind turbine rotor housing, and said oil ring radial channel is in communication with said oil ring thermal expansion gap, said oil ring spring contains oil spring pusher legs, oil ring spring protrusion rings and coil springs. 10. The wind turbine engine according to claim 5, characterized in that the rotor housing of the wind turbine engine has at least two main parts, which contain the first part and the second part, the specified first part and the specified second part are made with the possibility of separation from each other and with the possibility attached to each other to enable installation of the wind turbine rotor assembly in the specified wind turbine rotor housing, between the first part and the second part there is a gasket ring or other suitable sealing material of the parts, these two main parts with a liquid cooling system have known through openings, which pass through the spacer ring for the passage of liquid cooling. 11. The wind turbine engine according to claim 5, characterized in that the auxiliary air compression system has an auxiliary air compressor, said auxiliary air compressor includes an auxiliary air compressor housing, an auxiliary air compressor fan, a protective shell of the auxiliary air compressor fan, the first stationary blades in the auxiliary air compressor assembly air compressor, the second fixed blade assembly of the auxiliary air compressor, the blade assembly mounted on the shaft of the auxiliary air compressor, the shaft of the auxiliary air compressor and several bearing means assemblies, said auxiliary air compressor has means of communication with the air filtration system, said air filtration system comprises at least one filtration element housing having a filtration element, said auxiliary air compressor housing comprising a first auxiliary air compressor housing, a second auxiliary air compressor housing, auxiliary air compressor guide vanes, an oil pipeline, an air convergence zone, and an air pipeline, said first the auxiliary air compressor fixed vane assembly and the second auxiliary air compressor fixed vane assembly are partially inserted between said auxiliary air compressor shaft-mounted blade assemblies, and said second auxiliary air compressor fixed vane assembly prevents movement of said first auxiliary air compressor fixed vane assembly. compressor, said first fixed blade assembly of the auxiliary air compressor is attached or keyed to said first auxiliary air compressor housing, said second auxiliary air compressor housing is attached to said first auxiliary air compressor housing, said auxiliary air compression system has an air compression booster system, specified the booster air compression system compresses air from said auxiliary air compressor, said booster air compression system comprises a booster air compressor, said booster air compressor comprises a booster air compressor housing, first stationary vanes assembly of the booster air compressor, second fixed vanes assembly of the booster air compressor, mounted on the shaft of the booster air compressor, the blade assembly, the shaft of the booster air compressor, and a plurality of bearing means assemblies; said booster air compressor housing includes a first booster air compressor housing, a second booster air compressor housing, a plurality of oil conduits, an air convergence area, a dust cover, and a plurality of air conduits; said air convergence zone, said air conduit, air pipe assembly and compressed air receiving means have means of communication with the combustion chamber, said second booster air compressor housing is attached to said first booster air compressor housing, said first booster air compressor fixed vanes assembly of the booster air compressor and second fixed vane assemblies of the booster air compressor are partially inserted between said vanes assemblies mounted on the shaft of the booster air compressor, and said second fixed vanes of the booster air compressor assembly prevent said first fixed vanes of the booster air compressor from moving when said first fixed vanes the booster air compressor blade assemblies are attached or keyed to said first booster air compressor housing, said auxiliary air compression system is belt driven or driven by a first electric motor, and said booster air compression system is driven by belt or driven by a second electric motor. 12. Wind turbine engine according to claim 5, characterized in that at least one of the fourth guide vanes has a fourth root part, a fourth section, a fourth leading edge, a fourth trailing edge, a length of the fourth guide vanes, a substantially straight fourth line, and a section of the fourth of the guide vane, said section of the fourth guide vane is created by cutting said fourth guide vane along a radial arc, said radial arc cuts the fourth guide vanes between twenty percent and eighty percent of the length of the fourth guide vanes, said radial arc has a center that lies near the first axis of rotation of the main of the wind turbine shaft, said length of the first guide vane is the distance between the fourth root portion and the fourth section, the specified distance is measured along the fourteenth line, the specified fourth line is approximately perpendicular to the specified first axis of rotation, the specified fourteenth line intersects the specified fourth root portion and intersects the specified fourth section when said substantially straight fourth line connects said fourth leading edge and said fourth trailing edge of said fourth guide vane section, said fourth line forms a fourth angle with a fourth plane, said fourth plane substantially lies along said first axis of rotation of said wind turbine main shaft and intersects said fourth line, said fourth angle, measured perpendicular to said fourth plane, is in the range of approximately zero degrees to about sixty degrees from said fourth plane. 13. Wind turbine engine according to claim 5, characterized in that each of the first guide vanes has a first root portion, a first section, a first leading edge, a first trailing edge, a length of the first guide vanes, a substantially straight first line and a section of the first guide vane, said section of the first guide vane is created by cutting said first guide vane along a radial arc, said radial arc cuts the first guide vanes between twenty percent and eighty percent of the length of the first guide vanes, said radial arc has a center that lies near the first axis of rotation of the main shaft of the wind turbine engine , the specified length of the first guide vane is the distance between the first root portion and the first section, the specified distance is measured along the eleventh line, the specified eleventh line is approximately perpendicular to the first axis of rotation, the specified eleventh line intersects the specified first root portion and intersects the specified first section, the specified section of the first the guide vane has a first leading edge, a first trailing edge and a substantially straight first line, when said essentially straight first line connects said first leading edge and said first trailing edge of said section of the first guide vane, said first line forms a first angle with the first plane, said first plane substantially lies along said first axis of rotation of said wind turbine main shaft and intersects said first line, said first angle measured perpendicular to said first plane is in the range of approximately zero degrees to sixty degrees from said first plane. 14. Wind turbine engine according to claim 5, characterized in that the rotor blade of the wind turbine engine has a second leading and second trailing edge, which are essentially parallel to the fifth plane, the specified fifth plane is perpendicular to the first axis of rotation of the main shaft of the wind turbine engine, the specified second leading edge and the specified the second trailing edge is connected to the second edge in a curvilinear or other suitable manner, further the second space of the engine housing system in the wind turbine rotor housing for said wind turbine rotor is adapted to the shape of said wind turbine rotor to maintain an acceptable spacing between said wind turbine rotor and said rotor housing wind turbine engine. 15. Wind turbine engine according to claim 5, characterized in that the rotor housing of the wind turbine engine contains three main sections, said three main sections are the first engine casing, which contains the first wall, the second engine casing, which contains the second wall, and the third engine casing, which contains the third wall; said third motor housing is mounted between said first motor housing and said second motor housing, said first motor housing, said second motor housing and said third motor housing are detachable and attachable to each other to enable installation of a wind turbine rotor engine assembly into the specified rotor housing of the wind turbine engine.