CN112901347A - Novel turbine engine - Google Patents

Abstract

The invention provides a technical scheme of a novel turbine engine, which mainly comprises a machine body, an air compressing rotor, an acting rotor, a gas generating device and the like, wherein the air compressing rotor and the acting rotor are arranged on the same axis in the machine body, the air compressing rotor is provided with an air inlet and an air outlet, the acting rotor is provided with an air inlet and an air outlet, the gas generating device is composed of a combustion chamber, a fuel injector, a fuel supply device and an igniter, the air outlet of the air compressing rotor is communicated with the air inlet of the combustion chamber, the air outlet of the combustion chamber is communicated with the air inlet of an acting impeller, and the air inlet of the air compressing rotor and the air outlet of the acting rotor.

Description

Novel turbine engine

The technical field is as follows:

the invention relates to a power machine, in particular to a turbine engine.

Background art:

it is known that the reciprocating piston engine which is the most widely applied at present has been invented for hundreds of years, has undoubted importance and broad-ranging performance in power application all over the world, each technology of the reciprocating piston engine is mature, and can be said to reach the top point in manufacturing technology, but the reciprocating piston engine has large noise and vibration due to the congenital structural defect of a crank connecting rod, the contact friction of a piston causes higher mechanical loss, the diameter of a cylinder is fixed during operation, and the stroke of the piston is fixed, so the reciprocating piston engine can only work in a constant volume and constant pressure mode, in order to overcome the important defects, mechanical design engineers try many …, the most successful of which is typically a turbine engine without the contact friction and the crank connecting rod, and the technology which is the closest to the present application in the prior art is a novel turbine engine patent with the application number of 2013104649115 of 10.7.2013, in the patent technology, the air compressing device and the work doing device are all formed by serially assembling a plurality of single-stage impellers in various forms on a wheel shaft to form a multi-stage air compressing and work doing mechanism, although the multi-stage air compressing and work doing structure improves the energy conversion efficiency, the individual number of the air compressing device and the work doing device is multiplied, so that the whole engine becomes complicated and heavy, the manufacturing cost is multiplied, the efficiency of the single-stage impeller mechanism is low, the multi-stage impeller mechanism is complicated and heavy, the cost is obviously increased, the defects of complicated structure, high manufacturing cost, high oil consumption during low-speed work, low thermal efficiency, small output torsion and the like of the turbine engine are the worldwide problems which disturb the industrial development of the turbine engine, and the turbine engine cannot be widely applied and popularized on the road so far, and the problem is solved.

The invention content is as follows:

the invention aims to solve the technical problem that the prior art is insufficient, and provides a novel turbine engine which has the same effect of a multi-stage air compressing impeller and a multi-stage work doing impeller on a single air compressing unit and a single work doing unit.

The scheme is realized by the following technical measures: the gas generator mainly comprises components such as a machine body, a wheel shaft, an air compressing device, a work doing device, a gas generating device and the like, wherein the wheel shaft in the machine body can be provided with a starting device, a supporting bearing and a sealing device, the air compressing device comprises an air compressing wheel cavity and an air compressing rotor, the work doing device comprises a work doing wheel cavity and a work doing rotor, the air compressing rotor can comprise an air compressing wheel body and a plurality of air compressing rotor movable blades with certain bending angles, the work doing rotor comprises a work doing wheel body and a plurality of work doing rotor movable blades with certain bending angles, the air compressing wheel body, the air compressing rotor, the work doing wheel body and the work doing rotor are respectively arranged in the air compressing wheel cavity and the work doing wheel cavity on the same axis in the machine body, the gas generating device mainly comprises a combustion chamber, a porous flame stabilizer, a fuel injector, a fuel supply device, an igniter, a pressure sensor, a temperature sensor and the like, the wheel shaft is arranged in the center of an air compressing wheel body and a working wheel body in the engine body, the air compressing wheel cavity is provided with an air inlet and an air outlet, the combustion chamber is composed of a front cavity and a rear cavity, the front cavity of the combustion chamber is provided with an air inlet, the rear cavity of the combustion chamber is provided with an air jet, the working wheel cavity is provided with an air inlet and an air outlet, the air compressing rotor can be a roller-shaped air compressing rotor formed by a plurality of strip-shaped air compressing movable blades with certain bending degrees and arranged in the rotating direction of the air compressing wheel body according to a certain cutting angle and interval, one end of the air compressing rotor is arranged and fixed on the side surface of the air compressing wheel body, the other end of the air compressing rotor corresponds to the wall of the wheel cavity opposite to the air compressing wheel body and keeps a certain sealing gap, the roller-shaped air compressing rotor follows the same axis of the wheel shaft, the circumferential surface of the air compressing wheel body can be provided with wheel sheets, the movable compression blade can be composed of a large blade and a small blade, the large blade and the small blade are narrow at the top and wide at the bottom, the large blade is arranged on a large circumferential surface, the small blade is arranged on a small circumferential surface, the top edge of the large blade, the top edge of the small blade and the top edge of the turbine blade keep a non-contact sealing gap with the narrowest part of the inner wall of the corresponding compression turbine cavity, a large semi-circular auxiliary cavity is arranged outside the compression turbine cavity corresponding to the small blade side in the compression turbine cavity and communicated with the compression turbine cavity, the large semi-circular auxiliary cavity is wrapped on the compression turbine cavity corresponding to the small blade except the periphery of an exhaust port on the small blade side, the large and small blades keep a small airtight gap with the compression turbine cavity wall and are not contacted with the compression turbine cavity wall, a large semi-circular annular cavity ring is arranged between the large semi-circular auxiliary cavity and the turbine cavity, and the diameter of the large semi-circular annular cavity ring is smaller than that of the large, the cross section circle of the large semicircular annular cavity ring is matched with the radian of the axial side edge of the corresponding small blade and keeps a non-contact sealing gap, the cross section of the large semicircular auxiliary cavity is C-shaped, the upper opening of the large semicircular auxiliary cavity with the C-shaped cross section corresponds to the top edge of the small blade, the lower opening of the large semicircular auxiliary cavity with the C-shaped cross section corresponds to the bottom edge of the small blade, the large semicircular auxiliary cavity with the C-shaped cross section and the small blade cavity form an annular channel with the large semicircular cavity as an inner annular shaft, the air outlet of the air compressor cavity is of an involute structure from the air compressor cavity to the outside along the rotation direction of the air compressor cavity on the circumferential surface of the air compressor cavity corresponding to the top end of the small blade, the air outlet of the air compressor cavity is communicated with the air compressor cavity inwards and communicated with the air inlet of the combustion chamber, and the air inlet of the air compressor cavity is arranged at the center of the side surface of the air compressor cavity corresponding to the bottom, the air compressing wheel cavity corresponding to the top end of the big blade is of an involute structure along the rotating direction of the air compressing wheel body, the tail end, namely the maximum end, of the air compressing wheel cavity extends all the way across the air compressing wheel cavity air outlet and the upper opening of the big semi-circular auxiliary cavity corresponding to the top end of the small blade and having a C-shaped cross section, the axial width of the air compressing wheel cavity corresponding to the top end of the small blade starts to gradually shrink along the rotating direction of the air compressing wheel body from the air outlet to the other end until the air outlet of the air compressing wheel cavity is formed in a convergent manner, a plurality of C-shaped static blades matched with the cross section of the big semi-circular auxiliary cavity can be arranged in the big semi-circular auxiliary cavity, the C-shaped static blades divide the big semi-circular auxiliary cavity into a plurality of C-shaped auxiliary cavity sections, the bottoms, namely centripetal ends of the plurality of the C-shaped auxiliary cavity sections correspond to the cavity of the bottom end of the small blade and are communicated with the bottom of the small blade, the top parts of the C-shaped auxiliary cavity sections, namely centrifugal ends, are arranged on the outer circular surface of the air compressor cavity and are communicated with the small blade cavity at the top end of the small blade through the air compressor cavity, when the side edge of the small blade corresponds to the spacer in the large semi-circular auxiliary cavity, the small blade cavity and the C-shaped auxiliary cavity section form a spiral channel which takes the large semi-circular cavity ring as a shaft, the air outlet of the air compressor cavity is arranged on the outer circular surface of the air compressor cavity above the top end of the small blade corresponding to the bottom of the thinnest end at the tail end of the spiral channel, namely, the acting rotor consists of an acting wheel body and an acting movable blade, the acting movable blade is a roller-shaped wheel body formed by arranging a plurality of strip-shaped blades with certain bending degree along the rotating direction of the acting wheel body according to a certain cutting angle and interval, one end of the acting wheel body is arranged and fixed on the side surface of the acting wheel body, the other end of the, the compression wheel cavity air inlet is arranged at the center of the side surface of the compression wheel cavity, the compression wheel cavity air outlet is arranged on the circumferential wall of the compression wheel cavity, the working wheel cavity air inlet is arranged on the circumferential wall of the working wheel cavity, the working wheel cavity air outlet is arranged at the center of the side surface of the working wheel cavity, the combustion chamber is composed of a combustion chamber front cavity and a combustion chamber rear cavity, the combustion chamber front cavity is communicated with the combustion chamber air inlet, the combustion chamber rear cavity is communicated with the combustion chamber air outlet, the compression wheel cavity air outlet is communicated with the combustion chamber air inlet, the combustion chamber air outlet is communicated with the working wheel cavity air inlet, the compression wheel cavity air inlet is communicated with the working wheel cavity air outlet, a compression stator can be arranged in the compression wheel cavity, the compression stator is a plurality of strip-shaped stator blades with certain reverse bending degree are arranged in the rotation direction of the compression wheel cavity according to a certain tangential angle and interval, one end of the compression stator is installed and fixed on the inner wall of the wheel cavity opposite, the other end suit is in the form of cylinder compressed air rotor the inside with the form of cylinder compressed air rotor and keeps the small clearance contactless, cylindric compressed air stator is with the same axis of compressed air rotor, the other end of cylindric compressed air stator keeps certain sealed clearance with the wheel body side of compressing air that corresponds, can have the stator of doing work in the wheel chamber of doing work, the stator of doing work is arranged into cylindric its one end installation according to certain tangent angle and interval in the same direction of rotation of the wheel body of doing work by a plurality of rectangular shape quiet vanes that have certain reverse camber and is fixed on the opposite wheel intracavity wall of the wheel body of doing work, and the other end suit is in the form of cylinder rotor the inside of doing work and keeps the small clearance contactless with the rotor of doing work of cylinder, cylindric stator of doing work is with the same axis of rotor of doing work, the other end of cylindric stator of doing work keeps certain sealed clearance with the wheel body side of corresponding, the pneumatics device can constitute by the form The two roller-shaped air compressing rotors with different diameters are sleeved on the side surface of the air compressing wheel body according to the same axis, the other end of the air compressing rotor is kept in a micro air-tight gap with the corresponding air compressing wheel cavity wall, one end of the cylindrical air compressing stator is fixedly installed on the opposite air compressing wheel cavity wall of the air compressing wheel body, the other end of the cylindrical air compressing stator is sleeved between the two roller-shaped air compressing rotors and is kept in a micro air-tight gap with the corresponding air compressing wheel cavity wall, the cylindrical air compressing stator is kept in a micro air-tight gap with the inner and outer roller-shaped air compressing rotors, the acting device can be composed of two roller-shaped acting rotors with different diameters and a cylindrical acting stator, the two roller-shaped acting rotors with different diameters are sleeved on the side surface of the acting wheel body according to the same axis, the other end of the cylindrical acting stator is kept in a micro air-tight gap with, the other end of the air compressing device is sleeved between two roller-shaped working rotors to keep a tiny air-tight gap with the side surfaces of the corresponding working wheel bodies, the cylindrical working stator keeps a tiny sealing gap with the inner and outer roller-shaped working rotors, the air compressing device also can be composed of a plurality of roller-shaped air compressing rotors with different diameters and a plurality of cylindrical air compressing stators with different diameters, the plurality of roller-shaped air compressing rotors are sequentially sleeved on the side surfaces of the air compressing wheel bodies according to the diameter of the same axis, the other end of the air compressing device keeps a tiny air-tight gap with the corresponding cavity wall of the air compressing wheel, the plurality of cylindrical air compressing stators are sequentially sleeved between two adjacent roller-shaped air compressing rotors according to the diameter of the same axis and keep tiny air-tight gaps with the corresponding side surfaces of the air compressing wheel bodies, the other ends of the cylindrical air compressing stators are respectively installed and fixed on the inner wall of the air, The outer two roller-shaped air compression rotors keep a tiny sealing gap, the acting device can also be composed of a plurality of roller-shaped acting rotors and a plurality of cylindrical acting stators, the plurality of roller-shaped acting rotors are sequentially sleeved on the side surface of the acting wheel body according to the same axis and the diameter, the other ends of the roller-shaped acting rotors keep tiny air-tight gaps with the corresponding cavity wall of the acting wheel, the plurality of cylindrical acting stators are sequentially sleeved between two adjacent roller-shaped acting rotors and keep tiny air-tight gaps with the corresponding side surface of the acting wheel body respectively according to the diameter, the other ends of the roller-shaped acting stators are respectively installed and fixed on the inner wall of the cavity of the acting wheel opposite to the acting wheel body, the plurality of cylindrical acting stators respectively keep tiny sealing gaps with the adjacent inner and outer two roller-shaped acting rotors, the axial lengths of the plurality of air compression rotors can be the same, and the axial lengths of the plurality of air compression, the axial length of a plurality of working rotors can be the same, the axial length of a plurality of working stators can be the same, the axial length of a plurality of air compressing rotors can be different, the axial length of a plurality of air compressing stators can be different, the axial length of a plurality of working rotors can be different, the axial length of a plurality of working stators can be different, the axial length of air compressing rotors different in axial length and air compressing stators different in axial length can be inwards increased from the outmost layer in turn and also can inwards decrease in turn, the axial length of working rotors different in axial length and working stators different in axial length can be inwards increased from the outmost layer in turn and also can inwards decrease in turn from the outmost layer, a plurality of working stators different in axial length can be installed in series on the same wheel axle by air compressing device, The engine comprises a basic power unit consisting of a working device and a gas generating device, wherein a plurality of gas outlets can be arranged on the gas compressing device, a plurality of gas inlets can be arranged on the working device, a plurality of gas generating devices can be distributed on the outer circumference of the engine body, a plurality of gas outlets on the gas compressing device are respectively communicated with the gas inlets of combustion chambers on the plurality of gas generating devices, the gas nozzles of the combustion chambers on the plurality of gas generating devices are respectively communicated with a plurality of gas inlets on the working device, a booster igniter is arranged on the working wheel cavity wall in front of the gas inlet of a working wheel cavity, namely in front of the rotating direction of a working wheel body, a booster fuel injector can be arranged on the working wheel cavity wall in front of the booster igniter, an arc-shaped gas blocking block with the arc length larger than that of the gas inlet of the working wheel cavity can be arranged on a stator corresponding to the gas inlet of the working wheel cavity, and a water sprayer can, the outer end of the water sprayer is connected with a water supply device, an arc movable cavity wall can be arranged on the circumference of a wheel cavity at the air inlet of a working device in the machine body, one end of the arc movable cavity wall is connected with a fixed cavity wall through a movable shaft, the other end of the arc movable cavity wall is arranged in front of an air inlet and provided with a regulating device, an arc air blocking block on the stator keeps a micro air tight gap with a working rotor, a starting device and a speed change device can be arranged on a wheel shaft, the starting device can be a multipurpose motor compatible with power generation and power generation functions, the speed change device can be provided with a control mechanism, a gas generating device can be provided with sensing components such as a pressure sensor, a temperature sensor and the like, the multipurpose motor, the starting device, the water sprayer, the water spray supply device, the movable cavity wall regulating device, the control mechanism on the speed change device, Igniter, fuel vaporizer, booster igniter, booster fuel injector, fuel vaporization regulation and control device are connected with central processing controller through the pencil, be connected with storage battery on the central processing controller, speed change gear can constitute by planetary gear set and planetary gear set control motor of taking locking mechanism, planetary gear set control motor can be for the internal rotor for the big ring gear in planetary gear set also can be for the internal rotor for the planet gear shelf installation permanent magnet in planetary gear set, use the wire winding as outer stator and fix on the organism, one of shaft can be equipped with power distributor, power distributor can be the integrated motor of electricity generation electronic plus planetary gear speed change mechanism, the combustion chamber can be the cylinder, porous sleeve shape scalable flame stabilizer in the cylinder combustion chamber, the top end of the porous sleeve-shaped telescopic flame holder is provided with a position controller, the front cavity of the combustion chamber can be in a vortex shape, the nozzle of the fuel injector can be provided with a liquid fuel vaporizing device, the liquid fuel vaporizing device can be a high-frequency electromagnetic heating vaporizer or a high-frequency induction heating vaporizer or other heating vaporizers in the prior art, the motor on the starting device can be a rare earth permanent magnet brushless motor or other motors in the prior art, the motor can be a multifunctional multipurpose motor compatible with power generation and electric power functions, a basic power unit formed by a single air compressor, a single power generator and a single gas generator can be arranged in the engine body as a single-cylinder engine in the prior art, a plurality of basic power units are jointly arranged on the same wheel shaft in series to form the engine body to form a multi-unit engine or a multi-wheel engine In a multi-cylinder piston engine in the prior art, a sealing ring and a conventional lubricating device may be provided on a bearing, or a supporting bearing and a sealing mechanism in other forms which can be applied to the technical scheme in the prior art may be provided, the combustion chamber may be a scroll combustion chamber, a direct-current combustion chamber, or a combustion chamber in other forms which is applicable to the present scheme in the prior art, the engine body may further be provided with conventional auxiliary electronic and electrical equipment in other forms, the compressor may be a single compressor rotor or a multi-rotor compressor mechanism composed of a plurality of compressor rotors, the planetary gear set may be a single set of planetary gear set or a planetary gear combination composed of a plurality of sets of planetary gears, the planetary gear set may be provided with a planetary gear set locking mechanism and a control motor, and the planetary gear set locking mechanism may be a planetary gear set locking mechanism which is applicable to any two gears in the planetary gear set capable of locking in the present scheme in the prior art Any planetary gearset control mechanism that can lock or control the gear that is in the free state. Such as: the front end of the working rotor shaft is connected to the center of one side of the sun gear in the planetary gear set, the rear end of the air compression rotor shaft is connected to the center of the other side of the sun gear in the planetary gear set, a planetary gear carrier in the planetary gear set is controlled, and power is output through a large gear ring, a gear device and a power output shaft in the planetary gear set. Such as: the front end of the working rotor shaft is connected to the center of one side of the sun gear in the planetary gear set, the rear end of the air compressing rotor shaft is connected to the center of the other side of the sun gear in the planetary gear set, a large gear ring in the planetary gear set is controlled, and power is output through a planetary gear carrier, a gear device and a power output shaft in the planetary gear set. Such as: the front end of the working rotor shaft is connected to the center of a large gear ring in a planetary gear set, the rear end of the air compressing rotor shaft is connected to the center of a sun gear in the planetary gear set, the power is output through a planetary gear carrier, a gear device and a power output shaft in the planetary gear set, the planetary gear set can also be any planetary gear combination which can be used for the scheme, a generator can be installed on any one of the planetary gear sets, the power is output to an electric device in an electric power mode through a lead, a generator can be directly installed on the concentric shaft, the power is output in an electric transmission mode through the generator, the lead and the electric device, the control motor can be any power generation and electric integrated motor which can be used for the scheme in the prior art, the electric device can be any electric equipment which can be used for the scheme in the prior art, and a telescopic pipe can be arranged in a front cavity of the combustion chamber, the front end of the extension tube is connected with a fuel injector and communicated with the fuel injector, the rear end of the extension tube penetrates through the machine body and is communicated with a fuel supply device outside the machine body, a spring can be arranged on the extension tube in the front cavity of the combustion chamber, the front end of the spring is propped against the front cavity wall of the front cavity of the combustion chamber, the rear end of the spring is propped against a position controller at the top end of the porous flame holder, the fuel supply device can be fuel supply equipment which can supply various liquid fuels and gas fuels and can be suitable for the scheme in the prior art, the fuel injector can be a fuel nozzle or a nozzle or other fuel injection devices which can inject various gases and liquid fuels and can be suitable for the scheme in the prior art, a liquid fuel vaporization device can be arranged on the fuel injector, and the liquid fuel vaporization device can be a high-frequency electromagnetic heater or a conventional device such as a gasoline, The preheating vaporization loop on the kerosene stove and the diesel stove, the ignition device can be various ignition devices which can be used in the scheme in the prior art, the bearing can be a needle bearing with an oil seal, a roller bearing, a ball bearing, a magnetic suspension bearing, an oil suspension bearing, or bearings which can be applicable to the scheme in the prior art, the fuel injector, the planetary gear set control motor, the igniter and the fuel supply device can be an electric control device or an electric control mechanism and an electric control device which can be used in the scheme in the prior art, the machine body can be provided with a heat insulation material layer, a heat dissipation and cooling tube cavity can be arranged in the machine body, the scheme also comprises various conventional auxiliary electronic and electric equipment and facilities which can be used in the invention in the prior art, such as various sensing devices, controllers, actuators, computers, instruction input devices and the like, such as gas pressure sensors, liquid pressure sensors, voltage sensors, current sensors, rotational speed sensors, temperature sensors, oxygen sensors, flow sensors, carbon dioxide sensors, particle detection sensors, three-way catalysts, various pumps, meters, controlled motors, numeric keypads, central processing controllers, display screens, batteries, etc., will not be discussed or illustrated in detail herein for brevity and clarity of illustration.

The basic working principle is as follows: the novel turbine engine can be suitable for the combustion work of various gases and liquid fuels, when the air compressing device is only provided with one air compressing rotor, the mechanical energy output by a motor on a starting device drives the air compressing rotor to rotate at high speed through a wheel shaft, a gap between two adjacent movable blades in the air compressing rotor is called as movable blade space for short, air in the movable blade space in the air compressing rotor is thrown away from the air compressing rotor by a driven blade under the action of centrifugal force, negative pressure is generated in the movable blade space, the air in the inner cavity of the air compressing rotor enters the movable blade space of the air compressing rotor under the action of atmospheric pressure, the air pressure in the inner cavity of the air compressing rotor is reduced, the air continuously enters the inner cavity of the air compressing rotor through an air inlet of an air compressing wheel cavity under the action of atmospheric pressure, along with the continuous rotation of the air compressing rotor, the air in the middle movable blade space of the air compressing rotor is continuously thrown away from the air compressing rotor and enters a combustion chamber front, when the air compressing device is provided with an air compressing stator and two air compressing rotors, air entering the space between the movable blades of the first air compressing rotor is rotated along with the first air compressing rotor, simultaneously is thrown away from the first air compressing rotor at a high speed by the movable blades of the first air compressing rotor and collides with the fixed blades in the stator, then enters the space between the fixed blades for speed reduction and pressure boost to form compressed air, along with the high-speed rotation of the first air compressing rotor, the compressed air pressurized in the space between the fixed blades overflows along the outer edges of the fixed blades under the action of inertia and pressure, the compressed air overflowing outwards from the space between the fixed blades is swept into the space between the movable blades in the second air compressing rotor by the movable blades of the second air compressing rotor rotating at a high speed along with the second air compressing rotor, and the diameter of the second air compressing rotor is larger than that the air compressing rotor in the cavity of the stator is the diameter of the first air compressing rotor, the speed of the movable blades on the second air compressing rotor is faster than that of the movable blades on the first air compressing rotor, compressed air in the movable blades of the second air compressing rotor rotates at a high speed along with the second air compressing rotor with a higher speed and is simultaneously thrown away from the second air compressing rotor by the movable blades on the second air compressing rotor at a higher speed, the compressed air in the movable blades of the second air compressing rotor is thrown away at a high speed and then enters an exhaust port on the wall of an air compressing wheel cavity and enters a front cavity of a combustion chamber through an air inlet of a gas generating device, when the air compressing device is provided with a plurality of air compressing rotors and a plurality of air compressing rotors, air in an inner cavity of the first air compressing rotor firstly enters the movable blades of the first air compressing rotor and is thrown away by the movable blades on the first air compressing rotor at a high speed and then enters the static blades in the primary air compressing rotor, the air is cooled down and pressurized in the static blades of the primary air compressing rotor and then overflows along with the static blades of the second air compressing rotor with a higher speed and is swept, the compressed air entering the second compressor rotor blade space rotates at a high speed along with the second compressor rotor, because the diameter of the second compressor rotor is larger than that of the first compressor rotor, the speed of the blades on the second compressor rotor is higher than that of the blades on the first compressor rotor, the compressed air in the second compressor rotor blade space is spun off the second compressor rotor at a higher speed along with the second compressor rotor rotating at a higher speed, the compressed air spun off at a high speed by the second compressor rotor hits the stator blades of the secondary compressor stator again for reducing the speed and increasing the pressure, the compressed air enters the stator blades of the secondary compressor stator, the compressed air in the secondary compressor stator blade space sequentially overflows towards the outer edge, the compressed air overflowing from the secondary compressor stator is swept into the blades of the third compressor rotor again by the blades on the third compressor rotor at a higher speed, compressed air entering the third compressed air rotor blade space again rotates at a higher speed along with the third compressed air rotor, the compressed air in the third compressed air rotor blade space is simultaneously rotated at a higher speed along with the third compressed air rotor with a higher speed and is thrown away again at a higher speed by the movable blades on the third compressed air rotor, the compressed air thrown away at a high speed by the third compressed air rotor again collides with the fixed blades of the next-level compressed air stator, the compressed air is subjected to speed reduction and pressure boost again and then enters the fixed blades of the next-level compressed air stator, the compressed air is subjected to speed reduction and pressure boost again and overflows along the fixed blades in the fixed blades of the next-level compressed air stator, the compressed air overflowing from the next-level compressed air stator again overflows along the fixed blades in the fixed blades of the next-level compressed air stator, the compressed air overflowed from the next-level compressed air stator is swept into the movable blades of the fourth compressed air rotor again by the movable blades on the higher speed because the diameter of the fourth compressed air rotor is larger than that of the third compressed air rotor, compressed air entering among the movable blades of the fourth compressed air rotor rotates at a higher speed along with the fourth compressed air rotor, the compressed air in the movable blades of the fourth compressed air rotor is thrown away from the fourth compressed air rotor at a higher speed along with the fourth compressed air rotor at a higher speed, the compressed air thrown away at a high speed by the fourth compressed air rotor collides with the fixed blade of the secondary compressed air stator again, is subjected to speed reduction and pressurization again and enters the fixed blade of the secondary compressed air stator again, the compressed air subjected to speed reduction and pressurization again overflows from the fixed blade in the fixed blade of the secondary compressed air stator again and enters the movable blade of the fifth compressed air rotor along with the high-speed rotation of the fifth compressed air rotor to be sequentially and repeatedly circulated, the air is thrown away by the movable blades of the first compressed air rotor and then collides with the fixed blade of the primary stator, is subjected to speed reduction and pressurization again, the compressed air subjected to speed reduction and pressurization after overflowing from the primary stator and enters the next stage with a higher rotation speed, namely, the second compressed air The air in the cavity of the large blade on the air compressing wheel body generates centrifugal force along with the high-speed rotation of the large blade and generates side pressure air of the large blade under the action of centrifugal force The center of the rotor moves to the centrifugal end, namely the top end of the big blade, the pressure at the bottom of the cavity of the big blade is reduced to generate negative pressure, air in the atmosphere enters the bottom of the cavity of the big blade through the air inlet under the action of atmospheric pressure, the air at the air inlet is continuously sucked into the bottom of the cavity of the big blade by the cavity of the big blade along with the high-speed rotation of the air compressing wheel body, the energy and the speed of the air in the bottom of the cavity of the big blade are rapidly increased, the air subjected to the energy application of the big blade moves to the excircle of the impeller along the big blade under the action of centrifugal force and is gathered at the top end of the big blade to reduce the speed and increase the pressure, the compressed air after the pressure increase at the top end of the big blade enters the gradually-releasing air outlet to reduce the speed and increase the pressure when rotating to the air outlet, meanwhile, the air in the bottom of the cavity of the small blade generates centrifugal force along with the high-speed rotation, the air moving at high speed in the cavity of the small blade rotates forwards along with the small blade and is thrown away from the top end of the small blade to enter the upper opening of the front C-shaped auxiliary cavity section, negative pressure is generated at the bottom of the cavity of the small blade, the air in the lower opening of the C-shaped auxiliary cavity section corresponding to the bottom of the cavity of the small blade at the rear end of the large semi-circular auxiliary cavity is sucked into the cavity of the small blade and rotates forwards along with the cavity of the small blade, the compressed air pressurized by the large blade in the air outlet of the large blade is sucked into the rear end of the large semi-circular auxiliary cavity by the negative pressure generated in the rear end of the large semi-circular auxiliary cavity, and is also sucked into the cavity of the small blade and is thrown away from the top end of the small blade at high speed to enter the upper opening of the front C-shaped auxiliary cavity section while rotating forwards at high speed along with the cavity of the small blade, the compressed air in the upper opening of the C-shaped auxiliary cavity section moves along the fixed blade in the C-shaped auxiliary cavity and surrounds, compressed air after the speed reduction and pressurization again in the lower opening of the C-shaped auxiliary cavity section is swept into the cavity of the small blade again by the small blade which is then rotated to rotate at a high speed along the cavity of the small blade, the compressed air is thrown into the upper opening of the C-shaped auxiliary cavity section in front again after being applied with energy by the small blade again, the compressed air in the upper opening of the C-shaped auxiliary cavity section moves towards the lower opening of the C-shaped auxiliary cavity again along the fixed blade in the C-shaped auxiliary cavity and around the cavity ring, the compressed air in the C-shaped auxiliary cavity section is pushed by the small blade to do continuous spiral pressurization movement in the C-shaped auxiliary cavity and the cavity of the small blade along the fixed blade in the C-shaped auxiliary cavity and around the cavity ring, the compressed air is applied with energy by the small blade once every time, the compressed air forms high-energy gas after being continuously applied with energy by the small blade for multiple times, the high-energy compressed air enters into an exhaust port on the wall of the air compression wheel cavity and enters into a front cavity of the combustion chamber, because the combustion chamber is volute, the compressed air entering the front cavity of the combustion chamber firstly rotates around the porous bell-shaped flame holder in a vortex shape and then passes through the air holes of the porous bell-shaped flame holder to enter the rear cavity of the combustion chamber, the air holes on the porous bell-shaped flame holder are gradually enlarged from the top to the bottom, the flow rate of the high-compressed air in the porous bell-shaped flame holder is characterized in that the top flow rate is relatively slow, the bottom flow rate of the flame holder is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector from the fuel supply device, is sprayed into the top of the porous bell-shaped flame holder from the nozzle of the fuel injector to be mixed with the high-compressed air in the top of the porous bell-shaped flame holder to form combustible high-compressed mixed air, the combustible high-compressed mixed air is ignited by electric sparks released by the igniter when flowing to the bottom of the porous bell-shaped flame holder, and the ignited combustible, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like, the liquid fuel vaporizer control device is started and provides high-frequency electromagnetic waves for a liquid fuel vaporizer, namely a high-frequency electromagnetic heater, a nozzle of the fuel injector is heated by the liquid fuel vaporizer, the liquid fuel enters the fuel injector from a fuel supply device and is heated and vaporized at the nozzle of the fuel injector, the liquid fuel is vaporized and then injected into the top of the porous bell-shaped flame holder and is mixed with the high-pressure gas in the top of the porous bell-shaped flame holder to form combustible high-pressure compressed mixed gas, the liquid fuel can also be directly injected into the interior of the porous bell-shaped flame holder in an atomized state at high pressure through the fuel sprayer and is directly mixed with the high-pressure compressed gas in the porous bell-shaped flame holder to form combustible high-pressure compressed mixed gas, and the combustible high-pressure mixed gas is ignited by electric sparks released by an igniter when flowing to the bottom of, the ignited high-energy gas in the working wheel cavity air inlet is sprayed into the working wheel cavity air inlet at a high speed with a certain cutting angle to impact the dynamic rotor on the working rotor when only one working rotor is arranged on the working device When the working device is a working structure formed by a working rotor and a working stator, high-energy gas in an air inlet of a working wheel cavity is sprayed into the working wheel cavity at a high speed at a certain tangential angle through an air inlet to firstly impact the movable blades on the working rotor to drive the working rotor to rotate, the high-energy gas impacts the rotor blades to reduce the energy and slow down the flow speed, the high-energy gas after acting enters the gaps of the rotor blades of the acting rotor to continue decompression and expansion, the compressed air after decompression and expansion in the gaps of the rotor blades of the acting rotor is sprayed into the inner cavity of the acting rotor through the inner openings of the gaps of the rotor blades of the acting rotor at a certain tangential angle to impact the stator blades in the inner cavity of the acting rotor again so as to obtain a strong reverse thrust to continue to push the acting rotor to rotate, the high-energy gas after impacting the stator blades decelerates and slows down again and enters the inner cavity of the stator through the gaps of the stator blades of the stator and then is discharged from the exhaust port of the acting wheel cavity, the acting rotor obtains an impact force and a strong reverse thrust to drive the acting wheel body to rotate together, the pressure energy of the high-energy gas is converted into rotary mechanical energy to be output through the wheel shaft, when a plurality of acting rotors and a plurality of acting stators, namely a multistage, high-energy gas in an air inlet of a working wheel cavity is sprayed into the working wheel cavity at a high speed through an air inlet at a certain tangential angle to firstly impact a primary working rotor on the outermost edge of the side surface of a working wheel body, namely movable blades on the outermost first-stage working rotor to push the first-stage working rotor to rotate, the high-energy gas impacts the outermost first-stage working rotor movable blades to reduce the energy flow speed and slow down, then enters movable blade gaps of the outermost first-stage working rotor to continue decompression and expansion, the high-energy gas expanded in the first-stage working rotor movable blade gaps is sprayed into an inner cavity of the first-stage working rotor at a certain tangential angle to impact fixed blades of a primary stator in the inner cavity of the first-stage working rotor again so as to obtain a reverse thrust again to continue to push the first-stage working rotor to rotate, the high-energy gas impacts fixed blades on the primary stator to slow down and enters the fixed blade gaps of the primary stator, the high-energy gas after the secondary pressure reduction expansion in the primary stator gap is sprayed into the inner cavity of the primary stator from the inner opening of the primary stator stationary blade gap according to a certain tangential angle to continuously impact the next stage, namely the movable blade on the second stage working rotor pushes the second stage working rotor to rotate, the energy of the high-energy gas after the impact on the movable blade of the second stage working rotor reduces the flow speed again and slows down and enters the movable blade gap of the second stage working rotor to continue the pressure reduction expansion again, the high-energy gas after the pressure reduction expansion in the movable blade gap of the second working rotor continuously sprays into the inner cavity of the second stage working rotor according to a certain tangential angle to impact the secondary stator blade in the inner cavity of the second stage working rotor again so as to obtain a reverse thrust again to continuously push the second stage working rotor to rotate, the high-energy gas after the impact on the stationary blade on the secondary stator decelerates and enters the stationary blade gap of the secondary stator to reduce the pressure expansion again, and the high-energy gas after the pressure reduction expansion in the secondary stator gap The high-energy gas after secondary decompression expansion in the gap of the secondary stator continuously sprays the movable blade on the next stage, namely the fourth stage working rotor, from the inner cavity of the stator blade of the secondary stator according to a certain tangential angle to continuously push the movable blade on the fourth stage working rotor to do work, the energy after the high-energy gas impacts the movable blade of the third stage working rotor is reduced in flow speed again and is slowed down again, the high-energy gas enters the inner cavity of the stator blade of the secondary stator at a certain tangential angle, the high-energy gas obtains a reverse thrust again, the compressed air after the pressure reduction expansion in the gap of the secondary stator is sprayed into the inner cavity of the secondary stator at a certain tangential angle, the compressed air after the pressure reduction expansion in the gap of the secondary stator is reduced in speed again, the compressed air enters the inner cavity of the secondary stator blade of the secondary stator at a certain tangential angle, the high-energy gas after the pressure reduction expansion in the gap of the secondary stator blade continues to continuously push the movable blade on the next stage, namely the fourth stage working rotor The high-energy gas pushes the fourth-stage working rotor movable blades, the energy continues to reduce the flow speed and slow down again, the high-energy gas enters the movable blade gaps of the fourth-stage working rotor to continue decompression and expansion, the high-energy gas after decompression and expansion in the movable blade gaps of the fourth-stage working rotor continuously sprays into the inner cavity of the fourth-stage working rotor at a certain tangential angle to push the stator blades of the secondary stator in the inner cavity of the fourth-stage working rotor again so as to obtain a reverse thrust again and continue to push the fourth-stage working rotor to rotate, the high-energy gas after decompression and expansion in the gap of the secondary stator impacts the stator blades on the secondary stator and then slows down and enters the stator blade gaps of the secondary stator to decompress and expand again, the high-energy gas after decompression and expansion in the gap of the secondary stator continues to spray into the inner cavity of the secondary stator from the inner opening of the secondary stator at a certain tangential angle to push the movable blades on the next-stage working rotor, namely the fifth, by analogy, high-energy gas is inwards layer by layer until the final-stage working rotor is pushed to work and then enters the inner cavity of the final-stage working rotor and then is discharged from the working wheel cavity exhaust port, the working wheel body obtains a plurality of impact forces and a plurality of reverse thrusts from the multistage working rotor to drive the working wheel body to rotate together, most internal energy of the high-energy gas is converted into rotary mechanical energy to be output through the wheel shaft after being converted by the multistage working rotors, the pressure of the high-energy gas in the inner cavity of the final-stage working rotor is close to atmospheric pressure to become waste gas and finally is discharged through the working wheel cavity exhaust port, when an arc movable cavity wall is arranged at the air inlet of the working wheel cavity, the opening degree of the air inlet of the working wheel cavity can be controlled by regulating and controlling the movable angle of the arc movable cavity wall to realize regulation and control of air inflow, the movable cavity wall enables the air inlet to be converted into an adjustable air inlet, and, the movable cavity wall can be adjusted through the adjusting and controlling device, the air inlet is wider and longer, more high-energy gas can enter the working wheel cavity, the high-energy gas can simultaneously push more working rotor blades to generate larger torsion, when the torsion needs to be reduced, the movable cavity wall can be adjusted through the adjusting and controlling device, the air inlet of the working device is narrowed and shortened, the high-energy gas can be reduced to enter the working wheel cavity, the high-energy gas can push less working rotor blades to reduce the output torsion, when a boosting fuel injector and a boosting igniter are arranged at the air inlet of the working wheel cavity, different fuels can be sprayed into the working wheel cavity through the boosting fuel injector according to needs during work, the fuels are combusted and released among the working rotor blades to increase the gas pressure among the working rotor blades, and the boosting fuel injector can also work independently, namely the boosting fuel injector sprays the fuels and the fuels can work wheel cavity air inlet under the condition that the fuel injector on the combustion chamber does not work The compressed air is mixed to form combustible mixed gas and then enters the working rotor movable vane space, the combustible mixed gas in the rotor movable vane space is ignited by a pressurizing igniter to burn and release energy to do work, when a fuel oil vaporization heater is arranged on a pressurizing fuel injector, the fuel provided by a fuel supply device is vaporized by the heater and then is sprayed into an air inlet of a working wheel cavity through the pressurizing fuel injector to be mixed with the compressed air at an air inlet of the working wheel cavity to form combustible mixed gas and then enters the working rotor movable vane space, the combustible mixed gas in the rotor movable vane space is ignited by the pressurizing igniter to burn and release energy to do work, when an arc-shaped air blocking block is arranged on a stator corresponding to the air inlet of the working wheel cavity, the fuel sprayed by the fuel injector on a combustion chamber is mixed with the compressed air in the cavity behind the combustion chamber to form combustible mixed gas and then enters the working rotor movable vane space through the air inlet of the working wheel cavity, and the corresponding arc-shaped air blocking block is arranged at the air inlet, the combustible mixed gas in the working rotor movable vane space at the air inlet of the working wheel cavity can not be sprayed out from the lower port of the working rotor movable vane space, when the combustible mixed gas in the working rotor movable vane space rotates to the booster igniter in front of the air inlet of the working wheel cavity along with the working rotor, the booster igniter is ignited to burn and release energy to do work, when the air outlet of the combustion chamber on the fuel gas generating device is provided with a water sprayer, during the work of the engine, especially during the high-speed high-power work, a proper amount of atomized water can be sprayed into the air inlet of the working device through the water sprayer according to the temperature in the working wheel cavity, the atomized water in the air inlet of the working wheel cavity absorbs heat in the high-temperature high-pressure fuel gas to be rapidly vaporized and expanded to generate a large amount of high-temperature high-pressure steam which enters the working wheel cavity together with the high-temperature high-pressure fuel gas to push the working rotor to rotate to, The temperature of the working rotor and the working stator also improves the high-energy gas pressure in the working wheel cavity, reduces the damage of the working device caused by high temperature, and further improves the heat energy conversion efficiency of the fuel, when a speed change device is arranged on a wheel shaft, the working rotor and the air compressing rotor can automatically adjust the rotating speed ratio according to various working conditions during working, so that the self-adaptation between the working rotor and the air compressing rotor is realized, the air compressing rotor can output compressed air with different compression ratios under the condition that the rotating speed of the working rotor is not changed, the variable adjustment and the controllability of the compression ratio are realized, the compressed air with different compression ratios required by the combustion of various fuels can be provided for a combustion chamber under the condition that the hardware of a machine is not changed, the selection of one machine for multiple fuels is realized, when a power distributor is arranged on the wheel shaft, the air compressing rotor and the working rotor can be driven to, the control motor is used as a starter, the working rotor can drive the control motor to generate electricity to output electricity to electric equipment or charge a storage battery while driving the pressure rotor, the control motor can also be used for locking a large gear ring of a planetary gear set in a power distributor, namely the control motor rotor, in the work process, the working rotor outputs power to a power output shaft in a fixed gear ratio mode through the power distributor at the rear end of a wheel shaft, forward or reverse current can also be applied to the control motor stator, forward or reverse torque is applied to the control motor rotor, namely the large gear ring of the planetary gear set in a speed change device, the working rotor outputs power to the power output shaft in a variable gear ratio mode through the power distributor at the rear end of the wheel shaft, and when the rotating speed of the working rotor is reduced due to obstruction, forward or reverse current can also be applied to the control motor stator to apply an additional current to the control motor rotor, namely the large gear ring of the planetary gear set in the speed change device The boosting power is output to the power output shaft in a hybrid mode, the control motor on the power distributor can also output electric power to the power output shaft through the power distributor when the working rotor does not work, the power distributor enables the engine to achieve hybrid and energy recovery functions, and all working modes can be intelligently controlled through programming through the central processing unit.

Description of the drawings:

fig. 1 is an axial structural view of a first embodiment of the present invention.

Fig. 2 is a schematic view of the transverse structure of fig. 1 along the line a.

Fig. 3 is a schematic view of the transverse structure of fig. 1 and 4 along the line B.

Fig. 4 is an axial structural view of a second embodiment of the present invention.

Fig. 5 is a schematic view of the structure of fig. 4 along the line a.

Fig. 6 is an axial structural view of a third embodiment of the present invention.

Fig. 7 is a schematic view of the transverse configuration of fig. 6 and 23 taken along line a (when the active cavity walls are open).

Fig. 8 is a schematic view of the transverse configuration of fig. 6 and 23 taken along line a (when the active cavity walls are closed).

FIG. 9 is a schematic view of the transverse configuration of FIG. 6 taken along line B (with the active cavity walls closed).

Fig. 10 is an axial structural view of a fourth embodiment of the present invention.

Fig. 11 is a schematic view of the structure of fig. 10 taken along the line a.

Fig. 12 is a schematic view of the structure in the transverse direction along the line B in fig. 10.

Fig. 13 is an axial structural view of a fifth embodiment of the present invention.

Fig. 14 is a schematic view of the structure in the transverse direction along the line a in fig. 13.

Fig. 15 is a schematic view of the transverse structure of fig. 13, 19 and 23 along the line B.

Fig. 16 is an axial structural view of a sixth embodiment of the present invention.

Fig. 17 is a schematic view of the structure in the transverse direction along the line a in fig. 16.

Fig. 18 is a schematic view of the transverse structure of fig. 16, 21 and 24 along the line B.

Fig. 19 is an axial structural view of a seventh embodiment of the present invention.

Fig. 20 is a cross-sectional view taken along line a in fig. 19 and 30.

Fig. 21 is an axial structural view of an eighth embodiment of the present invention.

Fig. 22 is a schematic view of the transverse structure of fig. 21 and 24 along the line a.

Fig. 23 is an axial structural view of a ninth embodiment of the present invention.

Fig. 24 is an axial structural view of a tenth embodiment of the present invention.

Fig. 25 is an axial structural view of the eleventh embodiment of the present invention.

Fig. 26 is a schematic view of the structure of fig. 25 taken along the line a.

Fig. 27 is a schematic view of the transverse structure of fig. 25 taken along the line B.

Fig. 28 is a schematic view of the lateral structure of fig. 25 taken along the line a'.

Fig. 29 is a schematic view of the transverse structure of fig. 25 taken along line B'.

Fig. 30 is an axial structural view of a twelfth embodiment of the present invention.

Fig. 31 is a schematic view of the structure of fig. 30 taken along the line a.

Fig. 32 is a schematic view of the structure of fig. 30 taken along the line B.

Fig. 33 is an axial structural view of a thirteenth embodiment of the present invention.

FIG. 34 is a schematic view of the transverse configuration of FIG. 33 taken along line A (with the active cavity walls open).

FIG. 35 is a schematic view of the transverse configuration of FIG. 33 taken along line A (with the active cavity walls closed).

Fig. 36 is a schematic view of the structure in the transverse direction along the line B in fig. 33.

Fig. 37 is a schematic view of the structure in the transverse direction along the line C in fig. 33.

Fig. 38 is a schematic view of the structure in fig. 36 and 37, which is inclined along the line D.

In the figure, 1 is a machine body, 2 is a first compressor wheel body, 2 'is a second compressor wheel body, 3 is a wheel shaft, 4 is a first compressor rotor movable blade, 4' is a second compressor rotor movable blade, 4 'is a third compressor rotor movable blade, 4v is a fourth compressor rotor movable blade, 5 is a first compressor rotor movable blade space, 5' is a second compressor rotor movable blade space, 5 'is a third compressor rotor movable blade space, 5v is a fourth compressor rotor movable blade space, 6 is a first compressor stator blade, 6' is a second compressor stator blade, 6 'is a third compressor stator blade, 7 is a first compressor stator blade space, 7' is a second compressor stator blade space, 7 'is a third stator blade space, 8 is a first working wheel body, 8' is a second working wheel body, 9 is a first working rotor movable blade, 9 'is a second working rotor movable blade, 9' is a third working rotor movable blade, 9v is a fourth working rotor blade, 10 is a first working rotor blade space, 10 ' is a second working rotor blade space, 10 "is a third working rotor blade space, 10v is a fourth working rotor blade space, 11 is a first working stator blade, 11 ' is a second working stator blade, 11" is a third working stator blade, 12 is a first working stator blade space, 12 ' is a second working stator blade space, 12 "is a third working stator blade space, 13 is a first compressor cavity, 13 ' is a second compressor cavity, 14 is a first working wheel cavity, 14 ' is a second working wheel cavity, 15 is a first compressor cavity inlet, 15 ' is a second compressor cavity inlet, 16 is a first compressor cavity outlet, 16 ' is a second compressor cavity outlet, 17 is a first working wheel cavity, 17 ' is a second working wheel cavity, 18 ' is a second compressor cavity outlet, 18 'is a second power wheel chamber exhaust port, 19 is a first combustion chamber front chamber, 19' is a second combustion chamber front chamber, 20 is a first combustion chamber rear chamber, 20 'is a second combustion chamber rear chamber, 21 is a first flame holder, 21' is a second flame holder, 22 is a first fuel injector, 22 'is a second fuel injector, 23 is a first fuel supply means, 23' is a second fuel supply means, 24 is a fuel vaporization heater, 24 'is a second fuel vaporization heater, 25 is a first vaporizer control means, 25' is a second vaporizer control means, 26 is a first igniter, 26 'is a second igniter, 27 is a first combustion chamber nozzle, 27' is a second combustion chamber nozzle, 28 is a pressurized fuel injector, 29 is a pressurized igniter, 30 is a cable, 31 is a battery pack, 32 is a central processing controller, 33 is a first temperature sensor, 33 'is a second temperature sensor, 34 is a first pressure sensor, 34' is a second pressure sensor, 35 is a speed changing device, 36 is a control motor rotor, 37 is a control motor stator, 38 is a power distributor, 39 is a radiating fin, 40 is a power output shaft, 41 is an arc-shaped air blocking block, 42 is a central wheel piece, 43 is a large blade, 44 is a small blade, 45 is a large semi-circular auxiliary cavity, 46 is a large semi-circular annular cavity ring, 47 is a regulating device, 48 is a water sprayer, 49 is a movable cavity wall, 50 is a movable shaft, 51 is a water supply device, 52 is a starting device, 53 is a bearing and a sealing device, 54 is a position controller, 55 is a telescopic pipe, 56 is a spring, 57 is a vaporization loop, 58 is a sheet type reinforcing rib, 59 is a large blade air outlet, 60 is an annular air tight groove, 61 is a large semi-circular auxiliary cavity air inlet, 62 is a large blade cavity, and 63 is a small blade cavity.

The specific implementation mode is as follows:

in order to more clearly illustrate the technical features of the present solution, the present solution is further illustrated by the following thirteen embodiments in combination with the attached drawings.

The following are particularly noted: the above components and devices labeled with numerals indicate "first" only by names in the following description of the embodiments, for example, the first air compressor rotor, the first air compressor wheel body, the first air compressor wheel cavity, the first power rotor, the first power wheel body, the first power wheel cavity, etc. are all called as air compressor rotor, air compressor wheel body, air compressor wheel cavity, power rotor, power wheel body, power wheel cavity, and other similarities and differences.

Fig. 1, 2, and 3 collectively show a first embodiment of this scheme, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is a basic power unit formed by a machine body 1, a wheel shaft 3, an air compressing device, a work doing device, a gas generating device, and the like, the basic power unit is a most basic power structure like a single-cylinder piston engine, the air compressing device is provided with an air compressing rotor, the work doing device is provided with a work doing rotor, the air compressing rotor and the work doing rotor are respectively installed in an air compressing wheel cavity 13 and a work doing wheel cavity 14 on the same axis in the machine body 1, the air compressing rotor is formed by an air compressing wheel body 2 and a plurality of air compressing rotor moving blades 4 with a certain bending angle, the plurality of strip-shaped air compressing rotor moving blades 4 with a certain bending angle for short are arranged into a roll shape along the rotation direction of the air compressing wheel body 2 according to a certain tangential angle and a certain distance, one end of the working rotor is fixed on the side surface of the air compressing wheel body 2, the other end of the working rotor corresponds to the wall of an air compressing wheel cavity 13 opposite to the air compressing wheel body 2 and keeps a certain sealing gap, the roller-shaped air compressing rotor follows the same axis of a wheel shaft 3, the working rotor is composed of a working wheel body 8 and a plurality of working rotor movable blades 9 with a certain bending angle, the plurality of strip-shaped working rotor movable blades 9 with a certain bending angle are arranged into a roller shape according to a certain tangential angle and a certain interval against the rotating direction of the working wheel body 8, one end of the working rotor movable blades is fixed on the side surface of the working wheel body 8, the other end of the working rotor movable blades corresponds to the wall of the working wheel cavity 14 opposite to the working wheel body 8 and keeps a certain sealing gap, the roller-shaped working rotor follows the same axis of the wheel shaft 3, the wheel shaft 3 is installed on the centers of the air compressing wheel body 2 and, the utility model provides a gas compressor wheel chamber 13 air inlet 15 is in gas compressor wheel chamber 13 side center department, gas compressor wheel chamber 13 gas outlet 16 is on gas compressor wheel chamber 13 circumference wall, do work wheel chamber 14 air inlet 17 is on do work wheel chamber 14 circumference wall, do work wheel chamber 14 air inlet 17 department has pressure boost fuel injector 28, pressure boost fuel injector 28 communicates with fuel feeding device 23, pressure boost fuel injector 28 spout department has fuel vaporization heater 24, pressure boost fuel injector 28 has pressure boost point firearm 29 on the preceding do work wheel chamber circumference wall, do work wheel chamber 14 gas vent 18 in do work wheel chamber 14 side center department, gas generating device is by combustion chamber front chamber 19, combustion chamber rear chamber 20, porous bell-shaped flame stabilizer 21, fuel injector 22, fuel feeding device 23, point firearm 26 constitution above rotor and the rotor of doing work of calming the anger of the porous bell-shaped flame stabilizer 21 from porous bell-shaped flame stabilizer 21 top beginning to grow gradually until porous bell-shaped flame stabilizer 21 top Shape flame holder 21 bottom, fuel injector 22 is installed on the porous bell-shaped flame holder 21 top center in the vortex form combustion chamber, fuel injector 22 is through the pipeline with the outer fuel feeding device 23 intercommunication of organism 1, some firearm 26 is installed in the porous bell-shaped flame holder 21 bottom of cavity 20 air jet 27 end behind the combustion chamber, there is combustion chamber air inlet 29 on the cavity 19 before the combustion chamber, there is combustion chamber air jet 27 behind the combustion chamber on the cavity 20, pressure wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, combustion chamber air jet 27 communicates with acting wheel chamber 14 air inlet 17, pressure wheel chamber 13 air inlet 15 and acting wheel chamber 14 gas vent 18 communicate with each other with the atmosphere.

The basic working principle is as follows: when the gas compressing rotor works, the motor on the starting device 52 outputs mechanical energy to drive the gas compressing wheel body 2 and the acting wheel body 8 to drive the gas compressing rotor and the acting rotor to rotate at high speed through the wheel shaft 3, air in the movable blade space 5 of the gas compressing rotor is thrown away from the gas compressing rotor by the movable blades 4 under the action of centrifugal force, negative pressure is generated in the movable blade space 5, air in the inner cavity of the gas compressing rotor enters the movable blade space 5 of the gas compressing rotor under the action of atmospheric pressure, the air pressure in the inner cavity of the gas compressing rotor is reduced, the air continuously enters the inner cavity of the gas compressing rotor through the air inlet 15 of the gas compressing wheel cavity 13 under the action of atmospheric pressure, and along with the continuous rotation of the gas compressing rotor, the air in the movable blade space 5 of the gas compressing rotor is continuously thrown away from the gas compressing rotor by the movable blades 4 of the gas compressing rotor and then enters the air, the compressed air in the front chamber 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear chamber 20 of the combustion chamber, the air holes on the flame stabilizer 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed air in the flame stabilizer 21 is characterized in that the top flow rate is relatively slow, the bottom flow rate of the flame stabilizer 21 is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected into the top of the flame stabilizer 21 from the nozzle of the fuel injector 22 to be mixed with the high-compressed air in the top of the flame stabilizer 21 to form combustible high-compressed mixed air, when the bell-shaped combustible high-compressed mixed air flows to the bottom of the porous flame stabilizer 21, the combustible high-compressed mixed air is ignited by electric sparks released by the igniter 26, and the ignited combustible high-compressed mixed air, when liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like is used, the liquid fuel is pressurized by a fuel supply device 23 and then is sprayed into the top of a flame stabilizer 21 at a high speed in an atomized manner through a fuel injector 22 to be mixed with compressed air in the top of the flame stabilizer 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by an igniter 26 when flowing to the bottom of the flame stabilizer 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, the high-temperature high-pressure gas is sprayed into an air inlet 17 of a working wheel cavity 14 at a high speed through an air nozzle 27 of a combustion chamber, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle to impact working blades 9 on a working rotor to push the working rotor to rotate, and part of energy is converted into rotary mechanical energy to, the high-energy gas after the flow rate is slowed down enters the working rotor moving vane chamber 10 to continue expanding, the high-energy gas after pressure reduction and expansion in the working rotor moving vane chamber 10 is injected into the inner cavity of the working rotor through the inner opening of the working rotor moving vane chamber 10 in a certain reverse tangential angle against the rotation direction of the working wheel body 8 to generate a reverse thrust to push the working rotor to rotate again, the working rotor drives the working wheel body 8 to rotate together, the pressure energy of the high-energy gas is converted into rotary mechanical energy to drive the compressing wheel body 2 to drive the compressing rotor to rotate through the wheel shaft 3, the residual power is output through the wheel shaft 3, when a pressurizing fuel injector 28 and a pressurizing igniter 29 are arranged at the air inlet 17 of the working wheel cavity 14, different fuels can be injected into the working wheel cavity 14 through the pressurizing fuel injector 28 according to needs to increase the pressure in the working rotor moving vane chamber 10 by burning and releasing energy in the rotor working moving vane chamber 10, the pressurizing fuel injector 28 can also work independently, that is, under the condition that the fuel injector 22 on the combustion chamber does not work, the pressurizing fuel injector 28 alone injects fuel to mix with the compressed air at the air inlet 17 of the working wheel cavity 14 to form combustible mixed gas, then the combustible mixed gas enters the working rotor blade compartment 10, when the combustible mixed gas in the rotor blade compartment 10 reaches the pressurizing igniter 29, the combustible mixed gas is ignited by the pressurizing igniter 29 to burn and release energy to work, when the fuel vaporizing heater 24 is arranged on the pressurizing fuel injector 28, the fuel provided by the fuel supply device 23 is vaporized by the heater 24, then the fuel is injected into the air inlet 17 of the working wheel cavity 14 through the pressurizing fuel injector 28 to mix with the compressed air at the air inlet 17 of the working wheel cavity 14 to form combustible mixed gas, then the combustible mixed gas enters the working rotor blade compartment 10, and the combustible mixed gas in the rotor blade compartment 10 is ignited by the pressurizing igniter 29 to burn and, the waste gas with certain excess pressure after working is finally exhausted through the exhaust port 18 of the working wheel cavity 14.

Fig. 3, 4 and 5 collectively show a second embodiment of the present invention, and it can be seen from the attached drawings that the novel wheel engine shown in this embodiment is also a basic power unit formed by a machine body 1, an air compressing device, a work doing device, a gas generating device and other members, the air compressing device is provided with an air compressing rotor, the work doing device is provided with a work doing rotor and a work doing stator, the air compressing rotor and the work doing rotor are respectively installed in an air compressing wheel cavity 13 and a work doing wheel cavity 14 on the same axis in the machine body 1, the air compressing rotor is composed of an air compressing wheel body 2 and a plurality of air compressing rotor moving blades 4 with a certain bending angle, the plurality of strip-shaped air compressing rotor moving blades 4 with a certain bending angle are arranged into a roll shape along the rotating direction of the air compressing wheel body 2 according to a certain tangential angle and interval, one end of each of the strip-shaped air compressing rotor moving, the other end of the working stator corresponds to the wall of the air compressing wheel cavity 13 opposite to the air compressing wheel body 2 and keeps a certain sealing gap, the roller-shaped air compressing rotor and the same axis of the wheel shaft 3, the working rotor consists of a working wheel body 8 and a plurality of working rotor movable blades 9 with a certain bending angle, the plurality of strip-shaped working rotor movable blades 9 with a certain bending angle, namely the bending angle, are arranged into a roller shape according to a certain tangential angle and a certain interval along the rotating direction of the working wheel body 8, one end of the roller-shaped working rotor movable blade is installed and fixed on the side surface of the working wheel body 8, the other end of the roller-shaped working rotor movable blade corresponds to the wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8 and keeps a certain sealing gap, the roller-shaped working rotor and the same axis of the wheel shaft 3 are also composed of a plurality of working stator blades 11 with a certain reverse bending angle, the plurality of strip-shaped working stator blades 11 with a certain reverse bending angle are arranged into a cylinder shape according to a, one end of the working wheel is fixedly arranged on the wall of a working wheel cavity 14 opposite to the side of the working wheel body 8, the other end of the working wheel is sleeved in the inner cavity of a working rotor and keeps a certain sealing gap with the side of the corresponding working wheel body 8, the cylindrical working stator is arranged on the same axis with the wheel shaft 3, the wheel shaft 3 is arranged at the centers of the air compression wheel body 2 and the working wheel body 8, the inner wheel shaft 3 of the machine body 1 is provided with a starting device 52, a supporting bearing and a sealing device 53, an air inlet 15 of the air compression wheel cavity 13 is arranged at the center of the side of the air compression wheel cavity 13, an air outlet 16 of the air compression wheel cavity 13 is arranged on the circumferential wall of the air compression wheel cavity 13, an air inlet 17 of the working wheel cavity 14 is arranged on the circumferential wall of the working wheel cavity 14, an air outlet 18 of the working wheel cavity 14 is arranged at the center of the side, The fuel injector 22, the fuel supply device 23, the igniter 26, the storage battery 31, the central processing controller 32, the temperature sensor 33 and the vaporization loop 57, wherein the air holes on the porous bell-shaped flame holder 21 are gradually enlarged from the top of the porous bell-shaped flame holder 21 to the bottom of the porous bell-shaped flame holder 21, the fuel injector 22 is arranged on the center of the top of the porous bell-shaped flame holder 21 in the cylindrical combustion chamber, the fuel injector 22 is communicated with the fuel supply device 23 outside the machine body 1 through the vaporization loop 76, the vaporization loop 57 is arranged in the rear combustion chamber 20, the igniter 26 is arranged at the bottom of the porous bell-shaped flame holder 21 at the air outlet 27 end of the rear cylindrical combustion chamber 20, the fuel supply device 23, the igniter 26, the storage battery 31 and the temperature sensor 33 are connected with the central processing controller 32 through the cable 30, the combustion chamber air inlet 29 is arranged on the front combustion chamber 19, there is the combustion chamber air jet 27 behind the combustion chamber on the chamber 20, the compressor wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, the combustion chamber air jet 27 communicates with acting wheel chamber 14 air inlet 17, compressor wheel chamber 13 air inlet 15 and acting wheel chamber 14 gas vent 18 communicate with each other with the atmosphere.

The basic working principle is as follows: when the air compressor works, the central processing unit 32 is connected with the storage battery 31 and a circuit on the starting device 52, a motor on the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2 and the acting wheel body 8 to drive the air compressing rotor and the acting rotor to rotate at high speed through the wheel shaft 3, air in the movable vane space 5 of the air compressing rotor is thrown away from the air compressing rotor by the movable vanes 4 under the action of centrifugal force, negative pressure is generated in the movable vane space 5, the air in the inner cavity of the air compressing rotor enters the movable vane space 5 of the air compressing rotor under the action of atmospheric pressure, the air pressure in the inner cavity of the air compressing rotor is reduced at the moment, the air continuously enters the inner cavity of the air compressing rotor through the air inlet 15 of the air compressing wheel cavity 13 under the action of atmospheric pressure, along with the continuous rotation of the air compressing rotor, the air in the movable vane space 5 of the air compressing rotor is continuously thrown away from the air compressing rotor by the movable vanes 4 and, the compressed air in the front chamber 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear chamber 20 of the combustion chamber, the air holes on the flame stabilizer 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed air in the flame stabilizer 21 is characterized in that the top flow rate is relatively slow, the bottom flow rate of the flame stabilizer 21 is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected into the top of the flame stabilizer 21 from the nozzle of the fuel injector 22 to be mixed with the high-compressed air in the top of the flame stabilizer 21 to form combustible high-compressed mixed air, when the bell-shaped combustible high-compressed mixed air flows to the bottom of the porous flame stabilizer 21, the combustible high-compressed mixed air is ignited by electric sparks released by the igniter 26, and the ignited combustible high-compressed mixed air, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like, the liquid fuel can be directly pressurized by the fuel supply device 23 and then sprayed into the top of the flame holder 21 in an atomized manner through the fuel injector 22 at a high speed to be mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure fuel gas, the liquid fuel can also be pressurized by the fuel supply device 23 and then enters the fuel injector 22 through the vaporization loop 57 to be sprayed into the top of the flame holder 21 in a vaporized manner at a high speed to be mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, and the combustible compressed mixed gas is ignited by the electric sparks released by the igniter 26 when flowing, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is short for high-energy gas and is sprayed into an air inlet 17 of a working wheel cavity 14 at a high speed through an air spraying opening 27 of a combustion chamber, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle to impact movable blades 9 on a working rotor to push the working rotor to rotate, when the high-energy gas impacts the movable blades 9 of the working rotor, part of energy is converted into rotary mechanical energy to reduce the flow velocity of the rotary mechanical energy, the high-energy gas enters movable blade spaces 10 of the working rotor to continue to expand after the flow velocity of the high-energy gas is reduced, the high-energy gas after pressure expansion in the movable blade spaces 10 of the working rotor is sprayed into an inner cavity of the working rotor through an inner opening of the movable blade spaces 10 of the working rotor with, the pressure energy of the high-energy gas is converted into rotary mechanical energy to drive the air compressing wheel body 2 to drive the air compressing rotor to rotate through the wheel shaft 3, the residual power is output through the wheel shaft 3, and the waste gas with certain residual pressure after acting enters the inner cavity of the acting stator through the acting stator vane space 12 and is discharged through the exhaust port 18 of the acting wheel cavity 14.

Fig. 6, 7, 8, and 9 collectively show a third embodiment of this scheme, and it can be seen from the attached drawings that the novel turbine engine shown in this embodiment is also a basic power unit composed of a machine body 1, a wheel shaft 3, an air compressing device, a work doing device, a gas generating device, and the like, the air compressing device is composed of two roller-shaped air compressing rotors with different diameters and a cylindrical air compressor stator, the axial lengths of the two roller-shaped air compressing rotors with different diameters and the cylindrical air compressor stator are the same, the two roller-shaped air compressing rotors with different diameters are sleeved on the side surface of the air compressing wheel body 2 according to the same axis, the other end of the two roller-shaped air compressing rotors keeps a micro air-tight gap with the corresponding wall of the air compressing wheel cavity 13, one end of the cylindrical air compressor stator is installed and fixed on the inner wall of the air compressing wheel cavity 13 opposite to the side surface of the air compressing wheel body 2, the other end of, the cylindrical stator keeps a tiny sealing gap with the inner and outer two roller-shaped rotors, the acting device is composed of two roller-shaped acting rotors with different diameters and a cylindrical acting stator, the axial lengths of the two roller-shaped acting rotors with different diameters and the cylindrical acting stator are the same, the two roller-shaped acting rotors with different diameters are sleeved on the side surface of the acting wheel body 8 according to the same axis, the other end of the roller-shaped acting rotor keeps a tiny airtight gap with the corresponding wall of the acting wheel cavity 14, one end of the cylindrical acting stator is installed and fixed on the inner wall of the acting wheel cavity 14 opposite to the side surface of the acting wheel body 8, the other end of the cylindrical acting stator is sleeved between the two roller-shaped acting rotors and keeps a tiny airtight gap with the corresponding side surface of the acting wheel body 8, and the cylindrical acting stator keeps a tiny sealing gap with the inner and outer two roller-shaped acting rotors, the wheel shaft 3 is arranged in the centers of the acting wheel body 8 and the air compressing wheel body 2, the wheel shaft 3 is provided with a starting and speed changing device 35, a supporting bearing and a sealing device 53, the center of the air compressing wheel cavity 13 is provided with an air inlet 15, the center of the acting wheel cavity 14 is provided with an air outlet 18, the circumference of the air compressing wheel cavity 13 is provided with an air outlet 16, the circumference of the acting wheel cavity 14 is provided with an air inlet 17, the speed changing device 35 is composed of a planetary gear set with a locking mechanism and a planetary gear set control motor, the planetary gear set control motor is composed of a motor rotor 36 arranged on a large gear ring in the planetary gear set and a motor stator 37 fixed on the machine body 1, the motor stator 37 is connected with a central processing controller 32 through a cable 30, and the gas generating device is composed of a cylindrical combustion chamber front cavity 19, a cylindrical combustion chamber rear cavity 20, a porous bell-shaped flame, The fuel injector 22, the fuel supply device 23, the igniter 26, the storage battery 31, the central processing controller 32, the pressure sensor 34 and the vaporization heater 24 are formed, the air holes on the porous bell-shaped flame holder 21 are gradually enlarged from the top of the porous bell-shaped flame holder 21 to the bottom of the porous bell-shaped flame holder 21, the fuel injector 22 is arranged on the center of the top of the porous bell-shaped flame holder 21 in the cylindrical combustion chamber, the fuel injector 22 is communicated with the fuel supply device 23 outside the machine body 1, the vaporization heater 24 is arranged on a pipeline at the nozzle of the fuel injector 22, the igniter 26 is arranged at the bottom of the porous bell-shaped flame holder 21 at the nozzle 27 of the cylindrical combustion chamber rear chamber 20, the pressure sensor 34 is arranged on the combustion chamber front chamber 19, and the fuel supply device 23, the igniter 26, the storage battery 31, the pressure sensor 34, A control motor stator 37 on the speed changing device 35 and a control device 25 on the fuel vaporization heater 24 are connected with a central processing controller 32 through a cable 30, a water sprayer 48 is arranged at the position of a combustion chamber air nozzle 27 and is communicated with the combustion chamber air nozzle 27, the other end of the water sprayer 48 is connected with a water supply device 51, an arc movable chamber wall 49 is arranged on the circumference of a working wheel chamber 14 at the position of an air inlet 17 of a working wheel chamber 14 in the machine body 1, one end of the arc movable chamber wall 49 is connected with a fixed chamber wall through a movable shaft 50, the other end of the arc movable chamber wall is arranged at the position of the air inlet 17 of the working wheel chamber 14 and is provided with a regulating device 47, a combustion chamber air inlet 29 is arranged on a combustion chamber front chamber 19, a combustion chamber air nozzle 27 is arranged on a combustion chamber rear chamber 20, an air outlet 16 of the combustion wheel chamber 13 is communicated with the combustion chamber air inlet, the air inlet 15 of the air compression wheel cavity 13 and the air outlet 18 of the power wheel cavity 14 are communicated with the atmosphere.

The basic working principle is as follows: when the air compressor works, the central processing unit 32 locks any two gears in the planetary gear set on the speed change device 35 through the locking mechanism on the speed change device 35, the storage battery 31 is connected with a circuit of a control motor stator 37 on the speed change device 35, the control motor rotor 36 is started to output mechanical energy, the wheel shaft 3 is driven by the speed change device 35 to drive the air compressing wheel body 2, the two air compressing rotors, the acting wheel body 8 and the two acting rotors to rotate at high speed, air in the movable vane chamber 5 in the first air compressing rotor is thrown away from the first air compressing rotor by the driven vane 4 under the action of centrifugal force, negative pressure is generated in the movable vane chamber 5 of the first air compressing rotor, air in the inner chamber of the first air compressing rotor enters the movable vane chamber 5 of the first air compressing rotor under the action of atmospheric pressure, the air pressure in the inner chamber of the first air compressing rotor is reduced, the air continuously enters the inner chamber of the first, along with the continuous rotation of the first compressed air rotor, the air in the movable blade space 5 in the first compressed air rotor is continuously thrown away from the first compressed air rotor by the first compressed air rotor movable blades 4 and is collided on the compressed air stator blades 6 to be decelerated and boosted, the air after being decelerated and boosted enters the compressed air stator blades space 7 to be continuously decelerated and boosted to form compressed air, the compressed air in the compressed air stator blades space 7 overflows out of the compressed air stator along with the compressed air stator under the pressure and inertia, the second compressed air rotor movable blades 4 'of the compressed air overflowing the compressed air stator space 7 and rotating at a high speed outside the compressed air stator are swept into the second compressed air rotor movable blades space 5' to rotate at a high speed along with the second compressed air rotor, the compressed air in the second compressed air rotor movable blade space 5 'is simultaneously rotated at a high speed along with the second compressed air rotor and is simultaneously applied by the second compressed air rotor to generate a larger centrifugal force, and the compressed air in the second compressed air rotor movable blade space 5' is thrown away from the second compressed air rotor at a higher speed by the second compressed air rotor and then is collided The compressed air which is impacted on the wall of the gas compression wheel cavity 13 and is subjected to speed reduction and pressure increase again enters the gas outlet 16 of the gas compression wheel cavity 13 along with the rotation of a second gas compression rotor, the compressed air in the gas outlet 16 of the gas compression wheel cavity 13 enters the front chamber 19 of the combustion chamber through the gas inlet 29 of the combustion chamber on the gas generator, the compressed air in the front chamber 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear chamber 20 of the combustion chamber, the air holes on the flame stabilizer 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed gas in the flame stabilizer 21 is characterized in that the flow rate at the top is relatively slow, the flow rate at the bottom of the flame stabilizer 21 is relatively fast, and when gas fuels such as hydrogen, natural gas, coal gas, methane and the like are used, the gas fuel enters the fuel supply device 23 into the fuel injector 22 and is sprayed from the nozzle of the fuel injector 22 into the top of the flame stabilizer 21 to be When liquid fuel with poor volatility, such as gasoline, kerosene, alcohol, diesel oil and the like, is used, the liquid fuel can be directly pressurized by the fuel supply device 23 and then sprayed into the top of the flame holder 21 in an atomized manner at a high speed through the fuel injector 22 to be mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, and the central processing unit can also provide high-frequency electromagnetic pulse waves to the fuel vaporization heater 24 through the fuel vaporizer control device 25 to heat a pipeline at the nozzle of the fuel injector 22, fuel is sprayed into the top of the flame holder 21 in a vaporized form at a high speed in the fuel injector 22 and is mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is short for being called high-energy gas and is sprayed into the air inlet 17 of the working wheel cavity 14 at a high speed through the air nozzle 27 of the combustion chamber, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle to impact the movable blades 9 on the first working rotor to drive the first working rotor to rotate, when the high-energy gas impacts the first working rotor blades 9, partial energy is converted into rotating mechanical energy to reduce the flow speed, the high-energy, the high-energy gas after decompression expansion in the movable blade space 10 of the first working rotor is sprayed into the inner cavity of the first working rotor through the inner opening of the movable blade space 10 of the first working rotor in a certain reverse tangential angle and in a reverse working wheel body 8 rotating direction to impact the stationary blade 11 on the working stator to generate a strong reverse thrust to push the first working rotor to drive the working wheel body 8 to rotate together, the high-energy gas after impacting the stationary blade 11 of the working stator to do work is reduced in speed and slowed down again, the high-energy gas after impacting the stationary blade 11 of the working stator enters the movable blade space 12 of the working stator to continue to be expanded and decompressed, the high-energy gas after expansion and decompression is sprayed out from the lower opening of the stationary blade space 12 of the working stator at a high speed to push the movable blade 9 'of the second working rotor in the inner cavity of the working stator again to do work, the high-energy gas after secondary work is reduced again and enters the movable blade space 10' of the second working rotor, and the movable blade gas in the space 10 'of the second working rotor expands again and decompresses and reversely decompresses from the movable blade 10' of the second rotor The working wheel body 8 is sprayed out in the rotating direction to provide a reverse thrust for the second working rotor again to push the second working rotor to rotate for working, and the waste gas with certain residual pressure after working is discharged through the exhaust port 18 of the working wheel cavity 14. In operation, the cpu 32 may apply a forward or reverse current to the stator 37 of the control motor, apply a forward or reverse force to the rotor 36 of the control motor, i.e., the big gear ring of the planetary gear set in the transmission 35, so that the working rotor outputs power to the compressor rotor through the wheel shaft 3 via the transmission 35 in a variable transmission ratio mode, and when the working rotor is decelerated due to the rotation speed, apply a forward or reverse current to the stator 37 of the control motor, i.e., the big gear ring of the planetary gear set in the transmission 35, so as to output power to the compressor rotor in a hybrid mode, or lock the sun gear and the planetary gear of the planetary gear set in the transmission 35, drive the compressor rotor and the working rotor to rotate by controlling the motor, use the control motor as a starter, and drive the working rotor to control the motor to generate power to output power to the electrical equipment or to output power to the battery while driving the compressor rotor Charging, in operation, when needing shaft 3 output great torsion, can adjust the aperture of activity chamber wall 49 through regulation and control device 47, increase the aperture of activity chamber wall 49, let more high temperature high pressure gas get into doing work wheel chamber 14, make high temperature high pressure gas promote more doing work rotor movable blades 9 simultaneously in order to produce bigger torsion, when needs reduce torsion, can carry out the callback to activity chamber wall 49 through regulation and control device 47 equally, reduce the aperture of activity chamber wall 49, reduce high temperature high pressure gas and get into doing work wheel chamber 14, let high temperature high pressure gas promote less doing work rotor movable blades 9 in order to reduce the torsion of output. When the high-power working is carried out, the water sprayer 48 at the air jet 27 of the combustion chamber can spray a proper amount of water mist into the working wheel cavity 14 according to the temperature in the working wheel cavity 14, so that a large amount of water vapor can be generated while the temperature in the working wheel cavity 14 is reduced, the pressure in the working wheel cavity 14 is further improved, the central processor 32 calculates and processes the information of the pressure and the temperature of the gas, the combustible mixed gas and the compressed air, the rotating speed of the working rotor and the air compressing rotor and the like collected by various sensors and outputs instructions to various actuators such as the igniter 26, the fuel supply device 23, the water sprayer 48, the regulating device 47 on the movable cavity wall 49, the control motor on the speed changing device 35 and the like to timely regulate the fuel spraying amount, the spraying amount of the atomized water, the opening degree of the movable cavity wall 49 and the rotating speed ratio of the working rotor and the air compressing rotor, so that the, The pressure of the compressed air, the rotation speed of the wheel shaft 3 and the like are all kept at the optimal values to ensure that the engine works in the optimal state.

Fig. 10, 11, and 12 show a fourth embodiment of this embodiment together, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is a basic power unit also composed of components such as a machine body 1, a wheel shaft 3, an air compressing device, an acting device, and a gas generating device, where the air compressing device is composed of three roller-shaped air compressing rotors with different diameters and two cylindrical air compressing stators with different diameters, the axial lengths of the three roller-shaped air compressing rotors with different diameters and the two cylindrical air compressing stators with different diameters are the same, the three roller-shaped air compressing rotors with different diameters are sequentially sleeved on the same axis according to the diameters, one end of each of the three roller-shaped air compressing rotors is fixed on the side surface of the air compressing wheel body 2, and the other end of each of the two cylindrical air compressing rotors with different diameters is sequentially sleeved between the three roller-shaped air compressing rotors according to the diameters and is located on the side surface of the corresponding air compressing wheel body 2 The surface keeps a small airtight gap, the other end is installed and fixed on the inner wall of the air compressing wheel cavity 13 opposite to the side of the air compressing wheel body 2, the two cylindrical air compressing stators with different diameters respectively keep a small sealing gap with the inner and outer adjacent cylindrical air compressing rotors, the acting device is composed of three cylindrical acting rotors with different diameters and two cylindrical acting stators with different diameters, the axial lengths of the three cylindrical acting rotors with different diameters and the two cylindrical acting stators with different diameters are the same, the three cylindrical acting rotors with different diameters are sequentially sleeved on the same axis according to the diameters, one end of the three cylindrical acting rotors is fixed on the side surface of the acting wheel body 8, the other end of the other cylindrical acting stators with different diameters is sequentially sleeved between the three cylindrical acting rotors according to the diameters and keeps a small airtight gap with the corresponding side surface of the acting wheel body 8, and one end of the two cylindrical acting stators with different diameters are sequentially sleeved between the three cylindrical acting rotors according to the diameters The gas generator comprises a cylindrical combustion chamber front chamber 19, a cylindrical combustion chamber rear chamber 20, a porous bell-shaped flame stabilizer 21, a fuel injector 22, a fuel supply device 23 and an igniter 26, wherein the gas holes in the porous bell-shaped flame stabilizer 21 are gradually enlarged from the top of the porous bell-shaped flame stabilizer 21 to the bottom of the porous bell-shaped flame stabilizer 21 Portion, fuel injector 22 is installed in the cylindrical combustion chamber on the porous bell-shaped flame holder 21 top center, fuel injector 22 communicates with the outer fuel feeding device 23 of organism 1, cavity 20 air jet 27 department porous bell-shaped flame holder 21 bottom behind the cylindrical combustion chamber installs some firearms 26, there is combustion chamber air inlet 29 on the cavity 19 before the combustion chamber, there is combustion chamber air jet 27 on the cavity 20 behind the combustion chamber, compressor wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, combustion chamber air jet 27 communicates with working wheel chamber 14 air inlet 17, compressor wheel chamber 13 air inlet 15 and working wheel chamber 14 gas vent 18 communicate with each other with the atmosphere.

The basic working principle is as follows: when the pneumatic rotor works, the starting device 52 outputs mechanical energy to drive the pneumatic wheel body 2, the three pneumatic rotors, the working wheel body 8 and the three working rotors to rotate at high speed through the wheel shaft 3, air in the movable blade space 5 of the first pneumatic rotor is thrown away from the first pneumatic rotor by the driven blade 4 under the action of centrifugal force, negative pressure is generated in the movable blade space 5 of the first pneumatic rotor, air in the inner cavity of the first pneumatic rotor enters the movable blade space 5 of the first pneumatic rotor under the action of atmospheric pressure, the air pressure in the inner cavity of the first pneumatic rotor is reduced at the moment, the air continuously enters the inner cavity of the first pneumatic rotor through the air inlet 15 of the pneumatic wheel cavity 13 under the action of atmospheric pressure, along with the continuous rotation of the first pneumatic rotor, the air in the movable blade space 5 of the first pneumatic rotor is continuously thrown away from the first pneumatic rotor by the movable blade 4 of the first pneumatic rotor and impacts on the static pneumatic stator blade 6 to decelerate and, the air after speed reduction and pressure increase enters the stator blade space 7 to continue speed reduction and pressure expansion to form compressed air, the compressed air in the stator blade space 7 overflows towards the outside of the stator along with the stator under the pressure and inertia, the compressed air overflowing the stator blade space 7 is swept into the second rotor blade space 5 'by the second rotor blade 4' rotating at high speed along with the rotor rotating at high speed, the compressed air in the second rotor blade space 5 'is exerted by the second rotor to generate larger centrifugal force along with the high-speed rotation of the second rotor, the compressed air in the second rotor blade space 5' is thrown away from the second rotor at higher speed by the second rotor and then impacts the second rotor blade 6 'to reduce and increase the pressure again, the compressed air after speed reduction and pressure increase enters the second stator blade space 7' to cohere and increase the pressure, the compressed air gathered in the second compressor stator blade space 7 'overflows from the outer port of the second compressor stator blade space 7' under the action of inertia and pressure, then is swept into a third compressor rotor blade space 5 "by a third compressor rotor blade 4" rotating at a high speed outside the second compressor stator and rotates at a high speed along with a third compressor rotor, the compressed air in the third compressor rotor blade space 5 "rotates at a high speed along with the third compressor rotor and is applied by the third compressor rotor to generate a larger centrifugal force, the compressed air in the third compressor rotor blade space 5" is thrown away from the third compressor rotor at a higher speed by the third compressor rotor and collides with the wall of the compressor wheel cavity 13 to reduce the speed and increase the pressure again, the compressed air after reducing the speed and increasing the pressure again enters the air outlet 16 of the compressor wheel cavity 13 along with the rotation of the third compressor rotor, and the compressed air in the air outlet 16 of the compressor wheel cavity 13 enters the combustion chamber front cavity 19 through the combustion chamber air inlet 29 on the gas generator, the compressed air in the front chamber 19 of the combustion chamber firstly pushes the flame holder 21 and the fuel injector 22 to slide towards the rear chamber 20 together, the flame holder 21 rotates around the flame holder 21 in a spiral shape and then passes through the air holes of the flame holder 21 to enter the rear chamber 20 of the combustion chamber, the flame holder 21 is overlapped in a retracting layer, the speed of the compressed air passing through the flame holder 21 is reduced, the flow rate of the compressed air in the flame holder 21 is relatively low, when gas fuel such as hydrogen, natural gas, coal gas, methane and the like is used, the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected into the flame holder 21 from the nozzle of the fuel injector 22 to be mixed with the compressed air in the flame holder 21 to form combustible compressed mixed air, the combustible compressed mixed air is ignited by electric sparks released by the igniter 26, the ignited combustible compressed mixed air is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure fuel gas, when gasoline is used, When liquid fuel with poor volatility such as kerosene, alcohol, diesel oil and the like is used, the liquid fuel is directly pressurized by a fuel supply device 23 and then is atomized by a fuel injector 22 and is sprayed into the inner part of a flame holder 21 at a high speed to be mixed with compressed air in the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by an igniter 26, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is short of high-energy gas, the high-temperature and high-pressure gas rapidly pushes the flame holder 21 and the fuel injector 22 to slide towards a combustion chamber front cavity 19 and simultaneously is sprayed into an air inlet 17 of a working wheel cavity 14 at a high speed through a combustion chamber air nozzle 27, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle to impact a movable blade 9 on a first working rotor to push the first working, the high-energy gas after the flow velocity is slowed down enters the first working rotor movable vane space 10 to continue to expand, the high-energy gas after the pressure reduction expansion in the first working rotor movable vane space 10 is sprayed into the inner cavity of the first working rotor through the inner opening of the first working rotor movable vane space 10 in a certain reverse tangential angle and against the rotating direction of the working wheel body 8 to impact the stationary vanes 11 on the working stator to generate a strong reverse thrust to push the first working rotor again to drive the working wheel body 8 to rotate together, the high-energy gas after the power application from the stationary vanes 11 of the working stator is slowed down again, the high-energy gas after the power application from the stationary vanes 11 of the working stator enters the stationary vanes 12 of the working stator to continue to expand and reduce the pressure, the high-energy gas after the expansion and pressure reduction is sprayed out from the lower opening of the stationary vanes 12 of the working stator at a high speed to push the second working movable vane 9 'in the inner cavity of the working stator again to work, the high-energy after the power application again is reduced and enters the second working rotor movable vane space 10' of the working rotor, the high-energy gas in the second working rotor movable blade space 10 'expands again to reduce pressure, and is ejected from the second working rotor movable blade space 10' against the rotation direction of the working wheel body 8 to provide a reverse thrust to push the second working rotor to rotate to work, the high-energy gas after being decompressed and expanded in the second working rotor movable blade space 10 'is ejected again into the inner cavity of the second working rotor through the inner opening of the second working rotor movable blade space 10' against the rotation direction of the working wheel body 8 at a certain reverse tangential angle to impact the stationary blade 11 'on the second working stator to generate a reverse thrust to push the second working rotor to drive the working wheel body 8 to rotate to work, the energy of the high-energy gas after impacting the stationary blade 11' of the second working stator is slowed down again, the high-energy gas after impacting the stationary blade 11 'of the second working stator enters the second working stator blade space 12' to expand and reduce pressure continuously, the high-energy gas after the secondary expansion and pressure reduction is sprayed out at high speed from the lower opening of the stationary blade space 12 ' of the second working stator again to push the third working rotor moving blade 9 ' in the inner cavity of the second working stator to work, the energy of the high-energy gas after the secondary working is reduced again and enters the movable blade space 10 ' of the third working rotor, the high-energy gas in the movable blade space 10 ' of the third working rotor passes through the inner opening of the movable blade space 10 ' of the third working rotor and is sprayed into the inner cavity of the third working rotor again in a certain reverse tangential angle, namely in the direction opposite to the rotation direction of the working wheel body 8, and then a reverse thrust is generated again to push the third working rotor to drive the working wheel body 8 to rotate to work, the waste gas with a certain residual pressure after the working in the inner cavity of the third working rotor is discharged from the exhaust opening 18 of the working wheel cavity 14, during the work, when the high-power output is needed, the fuel injector 22 sprays more fuel into the flame stabilizer 21, the temperature of the rear cavity 20 of the combustion, the gas with increased pressure pushes the flame holder 21 and the fuel injector 22 to slide towards the combustion chamber front cavity 19, the flame holder 21 overlapped together is stretched, the resistance of the compressed air passing through the flame holder 21 is reduced, the flow rate is increased, the compressed air entering the combustion chamber rear cavity 20 is increased, and the combustion in the combustion chamber rear cavity 20 is more violent and more sufficient.

Fig. 13, 14 and 15 together show a fifth embodiment of the solution, which can be seen from the figures,

the novel turbine engine shown in the embodiment is also a basic power unit formed by components such as a machine body 1, a wheel shaft 3, an air compressing device, an acting device and a gas generating device, wherein the air compressing device is formed by four roller-shaped air compressing rotors with different diameters and three cylindrical air compressing stators with different diameters, the respective axial lengths of the four roller-shaped air compressing rotors with different diameters and the three cylindrical air compressing stators with different diameters are different, the axial lengths of the four roller-shaped air compressing rotors with different diameters are gradually reduced from the innermost layer to the outer layer in a gradually-decreasing manner or are gradually increased from the outermost layer to the inner layer in a gradually-increasing manner, the four roller-shaped air compressing rotors with different diameters are sequentially sleeved on the same axis according to the diameters, one ends of the four roller-shaped air compressing rotors are fixed on the side surface of an air compressing wheel body 2, the other ends of the four roller-shaped air compressing rotors are sequentially sleeved with the corresponding air compressing wheel cavity 13 The side surface of the air compressing wheel body 2 keeps a tiny airtight gap, the other end of the air compressing wheel body is fixedly arranged on the inner wall of an air compressing wheel cavity 13 opposite to the side surface of the air compressing wheel body 2, three cylindrical air compressing stators with different diameters respectively keep tiny airtight gaps with an inner adjacent roller-shaped air compressing rotor and an outer adjacent roller-shaped air compressing rotor, the acting device is composed of four roller-shaped acting rotors with different diameters and three cylindrical acting stators with different diameters, the axial lengths of the four roller-shaped acting rotors with different diameters and the three cylindrical acting stators with different diameters are different, the axial lengths of the four roller-shaped acting rotors are sequentially lengthened from the outermost layer to the inner layer, the four roller-shaped acting rotors with different diameters are sequentially sleeved on the same axis according to the diameter, one end of the four roller-acting rotors is fixed on the side surface of the acting wheel body 8, and the other, one end of each of the three cylindrical working stators with different diameters is sequentially sleeved between the four roller-shaped working rotors according to the diameter and keeps a tiny airtight gap with the side surface of the corresponding working wheel body 8, the other end of each cylindrical working stator is fixedly arranged on the inner wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8, the three cylindrical working stators respectively keep tiny sealing gaps with the inner and the outer adjacent roller-shaped working rotors, the wheel shaft 3 is arranged on the centers of the working wheel body 8 and the air compression wheel body 2, the wheel shaft 3 is provided with a starting device 52, a supporting bearing and a sealing device 53, the center of the air compression wheel cavity 13 is provided with an air inlet 15, the center of the working wheel cavity 14 is provided with an air outlet 18, the circumference of the air compression wheel cavity 13 is provided with an air outlet 16, the circumference of the working wheel cavity 14 is provided with an air inlet 17, and the circumference wall of the working wheel cavity, the gas generator is characterized in that a gas blocking block 41 with radian larger than the opening radian of the gas inlet 17 is arranged on a stator corresponding to the gas inlet 17, the gas generator is composed of a cylindrical combustion chamber front cavity 19, a cylindrical combustion chamber rear cavity 20, a porous bell-shaped flame holder 21, a fuel injector 22, a fuel supply device 23 and an igniter 26, gas holes in the porous bell-shaped flame holder 21 are gradually enlarged from the top of the porous bell-shaped flame holder 21 to the bottom of the porous bell-shaped flame holder 21, the fuel injector 22 is arranged on the center of the top of the porous bell-shaped flame holder 21 in the cylindrical combustion chamber, the fuel injector 22 is communicated with the fuel supply device 23 outside the machine body 1, the igniter 26 is arranged at the bottom of the porous bell-shaped flame holder 21 at the gas outlet 27 of the cylindrical combustion chamber rear cavity 20, a combustion chamber gas inlet 29 is arranged on the combustion chamber front cavity 19, and a combustion chamber gas outlet 27 is arranged on the combustion chamber, the air outlet 16 of the air compressor wheel cavity 13 is communicated with the air inlet 29 of the combustion chamber, the air outlet 27 of the combustion chamber is communicated with the air inlet 17 of the working wheel cavity 14, and the air inlet 15 of the air compressor wheel cavity 13 and the air outlet 18 of the working wheel cavity 14 are communicated with the atmosphere.

The basic working principle is as follows: the working mode can be two, namely a mode I; the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2, the four air compressing rotors, the acting wheel body 8 and the four acting rotors to rotate at high speed through the wheel shaft 3, air in the movable blade space 5 of the first air compressing rotor is thrown away from the first air compressing rotor by the driven blade 4 under the action of centrifugal force, negative pressure is generated in the movable blade space 5 of the first air compressing rotor, air in the inner cavity of the first air compressing rotor enters the first air compressing rotor space 5 under the action of atmospheric pressure, at the moment, the air pressure in the inner cavity of the first air compressing rotor is reduced, the air continuously enters the inner cavity of the first air compressing rotor through the air inlet 15 of the air compressing wheel cavity 13 under the action of atmospheric pressure, along with the continuous rotation of the first air compressing rotor, the air in the movable blade space 5 of the first air compressing rotor is continuously thrown away from the first air compressing rotor by the movable blade 4 of the first air compressing rotor and impacts the static blade 6 of the first air compressing rotor for speed reduction and pressure increase, the air after speed reduction and pressure increase is continuously enters the, the compressed air in the first stator vane space 7 overflows outside the stator along the stator under pressure and inertia, the compressed air overflowing the stator space 7 is swept into the second rotor blade space 5 ' by the second rotor blades 4 ' rotating at high speed outside the first stator blade space and rotates at high speed along with the second rotor, the compressed air in the second rotor blade space 5 ' is exerted by the second rotor while rotating at high speed along with the second rotor, the compressed air in the second rotor blade space 5 ' is thrown away from the second rotor at higher speed by the second rotor and then impacts on the second stator vane 6 ' to decelerate and boost again, the compressed air after decelerating and boosting enters the second stator vane space 7 ' to concentrate and boost, the compressed air gathered in the second stator vane space 7 ' is overflowed from the second stator vane space 7 ' by the second stator vane space 7 ' under inertia and pressure action The third compressed air rotor blade 4 'rotating at high speed outside the two compressed air stators sweeps into the third compressed air rotor blade space 5' and rotates at high speed along with the third compressed air rotor, the compressed air in the third compressed air rotor blade space 5 'is exerted by the third compressed air rotor to generate larger centrifugal force while rotating at high speed along with the third compressed air rotor, the compressed air in the third compressed air rotor blade space 5' is thrown away from the third compressed air rotor at higher speed by the third compressed air rotor and then collides with the third compressed air stator blade 6 'to decelerate and boost again, the compressed air after decelerating and boosting enters the third compressed air stator blade space 7' to be condensed and boosted, the compressed air condensed in the third compressed air stator blade space 7 'overflows from an outer port of the third compressed air stator blade space 7' under the actions of inertia and pressure and then is swept into the fourth compressed air rotor blade space 5V by the fourth compressed air rotor blade 4V rotating at high speed outside the third compressed air stator blade space 5V to rotate along with the fourth compressed air rotor at high speed, compressed air in the space 5v between the movable blades of the fourth air compressor rotor is thrown away from the fourth air compressor rotor at a higher speed by the fourth air compressor rotor and then collides with the wall of the air compressor cavity 13 to reduce the speed and increase the pressure again, the compressed air after reducing the speed and increasing the pressure again enters the air outlet 16 of the air compressor cavity 13 along with the rotation of the fourth air compressor rotor, the compressed air in the air outlet 16 of the air compressor cavity 13 enters the front combustion chamber 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front combustion chamber 19 firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear combustion chamber 20 of the combustion chamber, and the flow rate of the compressed air in the bottom of the flame stabilizer 21 is relatively high, the flow rate of the compressed gas in the top of the flame holder 21 is relatively slow, when using gas fuel such as hydrogen, natural gas, coal gas, biogas, etc., the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected into the flame holder 21 from the nozzle of the fuel injector 22 to be mixed with the compressed gas in the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26, the ignited combustible high-compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel, etc., the liquid fuel is directly pressurized by the fuel supply device 23 and then is injected into the flame holder 21 at high speed through the fuel injector 22 to be mixed with the compressed gas in the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is short for being high-energy gas and is rapidly sprayed into an air inlet 17 of a working wheel cavity 14 through an air nozzle 27 of a combustion chamber at a high speed, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle and impacts movable blades 9 on a first working rotor to drive the first working rotor to rotate, when the high-energy gas impacts the movable blades 9 of the first working rotor, part of energy is converted into rotary mechanical energy to reduce the flow velocity of the rotary mechanical energy, the high-energy gas enters a movable blade space 10 of the first working rotor to continue to expand after the flow velocity of the high-energy gas is slowed down and is sprayed into stationary blades 11 on the working stator in an inner cavity of the first working rotor through an inner port 10 of the movable blade space of the first working rotor at a certain reverse tangential angle and in the rotating direction of the working wheel body 8 to generate strong reverse thrust to The high-energy gas after impacting the stator blades 11 of the working stator to do work is reduced in speed again, the high-energy gas after impacting the stator blades 11 of the working stator to do work enters the stator blade space 12 of the working stator to continue to expand and reduce the pressure, the high-energy gas after expanding and reducing the pressure is ejected from the lower opening of the stator blade space 12 of the working stator at a high speed to push the movable blades 9 'of the second working rotor in the inner cavity of the working stator again to do work, the high-energy gas after doing work again is reduced in energy and enters the movable blades 10' of the second working rotor again, the high-energy gas in the movable blades 10 'of the second working rotor expands and reduces the pressure again and is ejected from the movable blades 10' of the second working rotor in the direction opposite to the rotating direction of the working rotor 8 to provide a reverse thrust to push the second working rotor to do work again, and the high-energy gas after reducing and expanding in the movable blades 10 'of the second working rotor is ejected from the inner opening of the movable blades 10' of the second working rotor in the direction opposite to provide a reverse tangential angle to push the rotating direction of the second working rotor 8 to do work The static blade 11 ' impacting the second working stator in the cavity generates a reverse thrust to push the second working rotor again to drive the working wheel body 8 to rotate and work, the high-energy gas energy impacting the second working stator static blade 11 ' to work is reduced in speed again, the high-energy gas impacting the second working stator static blade 11 ' enters the second working stator static blade space 12 ' to continue to expand and reduce the pressure, the high-energy gas expanded and reduced in pressure again is sprayed out at high speed from the lower opening of the second working stator static blade space 12 ' again to push the third working rotor movable blade 9 ' in the inner cavity of the second working stator to work, the high-energy gas energy exerted to work again is reduced and enters the third working rotor movable blade space 10 ' and the high-energy gas in the third working rotor movable blade space 10 ' is sprayed into the third working rotor movable blade space 10 ' through the inner opening of the third working rotor movable blade space 10 ' in a reverse tangential angle, namely, which is the reverse working rotor working 8 rotating direction to generate a reverse thrust to generate a reverse static wheel body 11 ' in the third working rotor inner cavity The thrust pushes the third working rotor again to drive the working wheel body 8 to rotate together to work, the energy of the high-energy gas impacting the third working stator blade 11 'to work is reduced again in speed and then slowed down, the high-energy gas impacting the third working stator blade 11' enters the third working stator blade chamber 12 'to continue to expand and reduce the pressure, the high-energy gas expanded and reduced in pressure again is ejected at high speed from the lower opening of the third working stator blade chamber 12' to push the fourth working rotor movable blade 9v in the inner chamber of the third working stator to work, the energy of the high-energy gas working again is reduced and enters the fourth working rotor movable blade chamber 10v, the high-energy gas in the fourth working rotor movable blade chamber 10v is ejected again in the inner chamber of the fourth working rotor blade chamber through the inner opening of the fourth working rotor movable blade chamber 10v and then again with a certain reverse tangential angle, namely the reverse working wheel body 8 rotating direction is ejected again to generate a reverse thrust to drive the fourth working rotor 8 to work again to work and drive the fourth working rotor to work together to work, high-energy gas which is repeatedly applied for multiple times in the inner cavity of the fourth acting rotor becomes waste gas with extremely low pressure and is discharged through the exhaust port 18 of the acting wheel cavity 14, and the working mode is II; when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel injector 22 nozzle from the fuel injector 22 and is injected into the flame holder 21 to be mixed with the compressed gas in the flame holder 21 to form combustible compressed mixed gas, the combustible mixed gas enters the first working rotor movable blade compartment 10 through the working wheel cavity air inlet 17, the combustible mixed gas in the first working rotor movable blade compartment 10 at the working wheel cavity air inlet 17 cannot be injected from the lower opening of the first working rotor movable blade compartment 10 due to the corresponding stator arc-shaped choke block 41 at the working wheel cavity air inlet 17, when the combustible mixed gas in the first working rotor movable blade compartment 10 rotates to the booster igniter 29 in front of the working wheel cavity air inlet 17 along with the first working rotor, the booster igniter 29 is ignited by the booster igniter 29 to burn and release heat energy to generate high temperature and high pressure, when using gasoline, kerosene, methane and the like, When the liquid fuel with poor volatility such as alcohol, diesel oil, etc. is pressurized by the fuel supply device 23, the liquid fuel is atomized by the fuel injector 22 and sprayed into the inner portion of the flame holder 21 at a high speed to form a combustible compressed mixed gas, the combustible mixed gas enters the first working rotor movable vane compartment 10 through the working wheel cavity air inlet 17, similarly, because the corresponding stator arc-shaped air blocking block 41 is arranged at the working wheel cavity air inlet 17, the combustible mixed gas in the first working rotor movable vane compartment 10 at the working wheel cavity air inlet 17 cannot be sprayed out from the lower opening of the first working rotor movable vane compartment 10, when the combustible mixed gas in the first working rotor movable vane compartment 10 rotates to the booster igniter 29 in front of the working wheel cavity air inlet 17 along with the first working rotor, the booster igniter 29 ignites to release heat energy to generate high-temperature high-pressure gas, the high-temperature high-pressure gas is abbreviated as high-energy gas, and rapidly rotates in a certain reverse tangential angle 8 through the inner opening of the first working rotor movable vane compartment 10 to perform work reversely at a certain tangential angle 8 The high-energy gas which is sprayed into the inner cavity of the first working rotor in the direction to impact the stator blade 11 on the working stator generates a strong reverse thrust to push the first working rotor again to drive the working wheel body 8 to rotate together, the high-energy gas energy which impacts the stator blade 11 to do work is reduced in speed again, the high-energy gas which impacts the stator blade 11 to do work enters the stator blade space 12 of the working stator to continue to expand and reduce the pressure, the high-energy gas which is expanded and reduced in pressure is sprayed out from the lower opening of the stator blade space 12 of the working stator at a high speed to push the second working rotor blade 9 'in the inner cavity of the working stator again to do work, the high-energy gas which does work again is reduced again and enters the second working rotor blade space 10', the high-energy gas in the second rotor blade space 10 'is expanded and reduced in pressure again and is sprayed out from the second working rotor blade space 10' against the rotating direction of the working wheel body 8 to provide a reverse thrust to the second working rotor to push the second working rotor to do work, the high-energy gas after decompression and expansion in the movable blade space 10 'of the second working rotor is sprayed into the inner cavity of the second working rotor through the inner opening of the movable blade space 10' of the second working rotor in a reverse direction of the rotation direction of the working wheel body 8 at a certain reverse tangential angle again to generate a reverse thrust to drive the second working rotor to drive the working wheel body 8 to work, the high-energy gas energy after impacting the stationary blade 11 'to work is reduced in speed again, the high-energy gas after impacting the stationary blade 11' of the second working stator enters the stationary blade space 12 'of the second working stator to continue to be expanded and decompressed, the high-energy gas after being expanded and decompressed again is sprayed out at a high speed again from the lower opening of the stationary blade space 12' of the second working stator to drive the third movable blade 9 'in the inner cavity of the second working stator to work, the high-energy gas after being decompressed again is reduced and enters the movable blade space 10' of the third working rotor, the high-energy gas in the third working rotor movable blade space 10 'is sprayed into the inner cavity of the third working rotor again through the inner opening of the third working rotor movable blade space 10' with a certain reverse tangential angle, namely, the reverse working rotor body 8 rotates to generate a reverse thrust to drive the third working rotor to drive the working wheel body 8 to rotate and work, the high-energy gas energy after impacting the third working stator blade 11 'to work is reduced in speed again and becomes slow, the high-energy gas after impacting the third working stator blade 11' enters the third working stator blade space 12 'to continue to expand and reduce the pressure, the high-energy gas after being expanded and reduced in pressure again is sprayed out at a high speed from the lower opening of the third working stator blade space 12' again to drive the fourth working movable blade rotor 9v in the inner cavity of the third working stator to work, the high-energy after being expanded and reduced again and enters the fourth working rotor movable blade space 10v, the high-energy gas in the movable vane space 10v of the fourth working rotor passes through the inner opening 10v of the movable vane space of the fourth working rotor and is sprayed into the inner cavity of the fourth working rotor again in a certain reverse tangential angle, namely, in the direction opposite to the rotation direction of the working vane body 8, and then a reverse thrust is generated again to push the fourth working rotor to drive the working vane body 8 to rotate and work, and the high-energy gas which is repeatedly used for multiple times in the inner cavity of the fourth working rotor becomes waste gas with extremely low pressure and is discharged through the exhaust port 18 of the working vane cavity 14.

Fig. 16, 17, and 18 collectively show a sixth embodiment of this embodiment, and it can be seen from the accompanying drawings that the novel turbine engine shown in this embodiment is also a basic power unit formed by a machine body 1, a wheel shaft 3, an air compressing device, an acting device, a gas generating device, and the like, where the air compressing device is formed by eight roller-shaped air compressing rotors and six cylindrical air compressing stators, the eight roller-shaped air compressing rotors are divided into two same groups of sequentially decreasing axial lengths and different diameters, the six cylindrical air compressing stators are divided into two same groups of sequentially decreasing axial lengths and different diameters, the two groups of roller-shaped air compressing rotors with different axial lengths are respectively sleeved and fixed on two sides of an air compressing wheel body 2 according to the diameters and are on the same axis with the wheel shaft 3, and the other ends of the groups maintain a small air-tight gap with the inner wall of an air compressing wheel cavity 13 corresponding to two sides of the, the two groups of cylindrical air compression stators with different axial lengths are respectively sleeved between eight roller-shaped air compression rotors on the two side faces of the air compression wheel body 2 in turn according to the diameter and keep small airtight gaps with the same axis of the eight roller-shaped air compression rotors on the two side faces of the air compression wheel body 2 and the two side faces of the air compression wheel body 2, the other ends of the groups of cylindrical air compression stators are respectively fixed on the inner walls of the air compression wheel cavities 13 corresponding to the two side faces of the air compression wheel body 2, the six cylindrical air compression stators respectively keep small airtight gaps with the respective inner and outer adjacent roller-shaped air compression rotors, the acting device consists of eight roller-shaped acting rotors and six cylindrical acting stators, the eight roller-shaped acting rotors are divided into two groups of same groups with gradually decreased axial lengths and different diameters, and the six cylindrical acting stators are divided into two groups of same groups with gradually decreased axial lengths and, the two groups of the roller-shaped working rotors with different axial lengths are respectively sleeved and fixed on two sides of the working wheel body 8 and on the same axial line with the wheel shaft 3 according to the diameter, the other end of each group keeps a tiny airtight gap with the inner wall of the working wheel cavity 14 corresponding to two sides of the working wheel body 8, the two groups of the cylindrical working stators with different axial lengths are respectively sleeved and arranged between the eight roller-shaped working rotors on two side surfaces of the working wheel body 8 according to the diameter and keep tiny airtight gaps with the same axial line of the eight roller-shaped working rotors on two side surfaces of the working wheel body 8 and with two side surfaces of the working wheel body 8, the other end of each group of the cylindrical working stators is respectively fixed on the inner wall of the working wheel cavity 14 corresponding to two side surfaces of the working wheel body 8, and the six cylindrical working stators respectively keep tiny airtight gaps with the inner and outer adjacent roller-shaped, the wheel shaft 3 is arranged on the centers of the working wheel body 8 and the air pressure wheel body 2, the outer machine body 1 of the air pressure wheel cavity 13 and the working wheel cavity 14 is provided with a radiating fin 39, the bearing seat is fixedly connected with the shell 1 through a sheet type reinforcing rib 58, the centers of two sides of the air pressure wheel cavity 13 are respectively provided with an air inlet 15, the centers of two sides of the working wheel cavity 14 are respectively provided with an air outlet 18, the circumference of the air pressure wheel cavity 13 is provided with an air outlet 16, the circumference of the working wheel cavity 14 is provided with an air inlet 17, the wheel shaft 3 is provided with a starting device 52, a support bearing and a sealing device 53, the gas generating device is composed of a cylindrical combustion chamber front cavity 19, a cylindrical combustion chamber rear cavity 20, a porous bell-shaped flame stabilizer 21, a fuel injector 22, a fuel supply device 23 and a sealing device 26, the air holes on the porous bell-shaped flame stabilizer 21 are gradually enlarged from the top of the porous bell-shaped, fuel injector 22 installs in the cylindrical combustion chamber on the porous bell-shaped flame holder 21 top center, fuel injector 22 communicates with the outer fuel feeding device 23 of organism 1, the porous bell-shaped flame holder 21 bottom in cavity 20 air jet 27 department is installed to the cylindrical combustion chamber back, there is combustion chamber air inlet 29 on the cavity 19 before the combustion chamber, there is combustion chamber air jet 27 on the cavity 20 behind the combustion chamber, compression wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, combustion chamber air jet 27 communicates with working wheel chamber 14 air inlet 17, compression wheel chamber 13 both sides air inlet 15 and working wheel chamber 14 both sides gas vent 18 communicate with each other with the atmosphere.

The basic working principle is as follows: when the air compressor works, the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2, the eight air compressing rotors on two side surfaces of the air compressing wheel body 2 and the eight working rotors on two side surfaces of the working wheel body 8 through the wheel shaft 3 to rotate at a high speed, air in the first air compressing rotor movable vane rooms 5 with the same diameter on two side surfaces of the air compressing wheel body 2 is thrown away from the first air compressing rotor by the driven vanes 4 under the action of centrifugal force, negative pressure is generated in the first air compressing rotor movable vane rooms 5, external air continuously enters the first air compressing rotor inner cavities on two sides of the air compressing wheel body 2 through the air inlets 15 on two sides of the air compressing wheel cavity 13 under the action of atmospheric pressure, the air in the first air compressing rotor inner cavities on two sides of the air compressing wheel body 2 is sucked into the first air compressing rotor movable vane rooms 5 on two sides of the air compressing wheel body 2 by the negative pressure in the first air compressing rotor movable vane rooms, the air in the first compressed air rotor movable vane rooms 5 on the two sides of the compressed air wheel body 2 continuously is thrown away from the first compressed air rotors on the two sides of the compressed air wheel body 2 by the first compressed air rotor movable vane rooms 4 on the two sides of the compressed air wheel body 2 and is impacted on the first compressed air stator vanes 6 on the two sides of the compressed air wheel body 2 to be decelerated and boosted, the air after deceleration and boosting respectively enters the first compressed air stator vane rooms 7 on the two sides of the compressed air wheel body 2 to be decelerated and boosted to form compressed air, the compressed air in the first compressed air stator vane rooms 7 on the two sides of the compressed air wheel body 2 flows out along the compressed air stators on the two sides of the compressed air wheel body 2 under the pressure and inertia, the compressed air overflowing from the compressed air stator rooms 7 is swept into the second compressed air rotor movable vane rooms 5 'on the two sides of the compressed air wheel body 2 by the second compressed air rotor movable vane rooms 5' on the two sides of the compressed air wheel body 2 to rotate at, compressed air in the second compressed air rotor movable blade spaces 5 'on two sides of the compressed air wheel body 2 is exerted by the second compressed air rotors on two sides of the compressed air wheel body 2 to generate larger centrifugal force, the compressed air in the second compressed air rotor movable blade spaces 5' on two sides of the compressed air wheel body 2 is thrown away from the second compressed air rotors on two sides of the compressed air wheel body 2 at a higher speed and then collides with the second compressed air stator blades 6 'on two sides of the compressed air wheel body 2 to decelerate and boost again, the compressed air after decelerating and boosting enters the second compressed air stator blade spaces 7' on two sides of the compressed air wheel body 2 to be concentrated and boosted, and the compressed air collected in the second compressed air stator blade spaces 7 'is swept into the third compressed air rotor 4' in the third compressed air rotor spaces 5 'on two sides of the compressed air wheel body 2 along with the first compressed air rotor blades 2 on two sides of the compressed air wheel body 2 after overflowing from the outer ports of the second compressed air stator blade spaces 7' on two sides of the compressed air wheel body 2 under the action of inertia and pressure The three-compressor rotor rotates at high speed, compressed air in the third compressor rotor movable blade spaces 5 ' on two sides of the compressor wheel body 2 is exerted by the third compressor rotors on two sides of the compressor wheel body 2 to generate larger centrifugal force, the compressed air in the third compressor rotor movable blade spaces 5 ' on two sides of the compressor wheel body 2 is thrown away from the third compressor rotors on two sides of the compressor wheel body 2 by the third compressor rotors at higher speed and then collides with the third compressor stator blades 6 ' on two sides of the compressor wheel body 2 to decelerate and boost again, the compressed air after decelerating and boosting enters the third compressor stator blade spaces 7 ' on two sides of the compressor wheel body 2 to be gathered and boosted, the compressed air gathered in the third compressor stator blade spaces 7 ' is swept into the fourth compressor rotor movable blade spaces 5v by the third compressor stator blades on two sides of the compressor wheel body 2 to rotate at high speed along with the fourth compressor rotor under the action of inertia and pressure, compressed air in the space 5v between the movable blades of the fourth compressor rotors on two sides of the compressor wheel body 2 is applied by the fourth compressor rotors to generate larger centrifugal force, the compressed air in the space 5v between the movable blades of the fourth compressor rotors on two sides of the compressor wheel body 2 is thrown away from the fourth compressor rotors at higher speed by the fourth compressor rotors and then collides with the wall of the compressor wheel cavity 13 to be decelerated and boosted again, the compressed air after being decelerated and boosted again enters the air outlet 16 of the compressor wheel cavity 13 along with the rotation of the fourth compressor rotors on two sides of the compressor wheel body 2, the compressed air in the air outlet 16 of the compressor wheel cavity 13 enters the front cavity 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front cavity 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear cavity 20 of the combustion chamber, and the compressed air in the bottom of the flame stabilizer, the flow rate of the compressed gas in the top of the flame holder 21 is relatively slow, when using gas fuel such as hydrogen, natural gas, coal gas, biogas, etc., the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected into the flame holder 21 from the nozzle of the fuel injector 22 to be mixed with the compressed gas in the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26, the ignited combustible high-compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel, etc., the liquid fuel is directly pressurized by the fuel supply device 23 and then is injected into the flame holder 21 at high speed through the fuel injector 22 to be mixed with the compressed gas in the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is short for being high-energy gas and is rapidly sprayed into the air inlet 17 of the working wheel cavity 14 through the air jet port 27 of the combustion chamber, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle and collides with the movable blades 9 on the first working rotors on two sides of the working wheel body 8 to push the first working rotors on two sides of the working wheel body 8 to rotate, when the high-energy gas collides with the movable blades 9 on the first working rotors on two sides of the working wheel body 8, partial energy is converted into rotary mechanical energy to reduce the flow speed of the high-energy gas, the high-energy gas after the flow speed of the high-energy gas is slowed down, the high-energy gas respectively enters the movable blades 10 of the first working rotors on two sides of the working wheel body 8 to be continuously sprayed into the movable blades 10 of the first working rotors on two sides of the working The stationary blades 11 impacting the working stators on the two sides of the working wheel body 8 in the inner cavities of the first working rotors on the two sides of the wheel body 8 generate a strong reverse thrust to push the first working rotors on the two sides of the working wheel body 8 to drive the working wheel body 8 to rotate together again, the energy of the high-energy gas after the two sides of the working wheel body 8 impact the working stator blades 11 to do work is reduced in speed again, the high-energy gas after the two sides of the working wheel body 8 impact the working stator blades 11 enters the working stator blade spaces 12 on the two sides of the working wheel body 8 to continue to expand and reduce the pressure, the high-energy gas after expansion and reduction is respectively ejected from the lower openings of the working stator blade spaces 12 on the two sides of the working wheel body 8 at a high speed to push the second working rotor blades 9 'in the inner cavities of the working stators on the two sides of the working wheel body 8 to do work again, and the energy of the high-energy after secondary work is reduced and enters the second working rotor blade spaces 10' on the two, the high-energy gas in the second working rotor movable vane space 10 ' on both sides of the working wheel body 8 expands again to reduce pressure and is ejected from the second working rotor movable vane space 10 ' on both sides of the working wheel body 8 against the rotation direction of the working wheel body 8 to provide a reverse thrust to the second working rotor on both sides of the working wheel body 8 again to push the second working rotor to do work, the high-energy gas which is expanded in the second working rotor movable vane space 10 ' on both sides of the working wheel body 8 is ejected from the inner opening of the second working rotor movable vane space 10 ' again against the rotation direction of the working wheel body 8 at a certain reverse tangential angle through the inner opening of the second working rotor movable vane space 10 ' to generate a reverse thrust to push the second working rotor again to drive the working wheel body 8 to do work, the high-energy which impacts the second stator vanes 11 ' on both sides of the working wheel body 8 to do work again, the high-energy reduces the speed and then enters the second stator vanes 12 ' to continue to do work Expanding and reducing the pressure, jetting out the high-energy gas after being expanded and reduced pressure again at high speed from the lower openings of the stationary blades 12 ' of the second working stators on the two sides of the working wheel body 8 to push the movable blades 9 ' of the third working rotor in the inner cavities of the second working stators on the two sides of the working wheel body 8 to work, reducing the energy of the high-energy gas after being worked again and entering the movable blades 10 ' of the third working rotor on the two sides of the working wheel body 8, jetting the high-energy gas in the movable blades 10 ' of the third working rotor on the two sides of the working wheel body 8 into the inner cavity of the third working rotor through the inner openings of the movable blades 10 ' of the third working rotor, and then jetting the high-energy gas in the inner cavity of the third working rotor by a certain reverse tangential angle, namely the reverse working wheel body 8 rotating direction, to generate a reverse thrust to push the third working rotor again to drive the working wheel body 8 to rotate to work, and then the gas after impacting the stationary blades 11 ' of the third working stator to work enters the stationary blades 11 ' of the third working stator to work to reduce the working stator on the working The high-energy gas after the secondary expansion and pressure reduction is sprayed out again at high speed from the lower opening of the 12' lower opening of the third working stator stationary blade space at the two sides of the working wheel body 8 to push the fourth working rotor movable blade 9v in the inner cavity of the third working stator to work, the energy of the high-energy gas after the secondary working is reduced again and enters the 10v inner opening of the fourth working rotor movable blade space at the two sides of the working wheel body 8, the high-energy gas in the 10v inner opening of the fourth working rotor movable blade space at the two sides of the working wheel body 8 is sprayed into the inner cavity of the fourth working rotor through the 10v inner opening of the fourth working rotor movable blade space again with a certain reverse tangential angle, namely the reverse working wheel body 8 rotating direction, and then a reverse thrust is generated again to push the fourth working rotor to drive the working wheel body 8 to rotate together to work, high-energy gas which is repeatedly applied for multiple times in the inner cavities of the fourth working rotors at the two sides of the working wheel body 8 becomes waste gas with extremely low pressure and is discharged through the exhaust ports 18 at the two sides of the working wheel cavity 14 respectively.

Fig. 15, 19 and 20 collectively show a seventh embodiment of the present invention, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is also a basic power unit formed by components such as the engine body 1, the wheel shaft 3, the air compressing device, the acting device, the gas generating device, the central processing unit 32, the battery pack 31, and the like, the air compressing device is formed by four roller-shaped air compressing rotors with different diameters and three cylindrical air compressing stators with different diameters, the respective axial lengths of the four roller-shaped air compressing rotors with different diameters and the three cylindrical air compressing stators with different diameters are different, the axial lengths thereof are gradually reduced from the innermost layer to the outside layer by layer, that is, the axial lengths thereof are gradually increased from the outermost layer to the inside layer by layer, the four roller-shaped air compressing rotors with different diameters are sequentially sleeved on the same axis according to the diameter, and one end thereof is fixed on the, the other end of the cylinder-shaped air compression stator with different diameters is sequentially sleeved among the four cylinder-shaped air compression rotors according to the diameter and keeps the micro air-tight gap with the side surface of the corresponding air compression wheel body 2, the other end of the cylinder-shaped air compression stator with different diameters is installed and fixed on the inner wall of the air compression wheel cavity 13 opposite to the side surface of the air compression wheel body 2, the cylinder-shaped air compression stators with different diameters respectively keep the micro sealing gap with the inner and the outer adjacent cylinder-shaped air compression rotors, the power applying device is composed of the four cylinder-shaped power applying rotors with different diameters and the three cylinder-shaped power applying stators with different diameters, the axial lengths of the four cylinder-shaped power applying rotors with different diameters and the three cylinder-shaped power applying stators with different diameters are different, the axial lengths of the four cylinder-shaped power applying rotors with different diameters are sequentially lengthened from the outermost layer to the inner layer, and the four cylinder-shaped power applying rotors, one end of each cylindrical working stator with different diameters is fixed on the side surface of the working wheel body 8, the other end of each cylindrical working stator with different diameters keeps a micro air-tight gap with the wall of the working wheel cavity 14 corresponding to the side surface of the working wheel body 8, one end of each cylindrical working stator with different diameters is sequentially sleeved between the four roller-shaped working rotors according to the diameter size and keeps the micro air-tight gap with the side surface of the corresponding working wheel body 8, the other end of each cylindrical working stator is fixed on the inner wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8, the three cylindrical working stators respectively keep the micro sealing gaps with the inner and the outer adjacent roller-shaped working rotors, the wheel shaft 3 is arranged on the centers of the working wheel body 8 and the air compressing wheel body 2, the air compressing wheel cavity 13 and the outer machine body 1 of the working wheel cavity 14 are provided with radiating fins 39, the wheel shaft, there is the gas vent 18 in power wheel chamber 14 center department, there is the gas outlet 16 on the compressor wheel chamber 13 circumference, there is the air inlet 17 on power wheel chamber 14 circumference, gas generating device is by chamber 19 before the cylinder combustion chamber, cylinder combustion chamber rear chamber 20, porous bell-shaped flame holder 21, fuel injector 22, fuel feeding device 23, some firearm 26, pressure sensor 34 constitute, the gas pocket on the porous bell-shaped flame holder 21 begins to grow gradually till porous bell-shaped flame holder 21 bottom from porous bell-shaped flame holder 21 top, fuel injector 22 installs on the center of porous bell-shaped flame holder 21 top in the cylinder combustion chamber, fuel injector 22 communicates with the fuel feeding device 23 outside the organism 1, porous bell-shaped flame holder 21 bottom is installed to chamber 20 gas jet 27 department in the cylinder combustion chamber rear chamber has some firearm 26, fuel feeding device 23, Point firearm 26, pressure sensor 34, starting drive 52, storage battery 31 are connected with central processing unit 32 through cable conductor 30, there is combustion chamber air inlet 29 on the cavity 19 before the combustion chamber, there is combustion chamber air jet 27 on the cavity 20 behind the combustion chamber, gas wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, combustion chamber air jet 27 communicates with acting wheel chamber 14 air inlet 17, gas wheel chamber 13 air inlet 15 and acting wheel chamber 14 gas vent 18 communicate with the atmosphere.

The basic working principle is as follows: when the compressor works, the central processing unit 32 is connected with a power supply on the starting device 52, a starting motor on the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2, the four air compressing rotors, the acting wheel body 8 and the four acting rotors to rotate at a high speed through the wheel shaft 3, air in the movable blade space 5 of the first air compressing rotor is thrown away from the first air compressing rotor by the driven blades 4 under the action of centrifugal force, negative pressure is generated in the movable blade space 5 of the first air compressing rotor, air in the inner cavity of the first air compressing rotor enters the movable blade space 5 of the first air compressing rotor under the action of atmospheric pressure, the air in the inner cavity of the first air compressing rotor is reduced in pressure, the air continuously enters the inner cavity of the first air compressing rotor through the air inlet 15 of the air compressing wheel cavity 13 under the action of atmospheric pressure, along with the continuous rotation of the first air compressing rotor, the air in the movable blade space 5 of the first air compressing rotor is continuously thrown away from the first air compressing rotor by the movable blades 4, the air after speed reduction and pressure increase enters a first compressor stator blade space 7 to continue speed reduction and pressure expansion to form compressed air, the compressed air in the first compressor stator blade space 7 overflows out of the compressor stator along with the compressor stator under the pressure and inertia, the compressed air overflowing the compressor stator blade space 7 is swept into a second compressor rotor blade space 5 'by a second compressor rotor blade 4' rotating at a high speed outside the first compressor stator and rotates at a high speed along with a second compressor rotor, the compressed air in the second compressor rotor blade space 5 'is exerted by the second compressor rotor while rotating at a high speed along with the second compressor rotor to generate a larger centrifugal force, the compressed air in the second compressor rotor blade space 5' is thrown away from the second compressor rotor at a higher speed by the second compressor rotor and then impacts on the second compressor stator blade 6 'to reduce and increase the pressure again, the compressed air after speed reduction and pressure increase enters the second compressor stator blade space 7' to be concentrated and increased in pressure, the compressed air gathered in the second compressor stator blade space 7 ' overflows from an outer port of the second compressor stator blade space 7 ' under the action of inertia and pressure, then is swept into a third compressor rotor blade space 5 ' by a third compressor rotor blade 4 ' rotating at a high speed outside the second compressor stator blade space and rotates at a high speed along with a third compressor rotor, the compressed air in the third compressor rotor blade space 5 ' is exerted by the third compressor rotor while rotating at a high speed along with the third compressor rotor to generate a larger centrifugal force, the compressed air in the third compressor rotor blade space 5 ' is thrown away from the third compressor rotor at a higher speed by the third compressor rotor and then impacts on the third compressor stator blade 6 ' to decelerate and boost pressure again, the compressed air after decelerating and boosting enters the third compressor stator blade space 7 ' to be concentrated and boosted, and the compressed air gathered in the third compressor stator blade space 7 ' is overflowed from an outer port of the third compressor stator blade space 7 ' under the action of inertia and pressure and then is overflowed from an outer port of the third compressor stator blade space 7 ' by the third compressor stator blade space The fourth air compressor rotor moving blades 4v rotating at high speed outside the rotor sweep into the fourth air compressor rotor moving blade space 5v to rotate at high speed along with the fourth air compressor rotor, compressed air in the fourth air compressor rotor moving blades 5v rotates at high speed along with the fourth air compressor rotor and is simultaneously applied by the fourth air compressor rotor to generate larger centrifugal force, the compressed air in the fourth air compressor rotor moving blade space 5v is thrown away from the fourth air compressor rotor at higher speed and then impacts on the wall of the air compressor cavity 13 to reduce the speed and boost the pressure again, the compressed air after reducing the speed and boosting again enters the air outlet 16 of the air compressor cavity 13 along with the rotation of the fourth air compressor rotor, the compressed air in the air outlet 16 of the air compressor cavity 13 enters the front cavity 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front cavity 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear cavity 20 of the combustion chamber, the flow rate of the compressed air in the bottom of the flame stabilizer 21 is relatively fast, the flow rate of the compressed air in the top of the flame stabilizer 21 is relatively slow, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected into the flame stabilizer 21 from the nozzle of the fuel injector 22 to be mixed with the compressed air in the flame stabilizer 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by the igniter 26, the ignited combustible high-pressure compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure fuel gas, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel and the like, the liquid fuel is directly pressurized by the fuel supply device 23 and then is injected into the flame stabilizer 21 in an atomized high speed through the fuel injector 22 to be mixed with the compressed air in the flame stabilizer 21 to form the combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric spark released by an igniter 26, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, the high-temperature high-pressure gas for short is rapidly sprayed into an air inlet 17 of a working wheel cavity 14 through an air jet port 27 of a combustion chamber, the high-temperature gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle and collides with movable blades 9 on a first working rotor to push the first working rotor to rotate, part of energy is converted into rotary mechanical energy when the high-temperature gas collides with the movable blades 9 of the first working rotor to reduce the flow speed of the high-temperature gas, the high-temperature gas after the pressure reduction and expansion in the movable blade space 10 of the first working rotor enters into the movable blade space 10 of the first working rotor to continue to expand after the high-temperature gas is sprayed into a fixed blade 11 on a working stator in the inner cavity of the first working rotor through an inner port 10 of the first working rotor at a certain reverse tangential angle and in the The first working rotor is pushed again to drive the working wheel body 8 to rotate together, the energy of the high-energy gas impacting the working stator stationary blade 11 to do work is reduced in speed again and slowed down, the high-energy gas impacting the working stator stationary blade 11 enters the working stator stationary blade space 12 to continue to expand and reduce the pressure, the high-energy gas after expansion and pressure reduction is ejected from the lower opening of the working stator stationary blade space 12 at a high speed to push the second working rotor movable blade 9 'in the inner cavity of the working stator again to do work, the high-energy gas after secondary working is reduced again and enters the second working rotor movable blade space 10', the high-energy gas in the second working rotor movable blade space 10 'is expanded and reduced again and ejected from the second working rotor movable blade space 10' in the opposite direction to the rotating direction of the working wheel body 8 to provide a reverse thrust again to the second working rotor to push the second working rotor to do work again, and the high-energy gas after pressure reduction and expansion in the second working rotor movable blade space 10 'is ejected from the second working rotor blade space 10' in the opposite direction to provide a reverse direction to push the second working rotor blade to do work again to do work The tangential angle is sprayed into the inner cavity of the second working rotor against the rotation direction of the working wheel body 8 to impact the stationary blade 11 ' on the second working stator to generate a reverse thrust to push the second working rotor again to drive the working wheel body 8 to rotate and work, the energy of the high-energy gas after impacting the stationary blade 11 ' of the second working stator to work is reduced again, the high-energy gas after impacting the stationary blade 11 ' of the second working stator enters the stationary blade chamber 12 ' of the second working stator to continue to expand and reduce the pressure, the high-energy gas after expanding and reducing the pressure again is sprayed out again from the lower opening of the stationary blade chamber 12 ' of the second working stator at a high speed to push the movable blade 9 ' of the third rotor in the inner cavity of the second working stator to work, the energy of the high-energy gas after doing work again is reduced and enters the movable blade chamber 10 ' of the third working rotor, the high-energy gas in the movable blade chamber 10 ' of the third working rotor passes through the inner opening of the movable blade chamber 10 ' of the third working rotor and then is sprayed into the rotor against the tangential angle, namely, the rotation direction of the third working rotor against the working rotor 8 to do work The static blade 11 ' in the cavity impacting the third doing work stator generates a reverse thrust to push the third doing work rotor again to drive the doing work wheel body 8 to rotate and do work, the high-energy gas energy impacting the static blade 11 ' of the third doing work stator to do work is reduced in speed again and slowed down, the high-energy gas impacting the static blade 11 ' of the third doing work stator enters the static blade space 12 ' of the third doing work stator to continue to expand and reduce the pressure, the high-energy gas expanded and reduced in pressure again is sprayed out at high speed from the lower opening of the static blade space 12 ' of the third doing work stator again to push the movable blade 9v of the fourth doing work rotor in the inner cavity of the third doing work stator to do work, the high-energy gas energy after doing work again is reduced and enters the movable blade space 10v of the fourth doing work rotor, the high-energy gas in the movable blade space 10v of the fourth doing work rotor is sprayed into the inner cavity of the fourth doing work rotor again in a reverse tangential angle, namely a reverse tangential angle 8 rotating direction to push the fourth doing work wheel body again to generate a reverse thrust again The working rotor drives the working wheel body 8 to rotate together to do work, the high-energy gas in the inner cavity of the fourth working rotor after repeated working becomes waste gas with extremely low pressure and is exhausted through the exhaust port 18 of the working wheel cavity 14, and in operation, the central processing unit 32 can control the fuel injection amount of the fuel injector 22 and the starting device 52 according to the pressure signal provided by the pressure sensor 34.

Fig. 18, 21, and 22 collectively show an eighth embodiment of this embodiment, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is a basic power unit also composed of a machine body 1, a wheel axle 3, an air compressing device, an acting device, a gas generating device, a central processing unit 32, a storage battery 31, and the like, where the air compressing device is composed of eight roller-shaped air compressing rotors and six cylindrical air compressing stators, the eight roller-shaped air compressing rotors are divided into two same groups of which axial lengths are sequentially decreased progressively and have different diameters, the six cylindrical air compressing stators are divided into two same groups of which axial lengths are sequentially decreased progressively and have different diameters, the two groups of roller-shaped air compressing rotors with different axial lengths are respectively sleeved and fixed on two sides of the air compressing wheel body 2 in turn according to the size of the diameter and are on the same axial line with the wheel axle 3, and the other ends of each group keep a small air-tight gap, the two groups of cylindrical air compression stators with different axial lengths are respectively sleeved between eight roller-shaped air compression rotors on the two side surfaces of the air compression wheel body 2 in sequence according to the diameter and keep small airtight gaps with the same axis of the eight roller-shaped air compression rotors on the two side surfaces of the air compression wheel body 2 and with the two side surfaces of the air compression wheel body 2, the other ends of the cylindrical air compression stators are respectively fixed on the inner walls of the air compression wheel cavities 13 corresponding to the two side surfaces of the air compression wheel body 2, the six cylindrical air compression stators respectively keep small airtight gaps with the respective inner and outer two adjacent roller-shaped air compression rotors, the acting device is composed of the four roller-shaped acting rotors with different diameters and the three cylindrical acting stators with different diameters, and the four roller-shaped acting rotors with different diameters and the three cylindrical acting stators with different diameters have different axial lengths, the axial length of the working rotor is sequentially lengthened from the outermost layer to the inner layer, the four roller-shaped working rotors with different diameters are sequentially sleeved on the same axis according to the diameter, one end of the working rotor is fixed on the side surface of the working wheel body 8, the other end of the working rotor keeps a micro air-tight gap with the wall of the working wheel cavity 14 corresponding to the side surface of the working wheel body 8, one end of each of the three cylindrical working stators with different diameters is sequentially sleeved between the four roller-shaped working rotors according to the diameter and keeps a micro air-tight gap with the corresponding side surface of the working wheel body 8, the other end of each of the three cylindrical working stators is fixed on the inner wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8, the three cylindrical working stators respectively keep a micro air-tight gap with the inner roller-shaped working rotor and the outer roller-shaped working rotor, the wheel shaft 3 is, Support bearing and sealing device 53, each there is an air inlet 15 in compressor wheel chamber 13 both sides center department, there is gas vent 18 in the center department of doing work wheel chamber 14 side, there is gas outlet 16 on the compressor wheel chamber 13 circumference, there is air inlet 17 on the circumference of doing work wheel chamber 14, gas generating device comprises cavity 19 before the cylinder combustion chamber, cylinder combustion chamber rear chamber 20, the scalable flame holder 21 of porous bell, fuel injector 22, fuel feeding device 23, some firearm 26, temperature sensor 33, pressure sensor 34, position controller 54, spring 56, the gas pocket on the scalable flame holder 21 of porous bell begins grow gradually until the scalable flame holder 21 bottom of porous bell from the scalable flame holder 21 top of porous bell, fuel injector 22 installs on the scalable flame holder 21 top center of porous bell in the cylinder combustion chamber, there are fin 39 on the outer organism 1 in pressure wheel chamber 13 and the power wheel chamber 14, the bearing frame is connected fixedly with casing 1 through piece formula strengthening rib 58, fuel injector 22 is through the flexible pipe 55 with the outer fuel feeding device 23 intercommunication of organism 1, position controller 54 installs at the scalable flame holder 21 top of porous bell-shaped, spring 56 installs one end top in the preceding cavity 19 of combustion chamber and pushes up the front end at the preceding cavity 19 of combustion chamber, the other end presses on position controller 54, pressure sensor 34 installs on the preceding cavity 19 of combustion chamber, cylinder combustion chamber rear chamber 20 gas orifice 27 department porous bell-shaped flame holder 21 bottom is installed and is had some firer 26 and temperature sensor 33, fuel feeding device 23, some firer 26, temperature sensor 33, pressure sensor 34, starting drive 52, storage battery 31 are connected with central processing unit 32 through cable 30, there is combustion chamber air inlet 29 on the preceding cavity 19 of combustion chamber, there is the combustion chamber gas vent 27 on the cavity 20 behind the combustion chamber, the compressor wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, the combustion chamber gas vent 27 communicates with acting wheel chamber 14 air inlet 17, compressor wheel chamber 13 both sides air inlet 15 and acting wheel chamber 14 gas vent 18 communicate with each other with the atmosphere.

The basic working principle is as follows: when the compressor works, the central processing unit 32 is connected with a power supply on the starting device 52, the starting motor on the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2, the eight air compressing rotors on the two side surfaces of the air compressing wheel body 2 and the four acting rotors on the acting wheel body 8 and the side surface of the acting wheel body 8 to rotate at high speed through the wheel shaft 3, air in the first air compressing rotor movable vane rooms 5 with the same diameter on the two side surfaces of the air compressing wheel body 2 is thrown away from the first air compressing rotor by the blades 4 under the action of centrifugal force, negative pressure is generated in the first air compressing rotor movable vane rooms 5, external air continuously enters the first air compressing rotor inner cavities on the two sides of the air compressing wheel body 2 through the air inlets 15 on the two sides of the air compressing wheel cavity 13 under the action of atmospheric pressure, the air in the first air compressing rotor inner cavities on the two sides of the air compressing wheel body 2 is sucked into the first air, along with the continuous rotation of the first compressed air rotors on the two sides of the compressed air wheel body 2, the air in the first compressed air rotor movable blade spaces 5 on the two sides of the compressed air wheel body 2 is continuously thrown away from the first compressed air rotors on the two sides of the compressed air wheel body 2 by the first compressed air rotor movable blades 4 on the two sides of the compressed air wheel body 2 and impacts the first compressed air stator blades 6 on the two sides of the compressed air wheel body 2 to be decelerated and boosted, the air after being decelerated and boosted respectively enters the first compressed air stator blade spaces 7 on the two sides of the compressed air wheel body 2 to be decelerated and boosted to form compressed air, the compressed air in the first compressed air stator blade spaces 7 on the two sides of the compressed air wheel body 2 flows out along with the compressed air stators on the two sides of the compressed air wheel body 2 under the pressure and inertia, the compressed air flowing out of the compressed air stator spaces 7 is swept into the second compressed air rotor movable blade spaces 5' on the two sides of the compressed air wheel body 2 by the first compressed air stators on the two sides of the compressed air, compressed air in the second compressed air rotor movable blade spaces 5 'on two sides of the compressed air wheel body 2 is exerted by the second compressed air rotors on two sides of the compressed air wheel body 2 to generate larger centrifugal force, the compressed air in the second compressed air rotor movable blade spaces 5' on two sides of the compressed air wheel body 2 is thrown away from the second compressed air rotors on two sides of the compressed air wheel body 2 at a higher speed and then collides with the second compressed air stator blades 6 'on two sides of the compressed air wheel body 2 to decelerate and boost again, the compressed air after decelerating and boosting enters the second compressed air stator blade spaces 7' on two sides of the compressed air wheel body 2 to be concentrated and boosted, and the compressed air collected in the second compressed air stator blade spaces 7 'is swept into the third compressed air rotor 4' in the third compressed air rotor spaces 5 'on two sides of the compressed air wheel body 2 along with the first compressed air rotor blades 2 on two sides of the compressed air wheel body 2 after overflowing from the outer ports of the second compressed air stator blade spaces 7' on two sides of the compressed air wheel body 2 under the action of inertia and pressure The three-compressor rotor rotates at high speed, compressed air in the third compressor rotor movable blade spaces 5 ' on two sides of the compressor wheel body 2 is exerted by the third compressor rotors on two sides of the compressor wheel body 2 to generate larger centrifugal force, the compressed air in the third compressor rotor movable blade spaces 5 ' on two sides of the compressor wheel body 2 is thrown away from the third compressor rotors on two sides of the compressor wheel body 2 by the third compressor rotors at higher speed and then collides with the third compressor stator blades 6 ' on two sides of the compressor wheel body 2 to decelerate and boost again, the compressed air after decelerating and boosting enters the third compressor stator blade spaces 7 ' on two sides of the compressor wheel body 2 to be gathered and boosted, the compressed air gathered in the third compressor stator blade spaces 7 ' is swept into the fourth compressor rotor movable blade spaces 5v by the third compressor stator blades on two sides of the compressor wheel body 2 to rotate at high speed along with the fourth compressor rotor under the action of inertia and pressure, compressed air in the space 5v between the fourth air compressor rotor movable blades on two sides of the air compressor wheel body 2 is exerted by the fourth air compressor rotor to generate larger centrifugal force, the compressed air in the space 5v between the fourth air compressor rotor movable blades on two sides of the air compressor wheel body 2 is thrown away from the fourth air compressor rotor by the fourth air compressor rotor at higher speed and then collides with the wall of the air compressor wheel cavity 13 to be decelerated and boosted again, the compressed air after being decelerated and boosted again enters the air outlet 16 of the air compressor wheel cavity 13 along with the rotation of the fourth air compressor rotors on two sides of the air compressor wheel body 2, the compressed air in the air outlet 16 of the air compressor wheel cavity 13 enters the front combustion chamber 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front combustion chamber 19 of the combustion chamber firstly rotates around the porous bell-shaped telescopic flame stabilizer 21 in a vortex shape and then passes through the air holes of the porous bell-, because the air holes on the porous bell-shaped telescopic flame holder 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed air in the porous bell-shaped telescopic flame holder 21 is characterized in that the flow rate at the top is relatively slow, the flow rate at the bottom is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the extension pipe 55 from the fuel supply device 23 and is sprayed into the top of the porous bell-shaped telescopic flame holder 21 through the nozzle of the fuel injector 22 to be mixed with the compressed air to form combustible high-pressure compressed mixed gas, the combustible high-pressure compressed mixed gas is ignited by electric sparks released by the igniter 26 when flowing to the bottom of the porous bell-shaped flame holder 21, the ignited combustible high-pressure compressed mixed gas is rapidly combusted and expanded to release heat energy to generate high-temperature and high-pressure fuel gas, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel and the like, the liquid fuel is directly pressurized by the fuel supply The inner part of the working wheel cavity 14 is mixed with the compressed gas in the flame stabilizer 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by an igniter 26, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, the rapidly generated high-temperature high-pressure gas firstly pushes the top part of the porous bell-shaped telescopic flame stabilizer 21, namely the fuel injector 22 and the position controller 54 to press the spring 56 to move towards the front end of the combustion chamber front cavity 19, meanwhile, the high-temperature high-pressure gas is sprayed into the air inlet 17 of the working wheel cavity 14 through the combustion chamber air nozzle 27 at high speed, the high-temperature high-pressure gas, short for high-energy gas, is rapidly sprayed into the air inlet 17 of the working wheel cavity 14 through the combustion chamber air nozzle 27 at high speed, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14, when the high-energy gas impacts the first working rotor movable blades 9, part of energy is converted into rotary mechanical energy to reduce the flow speed of the high-energy gas, the high-energy gas enters the first working rotor movable blade spaces 10 to continuously expand after the flow speed of the high-energy gas is slowed, the high-energy gas after pressure reduction and expansion in the first working rotor movable blade spaces 10 is sprayed into the inner cavity of the first working rotor through the inner openings of the first working rotor movable blades spaces 10 in a certain reverse tangential angle and against the rotating direction of the working wheel body 8 to impact the stationary blades 11 on the working stator to generate a strong reverse thrust to push the first working rotor to drive the working wheel body 8 to rotate together again, the energy of the high-energy gas after impacting the stationary blades 11 to do work is slowed down again, the high-energy gas after impacting the stationary blades 11 of the working stator enters the stationary blades 12 of the working stator to continuously expand and reduce the pressure, the high-energy gas after expansion and pressure reduction is sprayed out from the lower openings of the stationary blades 12 of the working stator at a high speed to push the second working rotor movable blades 9' in the inner cavity, the energy of the high-energy gas after doing work again is reduced again and enters the second working rotor movable blade space 10 ', the high-energy gas in the second working rotor movable blade space 10' expands again to reduce pressure and is sprayed out from the second working rotor movable blade space 10 'in the direction opposite to the rotation direction of the working wheel body 8 to provide a reverse thrust for the second working rotor again to push the second working rotor to do work, the high-energy gas after pressure reduction and expansion in the second working rotor movable blade space 10' is sprayed into the inner cavity of the second working rotor through the inner opening of the second working rotor movable blade space 10 'in the reverse tangential angle and in the rotation direction of the working wheel body 8 again to impact the stator blades 11' on the second working stator to generate a reverse thrust to push the second working rotor again to drive the working wheel body 8 to do work together, the energy of the high-energy gas after impacting the stator blades 11 'of the second working stator to do work is reduced again, and the high-energy of the high-energy gas after impacting the stator blades 11' of the second working stator blades 11 'enters the second working rotor stator 12' to do work again, and the high-energy of the high-energy gas after impacting the Expanding and depressurizing, the high-energy gas after being expanded and depressurized again is sprayed out at high speed from the lower opening of the stationary blade space 12 ' of the second working stator again to push the third working rotor movable blade 9 ' in the inner cavity of the second working stator to work, the energy of the high-energy gas after being worked again is reduced again and enters the movable blade space 10 ' of the third working rotor, the high-energy gas in the movable blade space 10 ' of the third working rotor passes through the inner opening of the movable blade space 10 ' of the third working rotor and is sprayed into the inner cavity of the third working rotor again with a certain reverse tangential angle, namely in the direction opposite to the rotation direction of the working rotor body 8 to impact the stationary blade 11 ' on the third working stator to generate a reverse thrust to push the third working rotor again to drive the working rotor body 8 to work together, the energy of the high-energy gas after impacting the stationary blade 11 ' of the third working stator to work is reduced again in speed and is reduced again, the high-energy gas after impacting the stationary blade 11 ' of the third working stator enters the stationary blade space 12 ' of the third working stator to continue to be expanded and depressurized, the high-energy gas after re-expansion and pressure reduction is sprayed out at high speed from the lower opening of the 12' between the stationary blades of the third working stator again to push the movable blades 9v of the fourth working rotor in the inner cavity of the third working stator to work, the energy of the high-energy gas after re-working is reduced again and enters the movable blades 10v of the fourth working rotor, the high-energy gas in the movable blades 10v of the fourth working rotor passes through the inner opening of the movable blades 10v of the fourth working rotor and is sprayed into the inner cavity of the fourth working rotor again in a certain reverse tangential angle, namely the rotating direction of the reverse working wheel body 8, and then a reverse thrust is generated again to push the fourth working rotor to drive the working rotor to rotate and work, the high-energy gas after repeated and multiple times of working in the inner cavity of the fourth working rotor becomes waste gas with extremely low pressure and is discharged from the exhaust opening 18 of the working wheel cavity 14, and in work, the pressure difference between the rear cavity 20 of the cylindrical combustion chamber and the front cavity 19 is reduced, the top of the perforated bell-shaped retractable flame holder 21, i.e. the fuel injector 22, is also moved back to the starting position towards the rear cylindrical combustion chamber 20 by the action of the spring 56 in front of the position controller 54. the central processor 32 can control the fuel injection amount of the fuel injector 22 and the actuating means 52 according to the pressure signals provided by the temperature sensor 33 and the pressure sensor 34.

Fig. 7, 8, 15, and 23 collectively show a ninth embodiment of the present invention, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is also a basic power unit formed by components such as a machine body 1, a wheel shaft 3, an air compressing device, a work doing device, a gas generating device, a central processing unit 32, and a battery pack 31, where the air compressing device is formed by four roller-shaped air compressing rotors with different diameters and three cylindrical air compressing stators with different diameters, the respective axial lengths of the four roller-shaped air compressing rotors with different diameters and the three cylindrical air compressing stators with different diameters are different, and the axial lengths thereof are gradually reduced from an innermost layer to an outer layer, that is, gradually increased from an outermost layer to an inner layer, the four roller-shaped air compressing rotors with different diameters are sequentially sleeved on the same axis, and one end of each of the four roller-shaped air compressing rotors is fixed on a side surface of an, the other end of the cylinder-shaped air compression stator with different diameters is sequentially sleeved among the four cylinder-shaped air compression rotors according to the diameter and keeps the micro air-tight gap with the side surface of the corresponding air compression wheel body 2, the other end of the cylinder-shaped air compression stator with different diameters is installed and fixed on the inner wall of the air compression wheel cavity 13 opposite to the side surface of the air compression wheel body 2, the cylinder-shaped air compression stators with different diameters respectively keep the micro sealing gap with the inner and the outer adjacent cylinder-shaped air compression rotors, the power applying device is composed of two cylinder-shaped power applying rotors with different diameters and a cylinder-shaped power applying stator with different diameters, the axial lengths of the two cylinder-shaped power applying rotors with different diameters are different, the axial lengths of the two cylinder-shaped power applying rotors are sequentially lengthened from the innermost layer to the outer layer by layer, and the two cylinder-shaped power applying rotors with different diameters are sequentially sleeved on the same axial line according to, one end of the cylindrical working stator is fixed on the side surface of the working wheel body 8, the other end of the cylindrical working stator keeps a tiny airtight gap with the wall of the working wheel cavity 14 corresponding to the side surface of the working wheel body 8, one end of the cylindrical working stator is sleeved between the two roller-shaped working rotors and keeps a tiny airtight gap with the side surface of the corresponding working wheel body 8, the other end of the cylindrical working stator is installed and fixed on the inner wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8, the three cylindrical working stators respectively keep tiny airtight gaps with the inner and the outer adjacent roller-shaped working rotors, the wheel shaft 3 is installed on the centers of the working wheel body 8 and the air compression wheel body 2, the wheel shaft 3 is provided with a speed change device 35, a support bearing and a sealing device 53, the center of the side surface of the air compression wheel cavity 13 is provided with an air inlet 15, the center of the side surface of the working wheel cavity 14 is provided with, the speed changing device 35 is composed of a planetary gear set with a locking mechanism and a planetary gear set control motor, the planetary gear set control motor is composed of a motor rotor 36 arranged on a large gear ring in the planetary gear set and a motor stator 37 fixed on the machine body 1, the motor stator 37 is connected with the central processing controller 32 through a cable 30, the gas generating device is composed of a cylindrical combustion chamber front cavity 19, a cylindrical combustion chamber rear cavity 20, a porous bell-shaped flame holder 21, a fuel injector 22, a fuel supply device 23, a fuel vaporization heater 24, a fuel vaporizer control device 25, an igniter 26, a storage battery pack 31, the central processing controller 32 and a pressure sensor 34, gas holes on the porous bell-shaped flame holder 21 are gradually enlarged from the top of the porous bell-shaped flame holder 21 to the bottom of the porous bell-shaped flame holder 21, the fuel injector 22 is arranged on the center of the top of the porous bell-shaped flame holder 21 in the cylindrical combustion chamber, the outer machine body 1 of the working wheel cavity 14 is provided with a cooling fin 39, the fuel injector 22 is communicated with a fuel supply device 23 outside the machine body 1, the fuel vaporization heater 24 is arranged at a nozzle of the fuel injector 22, the fuel vaporization heater 24 is connected with a fuel vaporizer control device 25, the bottom of a porous bell-shaped flame stabilizer 21 at the nozzle 27 of the cylindrical combustion chamber rear cavity 20 is provided with an igniter 26, the combustion chamber front cavity 19 is provided with a pressure sensor 34, the nozzle 27 of the combustion chamber is provided with a water sprayer 48 which is communicated with the nozzle 27 of the combustion chamber, the other end of the water sprayer 48 is connected with a water supply device 51, the working wheel cavity 14 at the air inlet 17 of the working wheel cavity 14 in the machine body 1 is provided with an arc-shaped movable cavity wall 49 on the circumference, one end of the arc-shaped movable cavity wall 49 is connected with a fixed cavity wall through a movable shaft 50, the other end of the arc-shaped movable cavity wall 49 is arranged at, the fuel supply device 23, the igniter 26, the storage battery pack 31, the pressure sensor 34, the control motor stator 37 on the speed changing device 35, the injector 22, the water sprayer 48, the movable cavity wall 49 regulating device 47, the fuel vaporization heater 24 and the fuel vaporization device control device 25 are connected with the central processing controller 32 through a cable 30, the combustion chamber front cavity 19 is provided with a combustion chamber air inlet 29, the combustion chamber rear cavity 20 is provided with a combustion chamber air outlet 27, the air outlet 16 of the air compressor wheel cavity 13 is communicated with the combustion chamber air inlet 29, the combustion chamber air outlet 27 is communicated with the air inlet 17 of the working wheel cavity 14, and the air inlet 15 of the air compressor wheel cavity 13 and the air outlet 18 of the working wheel cavity 14 are communicated with the atmosphere.

The basic working principle is as follows: when the air compressor works, the central processing unit 32 locks any two gears in the planetary gear set on the speed changing device 35 through the locking mechanism on the speed changing device 35, the storage battery 31 is connected with a circuit of a control motor stator 37 on the speed changing device 35, the control motor rotor 36 is started to output mechanical energy, the wheel shaft 3 is driven by the speed changing device 35 to drive the air compressing wheel body 2, the four air compressing rotors, the acting wheel body 8 and the two acting rotors to rotate at high speed, air in a first air compressing rotor movable vane chamber 5 on the air compressing wheel body 2 is thrown away from the first air compressing rotor by the driven vane 4 under the action of centrifugal force, negative pressure is generated in the first air compressing rotor movable vane chamber 5, air in the first air compressing rotor inner chamber enters the first air compressing rotor movable vane chamber 5 under the action of atmospheric pressure, at the moment, the air pressure in the first air compressing rotor inner chamber is reduced, the air continuously enters the first air compressing rotor inner chamber through, along with the continuous rotation of the first compressed air rotor, the air in the movable blade space 5 in the first compressed air rotor is continuously thrown away from the first compressed air rotor by the first compressed air rotor movable blade 4 and is collided on the first compressed air stator blade 6 to be subjected to speed reduction and pressure rise, the air subjected to speed reduction and pressure rise enters the first compressed air stator blade space 7 to be subjected to speed reduction and pressure expansion continuously to form compressed air, the compressed air in the first compressed air stator blade space 7 overflows out of the compressed air stator along with the compressed air stator under the pressure and inertia, the compressed air overflowing out of the compressed air stator space 7 is swept into the second compressed air rotor movable blade space 5 'by the second compressed air rotor movable blade 4' rotating at a high speed along with the second compressed air rotor to rotate at a high speed, the compressed air in the second compressed air rotor movable blade space 5 'is applied by the second compressed air rotor to generate a larger centrifugal force, and the compressed air in the second compressed air rotor movable blade space 5' is thrown away from the first compressed air rotor at a higher speed by the second rotor The compressed air after the deceleration and pressure rise enters the second compressor stator blade space 7 'to be converged and pressure rise, the compressed air gathered in the second compressor stator blade space 7' overflows from the outer opening of the second compressor stator blade space 7 'under the action of inertia and pressure, then is swept into the third compressor rotor blade space 5' by the third compressor rotor blade 4 'rotating at high speed outside the second compressor stator blade space and rotates at high speed along with the third compressor rotor, the compressed air in the third compressor rotor blade space 5' is exerted by the third compressor rotor along with the high-speed rotation of the third compressor rotor to generate larger centrifugal force, the compressed air in the third compressor rotor blade space 5 'is thrown away from the third compressor rotor at higher speed by the third compressor rotor and then collides on the third compressor stator blade 6' to decelerate and pressure rise again, the compressed air after speed reduction and pressure increase enters a third compressor stator blade space 7 ' for cohesion and pressure increase, the compressed air gathered in the third compressor stator blade space 7 ' overflows from an outer port of the third compressor stator blade space 7 ' under the action of inertia and pressure, then is swept into a fourth compressor rotor blade space 5V by a fourth compressor rotor blade 4V which rotates at a high speed outside the third compressor stator blade space and rotates at a high speed along with the fourth compressor rotor, the compressed air in the fourth compressor rotor blade space 5V is exerted by the fourth compressor rotor while rotating at a high speed along with the fourth compressor rotor to generate a larger centrifugal force, the compressed air in the fourth compressor rotor blade space 5V is thrown away from the fourth compressor rotor at a higher speed by the fourth compressor rotor and then impacts on the wall of the compressor wheel cavity 13 for speed reduction and pressure increase again, the compressed air after speed reduction and pressure increase again enters the compressor wheel cavity 13 air outlet 16 along with the rotation of the fourth compressor rotor, the compressed air in the air outlet 16 of the air compression wheel cavity 13 enters the front chamber 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front chamber 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a spiral shape and then passes through the air holes of the flame stabilizer 21 to enter the rear chamber 20 of the combustion chamber, the air holes on the flame stabilizer 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed air in the flame stabilizer 21 is characterized in that the flow rate of the compressed air at the top is relatively slow, the flow rate of the compressed air at the bottom of the flame stabilizer 21 is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel injector 22 and is sprayed into the top of the flame stabilizer 21 from the nozzle of the fuel injector 22 to be mixed with the high-pressure compressed air in the top of the flame stabilizer 21 to form combustible high-pressure compressed air mixture, and the combustible high-pressure air, the ignited combustible high-pressure compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure fuel gas, when liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like is used, the liquid fuel can be directly pressurized by the fuel supply device 23 and then is atomized by the fuel injector 22 and sprayed into the top of the flame holder 21 at a high speed to be mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate the high-temperature high-pressure fuel gas, the central processing unit can also provide high-frequency electromagnetic pulse waves to the fuel vaporization heater 24 through the fuel vaporizer control device 25 to heat a pipeline at the nozzle of the fuel injector 22, and the fuel is sprayed into the top of the flame holder 21 in a vaporization form in the fuel injector 22 at a high speed to be mixed with the The mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom of the flame stabilizer 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, the high-temperature high-pressure gas is called high-energy gas for short and is sprayed into the air inlet 17 of the working wheel cavity 14 at a high speed through the air jet 27 of the combustion chamber, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle and impacts the movable blades 9 on the first working rotor to drive the first working rotor to rotate, part of energy is converted into rotary mechanical energy to reduce the flow speed of the high-energy gas when the high-energy gas impacts the movable blades 9 of the first working rotor, the high-energy gas enters the movable blade spaces 10 of the first working rotor after the flow speed of the high-energy gas is slowed down and is sprayed into the inner cavity of the first working rotor through the inner openings of the movable blade spaces 10 of the first working rotor to impact the inner The stator blade 11 generates a strong reverse thrust to push the first working rotor again to drive the working wheel body 8 to rotate together, the energy of the high-energy gas impacting the working stator blade 11 to do work is reduced slowly again, the high-energy gas impacting the working stator blade 11 enters the working stator blade space 12 to continue to expand and reduce the pressure, the high-energy gas after being expanded and reduced in pressure is ejected from the lower opening of the working stator blade space 12 at a high speed to push the second working rotor blade 9 'in the inner cavity of the working stator to do work again, the high-energy gas after being worked again is reduced again and enters the second working rotor blade space 10', the high-energy gas in the second working rotor blade space 10 'is expanded and reduced again and ejected from the second working rotor blade space 10' against the rotating direction of the working wheel body 8 to provide a reverse thrust to the second working rotor to push the second working rotor to do work again, the waste gas with certain excess pressure after working is discharged through the exhaust port 18 of the working wheel cavity 14. In operation, the cpu 32 may apply a forward or reverse current to the stator 37 of the control motor, apply a forward or reverse force to the rotor 36 of the control motor, i.e., the big gear ring of the planetary gear set in the transmission 35, so that the working rotor outputs power to the compressor rotor through the wheel shaft 3 via the transmission 35 in a variable transmission ratio mode, and when the working rotor is decelerated due to the rotation speed, apply a forward or reverse current to the stator 37 of the control motor, i.e., the big gear ring of the planetary gear set in the transmission 35, so as to output power to the compressor rotor in a hybrid mode, or lock the sun gear and the planetary gear of the planetary gear set in the transmission 35, drive the compressor rotor and the working rotor to rotate by controlling the motor, use the control motor as a starter, and drive the working rotor to control the motor to generate power to output power to the electrical equipment or to output power to the battery while driving the compressor rotor Charging, in operation, when needing shaft 3 output great torsion, can adjust the aperture of activity chamber wall 49 through regulation and control device 47, increase the aperture of activity chamber wall 49, let more high temperature high pressure gas get into doing work wheel chamber 14, make high temperature high pressure gas promote more doing work rotor movable blades 9 simultaneously in order to produce bigger torsion, when needs reduce torsion, can carry out the callback to activity chamber wall 49 through regulation and control device 47 equally, reduce the aperture of activity chamber wall 49, reduce high temperature high pressure gas and get into doing work wheel chamber 14, let high temperature high pressure gas promote less doing work rotor movable blades 9 in order to reduce the torsion of output. When the high-power working is carried out, the water sprayer 48 at the air jet 27 of the combustion chamber can spray a proper amount of water mist into the working wheel cavity 14 according to the temperature in the working wheel cavity 14, so that a large amount of water vapor can be generated while the temperature in the working wheel cavity 14 is reduced, the pressure in the working wheel cavity 14 is further improved, the central processor 32 calculates and processes the information of the pressure and the temperature of the gas, the combustible mixed gas and the compressed air, the rotating speed of the working rotor and the air compressing rotor and the like collected by various sensors and outputs instructions to various actuators such as the igniter 26, the fuel supply device 23, the water sprayer 48, the regulating device 47 on the movable cavity wall 49, the control motor on the speed changing device 35 and the like to timely regulate the fuel spraying amount, the spraying amount of the atomized water, the opening degree of the movable cavity wall 49 and the rotating speed ratio of the working rotor and the air compressing rotor, so that the, The pressure of the compressed air, the rotation speed of the wheel shaft 3 and the like are all kept at the optimal values to ensure that the engine works in the optimal state.

Fig. 18, 22 and 24 collectively show a tenth embodiment of this embodiment, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is a basic power unit also composed of a machine body 1, a wheel axle 3, an air compressing device, a work doing device, a gas generating device, a central processing unit 32, a storage battery 31 and other components, the air compressing device is composed of eight roller-shaped air compressing rotors and six cylindrical air compressing stators, the eight roller-shaped air compressing rotors are divided into two same groups with sequentially decreasing axial lengths and different diameters, the six cylindrical air compressing stators are divided into two same groups with sequentially decreasing axial lengths and different diameters, the two groups of roller-shaped air compressing rotors with different axial lengths are respectively sleeved and fixed on two sides of the air compressing wheel body 2 according to the diameters and on the same axial line with the wheel axle 3, and the other ends of the groups keep a small air-tight gap with the inner wall of the air compressing wheel cavity 13 corresponding to two sides of, the two groups of cylindrical air compression stators with different axial lengths are respectively sleeved between eight roller-shaped air compression rotors on the two side surfaces of the air compression wheel body 2 in sequence according to the diameter and keep small airtight gaps with the same axis of the eight roller-shaped air compression rotors on the two side surfaces of the air compression wheel body 2 and with the two side surfaces of the air compression wheel body 2, the other ends of the cylindrical air compression stators are respectively fixed on the inner walls of the air compression wheel cavities 13 corresponding to the two side surfaces of the air compression wheel body 2, the six cylindrical air compression stators respectively keep small airtight gaps with the respective inner and outer two adjacent roller-shaped air compression rotors, the acting device is composed of the four roller-shaped acting rotors with different diameters and the three cylindrical acting stators with different diameters, and the four roller-shaped acting rotors with different diameters and the three cylindrical acting stators with different diameters have different axial lengths, the axial length of the working rotor is sequentially lengthened from the outermost layer to the inner layer, the four roller-shaped working rotors with different diameters are sequentially sleeved on the same axis according to the diameter, one end of the working rotor is fixed on the side surface of the working wheel body 8, the other end of the working rotor keeps a micro air-tight gap with the wall of the working wheel cavity 14 corresponding to the side surface of the working wheel body 8, one end of each of the three cylindrical working stators with different diameters is sequentially sleeved between the four roller-shaped working rotors according to the diameter and keeps a micro air-tight gap with the corresponding side surface of the working wheel body 8, the other end of each of the three cylindrical working stators is fixed on the inner wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8, the three cylindrical working stators respectively keep a micro air-tight gap with the inner roller-shaped working rotor and the outer roller-shaped working rotor, the wheel shaft 3 is, Power distributor 38, support bearing and sealing device 53, power output shaft 40 is installed to power distributor 38's front end, each there is an air inlet 15 in the center department of compressor wheel chamber 13 both sides, there is gas vent 18 in the center department of working wheel chamber 14 side, there is gas outlet 16 on the compressor wheel chamber 13 circumference, there is air inlet 17 on the working wheel chamber 14 circumference, there is fin 39 on the organism 1, gas generating device comprises cylinder combustion chamber front chamber 19, cylinder combustion chamber rear chamber 20, the scalable flame holder 21 of porous bell, fuel injector 22, fuel feeding device 23, some firearm 26, temperature sensor 33, pressure sensor 34, position controller 54, spring 56, the gas pocket on the scalable flame holder 21 of porous bell begins progressively grow up to the scalable flame holder 21 bottom of porous bell from the scalable flame holder 21 top of porous bell, the fuel injector 22 is installed in the cylindrical combustion chamber on the center of the top of the porous bell-shaped telescopic flame holder 21, the outer machine body 1 of the air compressor cavity 13 and the working wheel cavity 14 is provided with a cooling fin 39, the bearing seat is fixedly connected with the shell 1 through a sheet-type reinforcing rib 58, the fuel injector 22 is communicated with the fuel supply device 23 outside the machine body 1 through an extension pipe 55, the position controller 54 is installed at the top of the porous bell-shaped telescopic flame holder 21, the spring 56 is installed in the front chamber 19 of the combustion chamber, one end of the spring is propped against the front end of the front chamber 19 of the combustion chamber, the other end of the spring is pressed on the position controller 54, the pressure sensor 34 is installed on the front chamber 19 of the combustion chamber, the igniter 26 and the temperature sensor 33 are installed at the bottom of the porous bell-shaped flame holder 21 at the air jet 27 of the rear chamber 20, Storage battery 31, temperature sensor 33, pressure sensor 34, power distributor 38, starting drive 52, through cable conductor 30 with central processing unit 32 connect, there is combustion chamber air inlet 29 on the chamber 19 before the combustion chamber, there is the combustion chamber air jet 27 on the chamber 20 behind the combustion chamber, compressor wheel chamber 13 gas outlet 16 communicates with combustion chamber air inlet 29, combustion chamber air jet 27 communicates with working wheel chamber 14 air inlet 17, compressor wheel chamber 13 both sides air inlet 15 and working wheel chamber 14 gas vent 18 communicate with each other with the atmosphere.

The basic working principle is as follows: when the compressor works, the central processing unit 32 is connected with a power supply on the starting device 52, the starting motor on the starting device 52 outputs mechanical energy to drive the eight air compressing rotors on the two side surfaces of the air compressing wheel body 2 and the acting wheel body 8 and the four acting rotors on the side surfaces of the acting wheel body 8 to rotate at high speed through the wheel shaft 3, the central processing unit 32 can also lock the sun wheel and the planetary gears in the power distributor 38, the control motor on the starting power distributor 38 outputs mechanical energy to drive the eight air compressing rotors on the two side surfaces of the air compressing wheel body 2 and the acting wheel body 8 and the four acting rotors on the side surfaces of the acting wheel body 8 to rotate at high speed through the wheel shaft 3, air in the movable vane chambers 5 of the first air compressing rotor with the same diameter on the two side surfaces of the air compressing wheel body 2 is thrown away from the first air compressing rotor by the driven vanes 4, the outside air continuously enters the first air compressing rotor cavities at both sides of the air compressing wheel body 2 from the air inlets 15 at both sides of the air compressing wheel cavity 13 under the action of atmospheric pressure, the air in the first air compressing rotor cavities at both sides of the air compressing wheel body 2 is sucked into the first air compressing rotor movable blade cavities 5 at both sides of the air compressing wheel body 2 by the negative pressure in the first air compressing rotor movable blade cavities 5 at both sides of the air compressing wheel body 2, along with the continuous rotation of the first air compressing rotors at both sides of the air compressing wheel body 2, the air in the first air compressing rotor movable blade cavities 5 at both sides of the air compressing wheel body 2 is continuously thrown away from the first air compressing rotors at both sides of the air compressing wheel body 2 by the first air compressing rotor movable blades 4 at both sides of the air compressing wheel body 2 and impacts the first air compressing stator blades 6 at both sides of the air compressing wheel body 2 to be decelerated and pressurized to be pressurized to form compressed air by continuous deceleration, the compressed air in the first stator blade spaces 7 on both sides of the compressed air wheel body 2 overflows towards the compressed air stators under the pressure and inertia along the compressed air stators on both sides of the compressed air wheel body 2, the compressed air overflowing the compressed air stators 7 is swept into the second compressed air rotor blade spaces 5 'on both sides of the compressed air wheel body 2 by the second compressed air rotor blades 4' rotating at high speed outside the first compressed air stators on both sides of the compressed air wheel body 2 to rotate at high speed along with the second compressed air rotors on both sides of the compressed air wheel body 2, the compressed air in the second compressed air rotor blade spaces 5 'on both sides of the compressed air wheel body 2 is exerted by the second compressed air rotors on both sides of the compressed air wheel body 2 to generate larger centrifugal force, the compressed air in the second compressed air rotor blade spaces 5' on both sides of the compressed air wheel body 2 is thrown away from the second compressed air rotors on both sides of the compressed air wheel body 2 at higher speed by the second compressed air rotors on both sides of the compressed air wheel body 2 and then collides with, the compressed air after speed reduction and pressure increase enters second stator blade spaces 7 'on two sides of the compressor wheel body 2 for cohesion and pressure increase, the compressed air gathered in the second stator blade spaces 7' overflows from outer openings of the second stator blade spaces 7 'on two sides of the compressor wheel body 2 under the action of inertia and pressure, then third compressor rotor blades 4' rotating at a high speed outside the second compressor blades on two sides of the compressor wheel body 2 sweep into third compressor rotor blade spaces 5 'on two sides of the compressor wheel body 2 and rotate at a high speed along with third compressor rotors on two sides of the compressor wheel body 2, the compressed air in the third compressor rotor blade spaces 5' on two sides of the compressor wheel body 2 is exerted by the third compressor rotors on two sides of the compressor wheel body 2 to generate a larger centrifugal force, and the compressed air in the third compressor rotor blade spaces 5 'on two sides of the compressor wheel body 2 is thrown away from the third compressor rotors on two sides of the compressor wheel body 2 at a higher speed by the third compressor rotors to collide with the third compressor rotor blades 6' on two sides of the compressor wheel body 2 and then again Boosting, the compressed air after speed reduction and boosting enters the third stator blade spaces 7 ' on both sides of the compressor wheel body 2 for cohesion boosting, the compressed air gathered in the third stator blade spaces 7 ' overflows from the outer openings of the third stator blade spaces 7 ' under the action of inertia and pressure, then the compressed air is swept into the fourth rotor blade spaces 5V by the fourth rotor blades 4v which rotate at high speed outside the third stator blades on both sides of the compressor wheel body 2 and rotates at high speed along with the fourth rotor, the compressed air in the fourth rotor blade spaces 5v on both sides of the compressor wheel body 2 is exerted by the fourth rotor to generate larger centrifugal force, the compressed air in the fourth rotor blade spaces 5v on both sides of the compressor wheel body 2 is thrown away from the fourth rotor at higher speed by the fourth rotor and then impacts on the wall of the compressor wheel cavity 13 to reduce the speed and boost again, and the compressed air after speed reduction and boosting again enters the outlet of the compressor wheel cavity 13 along with the rotation of the fourth rotor blades on both sides of the compressor wheel body 2 16, the compressed air in the air outlet 16 of the air wheel cavity 13 enters the front chamber 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front chamber 19 of the combustion chamber firstly rotates around the porous bell-shaped telescopic flame holder 21 in a vortex shape and then passes through the air holes of the porous bell-shaped telescopic flame holder 21 to enter the rear chamber 20 of the combustion chamber, and because the air holes on the porous bell-shaped telescopic flame holder 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed air in the porous bell-shaped telescopic flame holder 21 is characterized in that the top flow rate is relatively slow, the bottom flow rate is relatively fast, when using the gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the telescopic pipe 55 from the fuel supply device 23 and is sprayed into the top of the porous bell-shaped telescopic flame holder 21 through the nozzle of the fuel injector 22 to be mixed with the compressed air to form combustible, when liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like is used, the liquid fuel is directly pressurized by the fuel supply device 23 and then is sprayed into the inner part of the flame holder 21 in an atomized manner at high speed through the fuel injector 22 to be mixed with the compressed gas in the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26, the ignited combustible compressed mixed gas is quickly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, and the quickly generated high-temperature and high-pressure gas firstly pushes the top of the porous bell-shaped telescopic flame holder 21, namely the fuel injector 22 and the position controller 54 to press the spring 56 to move to the front end of the combustion chamber front cavity 19, meanwhile, high-temperature and high-pressure gas is sprayed into the air inlet 17 of the working wheel cavity 14 at a high speed through the combustion chamber air nozzle 27, high-temperature and high-pressure gas, which is called high-energy gas for short, is quickly sprayed into the air inlet 17 of the working wheel cavity 14 at a high speed through the combustion chamber air nozzle 27, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle to impact the movable blades 9 on the first working rotor to push the first working rotor to rotate, when the high-energy gas impacts the movable blades 9 of the first working rotor, part of energy is converted into rotary mechanical energy to reduce the flow speed of the rotary mechanical energy, the high-energy gas enters the movable blade space 10 of the first working rotor to continue to expand after the flow speed of the high-energy gas is sprayed into the inner cavity of the first working rotor through the inner port 10 of the first working rotor with a certain reverse tangential angle to the rotating direction of the working wheel body 8 to impact the stationary blades 11 on the working rotor to generate a strong reverse thrust The high-energy gas after impacting the stator blade 11 for doing work is reduced in speed again and slowed down, the high-energy gas after impacting the stator blade 11 for doing work enters the stator blade space 12 for doing work to continue to expand and reduce the pressure, the high-energy gas after expanding and reducing the pressure is ejected from the lower opening of the stator blade space 12 for doing work at a high speed to push the second rotor blade 9 'for doing work in the inner cavity of the stator for doing work again, the high-energy gas after doing work is reduced again and enters the second rotor blade space 10', the high-energy gas in the second rotor blade space 10 'for doing work again expands and reduces the pressure and is ejected from the second rotor blade space 10' in the reverse direction of the rotation of the rotor body 8 for doing work again to provide a reverse thrust to push the second rotor for doing work to do work again, the high-energy gas after expanding in the second rotor blade space 10 'for doing work is ejected again through the inner opening of the rotor blade space 10' in a certain reverse tangential angle to do work again to push the second rotor body 8 for doing work to do work The static blade 11 ' in the rotor cavity impacting the second working stator generates a reverse thrust to push the second working rotor again to drive the working wheel body 8 to rotate and work, the energy of the high-energy gas impacting the second working stator static blade 11 ' to work is reduced again, the speed of the high-energy gas impacting the second working stator static blade 11 ' is reduced again, the high-energy gas impacting the second working stator static blade 11 ' enters the second working stator static blade space 12 ' to continue to expand and reduce the pressure, the high-energy gas expanded and reduced in pressure again is sprayed out at a high speed from the lower opening of the second working stator static blade space 12 ' again to push the third working rotor movable blade 9 ' in the cavity of the second working stator to work, the energy of the high-energy gas after working again is reduced again and enters the third working rotor movable blade space 10 ', the high-energy gas in the third working rotor movable blade space 10 ' is sprayed into the third working rotor movable blade space 10 ' through the inner opening of the third working rotor movable blade space 10 ' and then generates a reverse tangential angle, namely, the reverse working rotor cavity 8 rotates in the reverse direction A reverse thrust pushes the third working rotor again to drive the working wheel body 8 to rotate and work, the energy of the high-energy gas impacting the third working stator blade 11 'to work is reduced again, the high-energy gas impacting the third working stator blade 11' enters the third working stator blade space 12 'to continue to expand and reduce the pressure, the high-energy gas expanded and reduced the pressure again is sprayed out at high speed from the lower opening of the third working stator blade space 12' to push the fourth working rotor blade 9v in the inner cavity of the third working stator to work, the energy of the high-energy gas after working again is reduced again and enters the fourth working rotor blade space 10v, the high-energy gas in the fourth working rotor blade space 10v is sprayed into the fourth working rotor in the inner cavity of the fourth working rotor again at a certain reverse tangential angle, namely, the reverse thrust is generated again to push the fourth working rotor to drive the fourth working rotor body 8 to rotate and work together, high-energy gas which is repeatedly applied for multiple times in the inner cavity of the fourth working rotor is changed into waste gas with extremely low pressure and is exhausted from the exhaust port 18 of the working wheel cavity 14, in operation, along with the reduction of the gas pressure difference in the rear cavity 20 of the cylindrical combustion chamber and the front cavity 19, the top of the porous bell-shaped telescopic flame stabilizer 21, namely the fuel injector 22, also moves to the initial position along with the rebound action of the spring 56 in front of the position controller 54 towards the rear cavity 20 of the cylindrical combustion chamber, the central processor 32 can control the fuel injection amount of the fuel injector 22 and the starting device 52 according to pressure signals provided by the temperature sensor 33 and the pressure sensor 34, in operation, the working rotor can drive the starting motor on the starting device 52 to generate electricity to output electricity for electric equipment or charge a storage battery at the same time of driving the air rotor, when the rotation speed of the working rotor is reduced, the cpu 32 can apply a forward or reverse current to the starter motor of the starter device 52 and the control motor stator 37 of the power distributor 38 to supply an additional assisting power to the control motor rotor 36, i.e., the ring gear of the planetary gear set, in a hybrid mode to output power via the hub 3 and the power output shaft 40, and in operation, can also apply a forward or reverse current to the control motor stator 37, and apply a forward or reverse force to the control motor rotor 36, i.e., the ring gear of the planetary gear set, in a variable gear ratio mode to output power to the power output shaft 40, by applying a power to the power distributor 38 in a fixed gear ratio mode, or applying a forward or reverse current to the control motor stator 37, and applying a forward or reverse force to the control motor rotor 36, i.e., the ring gear of the planetary gear set, and the control motor of the power distributor 38 can also apply a pure electric mode to the control motor rotor 38 alone when the work rotor does not operate The power output shaft 40 outputs electric power.

Fig. 25, fig. 26, fig. 27, fig. 28, and fig. 29 collectively show an eleventh embodiment of this embodiment, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is formed by a machine body 1, a wheel shaft 3, and two basic power units formed by an air compressing device, a work doing device, and a gas generating device, in a serial manner, the air compressing device of the first basic power unit is formed by an air compressing wheel body 2 and an air compressing rotor, the work doing device of the first basic power unit is formed by a work doing wheel body 8 and a work doing rotor, the air compressing device of the second basic power unit is formed by a second air compressing wheel body 2 'and a second air compressing rotor, the work doing device of the second basic power unit is formed by a second work doing wheel body 8' and a second work doing rotor, the air compressing wheel body 2 and the air compressing rotor, and the wheel body 8 and the work doing rotor on the first basic power unit are respectively installed on a first air compressing wheel cavity 13 and a first work doing wheel cavity 13 In the wheel cavity 14, the second compressor wheel body 2 'and the second compressor rotor and the second working wheel body 8' and the second working rotor on the second basic power unit are respectively installed in the second compressor wheel cavity 13 'and the second working wheel cavity 14' on the same axis in the machine body 1, the wheel shaft 3 is installed on the center of the compressor wheel body 2 and the working wheel body 8 as well as the second compressor wheel body 2 'and the second working wheel body 8', the wheel shaft 3 in the machine body 1 is provided with a starting device 52, a supporting bearing and a sealing device 53, the compressor rotor is composed of a plurality of compressor rotor movable blades 4 with a certain bending angle, the plurality of strip-shaped compressor rotor movable blades 4 with a certain bending angle are arranged into a roller shape along the rotation direction of the compressor wheel body 2 according to a certain tangential angle and interval, one end of each compressor rotor movable blade is installed and fixed on the side surface of the compressor wheel body 2, and the other end of each compressor rotor movable blade corresponds to the wall of the compressor wheel cavity 13 opposite to the compressor wheel body 2 and keeps a, the roller-shaped compressed air rotor is arranged along the same axis of the wheel shaft 3, the acting rotor is composed of an acting wheel body 8 and a plurality of acting rotor movable blades 9 with a certain bending angle, the plurality of strip-shaped acting rotor movable blades 9 with a certain bending angle, namely the bending angle, are arranged into a roller shape according to a certain cutting angle and intervals along the rotating direction of the acting wheel body 8, one end of each roller-shaped acting rotor movable blade is fixedly arranged on the side surface of the acting wheel body 8, the other end of each roller-shaped acting rotor movable blade corresponds to the wall of the acting wheel cavity 14 opposite to the acting wheel body 8 and keeps a certain sealing interval, the roller-shaped acting rotor is arranged along the same axis of the wheel shaft 3, the second compressed air rotor is composed of a plurality of second compressed air rotor movable blades 4 'with a certain bending angle, the plurality of strip-shaped second compressed air rotor movable blades 4' with a certain bending angle are arranged into a roller shape according to a certain cutting angle and intervals along the rotating, one end of the second air compression wheel body is fixedly arranged on the side surface of the second air compression wheel body 2 ', the other end of the second air compression wheel body corresponds to the wall of a second air compression wheel cavity 13' opposite to the second air compression wheel body 2 'and keeps a certain sealing gap, the rolling-shaped second air compression rotor and the same axis of the wheel shaft 3 are provided, the second acting rotor is composed of a plurality of second acting rotor movable blades 9' with a certain bending angle, the plurality of strip-shaped second acting rotor movable blades 9 'with a certain bending angle, namely the bending angle, are arranged into a rolling shape according to a certain tangential angle and intervals along the rotating direction of the second acting wheel body 8', one end of the rolling-shaped second acting rotor movable blades 9 'is fixedly arranged on the side surface of the second acting wheel body 8', the other end of the rolling-shaped second acting rotor and the same axis of the wheel shaft 3 correspond to the wall of the second acting wheel cavity 14 'opposite to the second acting wheel body 8' and keeps a certain sealing gap, the air compression wheel cavity, the gas compression wheel cavity 13 gas outlet 16 is on the gas compression wheel cavity 13 circumferential wall, the working wheel cavity 14 gas inlet 17 is on the working wheel cavity 14 circumferential wall, the working wheel cavity 14 gas outlet 18 is in the working wheel cavity 14 side center, the second gas compression wheel cavity 13 'gas inlet 15' is in the second gas compression wheel cavity 13 'side center, the second gas compression wheel cavity 13' gas outlet 16 'is on the second gas compression wheel cavity 13' circumferential wall, the second working wheel cavity 14 'gas inlet 17' is on the second working wheel cavity 14 'circumferential wall, the second working wheel cavity 14' gas outlet 18 'is in the second working wheel cavity 14' side center, the gas generator is above the gas compression rotor and the working rotor by the combustion chamber front chamber 19, the combustion chamber rear chamber 20, the porous bell-shaped flame stabilizer 21, the fuel injector 22, the fuel supply device 23, the fuel vaporizer 24, the fuel vaporizer control device 25, The gas hole on the porous bell-shaped flame holder 21 starts to gradually increase from the top of the porous bell-shaped flame holder 21 to the bottom of the porous bell-shaped flame holder 21, the fuel injector 22 is arranged on the center of the top of the porous bell-shaped flame holder 21 in the vortex-shaped combustion chamber, the fuel vaporizer 24 is arranged at the nozzle of the fuel injector 22, the fuel vaporizer 24 is connected with a fuel vaporizer control device 25, the fuel injector 22 is communicated with a fuel supply device 23 outside the machine body 1 through a pipeline, the igniter 26 is arranged at the bottom of the porous bell-shaped flame holder 21 at the gas nozzle 27 end of the rear combustion chamber 20, the front combustion chamber 19 is provided with a combustion chamber gas inlet 29, the rear combustion chamber 20 is provided with a combustion chamber gas nozzle 27, the gas outlet 16 of the gas compression wheel chamber 13 is communicated with the combustion chamber gas inlet 29, the combustion chamber gas nozzle 27 is communicated with the gas inlet 17 of the working wheel chamber 14, the air inlet 15 of the air compression wheel cavity 13 and the air outlet 18 of the power wheel cavity 14 are communicated with the atmosphere, the second fuel gas generating device on the second basic power unit is composed of a second combustion chamber front chamber 19 ', a second combustion chamber rear chamber 20', a second porous bell-shaped flame holder 21 ', a second fuel injector 22', a second fuel supply device 23 ', a second fuel vaporizer 24', a second fuel vaporizer control device 25 ', a second igniter 26' and a second pressure sensor 34 'above a second air compression rotor and a second power rotor, the air holes on the second porous bell-shaped flame holder 21' are gradually enlarged from the top of the second porous bell-shaped flame holder 21 'to the bottom of the second porous bell-shaped flame holder 21', the second fuel injector 22 'is installed on the center of the top of the second porous bell-shaped flame holder 21', the second fuel vaporizer 24 'is installed at the nozzle of the second fuel injector 22', the second fuel vaporizer 24 'is connected with a second fuel vaporizer control device 25', the second fuel injector 22 'is communicated with a second fuel supply device 23' outside the engine body 1 through a pipeline, the second igniter 26 'is installed at the bottom of a second porous bell-shaped flame stabilizer 21' at the end of an air jet 27 'of a rear chamber 20' of the second combustion chamber, a second combustion chamber air inlet 29 'is arranged on the front chamber 19' of the second combustion chamber, a second combustion chamber air jet 27 'is arranged on the rear chamber 20' of the second combustion chamber, an air outlet 16 'of the second air pressure wheel chamber 13' is communicated with the second combustion chamber air inlet 29 ', the second combustion chamber air jet 27' is communicated with an air inlet 17 'of the second work wheel chamber 14', an air inlet 15 'of the second air pressure wheel chamber 13' and an air outlet 18 'of the second work wheel chamber 14' are communicated with the atmosphere, and the fuel injector 22, the fuel supply device 23, the second fuel supply device 23 'and the second air outlet 18' are communicated with the atmosphere, The fuel vaporizer 24, the fuel vaporizer control device 25, the igniter 26, the pressure sensor 34, the starting device 52, the battery pack 31, the second fuel injector 22 ', the second fuel supply device 23', the second fuel vaporizer 24 ', the second fuel vaporizer control device 25', the second igniter 26 ', and the second pressure sensor 34' are connected with the central processing unit 32 through the electric cable 30.

The basic working principle is as follows: when the air compressor works, the central processing unit 32 is connected with a power supply on the starting device 52, a starting motor on the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2 and the acting wheel body 8 to drive the air compressing rotor and the acting rotor and the second air compressing wheel body 2 'and the second acting wheel body 8' to drive the second air compressing rotor and the second acting rotor to rotate at a high speed through the wheel shaft 3, air in the movable blade space 5 in the air compressing rotor is thrown away from the air compressing rotor by the movable blades 4 under the action of centrifugal force, negative pressure is generated in the movable blade space 5, air in the inner cavity of the air compressing rotor enters the movable blade space 5 of the air compressing rotor under the action of atmospheric pressure, the air pressure in the inner cavity of the air compressing rotor is reduced, the air continuously enters the inner cavity of the air compressing rotor through the air inlet 15 of the air compressing wheel cavity 13 under the action of atmospheric pressure, and the air in the movable blade space 5 of the air compressing rotor is continuously thrown away from the The gas enters the front chamber 19 of the combustion chamber through the air inlet 29 of the combustion chamber on the gas generator, the compressed air in the front chamber 19 of the combustion chamber firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the rear chamber 20 of the combustion chamber, the air holes on the flame stabilizer 21 are gradually enlarged from the top to the bottom, the flow rate characteristic of the compressed gas in the flame stabilizer 21 is that the top flow rate is relatively slow, the bottom flow rate of the flame stabilizer 21 is relatively fast, when using the gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel supply device 23, is sprayed into the top of the flame stabilizer 21 from the nozzle of the fuel injector 22 and is mixed with the high-compressed gas in the top of the flame stabilizer 21 to form combustible high-compressed mixed gas, and the combustible high-compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom, the ignited combustible high-pressure compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure fuel gas, when liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like is used, the liquid fuel is pressurized by the fuel supply device 23 and then is atomized by the fuel injector 22 and sprayed into the top of the flame holder 21 at a high speed to be mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure fuel gas, the central processor can also provide high-frequency electromagnetic pulse waves to the fuel vaporization heater 24 through the fuel vaporizer control device 25 to heat a pipeline at the nozzle of the fuel injector 22, so that the fuel is sprayed into the top of the flame holder 21 in a vaporization mode in the fuel injector 22 at a high speed to be mixed with the compressed gas in the, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom of the flame stabilizer 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is called high-energy gas for short and is sprayed into the air inlet 17 of the working wheel cavity 14 at a high speed through the air nozzle 27 of the combustion chamber, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is sprayed into the working wheel cavity 14 at a high speed with a certain tangential angle to collide with the movable blades 9 on the working rotor to push the working rotor to rotate, part of energy is converted into rotary mechanical energy to reduce the flow speed of the rotary mechanical energy when the high-energy gas collides with the movable blades 9 of the working rotor, the high-energy gas enters the movable blade space 10 of the working rotor to continue to expand after the flow speed of the high-energy gas is slowed down, the high-energy gas is sprayed into the inner cavity of the working rotor through, the working rotor drives the working wheel body 8 to rotate together, the pressure energy of the high-energy gas is converted into rotary mechanical energy to drive the air compressing wheel body 2 to drive the air compressing rotor to rotate through the wheel shaft 3, the residual power is output through the wheel shaft 3, the waste gas with certain residual pressure after working is finally exhausted through the exhaust port 18 of the working wheel cavity 14, the working principle of a second basic power unit connected in series on the wheel shaft 3 is the same as that of the first basic power unit, and the space is saved.

Fig. 30, fig. 31, and fig. 32 collectively show a twelfth embodiment of this embodiment, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is a basic power unit composed of a machine body 1, a wheel shaft 3, an air compressing device, a work applying device and two gas generating devices, the air compressing device is composed of an air compressing wheel body 2 and an air compressing rotor, the work applying device is composed of a work applying wheel body 8 and a work applying rotor, the air compressing wheel body 2, the air compressing rotor, the work applying wheel body 8 and the work applying rotor are respectively installed in an air compressing wheel cavity 13 and a work applying wheel cavity 14 on the same axis in the machine body 1, the wheel shaft 3 is installed in the centers of the air compressing wheel body 2 and the work applying wheel body 8, a starting device 52, a support bearing and a sealing device 53 are installed on the wheel shaft 3 in the machine body 1, the air compressing rotor is composed of a plurality, the plurality of strip-shaped air compressing rotor movable blades 4 with certain bending angles, short for being called as certain bending angles, are arranged into a roller shape along the rotating direction of the air compressing wheel body 2 according to certain cutting angles and certain intervals, one end of each roller-shaped air compressing rotor movable blade is fixedly arranged on the side surface of the air compressing wheel body 2, the other end of each roller-shaped air compressing rotor movable blade corresponds to the wall of an air compressing wheel cavity 13 opposite to the air compressing wheel body 2 and keeps certain sealing gaps, the roller-shaped air compressing rotor is arranged along the same axis of the wheel shaft 3, the acting rotor is composed of an acting rotor body 8 and a plurality of acting rotor movable blades 9 with certain bending angles, the plurality of strip-shaped acting rotor movable blades 9 with certain bending angles, namely certain bending angles, are arranged into a roller shape along the rotating direction of the acting wheel body 8 according to certain cutting angles and certain intervals, one end of each roller-shaped acting rotor movable blade 9 is fixedly arranged on the side surface of the acting wheel, the gas compressor comprises a gas compressor cavity 13, a gas inlet 15, a first gas outlet 16 and a second gas outlet 16 'of the gas compressor cavity 13, a first working wheel cavity 14, a second gas inlet 17' and a working wheel cavity 14, wherein the gas inlet 15 is arranged at the center of the side face of the gas compressor cavity 13, the first gas outlet 16 and the second gas outlet 16 'are uniformly distributed on the circumferential wall of the gas compressor cavity 13, the first working wheel cavity 14 and the second gas inlet 17' are uniformly distributed on the circumferential wall of the working wheel cavity 14, a gas outlet 18 of the working wheel cavity 14 is arranged at the center of the side face of the working wheel cavity 14, a first gas generating device is arranged above a gas compressor rotor and a working rotor and consists of a combustion chamber front cavity 19, a combustion chamber rear cavity 20, a porous bell-shaped flame stabilizer 21, a fuel injector 22, a fuel supply device 23 and an igniter 26, gas holes on the porous bell-shaped flame stabilizer 21 are gradually enlarged, the fuel injector 22 is communicated with a fuel supply device 23 outside the machine body 1 through a pipeline, the igniter 26 is installed at the bottom of a multi-hole bell-shaped flame holder 21 at the air injection port 27 end of a rear chamber 20 of a combustion chamber, a combustion chamber air inlet 29 is arranged on the front chamber 19 of the combustion chamber, a combustion chamber air injection port 27 is arranged on the rear chamber 20 of the combustion chamber, the second fuel generation device is arranged below a compressor rotor and a working rotor and consists of a second combustion chamber front chamber 19 ', a second combustion chamber rear chamber 20 ', a second multi-hole bell-shaped flame holder 21 ', a second fuel injector 22 ', a second fuel supply device 23 ' and a second igniter 26 ', air holes in the second multi-hole bell-shaped flame holder 21 ' are gradually enlarged from the top of the second multi-hole bell-shaped flame holder 21 ' to the bottom of the second multi-hole bell-shaped flame holder 21 ', the second fuel injector 22 ' is installed at the center of the top of the second multi-hole bell-shaped flame holder 21 ' in the vortex-shaped second combustion chamber, the second fuel injector 22 'is communicated with a second fuel supply device 23' outside the machine body 1 through a pipeline, the second igniter 26 'is arranged at the bottom of the second multi-hole bell-shaped flame holder 21' at the gas outlet 27 'end of the rear cavity 20' of the second combustion chamber, the second combustion chamber front chamber 19 'is provided with a second combustion chamber air inlet 29', the second combustion chamber rear chamber 20 'is provided with a second combustion chamber air outlet 27', the first air outlet 16 of the air compressor cavity 13 is communicated with the air inlet 29 of the combustion chamber, the air outlet 27 of the combustion chamber is communicated with the air inlet 17 of the working wheel cavity 14, the air inlet 15 of the air compression wheel cavity 13 and the air outlet 18 of the power wheel cavity 14 are communicated with the atmosphere, the second air outlet 16 'of the gas wheel cavity 13 is communicated with the second combustion chamber air inlet 29', the second combustion chamber exhaust port 27 'is in communication with the second intake port 17' of the power wheel chamber 14.

The basic working principle is as follows: when the air compressor works, a power supply on the starting device 52 is connected, a starting motor on the starting device 52 outputs mechanical energy to drive the air compressing wheel body 2 and the acting wheel body 8 to drive the air compressing rotor and the acting rotor to rotate at a high speed through the wheel shaft 3, air in a movable blade space 5 in the air compressing rotor is thrown away from the air compressing rotor by the movable blades 4 under the action of centrifugal force, negative pressure is generated in the movable blade space 5, the air in an inner cavity of the air compressing rotor enters the air compressing rotor space 5 under the action of atmospheric pressure, the air pressure in the inner cavity of the air compressing rotor is reduced at the moment, the air continuously enters the inner cavity of the air compressing rotor through the air inlet 15 of the air compressing wheel cavity 13 under the action of atmospheric pressure, and the air in the movable blade space 5 in the air compressing rotor is continuously thrown away from the air compressing rotor by the movable blades 4 of the air compressing rotor and then is distributed, the compressed air in the first air outlet 16 enters the combustion chamber front chamber 19 through the combustion chamber air inlet 29 on the first gas generator, the compressed air in the second air outlet 16 ' enters the combustion chamber front chamber 19 ' through the second combustion chamber air inlet 29 ' on the second gas generator, the compressed air in the combustion chamber front chamber 19 firstly rotates around the flame stabilizer 21 in a vortex shape and then passes through the air holes of the flame stabilizer 21 to enter the combustion chamber rear chamber 20, the air holes on the flame stabilizer 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed air in the flame stabilizer 21 is characterized in that the flow rate at the top is relatively slow, the flow rate at the bottom is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel supply device 23 and is injected from the fuel injector 22 into the top of the nozzle orifice flame stabilizer 21 and mixed with the high-pressure compressed air in the top of the flame stabilizer 21 to form combustible high-pressure mixed gas, when liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like is used, the liquid fuel is pressurized by the fuel supply device 23 and then is sprayed into the top of the flame holder 21 in an atomized manner at high speed through the fuel injector 22 to be mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is quickly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is sprayed into the air inlet 17 of the power doing wheel cavity 14 at high speed through the air outlet 27 of the combustion chamber, and the compressed air in the front cavity 19 'of the second combustion chamber firstly surrounds the second flame holder 21' in a vortex shape The gas holes of the second flame holder 21 ' are rotated and then pass through the gas holes of the second flame holder 21 ' to enter the rear cavity 20 ' of the second combustion chamber, the gas holes of the second flame holder 21 ' are gradually enlarged from top to bottom, the flow rate of the compressed gas in the second flame holder 21 ' is characterized in that the flow rate of the compressed gas in the second flame holder 21 ' is relatively slow at the top and the flow rate of the compressed gas in the bottom is relatively fast, when gas fuel such as hydrogen, natural gas, coal gas, methane and the like is used, the gas fuel enters the second fuel injector 22 ' from the second fuel supply device 23 ', is injected into the top of the second flame holder 21 ' from the nozzle of the second fuel injector 22 ' and is mixed with the high-compressed gas in the top of the second flame holder 21 ' to form combustible high-compressed mixed gas, the combustible high-compressed mixed gas flows to the bottom of the second porous bell-shaped flame holder 21 ' and is ignited by the electric spark released by the second igniter 26 ', when liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel oil and the like is used, the liquid fuel is pressurized by a second fuel supply device 23 ' and then is sprayed into the top of a second flame holder 21 ' in an atomized form at a high speed through a second fuel injector 22 ' to be mixed with the compressed gas in the top of the second flame holder 21 ' to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by electric sparks released by a second igniter 26 ' when flowing to the bottom of the second flame holder 21 ', the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature and high-pressure gas, the high-temperature and high-pressure gas is sprayed into a second air inlet 17 ' of a working wheel cavity 14 at a high speed through an air jet 27 ' of a second combustion chamber, the high-energy gas in a first air inlet 17 and a second air inlet 17 ' of the working wheel cavity 14 at a certain tangential angle in two upper and lower directions of the working wheel cavity 14 and simultaneously impacts movable blades 9 on the working rotor to drive the working rotor to rotate, when the high-energy gas impacts the rotor moving blades 9, part of energy is converted into rotary mechanical energy to reduce the flow speed of the high-energy gas, the high-energy gas enters the rotor moving blade space 10 of the working rotor after the flow speed of the high-energy gas is reduced, the high-energy gas after pressure reduction and expansion in the rotor moving blade space 10 of the working rotor is sprayed into the inner cavity of the working rotor through the inner opening of the rotor moving blade space 10 of the working rotor in a certain reverse tangential angle and in the direction opposite to the rotating direction of the working wheel body 8 to generate a reverse thrust to push the working rotor to rotate again, the working rotor drives the working wheel body 8 to rotate together, the pressure energy of the high-energy gas is converted into rotary mechanical energy, the compression wheel body 2 is driven by the wheel shaft 3 to drive the compression wheel body to rotate, the residual power is output by.

Fig. 33, fig. 34, fig. 35, fig. 36, fig. 37, and fig. 38 collectively show a thirteenth embodiment of the present invention, and it can be seen from the drawings that the novel turbine engine shown in this embodiment is also a basic power unit formed by components such as the engine body 1, the wheel shaft 3, the compressor, the working device, and the gas generator, the compressor is formed by a compressor rotor and a compressor wheel cavity 13, the compressor rotor is formed by a compressor wheel body 2 and a compressor rotor blade, a central wheel 42 is provided on the circumferential surface of the compressor wheel body 2, the central wheel 42 divides the circumferential surface of the compressor wheel body 2 into two parts, namely a large circumferential surface and a small circumferential surface, the circumferential surfaces of the two compressor wheel bodies 2 are oppositely-shaped arcs, the rotor blade is formed by a large blade 43 and a small blade 44, the large blade 43 and the small blade 44 are narrow in the top and wide in the bottom, the large blade 43 is installed on the large circumferential surface, the small blades 44 are arranged on the small circumferential surface, the top edge of the large blade 43, the top edge of the small blade 44 and the top edge of the central wheel 42 keep a non-contact sealing gap with the narrowest part of the inner wall of the corresponding compressor wheel cavity 13, a large semi-circular auxiliary cavity 45 is arranged outside the compressor wheel cavity 13 corresponding to the small blade 44 side in the compressor wheel cavity 13 and communicated with the compressor wheel cavity 13, the large semi-circular auxiliary cavity 45 is wrapped on the compressor wheel cavity 13 corresponding to the small blade 44 except for the air outlet 16 and the periphery of the small blade 44 side, the large blade 43 and the small blade 44 keep a small airtight gap with the wall of the compressor wheel cavity 13 and are not contacted with the wall of the compressor wheel cavity 13, a large semi-circular cavity ring 46 is arranged between the large semi-circular auxiliary cavity 45 and the compressor wheel cavity 13, the diameter of the large semi-circular cavity ring 46 is smaller than that of the large semi-circular auxiliary cavity 45, the cross section of the large semi-circular cavity ring 46 is matched with the radian of the corresponding axial side edge of the small blade 44 and keeps, the cross section of the large semicircular auxiliary cavity 45 is C-shaped, the upper opening of the large semicircular auxiliary cavity 45 with the C-shaped cross section corresponds to the top edge of the small blade 44, the lower opening of the large semicircular auxiliary cavity 45 with the C-shaped cross section corresponds to the bottom edge of the small blade 44, the large semicircular auxiliary cavity 45 with the C-shaped cross section and the small blade cavity 63 form an annular channel which takes a large semicircular cavity ring 46 as an inner annular shaft, the air outlet 16 of the air compressor cavity 13 is communicated with the air compressor cavity 13 along the rotating direction of the air compressor cavity 13 corresponding to the top end of the small blade 44 from the air compressor cavity 13 to the outside along the rotating direction of the air compressor 2, the air compressor cavity is communicated with the air compressor cavity 13 inwards, the working device is composed of two roller-shaped working rotors with different diameters and a cylindrical working stator, the axial lengths of the two roller-shaped working rotors with different diameters are the same as that of the cylindrical working stator, the two roller-shaped working rotors with different diameters are sleeved on the side surface of the working wheel body 8 according to the same axis, the other ends of the two roller-shaped working rotors keep a tiny airtight gap with the wall of the corresponding working wheel cavity 14, one end of the cylindrical working stator is fixedly arranged on the inner wall of the working wheel cavity 14 opposite to the side surface of the working wheel body 8, the other end of the cylindrical working stator is sleeved between the two roller-shaped working rotors and keeps a tiny airtight gap with the side surface of the corresponding working wheel body 8, the cylindrical working stator keeps a tiny airtight gap with the inner roller-shaped working rotor and the outer roller-shaped working rotor, the wheel shaft 3 is arranged on the centers of the working wheel body 8 and the air compressing wheel body 2, the wheel shaft 3 is provided with a starting and speed changing device 35, a supporting bearing and a sealing device 53, the center of the air compressing wheel cavity 13 is provided with an air inlet 15, the center of the, the working wheel chamber 14 is circumferentially provided with an air inlet 17,

The speed change device 35 is composed of a planetary gear set with a locking mechanism and a planetary gear set control motor, the planetary gear set control motor is composed of a motor rotor 36 arranged on a large gear ring in the planetary gear set and a motor stator 37 fixed on the machine body 1, the motor stator 37 is connected with a central processing controller 32 through a cable 30, the gas generating device is composed of a cylindrical combustion chamber front cavity 19, a cylindrical combustion chamber rear cavity 20, a porous bell-shaped flame stabilizer 21, a fuel injector 22, a fuel supply device 23, an igniter 26, a pressurizing fuel injector 28, a pressurizing ignition 29, a device storage battery pack 31, the central processing controller 32, a pressure sensor 34 and a vaporization heater 24, the combustion chamber front cavity 19 is provided with a combustion chamber air inlet 29, the combustion chamber rear cavity 20 is provided with a combustion chamber air outlet 27, an air pressure wheel cavity 13 air outlet 16 is communicated with the combustion chamber air inlet 29, the combustion chamber jet 27 communicates with the working wheel cavity 14 air inlet 17, the air inlet 15 of the air compressor cavity 13 and the air outlet 18 of the working wheel cavity 14 communicate with the atmosphere, there is a temperature sensor 33 on the air outlet 18, the air hole on the porous bell-shaped flame stabilizer 21 begins to grow gradually from the top of the porous bell-shaped flame stabilizer 21 to the bottom of the porous bell-shaped flame stabilizer 21, the fuel injector 22 is installed on the center of the top of the porous bell-shaped flame stabilizer 21 in the cylindrical combustion chamber, the fuel injector 22 and the pressurizing fuel injector 28 communicate with the fuel supply device 23 outside the engine body 1, the vaporizing heater 24 is installed on the pipelines at the jet ports of the fuel injector 22 and the pressurizing fuel injector 28, the vaporizing heater 24 is connected with a control device 25 of the vaporizing heater 24, the control device 25 is connected with a central processor 32, the igniter 26 is installed at the bottom of the porous bell-shaped flame stabilizer 21 at the jet 27 of the cylindrical combustion chamber back cavity 20, the combustion chamber front cavity 19 is provided with a pressure sensor 34, the fuel supply device 23, an igniter 26, a storage battery pack 31, a temperature sensor 33, the pressure sensor 34, a control motor stator 37 on a speed change device 35 and a control device 25 on a fuel vaporization heater 24 are connected with a central processing controller 32 through a cable 30, the booster igniter 29 and a booster fuel injector 28 are sequentially arranged on a combustion chamber air jet 27, namely the cavity wall of the working wheel cavity 14 in front of an air inlet 17 of the working wheel cavity 14, a water sprayer 48 is also arranged on the cavity wall of the working wheel cavity 14 in front of the air inlet 17 of the working wheel cavity 14 and communicated with the working wheel cavity 14, the other end of the water sprayer 48 is connected with a water supply device 51, the working wheel cavity 14 in the air inlet 17 of the working wheel cavity 14 in the machine body 1 is provided with an arc-shaped movable cavity wall 49 on the circumference, and one end of the arc-shaped movable cavity wall, the other end is arranged in front of the air inlet 17 of the working wheel cavity 14 and is provided with a regulating device 47.

The basic working principle is as follows: when the air compressor works, the central processing unit 32 locks any two gears in the planetary gear set on the speed change device 35 through the locking mechanism on the speed change device 35, the circuit of the battery 31 and the control motor stator 37 on the speed change device 35 is switched on, the control motor rotor 36 is started to output mechanical energy, the wheel shaft 3 is driven by the speed change device 35 to drive the air compressor wheel body 2 and the working wheel body 8 to rotate at high speed, air in the large blade cavity 62 on the air compressor wheel body 2 generates centrifugal force along with the high-speed rotation of the large blade 43 and moves from the bottom of the large blade cavity 62, namely the side face air compressor rotor center of the large blade 43, to the centrifugal end, namely the top end of the large blade 43 along the large blade 43 under the action of the centrifugal force, the pressure intensity at the bottom of the large blade cavity 62 is reduced to generate negative pressure, air in the atmosphere enters the bottom of the large blade cavity 62 through the air inlet 15 under the action of atmospheric pressure, and along with the high-speed, the energy and the speed of the air in the bottom of the large blade cavity 62 rise rapidly, the air with the energy applied by the large blade 43 moves outwards along the large blade 43 at a high speed under the action of centrifugal force and gathers at the top end of the large blade cavity 62 to reduce the speed and boost the pressure, the compressed air with the boosted top end of the large blade cavity 62 enters the gradually-releasing air outlet 59 to reduce the speed and boost the pressure when rotating to the air outlet 59 of the large blade 43, meanwhile, the air in the bottom of the small blade cavity 63 is pushed by the small blade 44 to generate centrifugal force along with the high-speed rotation of the air compressing wheel body 2, the air moves along the small blade 44 to the top end of the small blade cavity 63 under the action of the centrifugal force, the air moving at a high speed in the small blade cavity 63 rotates forwards along with the small blade 44 and is thrown away from the top end of the small blade 44 to enter the upper opening of the front C-shaped auxiliary cavity 45 section, negative pressure is generated at the bottom of the small blade cavity 63, and the air in the lower opening of the The blade cavity 63 rotates forwards along with the small blade 44, negative pressure is generated in the rear end of the large semi-circular auxiliary cavity 45, compressed air pressurized by the large blade 43 in the air outlet 59 of the large blade 43 is sucked into the rear end of the large semi-circular auxiliary cavity 45 through the air inlet 61 of the large semi-circular auxiliary cavity 45, similarly, the compressed air entering the rear end of the large semi-circular auxiliary cavity 45 is sucked into the small blade cavity 63 and is accelerated to be thrown away from the top end of the small blade 44 to enter the upper opening of the front C-shaped auxiliary cavity 45 section while the small blade 44 rotates forwards at a high speed, the compressed air in the upper opening of the C-shaped auxiliary cavity 45 section moves to the lower opening of the C-shaped auxiliary cavity 45 section along the C-shaped stationary blade 6 in the C-shaped auxiliary cavity 45 and surrounds the cavity ring 46, and is decelerated and pressurized at a low speed, the compressed air pressurized again in the lower opening of the C-shaped auxiliary cavity 45 section is swept into the small blade cavity 63 again by the small blade 44 which is then transferred to rotate at a high speed along, the compressed air in the section of the C-shaped auxiliary cavity 45 moves towards the lower port of the C-shaped auxiliary cavity 45 along the C-shaped stator blade 6 in the C-shaped auxiliary cavity 45 and around the cavity ring 46 again after being energized again by the small blades 44, the compressed air in the section of the C-shaped auxiliary cavity 45 is pushed by the small blades 44 to perform continuous spiral supercharging motion in the C-shaped auxiliary cavity 45 and the small blade cavities 63 along the C-shaped stator blade 6 in the C-shaped auxiliary cavity 45 and around the cavity ring 46, the compressed air is energized once by the small blades 44 once when entering the small blade cavities 63, the compressed air is energized for multiple times continuously by the small blades 44 to form compressed air, the compressed air enters the front combustion chamber 19 through the air outlet 16 of the air compression wheel cavity 13 and the combustion chamber air inlet 29 on the gas generating device, the compressed air in the front combustion chamber 19 firstly rotates in a spiral shape around the flame stabilizer 21 and then passes through the air holes of the rear combustion chamber 21 to enter the combustion chamber In the chamber 20, the air holes of the flame holder 21 are gradually enlarged from the top to the bottom, the flow rate of the compressed gas in the flame holder 21 is characterized in that the top flow rate is relatively slow, the bottom flow rate of the flame holder 21 is relatively fast, when using gas fuel such as hydrogen, natural gas, coal gas, methane and the like, the gas fuel enters the fuel injector 22 from the fuel supply device 23, is sprayed into the top of the flame holder 21 from the nozzle of the fuel injector 22 and is mixed with the high-pressure compressed gas in the top of the flame holder 21 to form combustible high-pressure compressed mixed gas, the combustible high-pressure compressed mixed gas is ignited by electric sparks released by the igniter 26 when flowing to the bottom of the porous bell-shaped flame holder 21, the ignited combustible high-pressure compressed mixed gas is rapidly combusted and expanded to release heat energy to generate high-temperature high-pressure gas, when using liquid fuel with poor volatility such as gasoline, kerosene, alcohol, diesel and the like, the liquid fuel can be directly pressurized by the fuel supply device 23 and then is sprayed into the top of the flame holder The compressed gas in the part is mixed to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, the central processor can also provide high-frequency electromagnetic pulse wave to the fuel vaporization heater 24 through the fuel vaporizer control device 25 to heat a pipeline at the nozzle of the fuel injector 22, so that the fuel is injected into the top of the flame holder 21 in a vaporization form at a high speed in the fuel injector 22 and is mixed with the compressed gas in the top of the flame holder 21 to form combustible compressed mixed gas, the combustible compressed mixed gas is ignited by the electric spark released by the igniter 26 when flowing to the bottom of the flame holder 21, the ignited combustible compressed mixed gas is rapidly combusted and expanded and releases heat energy to generate high-temperature high-pressure gas, the high-temperature high-pressure gas is short for short, and is injected into the air inlet, the high-energy gas at the air inlet 17 of the working wheel cavity 14 is injected into the working wheel cavity 14 at a high speed with a certain tangential angle to impact the movable blades 9 on the first working rotor to drive the first working rotor to rotate, when the high-energy gas impacts the movable blades 9 of the first working rotor, part of the energy is converted into rotary mechanical energy to reduce the flow rate of the high-energy gas, the high-energy gas enters the movable blade space 10 of the first working rotor after the flow rate of the high-energy gas is reduced, the high-energy gas continuously expands along with the forward rotation of the movable blades 9 of the first working rotor after entering the movable blade space 10 of the first working rotor, after the high-energy gas which is decompressed and expanded in the movable blade space 10 of the first working rotor after passing through the arc-shaped air-blocking block 41 on the working stator, the high-energy gas is injected into the inner cavity of the movable blade space 10 of the first working rotor with a certain tangential angle and in the reverse working direction to impact the stationary blades 11 on the working stator to generate a strong reverse thrust to drive the first working rotor to drive the working wheel body 8 to rotate together, the high-energy gas after impacting the stator vane 11 of the working stator enters the stator vane space 12 of the working stator to continue to expand and reduce the pressure, the high-energy gas after expanding and reducing the pressure is ejected from the lower opening of the stator vane space 12 of the working stator at a high speed to push the second rotor blade 9 'in the inner cavity of the working stator to work again, the energy of the high-energy gas after doing work again is reduced and enters the second rotor blade space 10', the high-energy gas in the second rotor blade space 10 'is expanded and reduced again and ejected from the second rotor blade space 10' against the rotating direction of the working wheel body 8 to provide a reverse thrust to push the second rotor to do work again, the waste gas with a certain residual pressure after doing work is exhausted from the exhaust port 18 of the working wheel cavity 14, during the work, the central processor 32 can apply a forward or reverse current to the stator 37 of the control motor to apply a forward or reverse force to the rotor 36 of the control motor, namely a large gear ring of a planetary gear set in the speed changing device 35, the working rotor outputs power to the air compressing rotor in a variable speed ratio mode through the wheel shaft 3 via the speed changing device 35, when the blocked rotating speed of the working rotor is reduced, the positive or reverse current can be applied to the control motor rotor 36, namely an extra assisting force is applied to a large gear ring of a planetary gear set in the speed changing device 35 to output power to the air compressing rotor in a hybrid mode, of course, a sun gear and a planetary gear of the planetary gear set in the speed changing device 35 can be locked, the air compressing rotor and the working rotor are driven to rotate by the control motor, the control motor is used as a starter, the working rotor can drive the control motor to generate power to output power to electric equipment or charge a storage battery while driving the air compressing rotor, in operation, when a large torsion is required to be output by the wheel shaft 3, the opening degree of the movable cavity wall 49 can be adjusted by the adjusting device 47, the opening degree of the movable cavity wall 49 is increased, more high-temperature high-pressure gas enters the acting wheel cavity 14, the high-temperature high-pressure gas simultaneously pushes more acting rotor movable blades 9 to generate larger torsion, when the torsion needs to be reduced, the adjustment and control device 47 can also adjust the movable cavity wall 49, the opening degree of the movable cavity wall 49 is reduced, the high-temperature high-pressure gas is reduced to enter the acting wheel cavity 14, and the high-temperature high-pressure gas pushes less acting rotor movable blades 9 to reduce the output torsion. When high-power work is needed, fuel can be directly sprayed into the working wheel cavity 14 through the pressurizing fuel injector 28 to be subjected to afterburning pressurization in high-temperature and high-pressure fuel gas, so that the fuel gas pressure in the working wheel cavity 14 is further improved, the working rotor movable blades 9 work under higher back pressure, the igniter 26 can be closed, so that combustible mixed gas in the combustion chamber rear cavity 20 enters the working wheel cavity 14 through the working wheel cavity 14 air inlet 17, due to the fact that the working stator in the working wheel cavity 14 is provided with the arc-shaped air blocking blocks 41 corresponding to the air inlet 17, the combustible mixed gas cannot be sprayed out from the lower opening of the working rotor movable blade space 10 temporarily, and only can rotate forwards along with the working rotor movable blades 9 in the working rotor movable blade space 10, when the working rotor movable blades 9 rotate through the arc-shaped air blocking blocks 41 on the working stator, reach the pressurizing igniter 29, the combustible mixed gas in the working rotor movable blade space 10 is ignited and combusted through the pressurizing igniter 29, and simultaneously is sprayed out towards the lower opening of the working rotor movable blades 10 in the opposite direction to impact the working rotor movable blades The combustion point and the combustion chamber are two relatively independent spaces, the high pressure generated by the combustion of the combustible mixture does not generate impact interference on the combustible mixture in the rear cavity 20 of the combustion chamber, the flow of the compressed mixture formed in the combustion chamber is not influenced, and the working wheel has the advantages that the pressure in the working wheel cavity 14 is further improved, namely the working backpressure of the working rotor movable blades 9 is further improved, the torsion output by the working rotor is further improved, the water sprayer 48 on the cavity wall of the working wheel cavity 14 can spray proper amount of water mist into the working wheel cavity 14 according to the exhaust temperature in the exhaust port 18 of the working wheel cavity 14 detected by the temperature sensor 33, the temperature in the working wheel cavity 14 is reduced, a large amount of water vapor can be generated, the pressure in the working wheel cavity 14 is further improved, and the central processor 32 collects gas through various sensors, After the information of the pressure, the temperature, the rotating speed of the working rotor and the air compressing rotor of the combustible mixed gas, the compressed air and the like is calculated and processed, an instruction is output to various actuators such as an igniter 26, a booster igniter 29, a fuel supply device 23, a fuel injector 22, a booster fuel injector 28, a water sprayer 48, a regulating device 47 on a movable cavity wall 49, a control motor on a speed changing device 35 and the like to adjust the fuel injection amount, the injection point, the combustion point, the atomized water injection amount, the opening degree of the movable cavity wall 49 and the rotating speed ratio of the working rotor and the air compressing rotor in time, so that the gas temperature, the air-fuel ratio of the combustible mixed gas, the pressure of the compressed air, the rotating speed of the wheel shaft 3 and the like are kept at the.

The application is not limited to the thirteen embodiments, and can have many changes, the thirteen embodiments can be interchanged, have intermodulation complementation, can also be respectively omitted, and can also combine all the structural advantages together to form a novel turbine engine, and can also be selectively and preferentially combined to form the novel turbine engine, furthermore, all the basic power units described in the above embodiments are not limited to the novel turbine engine with one basic power unit, and can be the same as a piston engine, more than one basic power units are connected in series to form a multi-unit novel wheel engine, more than one basic power units are connected in series to form the multi-unit novel turbine engine, the gas generating device can be one or more than one ring structure, the gas compressing device can be a multi-segment gas compressing mechanism formed by connecting one, two or more than two gas compressing devices in series, the air compressing device and the power generating device can be connected by a speed changing device consisting of gears, the speed changing connection mode can be a coaxial connection mode or a split shaft connection mode, and can be a concentric shaft connection mode or a non-concentric connection mode, the planetary gear set can be a planetary gear set with a locking mechanism, a control motor is arranged on the planetary gear set, the planetary gear set can be a single planetary gear set structure or a multi-planetary structure consisting of two or more planetary gear sets, the single planetary gear set structure and the multi-planetary structure can be started by a conventional mechanical mode in the prior art, the above changes are within the protection scope of the application, and as can be seen from the description of the above thirteen embodiments, the technical advantages of the application are as follows: the planetary gear set is a special gear structure, the structure form is changeable and easy to control, and the structure mode can be selected at will, so that the rotating speed ratio of the acting device and the air compressing device can be automatically adjusted according to various working conditions in work, the acting device and the air compressing device can be self-adaptive, the rotating speed ratio between the acting device and the air compressing device can be adjusted by controlling the motor through the planetary gear set, the air compressing device can output compressed air with different compression ratios under the condition of the same rotating speed of the acting device, the variable adjustment and the control of the compression ratio are realized, the compressed air with different compression ratios required by the combustion of various fuels can be provided for a combustion chamber under the condition of not changing the hardware of a machine, and the selection of one machine with multiple fuels is realized. II, secondly: the air compressing device and the work doing device of the novel turbine engine can compress air and do work for multiple times simultaneously in one rotation, and the working effect which can be realized by the multi-stage air compressing turbine and the multi-stage work doing turbine on the axial-flow turbine engine is realized on a single air compressing unit, namely a single air compressing wheel body, and a single work doing unit, namely a single work doing wheel body. Thirdly, the method comprises the following steps: the spring 56 is arranged on the extension pipe 55 in the front cavity 19 of the combustion chamber, in operation, the relative position of the porous sleeve-shaped telescopic flame stabilizer 21 between the front cavity and the rear cavity in the combustion chamber can be automatically adjusted under the assistance of the spring 56, the fuel vaporizer 24 is arranged at the nozzle of the fuel injector 22, liquid fuel is vaporized and then injected into the combustion chamber, the premixing speed of the fuel and compressed air is improved, the fuel application range is wider due to the variable, adjustable and controllable combustion chamber, the fuel can be combusted more fully, and the heat efficiency is higher. Fourthly, the method comprises the following steps: the novel turbine engine changes a multistage axial flow type turbine working technology in the turbine engine into a multistage centripetal type turbine working technology, axial working is changed into centripetal working, not only the direction is changed, but also the essence is the subversive change of a stress point, because the diameters of rotors of various stages of working turbines which do work axially in the prior art are in a relationship of increasing step by step, the diameter of the initial stage, namely the first stage working turbine, is minimum and increases step by step backwards, namely the working turbine with the minimum diameter is firstly pushed by high-energy gas, the diameter of the working turbine which is pushed by the step-by-step reduction of the internal energy of the high-energy gas is increased step by step, the speed of the tip of the working turbine is increased step by step, which is just opposite to the relationship that the internal energy of the high-energy gas attenuates step by step and weakens the flow speed and slows down after the high-energy gas works, and the conversion efficiency of the speed of active fluid is, the diameters of all stages of working turbines doing centripetal work are reduced step by step, namely the rotating speeds of the blade tips of all stages of working turbines doing centripetal work are reduced step by step, which exactly accords with the theory of hydromechanics, and secondly, the difference of the stress points is different, according to the lever principle in the mechanics, the difference between the stress points and the stress points is larger, so that the conversion efficiency is easy to improve, the novel turbine working technology just utilizes the characteristic to ensure that high-energy gas firstly does work on the turbine with the largest diameter, so that the output torque of the wheel shaft 3 is effectively improved, and the multistage axial flow turbine engine needs a plurality of air compressor wheel bodies 2 and a plurality of working wheel bodies 8 for installing air compressor blades and working blades, so that the relatively longer wheel shaft 3 is needed, the rigidity and the strength of the wheel shaft 3 are relatively weakened, the weight of the whole machine is increased, the inertia of the whole rotator is also increased, and the multistage air compressor turbine doing centripetal work does not need the longer wheel shaft 3, the plurality of air compressor wheel 8, the rigidity and the strength of the wheel shaft 3 are relatively improved, and the weight of the whole machine and the inertia of the whole swivel are reduced to the maximum extent. Fifthly: this novel turbine engine's the design has activity chamber wall 49 on the wheel chamber that does work, activity chamber wall 49 makes the wheel chamber 14 volume that does work realize variably, can control the air input through the activity aperture of regulation and control device 47 regulation and control activity chamber wall 49 in the work, can let more high temperature high pressure gas get into and make more rotor movable blades 9 that do work simultaneously promote in the wheel chamber 14 that do work under the unchangeable condition of admission pressure in order to produce bigger torsion, when needs reduce torsion, equally can carry out the callback to activity chamber wall 49 through regulation and control device 47, it gets into in the wheel chamber 14 to reduce high temperature high pressure gas, let high temperature high pressure gas promote less rotor movable blade 9 that do work in order to reduce the torsion of output. Sixthly, the method comprises the following steps: the hybrid power and energy recovery function can be realized by controlling a motor to lock a large gear ring of a planetary gear set in the speed change device 35, namely a control motor rotor 36, outputting power to the air compressing rotor through the wheel shaft 3 through the speed change device 35 in a fixed speed change ratio mode during work, applying forward or reverse current to a control motor stator 37, applying forward or reverse force to the control motor rotor 36, namely the large gear ring of the planetary gear set in the speed change device 35, enabling the work rotor to output power to the air compressing rotor through the wheel shaft 3 through the speed change device 35 in a variable speed change ratio mode, applying forward or reverse current to the control motor stator 37 to the control motor rotor 36, namely the large gear ring of the planetary gear set in the speed change device 35 to output power to the wheel shaft 3 in a hybrid power mode when the rotation speed of the work rotor is reduced, of course, the sun gear and the planetary gear of the planetary gear set in the speed changing device 35 may be locked, the control motor drives the pneumatic rotor and the working rotor to rotate, the control motor is used as a starter, the working rotor may drive the control motor to generate power to output power to the electric equipment or charge the battery at the same time of driving the pneumatic rotor, the control motor may be used to lock the big gear ring of the planetary gear set in the power divider 38, i.e. the control motor rotor 36, to make the working rotor output power to the power output shaft 40 in a fixed gear ratio mode through the power divider 38 via the wheel axle 3, or to apply a forward or reverse current to the control motor stator 37, to apply a forward or reverse force to the control motor rotor 36, i.e. the big gear ring of the planetary gear set in the power divider 38, to make the working rotor output power to the power output shaft 40 in a variable gear ratio mode through the wheel axle 3 via the power divider 38, when the blocked rotating speed of the working rotor is reduced, an additional boosting force can be applied to the control motor rotor 36, namely a large gear ring of a planetary gear set in the power divider 38 by applying a forward current or a reverse current to the control motor stator 37 to output power to the power output shaft 40 in a hybrid mode, and the control motor on the power divider 38 can also output electric power to the power output shaft 40 in a pure electric mode through the power divider 38 when the working rotor does not work. Seventhly, the method comprises the following steps: the booster igniter 29 is arranged in front of the air inlet 17 of the working wheel cavity 14, so that air inlet and combustion can be separately carried out, combustible high-pressure mixed gas is ignited and combusted in the working wheel cavity 14, high-temperature high-pressure gas generated by combustion cannot interfere with compressed air in the air inlet 17, namely, the high-temperature high-pressure gas generated by combustion cannot interfere with air compressing work of the air compressing device and cannot influence the air inflow of the compressed air, the pressure in the working wheel cavity 14 is further improved, higher back pressure is generated on the working rotor movable blades 9, and the working rotor outputs higher torque force. Eighthly: the multi-point combustion technology is characterized in that fuel can be sprayed into a combustion chamber rear cavity 20 through a fuel injector 22 and ignited by an igniter 26 to be combusted in the combustion chamber rear cavity 20, the fuel can also be directly sprayed into a working wheel cavity 14 through a pressurizing fuel injector 28 to be combusted in high-temperature and high-pressure gas, the igniter 26 can be closed to enable the fuel to be sprayed into the combustion chamber rear cavity 20 through the fuel injector 22 and mixed with compressed air to form combustible mixed gas, the combustible mixed gas enters the working wheel cavity 14 through a working air inlet 17 and rotates forwards along with a working rotor movable vane space 10 to pass through an arc-shaped gas blocking block 41 on a working stator, then the combustible mixed gas is ignited, combusted and expanded in the working wheel cavity 14 by the pressurizing igniter 29 and simultaneously sprayed out the working stator in the opposite direction through a lower port of the working rotor movable vane space 10, and the combustion point and the combustion chamber are two relatively independent spaces, and at the moment, high pressure generated by combustion of the combustible mixed gas cannot generate impact interference on the combustible mixed gas in the combustion chamber rear cavity 20, the flow of the compressed mixed gas formed in the combustion chamber is not influenced, and the working rotor has the great advantages that the pressure in the working wheel cavity 14 is further improved, namely the working backpressure of the working rotor movable blades 9 is further improved, and the torque output by the working rotor is further improved. Nine: the water sprayer 48 on the wall of the working wheel cavity 14 can spray a proper amount of water mist into the working wheel cavity 14 according to the temperature in the working wheel cavity 14, so that the temperature in the working wheel cavity 14 can be reduced, a large amount of water vapor can be generated to improve the pressure in the working wheel cavity 14, the energy in the fuel gas is squeezed to the maximum extent, the energy of the fuel gas is absorbed and converted to the maximum extent, the fuel utilization efficiency is further improved, the purposes of energy saving, consumption reduction and emission reduction are really realized, the water spraying temperature reduction and pressurization technology thoroughly solves the problem of ultrahigh temperature during high power, the water spraying absorbs the heat energy released by fuel combustion to generate a large amount of water vapor, the temperature in the working wheel cavity 14 is reduced, a working rotor and a working stator are protected, the pressure in the working wheel cavity 14 is effectively improved, and the heat efficiency is further improved.

To sum up, the novel turbine engine better conforms to the fluid dynamics principle, fully exerts the characteristics of the mechanical lever, the booster igniter 29 is arranged in front of the air inlet 17 of the working wheel cavity 14, the air inlet and the combustion are separately carried out, so that the combustible high-pressure mixed gas is ignited and combusted in the working wheel cavity 14, the high-temperature high-pressure gas generated by the combustion cannot interfere with the compressed air in the air inlet 17, namely, the high-temperature high-pressure gas generated by the combustion cannot interfere with the air compressing work of the air compressing device, the air input of the compressed air is not influenced, the pressure in the working wheel cavity 14 is further improved, higher back pressure is generated on the working rotor, higher torsion is output by the working rotor, the energy conversion rate is further improved by water spraying, the purposes of energy conservation and emission reduction are really realized, the structure is simple, the manufacture is easy, and therefore, the novel turbine engine has the advantages of strong back pressure working of the piston engine and the frictionless continuous operation Compared with the prior art, the operation and other advantages have the characteristics of novelty, substantive and remarkable progress, and the beneficial effects of the implementation are also obvious.

Claims (10)

1. The utility model provides a novel turbine engine, mainly comprises components such as organism, shaft, the device of calming the anger, do work device, gas generating device, be equipped with supporting bearing and sealing device between shaft and the organism, the device of calming the anger comprises the wheel chamber of calming the anger and the rotor of calming the anger, the device of doing work comprises the wheel chamber of doing work and the rotor of doing work, characterized by: the gas compression rotor and the acting rotor are respectively arranged in a gas compression wheel cavity and an acting wheel cavity on the same axis in the machine body, the gas generating device comprises components such as a combustion chamber, a porous flame stabilizer, a fuel injector, a fuel supply device, an igniter and the like, the wheel shaft is arranged in the center of a gas compression rotor wheel body and an acting rotor wheel body in the machine body, the gas compression wheel cavity is provided with a gas inlet and a gas outlet, the combustion chamber is provided with a gas inlet and a gas outlet, the acting wheel cavity is provided with a gas inlet and a gas outlet, the acting rotor comprises an acting wheel body and an acting movable blade, the movable blade is a roller formed by arranging a plurality of strip-shaped blades with certain bending angle against the rotating direction of the acting wheel body according to a certain tangential angle and interval, one end of each movable blade is arranged and fixed on the side surface of the acting wheel body, and the other end of each movable blade corresponds to, the utility model discloses a pneumatic wheel, including a cylinder shape acting rotor, wheel axle, wheel chamber, working wheel chamber, gas wheel chamber gas outlet, combustion chamber front chamber, combustion chamber air inlet, combustion chamber air outlet, wheel chamber gas outlet, the wheel chamber gas outlet communicates with the working wheel chamber gas inlet, wheel chamber gas outlet and the wheel chamber gas outlet of working communicate with each other with the atmosphere.

2. The new turbine engine as set forth in claim 1, wherein: the air compressing rotor is composed of an air compressing wheel body and air compressing movable blades, the air compressing movable blades are formed by arranging a plurality of strip-shaped blades with certain bending angles along the rotation direction of the air compressing wheel body according to certain cutting angles and intervals into a roller shape, one end of each blade is installed and fixed on the side face of the air compressing wheel body, the other end of each blade corresponds to the wall of a wheel cavity opposite to the air compressing wheel body and keeps a certain sealing gap, the roller-shaped air compressing rotor is arranged on the same axis of the wheel shaft, and an air inlet of the air compressing wheel cavity is arranged in the center of the side face of the.

3. The new turbine engine as set forth in claim 1, wherein: the pneumatic stator is a cylinder formed by a plurality of strip-shaped static blades with certain reverse bending degrees and arranged along the rotating direction of the pneumatic wheel body according to a certain cutting angle and intervals, one end of the pneumatic stator is fixedly arranged on the inner wall of the wheel cavity opposite to the pneumatic wheel body, the other end of the pneumatic stator is sleeved in the cylinder-shaped pneumatic rotor and keeps a tiny gap from being contacted with the cylinder-shaped pneumatic rotor, the cylinder-shaped pneumatic stator and the pneumatic rotor are arranged along the same axis, the other end of the cylinder-shaped pneumatic stator and the corresponding side surface of the pneumatic wheel body keep a certain sealing gap, the working wheel cavity is internally provided with a working stator, the working stator is also a cylinder formed by a plurality of strip-shaped static blades with certain reverse bending degrees and arranged along the rotating direction of the working wheel body according to a certain cutting angle and intervals, one end of the working stator is fixedly arranged on the inner wall of the wheel cavity opposite to the working wheel body, the other end of the working stator is sleeved in the cylinder-shaped, the cylindrical acting stator and the acting rotor have the same axis, and a certain sealing gap is kept between the other end of the cylindrical acting stator and the side face of the corresponding acting wheel body.

4. The new turbine engine as set forth in claim 1, wherein: the air compression rotor is composed of an air compression wheel body and an air compression movable blade, the circumferential surface of the air compression wheel body is provided with a blade, the circumferential surface of the air compression wheel body is divided into a large circumferential surface and a small circumferential surface by the blade, the circumferential surfaces of the two air compression wheel bodies are in two opposite arc shapes, the movable blade is composed of a large blade and a small blade, the large blade and the small blade are in a shape of narrow top and wide bottom, the large blade is installed on the large circumferential surface, the small blade is installed on the small circumferential surface, the top edge of the large blade, the top edge of the small blade and the top edge of the blade keep a non-contact sealing gap with the narrowest part of the inner wall of the air compression wheel cavity corresponding to the small side in the air compression wheel cavity, a large semi-circular auxiliary cavity is arranged outside the air compression wheel cavity corresponding to the small blade side except the periphery of an air exhaust port and is wrapped on the air compression wheel cavity corresponding to the small blade on the, the large semi-circular auxiliary cavity is C-shaped in cross section, the upper opening of the large semi-circular auxiliary cavity with the C-shaped cross section corresponds to the top edge of the small blade, the lower opening of the large semi-circular auxiliary cavity with the C-shaped cross section corresponds to the bottom edge of the small blade, the large semi-circular auxiliary cavity with the C-shaped cross section and the small blade cavity form an annular channel with the large semi-circular cavity as an inner annular shaft, and the air outlet of the air compression wheel cavity is of an gradually-opened structure from the air compression wheel cavity to the outside along the rotation direction of the air compression wheel cavity on the circumferential surface of the air compression wheel cavity corresponding to the top end of the small blade, its inside communicates with each other with the pressure wheel chamber, and outside communicates with each other with the combustion chamber air inlet, the pressure wheel chamber air inlet is in the pressure wheel chamber side center that big blade base corresponds, and is inwards communicated with big blade bottom cavity, and outside communicates with the atmosphere, the pressure wheel chamber that big blade top corresponds is involute line structure along pressure wheel body direction of rotation, and its end is the biggest end and extends all the time and the transversal big semicircular shape auxiliary chamber upper mouth intercommunication of personally submitting C shape that corresponds on pressure wheel chamber gas outlet heel leaflet top, the pressure wheel chamber axial width that little blade top corresponds begins to reduce gradually to the other end along pressure wheel body direction of rotation after the gas outlet and is the convergent structure until pressure wheel chamber gas outlet department.

5. The new turbine engine as set forth in claim 3, wherein: the air compressing device is composed of a plurality of roller-shaped air compressing rotors with different diameters and a plurality of cylindrical air compressing stators with different diameters, the number of the cylindrical air compressing stators is one less than that of the roller-shaped air compressing rotors, the plurality of roller-shaped air compressing rotors are sequentially sleeved on the side surface of the air compressing wheel body according to the same axis and the diameter, the plurality of cylindrical air compressing stators are respectively sleeved between two adjacent roller-shaped air compressing rotors according to the diameter, the other ends of the cylindrical air compressing stators are respectively installed and fixed on the inner wall of a wheel cavity opposite to the air compressing wheel body, the plurality of cylindrical air compressing stators keep tiny sealing gaps with the two adjacent inner and outer roller-shaped air compressing rotors, the acting device is composed of a plurality of roller-shaped acting rotors and a plurality of cylindrical acting stators, and the number of the acting cylindrical stators is one less than that of the roller-shaped acting rotors, the plurality of cylindrical working rotors are sequentially sleeved on the side surface of the working wheel body according to the same axis and the diameter, the plurality of cylindrical working stators are respectively sleeved between two adjacent cylindrical working rotors according to the diameter, the other ends of the cylindrical working stators are respectively installed and fixed on the inner wall of the wheel cavity opposite to the working wheel body, and the plurality of cylindrical working stators keep small sealing gaps with the adjacent inner and outer two cylindrical working rotors.

6. The new turbine engine as set forth in claim 4, wherein: a plurality of C-shaped static blades matched with the cross section of the large semi-circular auxiliary cavity are arranged in the large semi-circular auxiliary cavity with the C-shaped cross section, the C-shaped stationary blade divides the large semi-circular auxiliary cavity into a plurality of C-shaped auxiliary cavity sections, the bottoms of the C-shaped auxiliary cavity sections, namely the centripetal ends, correspond to the cavities at the bottoms of the small blades and are communicated with the bottoms of the small blade cavities of the small blades through the air compressor cavity, the tops of the C-shaped auxiliary cavity sections, namely centrifugal ends, are arranged on the outer circular surface of the air compressor wheel cavity and are communicated with the small blade cavity at the top end of the small blade through the air compressor wheel cavity, when the side edge of the small blade corresponds to the stator blade in the large semi-circular auxiliary cavity, the cavity of the small blade and the C-shaped auxiliary cavity form a spiral channel taking the large semi-circular cavity ring as an axis, and the air outlet of the air compression wheel cavity is arranged on the outer circular surface of the air compression wheel cavity above the top end of the small blade corresponding to the tail end of the spiral channel, namely the bottom of the narrowest end.

7. The new turbine engine as set forth in claim 5, wherein: the axial length of a plurality of air compressing rotors is different, the axial length of a plurality of air compressing stators is different, the axial length of a plurality of acting rotors is different, and the axial length of a plurality of acting stators is different.

8. The new turbine engine as set forth in claim 1, wherein: a plurality of basic power units consisting of air compressing devices, acting devices and gas generating devices are installed on the same wheel shaft in series.

9. The new turbine engine as set forth in claim 1, wherein: the gas compressing device is provided with a plurality of gas outlets, the acting device is provided with a plurality of gas inlets, a plurality of gas generating devices are distributed on the outer circumference of the machine body, the plurality of gas outlets on the gas compressing device are respectively communicated with the gas inlets of the combustion chambers on the gas generating devices, and the gas outlets of the combustion chambers on the gas generating devices are respectively communicated with the plurality of gas inlets on the acting device.

10. The new turbine engine as claimed in any one of claims 1 to 9, wherein: a booster igniter is arranged on the cavity wall of the working wheel cavity in front of the air inlet of the working wheel cavity, namely, in the forward direction of the rotation direction of the working wheel body, a booster fuel injector is arranged on the cavity wall of the working wheel in front of the booster igniter, an arc-shaped air blocking block which is longer than the arc length of the air inlet of the working wheel cavity is arranged on a stator corresponding to the air inlet of the working wheel cavity, a water sprayer is arranged on the cavity wall in front of the booster igniter on the cavity wall of the working wheel cavity, the outer end of the water sprayer is connected with a water supply device, an arc-shaped movable cavity wall is arranged on the circumference of the wheel cavity at the air inlet of the working device in the machine body, one end of the arc-shaped movable cavity wall is connected with the fixed cavity wall through a movable shaft, a regulating device is arranged in front of the air inlet, a starting device, a speed changing device and a power distributor are, the power distributor is provided with a speed change device, the fuel gas generating device is provided with a pressure sensor, a temperature sensor, a position controller, a flame stabilizer, a fuel injector, a fuel supply device and a fuel vaporization loop, the fuel injector is provided with a liquid fuel vaporizer, the fuel vaporizer is provided with a fuel vaporization regulating and controlling device, the multipurpose motor, the starting device, the water sprayer, the water spray supply device, the movable cavity wall regulating and controlling device, the control mechanism on the speed change device, the pressure sensor, the temperature sensor, the fuel supply device, the igniter, the fuel vaporizer, the booster igniter, the booster fuel injector and the fuel vaporization regulating and controlling device are connected with the central processing controller through wiring harnesses, and the central processing controller is connected with a storage battery pack.

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