CN203067082U - Novel combustion motor - Google Patents

Abstract

The utility model provides a novel combustion motor. The combustion motor comprises an air injection rotor, an acting rotor, a combustion chamber, a fuel supplying device and an ignition device. The air injection rotor and the acting rotor are on the same axis. The air injection rotor can be a one-level, two-level, multi-level or mixed multi-level air injection mechanism. The acting rotor is in a non-turbine type impeller structure and is not contacted with a cavity wall. A tongue piece which can move vertically and is the same as one blade in width is arranged between two adjacent blades of the acting rotor. One edge of each tongue piece is connected with the top edge of one blade of the two adjacent blades through a movable shaft. Using the connecting shaft as a circle center, the other edge of each tongue piece moves vertically within 90 degrees along the blade face of the other blade of the two adjacent blades. According to the combustion chamber, a cylindrical piston matched with the inner circle of the combustion chamber is arranged in a cylinder, and the piston divides the combustion chamber into a front cavity and a back cavity. The piston can slide in the front cavity and the back cavity of the combustion chamber. An air jet hole is formed in the center of the piston, and a fuel injector is arranged in the air jet hole. A spring is arranged in the back cavity of the combustion chamber at the back end of the piston. A piston position controller is arranged at the back end of the spring. A telescopic tube is arranged in spring rings. The front end of the telescopic tube is connected on the fuel injector and is communicated with the fuel injector, and the back end of telescopic tube is communicated with the fuel supplying device outside a machine body through the piston position controller and the machine body. The back end of the back cavity is communicated with an air outlet of the air injection rotor. The front end of the front cavity is communicated with an air inlet of the acting rotor. An igniter is arranged at the air inlet of the acting rotor. A movable cam shaft is arranged at the air inlet of the acting rotor. An air outlet of the acting rotor is communicated with an exhaust passage.

Description

A kind of internal combustion engine

Technical field:

The utility model relates to a kind of motor, especially a kind of explosive motor.

Background technique:

In the prior art, the technology that approaches the most with the application is gas turbine, combustion presses its rotating speed accommodation of gas turbine of coaxial single acting rotor narrower, the rotating ratio of calming the anger between rotor and the acting rotor is immutable, its a plurality of rotors that freely do work are in a blast tube on the gas turbine of a plurality of rotors that freely do work, a plurality of rotating speeds that freely do work between the rotor still are subjected to its mutual restriction of flow restriction, make the rotor of calming the anger export compressed-air actuated compression ratio or flow control scope relative narrower, though being the axial flow gas engine, split gas turbine accomplished combustion pressure split axle, acting rotor and power output acting rotor still coexists in the blast tube but it is calmed the anger, its acting rotor of calming the anger when tick-over is restricted by it still, can't accomplish that high low speed adapts to mutually, make its power output area and operating mode accommodation relative narrower, the acting rotor of gas turbine almost all is turbine or the page or leaf wheel of turbine-type in the prior art besides, its shape, week/air displacement all relative fixed is constant, make the air displacement relative fixed of its rotor that under identical operating air pressure, does work constant, oil consumption problem of higher place during Here it is gas turbine low speed, can not under low-speed conditions, use, be exactly the size of its puff prot in addition, the shape of firing chamber, volume immobilizes, make fuel from spraying, mix, igniting, the distance that is burned to the acting rotor all immobilizes, make fuel Applicable scope relative narrower, can not use pluralities of fuel, existing in prior technology deficiency that Here it is.

Summary of the invention:

Technical problem to be solved in the utility model, be exactly at the existing in prior technology deficiency, and providing a kind of rotor that does work in the shape of uniform pressure next week/air displacement and firing chamber and do work rotor and the rotating ratio adjustable variable controllable all between the rotor of calming the anger, its rotating speed Applicable scope is wideer, the power output area is wideer, can be in the technological scheme of working under the complex working condition condition, can realize that many fuel exchange under the situation of not changing machine hardware.

This programme is realized by following technical measures: mainly by body, the rotor of calming the anger, the acting rotor, firing chamber and fuel supplying device and ignition mechanism constitute, the described rotor of calming the anger is installed in the body chamber with the acting rotor, described body chamber can be that circle also can be oval, described depressor rotor is with doing work rotor on same axis, acting rotor and calming the anger has body wall at interval between the rotor, spring bearing is arranged in the body wall, porting and firing chamber and various pipeline are arranged in the body wall, the described rotor of calming the anger can be applicable to the various forms of gas pressure mechanisms of this programme in the prior art, as centrifugal turbocompressor, vane pump formula gas compressor or turbine-type page or leaf sheet gas compressor etc., the described rotor of calming the anger can be also can be that two-stage that two rotors of calming the anger the constitute structure of calming the anger can also be the multistage compressor structure that a plurality of rotors of calming the anger constitute by the single-stage that the single rotor of calming the anger the constitutes structure of calming the anger, as the multistage turbine gas compressor, multistage blade compressor etc., the hybrid multi-stage gas pressure mechanism that the gas compressor that the described rotor of calming the anger can also be various ways constitutes, be final stage as making elementary centrifugal turbocompressor with turbine page or leaf chip gas compressor, centrifugal turbocompressor is that elementary vane pump formula gas compressor is mixed construction such as middle final stage, can be that coaxial pattern also can be can also be that selectively to use planetary gear set to connect coaxial with the split axle pattern that planetary gear set connects between described multistage compressor structure or hybrid multi-stage gas pressure mechanism at different levels, split axle is used with, specifically can select integrated mode according to actual needs flexibly, the planetary gear set control gear is arranged on the described planetary gear set, described planetary gear set control gear can lock wantonly two gears in the planetary gear set also can locking or control be in that gear of free state, described acting rotor can be that single acting rotor also can be two acting rotors or a plurality of acting rotors more than two, when described acting rotor is two, it can coaxial connection can also be to connect through planetary gear set also that two acting rotor shafts can not connect, when described acting rotor is a plurality of, the first acting rotor is with can not connecting also and can coaxial connection can also connect with planetary gear set between the second acting rotor, it can also be selectively to use planetary gear set or axle to connect that other acting rotor can also can connect with planetary gear set with coaxial connection, described acting rotor is that two or more are when a plurality of, two acting rotors or a plurality of acting rotor can share a firing chamber or not share a firing chamber, it is combustion chamber shared selectively to divide into groups, described acting rotor shaft and to calm the anger between the rotor shaft can be that coaxial connection also can be to connect through planetary gear set, described acting rotor is non-turbine-type blade wheel structure, described impeller can be that unshrouded impeller also can be that blade all is made of the double shrouded wheel of wheel sheet shutoff single shrouded wheel or the blade both sides of the shutoff of wheel sheet on one side, blade on the described impeller can not contact with the machine body lumen wall with the contact of machine body lumen wall yet, blade on the described impeller can be the stator blade that is fixed on the wheel body, and described fixed blade can tilt also can tilt counterclockwise in the past clockwise in the past.Have with blade with tongue piece wide and can be up and down between adjacent two blades on the described impeller, a limit of described tongue piece is carried out activity with blade top margin in adjacent two blades with movable axis and is connected, described movable axis can be also can be on the top margin of the clockwise side of blade on the top margin of the counterclockwise side of blade, described tongue piece is that the blade face of another adjacent another blade in edge of axle center slides up and down in 90 degree scopes with the coupling shaft, its top dead center is no more than corresponding blade top margin, the slip radian on corresponding its radian of blade face camber of described tongue piece active edges and tongue piece slip limit is complementary, in the unshrouded impeller structure when tongue piece slip limit adjacent two blades during at top dead center, tongue piece, form a rotor cavity of sealing relatively between wheel body and acting rotary piston machine body cavity two walls.Blade on the described impeller also can be mounted in the movable blade in the wheel body axial notch, can have with blade with wide axial blade groove on the described blade tip face, there is roller to follow the contact of oval acting rotor chamber inner headed face in the described blade groove, have with the corresponding annular gas tank in axial notch bottom at acting rotary piston machine body cavity sidewall, the axial notch bottom communicates with the annular gas tank on the acting rotary piston machine body cavity sidewall, described movable blade can slide in axial notch from inside to outside, spring can be arranged at the axial notch bottom on the described blade interior edge face, in the described blade vane hole is arranged, have with blade with tongue piece wide and can be up and down between adjacent two blades on the described impeller, described tongue piece is to insert the scalable tongue piece that constitutes by tongue piece convex body and tongue piece concave volume string, on the described tongue piece concave volume internal tongue convex body top end spring is arranged, a limit of described tongue piece is carried out activity with blade top margin in adjacent two blades with movable axis and is connected, described tongue piece fillet can be that a limit of tongue piece convex body also can be a limit of tongue piece concave volume, described movable axis can be also can be on the top margin of the clockwise side of blade on the top margin of the counterclockwise side of blade, described tongue piece is that the blade face of another adjacent another blade in edge of axle center slides up and down in 90 degree scopes with the coupling shaft, its top dead center is no more than corresponding blade top margin, the slip radian on corresponding its radian of blade face camber of described tongue piece active edges and tongue piece slip limit is complementary, in the unshrouded impeller structure when tongue piece slip limit adjacent two blades during at top dead center, scalable tongue piece, form a rotor cavity of sealing relatively between wheel body and acting rotary piston machine body cavity two walls, described rotor cavity communicates with the axial notch bottom through vane hole, in the double shrouded wheel structure when tongue piece slip limit adjacent two blades during at top dead center, scalable tongue piece, form a rotor cavity of sealing relatively between wheel body and the blade two side wheel sheets, there is the annular gas tank of correspondence on vent and the acting rotary piston machine body cavity sidewall to communicate on the axial notch bottom wheel sheet, in the single shrouded wheel structure, when tongue piece active edges adjacent two blades during at top dead center, scalable tongue piece, form an impeller cavity of sealing relatively between the wheel sheet on wheel body and blade one side and the wheel chamber sidewall of blade another side, when the shutoff side of blade at the annular gas tank of correspondence on one side the time, blade shutoff side shaft has the annular gas tank of correspondence on vent and the acting rotary piston machine body cavity sidewall to communicate on bottom portion of groove wheel sheet, described annular gas tank communicates with acting rotor air outlet through the air flue hole, in the rotor cavity spring can be arranged below the described tongue piece, in the described body throat less chamber is arranged, described throat less chamber is on the acting rotor chamber, the cylindrical piston that is complementary with circle in the firing chamber is arranged in the described firing chamber, described cylindrical piston is divided into former and later two chambers to the firing chamber, cylindrical piston can slide in the chamber of the front and back of firing chamber, on the described cylindrical piston periphery sealed piston ring is arranged, there is fumarole at described cylindrical piston center, can there be guiding piece also guiding groove can be arranged on the described fumarole, in the described fumarole fuel injector is installed, described fuel injector can antero posterior axis in fumarole to activity, described fuel injector aperture minimum of fumarole during the front position in fumarole, described fuel injector aperture maximum of fumarole during the rearmost position in fumarole, in the firing chamber rear chamber of described cylindrical piston rear end spring is arranged, described spring rear end has the piston position controller, described piston position controller can promote spring or the pulling spring comes control piston residing position in the firing chamber, in the described spring ring telescopic pipe is arranged, described telescopic pipe front end is connected on the fuel injector and communicates with fuel injector, the telescopic pipe rear end is through the piston position controller, body communicates with body outer fuel supplier, can control the aperture size of fumarole and then the jet flow of control fumarole by the position of telescopic pipe fuel metering sparger in fumarole, described firing chamber rear chamber rear end is communicated with the rotor air outlet of calming the anger, described firing chamber front chamber front end is communicated with acting rotor suction port, on the described acting rotor suction port igniter is installed, described fuel supplying device can be applicable to the fuel-supplying unit that can supply with various liquid fuels and gaseous fuel of this programme in the prior art, described fuel injector can be in the prior art applicable to the fuel nozzle that can spray all gases and liquid fuel or shower nozzle or other fuel injector spare of this programme, described ignition mechanism can be the various ignition devices that can be used for this programme in the prior art.The concrete characteristics of this programme also have, there is the gas storage control valve to connect with the outer caisson of body on the described rotor air outlet of calming the anger, described caisson can be applicable to the various gas storage equipment that can storing compressed air of this programme in the prior art, described gas storage control valve can make the rotor air outlet of calming the anger, firing chamber rear chamber and caisson three intercommunication, the gas storage control valve can also communicate caisson separately in occlusion pressure air rotor air outlet with firing chamber rear chamber, the gas storage control valve can also be closed caisson makes the rotor air outlet of calming the anger communicate separately with firing chamber rear chamber, there is flameholder at acting rotor suction port place in the front chamber of described firing chamber, described flameholder is that the bell interior gas flow rate of flameholder that makes of porous is lower than the outer gas flow rate of flameholder, make the burning of inflammable mixture more stable, there is the rotatable cam axle at acting rotor suction port place, acting rotor suction port can be closed or open to described camshaft, can regulate the aperture size of acting rotor suction port by camshaft, gas flow and the direction of control acting rotor suction port, on the air flue that annular gas tank follows acting rotor air outlet to communicate on the described acting rotor chamber sidewall air valve is arranged, described air valve has two-way ventilation control function, can make in the air flue air-flow that air-flow can only be flowed toward another side and can also make air-flow two-way flow in the air flue, on the outer air outlet flue of the gas port that described acting rotor air outlet follows annular gas tank to communicate gas exhausting valve is arranged, can regulate and control exhaust pressure and the air displacement that acting rotor air outlet is located, described gas storage control valve by gas exhausting valve, air valve, gas exhausting valve, fuel injector, piston position controller and planetary gear set control gear all can be electric controller or the electrical apparatus element such as electric control mechanism and electronic control device that can be used for this programme in the prior art.

The beneficial effect of this programme can be learnt according to the narration to such scheme, because in this scheme one: piston is arranged in the firing chamber, in the work, residing relative position between the chamber before and after piston can be adjusted in the firing chamber according to the different operating condition under the interaction of forward compressed air pressure and gaseous-pressure backward and spring automatically, can also promote spring or spur spring position of piston is adjusted by the piston position controller, as: when using hydrogen, liquid gas, rock gas, during gaseous fuels such as coal gas, because the diffusivity of gaseous fuel, flammability is all the highest relatively, can promote the front position that the spring handle piston forward is pushed into firing chamber front chamber with the piston position controller, make firing chamber front chamber inner capacities less relatively, when using gasoline, lightweight kerosene, during volatile liquid fuel such as alcohol, because the diffusivity of this class A fuel A, flammability is higher, relative middle section position before and after can adjusting back piston in the firing chamber with piston position controller pulling spring between the chamber, when using kerosene, during not volatile heavy class A fuel A such as diesel oil, can piston be adjusted back with piston position controller pulling spring and lean on the position, back in the firing chamber in the rear chamber, make firing chamber front chamber length the longest relatively, prolonged fuel from spraying, be mixed into the distance of burning, prolonging fuel relatively does time in advance with compressed-air actuated, also have, when the pressurized air in the rear chamber of firing chamber sprays into firing chamber front chamber through fumarole, under the guide functions of pressurized air guiding piece and guiding groove in fumarole by several angle in the shape of a spiral eddy current spray into firing chamber front chamber, relatively further prolonged fuel from spraying, be mixed into the distance of burning, relatively further prolong fuel and improve mixture homogeneity diffusion time, make fuel combustion more abundant.Realizing that the variable adjustable of firing chamber is controlled makes wideer that fuel Applicable scope becomes.Two: on the blade of acting rotor tongue piece is arranged, described tongue piece is at outside exhaust gas pressure, can be adjusted in sliding position on the blade automatically according to different operating modes under the interaction of centrifugal force and inside acting gaseous-pressure, reach the week/air displacement of automatic adjusting acting rotor, air valve on the air flue that can also communicate with acting rotor air outlet by annular gas tank on the gas exhausting valve on the outer air outlet flue in acting rotor air outlet and the described acting rotor chamber sidewall is controlled in the rotor cavity gas pressure and then is adjusted week/air displacement that the relative position of tongue piece on the blade face that correspondence is slided regulated and control the acting rotor, make the acting rotor the week/air displacement realization variable adjustable is controlled.Three: at the acting rotor with calm the anger between the rotor and acting rotor and acting rotor, the rotor and calming the anger of calming the anger connects with planetary gear set between the rotor, because planetary gear set is a kind of special gear structure, the changeable choice structure pattern arbitrarily of its structural type makes the acting rotor and calms the anger and adjust rotating ratio automatically according to various working conditions at work between the rotor, allow acting rotor and calm the anger and accomplish self adaption between the rotor, can also adjust acting rotor and the rotating ratio between the rotor of calming the anger by the planetary gear set control gear, make the rotor of calming the anger under identical acting rotor speed condition, can export the pressurized air of different compression ratios, the variable adjustable that realizes compression ratio is controlled, under the condition that does not change machine hardware, can provide multifuel firing needed different pressurized gas pressure, realize the many fuel of a machine.Four: the fumarole aperture that can adjust inner carrier center, firing chamber as required by fuel injector, regulate compression gas blowout flow of the people, realize fuel, pressurized gas is two-way adjustable, the bell flameholder of porous can make the outer inflammable mixture flow velocity of the relative flameholder of part inflammable mixture flow velocity low, make the combustion gas can smooth combustion under high flow rate, can adjust gas flow rate and gas flow and the direction at acting rotor suction port place by camshaft.Five: when starting the machine, caisson is opened in gas storage control valve occlusion pressure air rotor air outlet, the caisson compressed air enters firing chamber front chamber through firing chamber rear chamber and starts with the fuel mix ignition and close caisson after the acting rotor rotates and open the rotor suction port of calming the anger, make and start become simple, reliably, easy to operate, the gas storage control valve can also be opened caisson as required and be used for excess compressed air in the storage work, when the extra reinforcing of needs, discharge again to use and reach purpose of energy saving, six: when the acting rotor is a plurality of, can can selectively use or stop one or several acting rotor to the requirement of output power according to operating mode, make the wideer of power output area and accommodation change.In sum, the technical program has higher self adaption degree and wideer modification scope and simple to operationly also can realize many fuel under the complex working condition condition, can realize full electronic control technology operation, be particularly suitable for the power platform exploitation of computer programming intelligent control system.This shows that the technical program compared with prior art has novelty, substantive distinguishing features and remarkable progress, the beneficial effect of its enforcement also is apparent.

Description of drawings:

Fig. 1 is the structural representation of first embodiment of this programme.

Fig. 2 is along A place line cross cut structure schematic representation among Fig. 1.

Fig. 3 is B place enlarged view among Fig. 2.

Fig. 4 is the structural representation of second embodiment of this programme.

Fig. 5 is along A place line cross cut structure schematic representation among Fig. 4.

Fig. 6 is the structural representation of the 3rd embodiment of this programme.

Fig. 7 is along A place line cross cut structure schematic representation among Fig. 6.

Fig. 8 is the structural representation of the 4th embodiment of this programme.

Fig. 9 is along A place line cross cut structure schematic representation among Fig. 8.

Figure 10 is C place enlarged view among Fig. 9.

Figure 11 is the structural representation of the 5th embodiment of this programme.

Figure 12 is Figure 11 front perspective structure schematic representation.

Figure 13 looks the sectional structure schematic representation under the end face of Figure 11.

Figure 14 is the structural representation of the 6th embodiment of this programme.

Figure 15 is along A place line cross cut structure schematic representation among Figure 14.

Figure 16 looks the sectional structure schematic representation under Figure 14 end face.

Figure 17 is the structural representation of the 7th embodiment of this programme.

Figure 18 is A place line plane of structure perspective structure schematic representation among Figure 17.

Figure 19 is the structural representation of the 8th embodiment of this programme.

Figure 20 is along A place line cross cut structure schematic representation among Figure 19, Figure 21, Figure 22, Figure 23, Figure 24, Figure 25.

Figure 21 is the structural representation of the 9th embodiment of this programme.

Figure 22 is the structural representation of the tenth embodiment of this programme.

Figure 23 is the structural representation of the 11 embodiment of this programme.

Figure 24 is the structural representation of the 12 embodiment of this programme.

Figure 25 is the structural representation of the 13 embodiment of this programme.

Among the figure, 1 is body, 2 are the centrifugal rotor of calming the anger, 3 are the acting rotor, 3 ' be the second acting rotor, 3 〞 are the 3rd acting rotor, 4 are the rotor suction port of calming the anger, 5 are the rotor shaft of calming the anger, 6 are the acting rotor shaft, 6 ' be the second acting rotor shaft, 6 〞 are the 3rd acting rotor shaft, 7 is bearing, 8 is piston, 9 is piston ring, 10 is firing chamber front chamber, 10 ' be the second firing chamber front chamber, 11 is firing chamber rear chamber, 11 ' be the second firing chamber rear chamber, 12 is fumarole, 13 is fuel injector, 14 is spring, and 15 is the piston position controller, and 16 is telescopic pipe, 17 is fuel supplying device, 18 are the rotor air outlet of calming the anger, and 19 are the gas storage valve, and 20 is caisson, 21 are acting rotor suction port, 21 ' the second acting rotor suction ports, 21 〞 are the 3rd acting rotor suction port, and 22 is ignition mechanism, 23 is flameholder, 24 is camshaft, 25 acting rotor air outlets, 25 ' be the second acting rotor air outlet, 25 〞 are the 3rd acting rotor air outlet, 26 is air outlet flue, 26 ' be second air outlet flue, 27 is guiding piece, 28 is blade, 29 is axial notch, and 30 is the groove spring, and 31 are the wheel sheet, 32 is planetary gear set, 33 planetary gear set control gear, 34 is annular gas tank, 35 is vent, 36 is air flue, 36 ' be second air flue, 36 〞 are the 3rd air flue, 37 is air valve, 38 is gas exhausting valve, 39 is tongue piece, and 40 is movable axis, and 41 is rotor cavity, 42 is the blade groove, 43 is roller, and 44 is the tongue piece concave volume, and 45 is the tongue piece convex body, 46 is the tongue piece spring, 47 is vane hole, and 48 is bull gear, and 49 is planetary carrier, 50 is sun gear, 51 are the vane pump formula rotor of calming the anger, and 52 are the previous stage vane pump formula rotor of calming the anger, and 53 are the previous stage rotor suction port of calming the anger, 54 are the previous stage rotor air outlet of calming the anger, 55 are the previous stage rotor shaft of calming the anger, and 56 are the turbine-type rotor of calming the anger, 56 ' be the previous stage turbine-type rotor of calming the anger, 56 〞 are the preceding secondary turbine-type rotor of calming the anger, 57 are the preceding secondary rotor shaft of calming the anger, and 58 are the preceding secondary rotor air outlet of calming the anger, and 59 are the preceding secondary rotor suction port of calming the anger, 60 are first three level rotor shaft of calming the anger, 61 are first three level rotor suction port of calming the anger, and 62 are first three level rotor air outlet of calming the anger, and 63 are the preceding level Four rotor shaft of calming the anger, 64 are the preceding level Four rotor suction port of calming the anger, and 65 are the preceding level Four rotor air outlet of calming the anger.

Embodiment:

For more clearly demonstrating the technical characterstic of this programme, below by 13 embodiments, and in conjunction with its accompanying drawing, this programme is further elaborated.

Fig. 1, Fig. 2, Fig. 3 shows first embodiment of this programme jointly, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and non-turbine-type acting rotor 3 formations of calming the anger, described calm the anger rotor 2 and acting rotor 3 are installed in cylindrical shape respectively and calm the anger in rotor 2 chambeies and rotor 3 chambeies of doing work on same axis body 1 in, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described acting rotor 3 is contained on the acting rotor shaft 6, the rotor suction port 4 of calming the anger on the described body 1 communicates with the centrifugal rotor 2 of calming the anger, described non-turbine-type acting rotor 3 is unshrouded impeller structures, described impeller upper blade 28 is fixed on the wheel body not with the contact of chamber wall, the described rotor shaft 5 of calming the anger is coaxial connections with acting rotor shaft 6, bearing 7 is housed in body 1 spacing wall on described calm the anger rotor shaft 5 and the acting rotor shaft 6, in the body 1 throat less chamber is arranged above described acting rotor 3 chambeies, the cylindrical piston 8 that is complementary with circle in the firing chamber is arranged in the described throat less chamber, on described cylindrical piston 8 peripheries sealed piston ring 9 is arranged, described cylindrical piston 8 is divided into front chamber 10 and rear chamber 11 to the firing chamber, cylindrical piston 8 can slide in the front chamber 10 of firing chamber and rear chamber 11, there is fumarole 12 at described piston 8 centers, fumarole 12 centers be equipped with can antero posterior axis to the fuel injector 13 of activity, on the described fumarole 12 guiding piece 27 is arranged, in the described cylindrical piston 8 rear end firing chamber rear chamber 11 spring 14 is arranged, in the described spring 14 rear end firing chamber rear chamber 11 piston position controller 15 is arranged, in described spring 14 circles telescopic pipe 16 is arranged, described telescopic pipe 16 front ends are communicated with fuel injector 13, the rear end is through piston position controller 15, body 1 is communicated with fuel supplying device 17, described firing chamber rear chamber 11 rear ends communicate with the rotor air outlet 18 of calming the anger, on the described rotor air outlet 18 of calming the anger gas storage valve 19 is arranged, described gas storage valve 19 communicates with body 1 outer caisson 20, described firing chamber front chamber 10 front ends are communicated with acting rotor suction port 21, on the described firing chamber front chamber 10 front ends acting rotor suction port 21 ignition mechanism 22 and flameholder 23 are installed, there is rotatable cam axle 24 at described acting rotor suction port 21 places, and described acting rotor air outlet 25 communicates with air outlet flue 26.

Basic functional principle and advantage: caisson 20 is opened in gas storage valve 19 occlusion pressure air rotor air outlets 18, pressurized air with certain pressure promotes piston 8 and strengthens fumarole 12 apertures to front slide in gas storage valve 19 enters firing chamber rear chamber 11, pressurized air sprays into firing chamber front chamber 10 while fuel injector, 13 ejection fuel and mixes the formation inflammable mixture with pressurized air from fumarole 12, an inflammable mixture part enters in the flameholder 23 to be converged by ignition mechanism 22 ignition combustions expansion generation high-temperature high-pressure fuel gas with the flameholder 23 outer inflammable mixtures that flow through through flameholder 23, high-temperature high-pressure fuel gas promotion piston 8 reduces the simultaneously little camshaft 24 that opens of fumarole 12 apertures to rear chamber's 11 sliding compression springs 14 and opens acting rotor 3 suction ports 21, high-temperature high-pressure fuel gas promotes blade 28 in acting rotor 3 suction ports 21 spray into acting rotor 3 chambeies rotate acting rotor 3 in the counterclockwise direction, waste gas enters air outlet flue 26 through acting rotor 3 air outlets 25 and discharges, acting rotor 3 drives coaxial rotor 2 rotations of calming the anger, air enters in the centrifugal rotor 2 of calming the anger through the centrifugal rotor 2 pressurization backs of calming the anger the pressurized air that in the air outlet 18 places formation has certain pressure through rotor 2 suction ports 4 of calming the anger, described gas storage valve 19 cuts out caisson 20 and opens rotor 2 air outlets 18 of calming the anger simultaneously, pressurized air sprays in the firing chamber front chamber 10 of people's High Temperature High Pressure through fumarole 12 in air outlet 18 enters firing chamber rear chamber 11, rotate acting with promoting acting rotor 3 with high-temperature high-pressure fuel gas burning expansion together after the fuel mix of fuel injector 13 ejections, acting rotor shaft 6 output powers.When needing the output of slow-speed of revolution low-power, telescopic pipe 16 elongations are moved along to foremost fuel injector 13 in fumarole 12, make fumarole 12 aperture minimums, jet amount is minimum under the uniform pressure, fuel injector 13 sprays into minimum fuel, gaseous-pressure is lower in the firing chamber front chamber 10, acting rotor 3 rotating speeds are lower, because acting rotor 3 is non-turbine-type impellers, it is less to compare the combustion gas breakage with the turbine-type impeller during low speed, low-speed running is steady, when needs improve rotating speed increasing output power, telescopic pipe 16 retractions increase fuel injector 13 pressurized gas that the fumarole of movement increasing backward 12 apertures spray in the firing chamber front chamber 10 in fumarole 12, fuel injector 13 strengthens the fuel straying quatity simultaneously, the fuel gas temperature gaseous-pressure improves simultaneously in the firing chamber front chamber 10, clockwise rotate the aperture of camshaft 24 increasing suction ports 21, the impetus power that acts on acting rotor 3 blades 28 improves, acting rotor 3 outputting torsions strengthen rotating speed and improve, fumarole 12 variable makes firing chamber rear chamber 11 spray into the controlled of compressed air stream quantitative change in the firing chamber front chamber 10 under identical operating air pressure, under need not to change the situation of pressure, can change the pressurized gas straying quatity that sprays in the firing chamber front chamber 10, also have, two the variable combustion/gas of inflammable mixture that make of fuel straying quatity and pressurized gas straying quatity are than more easy to control, combustion/the gas that in strengthening the process that output power namely improves outputting torsion and rotating speed, can make inflammable mixture under the identical working pressure than relative remain on the optimum value constant, this does not accomplish at the internal-combustion engine that can only individual event changes, the ubiquitous phenomenon of internal-combustion engine that existing individual event changes is---emit a burst of dense smoke during acceleration, have plenty of the acceleration of reduction and improve this defective, also have, when one timing of fumarole 12 sizes, jet amount is certain under the identical working pressure, its power range just is limited at the maximum combustion/gas of inflammable mixture than following between the minimum combustion/gas ratio, fuel straying quatity and pressurized gas straying quatity two are variable to make wideer that the power output area becomes, also have, in the work when the 3 load increases of acting rotor, its rotating speed reduces, amount of consumed gas reduces, and the gaseous-pressure rising makes piston 8 slide toward rear chamber 11 in the firing chamber front chamber 10, reduces fumarole 12 apertures, reduce the pressurized gas straying quatity, improved the combustion/gas ratio of inflammable mixture under the equal fuel straying quatity, the output gas quantity reduces in the firing chamber front chamber 10 simultaneous temperature and pressure raise, and the active force that acts on acting rotor 3 blades 28 raises, acting rotor 3 rotating speeds raise, amount of consumed gas raises, and gaseous-pressure descends in the firing chamber front chamber 10, and piston 8 slides toward front chamber 10 under the pressure of spring 14 and pressurized gas, strengthen fumarole 12 apertures, strengthen the pressurized gas straying quatity, reduced the combustion/gas ratio of inflammable mixture under the equal fuel straying quatity, the combustion gas output quantity increased when temperature and pressure reduced in the firing chamber front chamber 10, make it have very high adaptive ability, telescopic pipe 16 makes fuel obtain good preheating in firing chamber rear chamber 11 in the process by telescopic pipe 16, also has, and can adjust by the position of piston position controller 15 promotion springs 14 or 14 pairs of pistons 8 of pulling spring, as: when using hydrogen, liquid gas, rock gas, during gaseous fuels such as coal gas, because the diffusivity of gaseous fuel, flammability is all higher relatively, can promote springs 14 with piston position controller 15 piston 8 is pushed into the front position of firing chamber front chamber 10 forward, makes the capacity of firing chamber front chamber 10 less relatively, make piston 8 the shortest to the distance of acting rotor 3 suction ports 21, when using gasoline, lightweight kerosene, during volatile liquid fuel such as alcohol, because the diffusivity of this class A fuel A, flammability is higher, can piston 8 be adjusted back the relative middle section position between the chamber of front and back in the firing chamber with piston position controller 15 pulling springs 14, when using kerosene, during not volatile heavy class A fuel A such as diesel oil, can piston 8 be adjusted back with piston position controller 15 pulling springs 14 and lean on the position, back in the firing chamber in the rear chamber 11, make firing chamber front chamber 10 length the longest relatively, prolong fuel from spraying, be mixed into the distance of burning, having prolonged fuel relatively does time in advance with compressed-air actuated, also have, the pressurized air in the firing chamber rear chamber 11 when fumarole 12 sprays into firing chamber front chamber 10, under the guide functions of pressurized air guiding groove 27 fumarole 12 in by several angle in the shape of a spiral shape spray into formation eddy current in the firing chamber front chamber 10, relatively further prolonged fuel from spraying, be mixed into the distance of burning, relatively further prolong fuel and improved mixture homogeneity diffusion time, make fuel combustion more abundant, the variable adjustable of firing chamber is controlled to make wideer that fuel Applicable scope becomes.

Fig. 4, Fig. 5 shows second embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is equally by body 1, centrifugal rotor 2 and non-turbine-type acting rotor 3 formations of calming the anger, the described rotor 2 of calming the anger respectively is installed in body 1 in calm the anger rotor 2 chambeies on same axis with acting rotor 3 in body 1, in acting rotor 3 chambeies, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described acting rotor 3 is contained on the acting rotor shaft 6, comparing difference with first embodiment is: acting rotor shaft 6 is connected through planetary gear set 32 with the rotor shaft 5 of calming the anger, and in planetary gear set 32 planetary gear set control gear 33 is arranged.Because planetary gear set 32 is a kind of special gear structures, multiple connection mode can be arranged, now simply introduce single planetary gear set the most basic several connection modes in this programme, connection mode one: can be connected on the sun gear in the planetary gear set 32 with the rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected in the planetary carrier in the planetary gear set 32 in the heart, and the gear ring in the planetary gear set 32 is in free state; Connection mode two: also can be connected on the sun gear in the planetary gear set 32 with the rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected on the gear ring disc centre in the planetary gear set 32, and the planetary carrier in the planetary gear set 32 is in free state; Connection mode three: can also be connected in the planetary carrier in the planetary gear set 32 in the heart with the rotor shaft 5 of calming the anger, described acting rotor shaft 6 is connected on the sun gear in the planetary gear set 32, and the gear ring in the planetary gear set 32 is in free state; Connection mode four: can also be connected on the gear ring disc centre in the planetary gear set 32 with the rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected on the sun gear in the planetary gear set 32, and the planetary carrier in the planetary gear set 32 is in free state; Connection mode five: can also be connected on the gear ring disc centre in the planetary gear set 32 with the rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected in the planetary carrier in the planetary gear set 32 in the heart, and the sun gear in the planetary gear set 32 is in free state; Connection mode six: can also be connected on the planetary carrier in the planetary gear set 32 with the rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected on the gear ring disc centre in the planetary gear set 32, sun gear in the planetary gear set 32 is in free state, in above six kinds of connection modes: when planetary gear set control gear 33 during wantonly two lockings in the planetary gear set 32, acting rotor 3 is identical with first embodiment's coaxial transmission with the rotating speed transmission with the rotor 2 of calming the anger; When planetary gear set control gear 33 was given resistance that is in the planetary gear set 32 in the free state, the rotor 2 of calming the anger followed the rotating ratio of acting rotor 3 to change along with the increase of this resistance; When this resistance increase until infinity namely planetary gear set 32 in during the free term locking, the rotor 2 of calming the anger will compare transmission by maximum or the minimum speed set with acting rotor 3; Difference also has: described acting rotor 3 chambeies are oval, described acting rotor 3 is double shrouded wheel structures, described blade 28 both sides are by 31 shutoff of wheel sheet, described acting rotor 3 impeller upper blades 28 are installed in the wheel body axial notch 29, on described axial notch 29 bottom blades 28 interior edge faces spring 30 is arranged, annular gas tank 34 with axial notch 29 bottom correspondences is arranged on the described acting rotor 3 chamber sidewalls, the vent 35 of axial notch 29 bottoms on wheel sheet 31 communicates with annular gas tank 34, described annular gas tank 34 communicates with acting rotor air outlet 25 through air flue 36, the oval part in described acting rotor 3 chambeies follows blade 28 with wide, its circular portion is than the thickness of blade 28 wide two wheel sheets 31, the advantage of double shrouded wheel is the sealing that has improved acting rotor 3, make the combustion gas side leakage less, combuster in the body 1 above acting rotor 3 chambeies, described firing chamber and other basic structure are identical with first embodiment with working principle, in the work, high-pressure gas in the firing chamber front chamber 6 is in suction port 21 enters acting rotor 3 chambeies, promoting acting rotor 3 blades 28 rotates acting rotor 3 in the counterclockwise direction, blade 28 withstands on the oval acting rotor 3 chamber inner headed faces all the time at its end face under spring 30 thrust, waste gas under pump-absorb action in the air outlet 25 is through air flue 36, annular gas tank 34, vent 35 enters in axial notch 29 bottoms, described blade 28 turns over behind the central vertical line axially in groove 29 bottoms waste gas progressively through vent 35, annular gas tank 34, air flue 36 is discharged in the air outlet 25, the benefit of oval acting rotor chamber is to leave high-pressure gas that acting rotor 3 suction ports 21 backs are sealed by blade 28 at blade 28 to continue to promote blade 28 by himself expansive force acting rotor 3 is rotated, efficiency gas is higher, shortcoming is that blade 28 end faces are with the contact of acting rotor chamber inner headed face, produce certain surface friction drag, 28 wearing and tearing of hot environment lower blade are very fast, the advantage of planetary gear set 32 is to make the rotor 2 of calming the anger can improve rotating speed under the geostationary situation of acting rotor 3 rotating speeds also can reduce rotating speed, the pressurized air of different compression ratios can be provided to the firing chamber under the geostationary situation of acting rotor 3 rotating speeds, realize the adjustable variable controllable of compression ratio.

Fig. 6, Fig. 7 shows the 3rd embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is equally by body 1, centrifugal rotor 2 and non-turbine-type acting rotor 3 formations of calming the anger, the described rotor 2 of calming the anger respectively is installed in body 1 in calm the anger rotor 2 chambeies on same axis with acting rotor 3 in body 1, in acting rotor 3 chambeies, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described acting rotor 3 is contained on the acting rotor shaft 6, comparing difference with first embodiment is: described acting rotor 3 is thin body double shrouded wheel structures, blade 28 is fixed on the wheel body, blade 28 and wheel Zhou Kuandu are greater than the wheel body width, the blade both sides are by 31 shutoff of wheel sheet, advantage is to have improved intensity and the sealing of blade, alleviated the weight of impeller under the same size, difference: have with blade 28 with wide tongue piece 39 between adjacent two blades 28 on the described acting rotor 3, a limit of described tongue piece 39 connects through 40 one-tenth activity of movable axis with blade 28 top margins in adjacent two blades 28, described movable axis 40 is on acting rotor 3 blades 28 clockwise blade face top margins, tongue piece 39 is to slide up and down in the scope of blade face between the 0-90 degree of its adjacent another blade 28 in another edge of axle center with movable axis 40, its top dead center be no more than corresponding blade 28 top margins that slide, the slip radian on 28 its radians of camber of the corresponding blade in described tongue piece 39 slip limits and tongue piece 39 slip limits is complementary, when tongue piece 39 active edges adjacent two blades 28 during at top dead center, form a rotor cavity 41 of sealing relatively between the wheel sheet 31 on tongue piece 39 and wheel week and blade 28 both sides, there is the sub-cavity of annular gas tank 34 transfers 41 corresponding on the described acting rotor 3 chamber sidewalls, described annular gas tank 34 communicates with acting rotor 3 air outlets 25 through air flue 36, described rotor cavity 41 bottoms follow the annular gas tank 34 of correspondence on the acting rotor 3 chamber sidewalls to communicate through vent 35, and there is gas exhausting valve 38 acting rotor 3 air outlets 25 with on the outer air outlet flue 26 in air flue 36 places of communicating of annular gas tank 34.Its working principle is compared difference and advantage with first embodiment: in the work under the geostationary situation of the gaseous-pressure that firing chamber front chamber 10 provides, high-pressure gas is in acting rotor 3 suction ports 21 spray into acting rotor 3 chambeies, tongue piece 39 on acting rotor 3 blades 28 slides in rotor cavity 41 under the pressure of high-pressure gas, high-pressure gas promotes blade 28 rotates acting rotor 3 in the counterclockwise direction, waste gas enters air outlet flue 29 through acting rotor 3 air outlets 25 and discharges, acting rotor shaft 18 output powers, when acting rotor 3 needs the low speed light running, adjusting camshaft 24 makes suction port 21 apertures less, the gaseous-pressure that acts on acting rotor 3 blades 28 is less relatively, suitably turn the exhaust gas pressure of gas exhausting valve 38 raising acting rotors 3 air outlets 25 on the air outlet flue 26 down, adjusting air flue 26 interior air valves 37 only advances not toward going out waste gas in annular gas tank 34, exhaust gas pressure in the acting rotor 3 upper rotor part cavitys 41 is improved relatively, tongue piece 39 on acting rotor 3 blades 28 slides outside the upwards past rotor cavity 41 under the exhaust gas pressure effect that improves relatively and is in relative higher position, make the week/air displacement of acting rotor 3 relatively low, rotor 3 outputting torsions that do work this moment are compared less.When acting rotor 3 needs the low speed high-load operation, suitably strengthen camshaft 24 apertures, the gaseous-pressure that acts on acting rotor 3 blades 28 strengthens relatively, suitably transfer gas exhausting valve 38 apertures reduction acting rotor 3 air outlets 25 pressure on the big air outlet flue 26, adjust air flue 26 interior air valves 37 and make waste gas only export but no import in annular gas tank 34, rotor cavity 41 internal pressures on the acting rotor 3 are reduced relatively, act on the exhaust gas pressure reduction that tongue piece 39 makes progress below, tongue piece 39 on described acting rotor 3 blades 28 slides into lower dead center downwards in rotor cavity 41 under the effect of high-pressure gas pressure, week/the air displacement of rotor 3 of doing work this moment is maximum relatively, and outputting torsion is compared maximum.When acting rotor 3 needs the high speed high-load operation, continue to strengthen camshaft 24 apertures up to maximum, act on the gaseous-pressure maximum on acting rotor 3 blades 28, gas exhausting valve 38 standard-sized sheets on the air outlet flue 26, the same air flue 26 interior air valves 37 of adjusting make waste gas only export but no import in annular gas tank 34, make the rotor cavity 41 interior exhaust gas pressures on the acting rotor 3 minimum relatively, act on the reduction that upwards pressure below the tongue piece 39, acting rotor 3 rotating speeds improve relatively, act on that centrifugal force on the tongue piece 39 is higher to be made tongue piece 39 leave lower dead center in the rotor cavity 41 to slide outward and be in relatively low position, week/the air displacement of rotor 3 of doing work this moment is relatively large, and outputting torsion compares that to reduce output power maximum relatively.When acting rotor 3 needs the high speed light running, suitably turn gas exhausting valve 38 apertures raising acting rotor 3 air outlets 25 pressure on the air outlet flue 26 down, adjust air flue 26 interior air valves 37 and make waste gas only import but no export in annular gas tank 34, acting rotor 3 upper rotor part cavitys 41 internal pressures are improved relatively, the exhaust gas pressure that tongue piece 39 makes progress below raises and adds that the centrifugal force that acts on the tongue piece 39 is stronger, tongue piece 39 upwards slides into relative higher position, the aperture of suitably turning camshaft 24 down improves gas flow rate, the less relatively rotating speed of week/air displacement of rotor 3 of doing work this moment is higher, outputting torsion is compared less, difference also has: described acting rotor shaft 6 connects through planetary gear set 32 with the rotor shaft 5 of calming the anger, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, the advantage of planetary gear set 32 and planetary gear set control gear 33 is narrated in a second embodiment, here no longer carefully state, above-mentioned workflow will be accomplished the big torsion output of the big air displacement of the slow-speed of revolution fully under the cooperation fully of firing chamber and planetary gear set 32 and planetary gear set control gear 33, the low torsion output of the low air displacement of high rotating speed, the little torsion output of the low air displacement of low speed, the high-power output of the high air displacement of high speed.

Fig. 8, Fig. 9, Figure 10 shows the 4th embodiment of this programme jointly, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is equally by body 1, centrifugal rotor 2 and non-turbine-type acting rotor 3 formations of calming the anger, described acting rotor 3 chambeies equally are oval with acting rotor 3 chambeies among second embodiment, the described rotor 2 of calming the anger respectively is installed in body 1 in calm the anger rotor 2 chambeies on same axis with acting rotor 3 in body 1, in acting rotor 3 chambeies, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described acting rotor 3 is contained on the acting rotor shaft 6, described blade 28 is equally in wheel body axial notch 29, in the described blade 28 lower end surface axial notches 29 spring 30 is arranged, the described rotor shaft 5 of calming the anger is to connect with planetary gear set 32 with acting rotor shaft 6 equally, planetary gear set control gear 33 is arranged on the planetary gear set 32, difference also has: described acting rotor 3 is unshrouded impeller structures, between adjacent two blades 28 tongue piece 39 is arranged on the described impeller, described tongue piece 39 is to insert the Collapsible structure that constitutes by tongue piece convex body 45 and tongue piece concave volume 44 strings, on described tongue piece concave volume 44 internal tongue convex bodys 45 top ends tongue piece spring 46 is arranged, at described blade 28 top ends blade groove 42 is arranged, have in the described blade groove 42 with blade 28 and contact with oval acting rotor 3 chamber inner headed faces with wide roller 43, advantage is to become rolling friction by direct friction to have reduced wearing and tearing and reduced resistance, a limit of described tongue piece convex body 45 connects through 40 one-tenth activity of movable axis with blade 28 top margins in adjacent two blades 28, described movable axis 40 is on acting rotor 3 blades 28 counterclockwise blade face top margins, described tongue piece 39 is that the exterior rim of its tongue piece concave volume 44 of axle center is along sliding up and down in the scope of blade face between the 0-90 degree of adjacent another blade 28 with movable axis 40, its top dead center be no more than corresponding blade 28 top margins that slide, the slip radian of 28 its radians of camber of the corresponding blade in described tongue piece 39 slip limits and tongue piece 39 is complementary, 28 contacts of blade that its exterior rim is slided with correspondence all the time under the active force of spring 46 of described tongue piece concave volume 44, described tongue piece concave volume 44 exterior rim are adjacent two blades 28 when top dead center, the tongue piece 39 that tongue piece concave volume 44 constitutes with tongue piece convex body 45, form a rotor cavity 41 of sealing relatively between wheel body and 3 liang of chamber walls of acting rotor, in the rotor cavity 41 spring 30 is arranged below the described tongue piece 39, there is annular gas tank 34 corresponding with axial notch 29 bottoms on the described acting rotor 3 chamber sidewalls, described annular gas tank 34 communicates with acting rotor 3 air outlets 25 through air flue 36, axial notch 29 bottoms communicate with corresponding annular gas tank 34 on the acting rotor 3 chamber sidewalls, there is gas exhausting valve 38 acting rotor 3 air outlets 25 with on the outer air outlet flue 26 in air flue 36 places of communicating of annular gas tank 34, there is the lower end that communicates, the sub-cavity of its upper end transfers of vane hole 47 41 bottoms to communicate with axial notch 29 bottoms in the described blade 28, with second difference of comparing basic functional principle with the 3rd embodiment be: described tongue piece 39 its tongue piece concave volume 44 exterior rim under the active force of spring 30 are in corresponding 28 top edge of blade of sliding, the active force that blade 28 is subjected to tongue piece 39 lower springs 30 and axial notch 29 bottom springs 30 outwards slides in axial notch 29 and makes that roller 43 contacts with oval rotor 3 inner headed faces that do work its end face groove 42 in, high-pressure gas in the described firing chamber front chamber 10 enter in acting rotor 3 chambeies through camshaft 24 and suction port 21, high-pressure gas at first makes tongue piece 39 along 28 downslides of blade, promoting blade 28 rotates acting rotor 3 in the counterclockwise direction, roller 43 rolls along the inner headed face in ellipse acting rotor 3 chambeies in the described blade 28 end face grooves 42, described blade 28 is along with ellipse acting rotor 3 chamber faces outwards skid off in axial notch 29, described blade 28 turns in oval acting rotor 3 chambeies behind the big nose circle of longest diameter line along with the ellipse rotor 3 chamber inner headed faces that do work slide in axial notch 29, tongue piece concave volume 44 exterior rim of described tongue piece 39 withstand on all the time under the active force of spring 46 on 28 in the corresponding blade that slides, tongue piece concave volume 44 exterior rim of described tongue piece 39 the present position on 28 in the corresponding blade that slides be subjected to exhaust gas pressure in interior gaseous-pressure and the rotor cavity outward 41, spring 30 active forces, and the interaction of centrifugal force control, the present position of tongue piece concave volume 44 exterior rim that at work can be by exhaust gas pressures and then control tongue piece 39 in the gas exhausting valve 38 corresponding regulation and control rotor cavities 41 in air valves 37 in the air flue 36 and the air outlet flue 26 on 28 in the blade of the corresponding slip of institute, realization is to the control of the week/air displacement of acting rotor 3, and concrete working procedure is with the same no longer narration of narrating among the 3rd embodiment here.

Figure 11, Figure 12, Figure 13 shows the 5th embodiment of this programme jointly, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and the non-turbine-type acting rotor formation of calming the anger, described non-turbine-type acting rotor is by acting rotor 3 and the second acting rotor 3 ' constitute, described acting rotor 3 and the second acting rotor 3 ' all be the double shrouded wheel structure, the described rotor 2 of calming the anger, acting rotor 3 and the second acting rotor 3 ' in body 1, be installed in rotor 2 chambeies of calming the anger in the body 1 respectively on same axis, in acting rotor 3 chambeies and the second acting rotor, the 3 ' chamber, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described acting rotor 3 is contained on the acting rotor shaft 6, described second acting rotor 3 ' the be contained in acting rotor shaft 6 ' on, described acting rotor shaft 6 is with the second acting rotor shaft 6 ' do not connect, acting rotor shaft 6 with the second acting rotor shaft 6 ' on bearing 7 is arranged, described acting rotor shaft connects with the rotor shaft 5 of calming the anger through planetary gear set 32, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, a firing chamber of described acting rotor 3 and the second acting rotor 3 ' share is in acting rotor 3 chambeies with above the second acting rotor, 3 ' chamber in the body 1, described firing chamber is identical with the firing chamber of narrating among first embodiment, described rotor 2 air outlets 18 of calming the anger are communicated with firing chamber rear chamber 11 rear ends, on the described air outlet 18 gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described firing chamber front chamber 10 front ends are respectively through acting rotor suction port 21 and the second acting rotor suction port 21 ' with acting rotor 3 and second acting rotor 3 ' connection, described acting rotor suction port 21 and the second acting rotor suction port 21 ' on camshaft 24 is housed respectively, described acting rotor 3 is the same with the second acting rotor, 3 ' structure with acting rotor 3 differences among the 3rd embodiment to be: described acting rotor 3 and the second acting rotor 3 ' and be that wheel body follows blade 28 with wide double shrouded wheel structure, annular gas tank 34 on described second acting rotor 3 ' chamber sidewall with the annular gas tank 34 on the acting rotor 3 chamber sidewalls respectively on relative chamber, both sides wall, annular gas tank 34 on the described acting rotor 3 chamber sidewalls communicates with acting rotor air outlet 25 through air flue 36, annular gas tank 34 on second acting rotor 3 ' chamber sidewall is through second air flue 36 ' with the second acting rotor air outlet 25 ' communicate, described acting rotor 3 and second the acting rotor 3 ' on tongue piece 39 be connected movable axis 40 on the counterclockwise lateral lobe face of blade top margin, described acting rotor air outlet 25 and the second acting rotor air outlet 25 ' jointly are communicated with air outlet flue 26, share a gas exhausting valve 38, other structure is all identical with the 3rd embodiment.Its basic functional principle: caisson 20 is opened in described gas storage valve 19 occlusion pressure air rotors 2 air outlets 18, the pressurized air that has certain pressure in the described caisson 20 promotes piston 8 and strengthens fumarole 12 apertures to front chamber's 10 slips in gas storage valve 19 enters firing chamber rear chamber 11, pressurized air sprays into firing chamber front chamber 10 from fumarole 12, fuel injector 13 ejection fuel mix the formation inflammable mixture with pressurized air simultaneously, an inflammable mixture part enters in the flameholder 23 inflammable mixture that does not enter flameholder 23 with another part through flameholders 23 and converges and lighted the burning of expanding by igniter 22 and generate high-pressure gas, high-temperature high-pressure fuel gas promote piston 8 to rear chamber's 11 sliding compression springs 14 reduce fumarole 12 apertures simultaneously little open acting rotor suction port 21 and the second acting rotor suction port 21 ' on camshaft 24 open acting rotor suction port 21 and the second acting rotor suction port 21 ', high-temperature high-pressure fuel gas through acting rotor suction port 21 and the second acting rotor suction port 21 ' spray to acting rotor 3 and the second acting rotor 3 ', tongue piece 39 on described acting rotor 3 and the second acting rotor 3 ' blade 28 under the pressure of high-pressure gas promotes to lower slider, the described second acting rotor shaft 6 ' for power output shaft load act on more greatly the second acting rotor 3 ' on resistance just bigger, the resistance of comparing on the acting rotor 3 is less, high-pressure gas at first promote to do work rotor 3 rotates, described acting rotor 3 drives rotor 2 rotations of calming the anger through planetary gear set 32,18 formation have the pressurized air of certain pressure to air in the air outlet through the centrifugal rotor 2 pressurization back of calming the anger in the rotor suction port 4 of calming the anger enters the centrifugal rotor 2 of calming the anger, described gas storage valve 19 cuts out caisson 20 and opens the rotor air outlet 18 of calming the anger simultaneously, pressurized air becomes inflammable mixture through fumarole 12 spray people firing chamber front chamber 10 with the fuel mix that fuel injector 13 sprays in air outlet 18 enters firing chamber rear chamber 11, inflammable mixture further improves acting rotor 3 rotating speeds with high-temperature high-pressure fuel gas in the firing chamber front chamber 10 burning expansion together, when gaseous-pressure is brought up to a certain degree in the firing chamber front chamber 10, high-pressure gas act on the second acting rotor 3 ' on active force overcome the second acting rotor 3 ' on resistance promote second acting rotor 3 ' rotation, the second rotor shaft 6 ' terminal output power of doing work.Relevant planetary gear set 32 and planetary gear set control gear 33 are described in detail in a second embodiment, here repeated description no longer, present embodiment advantage: because two acting rotors are arranged, in the work when the second acting rotor 3 ' load when increasing its rotating speed reduce the corresponding reduction of air displacement, the corresponding raising of gaseous-pressure in the firing chamber front chamber 10, the gaseous-pressure of respective action on acting rotor 3 improves, the corresponding raising of the rotating speed of described acting rotor 3, the also corresponding raising of rotating speed of the rotor 2 of calming the anger that acting rotor 3 drives, pressurized gas flow and all corresponding raisings of pressurized gas pressure that the rotor 2 of calming the anger provides for firing chamber rear chamber 11, also corresponding being improved thereupon of gaseous-pressures in the firing chamber front chamber 10, act on second the acting rotor 3 ' on also corresponding raising of gaseous-pressure, second the acting rotor 3 ' rotating speed with regard to corresponding raising, when the second acting rotor 3 ' load corresponding raising with air displacement of its rotating speed when reducing, the corresponding reduction of gaseous-pressure in the firing chamber front chamber 10, the gaseous-pressure of respective action on acting rotor 3 also reduces, the also corresponding reduction of rotating speed of acting rotor 3, the also corresponding reduction of rotating speed of the rotor 2 of calming the anger that the rotor 3 that done work drives, the rotor 2 of calming the anger offers pressurized gas flow and all corresponding reductions of pressurized gas pressure of firing chamber rear chamber 11, also corresponding reduction thereupon of gaseous-pressure in the front chamber 10, act on second the acting rotor 3 ' on equally also corresponding reduction of gaseous-pressure, second the acting rotor 3 ' the corresponding reduction of rotating speed, when the second acting rotor 3 ' load increase to that infinitely great namely the second acting rotor 3 ' when stopping operating, described acting rotor 3 can also keep running alone.Pressing down air rotor in various complex working condition conditions can adjust according to the variation of payload automatically with the acting rotor, the acting rotor is accomplished self adaption with calming the anger between the rotor, in the power output procedure, can save clutch, can accomplish optimum Match with automatic transmission case, make in the power transmittance process loss still less operate simpler.

Figure 14, Figure 15, Figure 16 shows the 6th specific embodiment of this programme jointly, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and the non-turbine-type acting rotor formation of calming the anger, described acting rotor is by acting rotor 3, the second acting rotor 3 ' constitute with the 3rd rotor that does work three unshrouded impeller structures of rotor 3 〞, the described rotor 2 of calming the anger, acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 in body 1, be installed in rotor 2 chambeies of calming the anger in the body 1 respectively on same axis, acting rotor 3 chambeies, in second acting rotor 3 ' chamber and the 3rd acting rotor 3 〞 chambeies, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described acting rotor 3 is contained on the acting rotor shaft 6, described second acting rotor 3 ' the be contained in acting rotor shaft 6 ' on, described the 3rd acting rotor 3 〞 are contained on the 3rd acting rotor shaft 6 〞, the described rotor shaft 5 of calming the anger is coaxial connections with acting rotor shaft 6, described acting rotor shaft 6 connects with the second acting rotor shaft 6 ' usefulness planetary gear set 32, the described second acting rotor shaft 6 ' connect with planetary gear set 32 with the 3rd acting rotor shaft 6 〞, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described the 3rd acting rotor shaft 6 〞 end is power take-off, the independent air outlet flue 26 in described acting rotor 3 independent firing chambers, the described second acting rotor 3 ' and second air outlet flue 26 in the 3rd shared second firing chamber of acting rotor 3 〞 ', calm the anger rotor air outlet 18 with firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' communicate, described calm the anger rotor air outlet 18 with the second firing chamber rear chamber 11 ' between air valve 37 is arranged after the firing chamber rear chamber 11, described acting rotor suction port 21 communicates with firing chamber front chamber 10 front ends, the second acting rotor suction port 21 ' be communicated with at the second firing chamber front chamber, 10 ' front end jointly with described the 3rd acting rotor suction port 21 〞, described acting rotor suction port 21, the second acting rotor suction port 16 ' and the 3rd acting rotor suction port 16 〞 on camshaft 24 is arranged, have with blade 28 with wide tongue piece 39 between adjacent two blades 28 on the described acting rotor 3, a limit of described tongue piece 39 connects through 40 one-tenth activity of movable axis with blade 28 top margins in adjacent two blades 28, described movable axis 40 is on acting rotor 3 blades 28 counterclockwise blade face top margins, described tongue piece 39 is to slide up and down in the scope of blade face between the 0-90 degree of its adjacent another blade 28 in another edge of axle center with movable axis 40, its top dead center be no more than corresponding blade 28 top margins that slide, the slip radian on 28 its radians of camber of the corresponding blade in described tongue piece 39 slip limits and tongue piece 39 slip limits is complementary, when tongue piece 39 active edges adjacent two blades 28 during at top dead center, form a rotor cavity 41 of sealing relatively between the wheel sheet 31 on tongue piece 39 and wheel week and blade 28 both sides, there is the sub-cavity of annular gas tank 34 transfers 41 corresponding on the acting rotor 3 chamber sidewalls, described annular gas tank 34 communicates with acting rotor 3 air outlets 25 through air flue 36, rotor cavity 41 bottoms follow the annular gas tank 34 of correspondence on the acting rotor 3 chamber sidewalls to communicate through vent 35, there is gas exhausting valve 38 acting rotor 3 air outlets 25 with on the outer air outlet flue 26 in air flue 36 places of communicating of annular gas tank 34, the described second acting rotor 3 ' and the 3rd acting rotor 3 〞 chamber sidewalls on annular gas tank 34 is also arranged with the second acting rotor 3 ' corresponding with the 3rd rotor cavity 41 that does work on rotor 3 〞, annular gas tank 34 on second acting rotor 3 ' chamber and the 3rd acting rotor 3 〞 chamber sidewalls respectively through second air flue 36 ' and the 3rd air flue 36 〞 with the second acting rotor air outlet 25 ' and the 3rd acting rotor air outlet 25 〞 be communicated with, described air flue 36, second air flue 36 ' and the 3rd air flue 36 〞 on air valve 37 is arranged, the second acting rotor air outlet 25 ' and the 3rd acting rotor air outlet 25 〞 common be communicated with second air outlet flue 26 ' on, described second air outlet flue 26 ' on gas exhausting valve 38 is arranged, the described second acting rotor 3 ' all identical with acting rotor 3 with other basic structure of the 3rd acting rotor 3 〞, the basic structure of described firing chamber and second firing chamber all follows the firing chamber of narrating among first embodiment identical, described planetary gear set 32 is identical with planetary gear set control gear 33 with the planetary gear set of narrating among second embodiment 32 with planetary gear set control gear 33, is not repeated here.Its working principle: caisson 20 is opened in described gas storage valve 19 occlusion pressure air rotor air outlets 18, the pressurized air that has certain pressure in the caisson 20 through gas storage valve 19 enter firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' in, pressurized air with certain pressure through fumarole 12 spray into firing chamber front chamber 10 and the second firing chamber front chamber 10 ' in form inflammable mixture with the fuel mix of fuel injector 13 ejections, inflammable mixture is generated high-temperature high-pressure fuel gas by ignition mechanism 22 ignition combustions, little camshaft 24 that opens on each suction port is opened acting rotor suction port 21 simultaneously, the second acting rotor suction port 21 ' and the 3rd acting rotor suction port 21 〞, high-temperature high-pressure fuel gas is through acting rotor suction port 21, the second acting rotor suction port 21 ' spray to acting rotor 3 with the 3rd acting rotor suction port 21 〞, the second acting rotor 3 ' and the 3rd acting rotor 3 〞, acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 on tongue piece 39 under the pressure of high-pressure gas promotes to lower slider, high-pressure gas promote respectively to do work epitrochanterian blade 19 make acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 rotate acting, described acting rotor 3 drives rotor 2 rotations of calming the anger through planetary gear set 32, air is in the rotor suction port 4 of calming the anger enters the centrifugal rotor 2 of calming the anger, 18 formation have the pressurized air of certain pressure in the air outlet through the centrifugal rotor 2 pressurization back of calming the anger, described gas storage valve 19 cuts out caisson 20 and opens the rotor air outlet 18 of calming the anger, calm the anger pressurized air that 18 places, rotor air outlet have a certain pressure through air outlet 18 enter firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' in, the pressurized air with certain pressure from fumarole 12 spray people firing chamber front chamber 10 and the second firing chamber front chamber 10 ' with the fuel mix burning of fuel injector 11 ejections promote acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 rotate acting.Can also start a firing chamber earlier and enable other firing chamber, as: as described in gas storage valve 19 occlusion pressure air rotor air outlets 18 open caisson 20, close gas check valve 37 simultaneously and remove acting rotor shaft 6 with the second acting rotor shaft 6 ' between wantonly two locking and make free term be in free state to the control of free term in the planetary gear set 32 in 33 pairs of planetary gear set 32 of planetary gear set control gear, the pressurized air that has certain pressure in the described caisson 20 enters in the firing chamber rear chamber 11 through gas storage valve 19, pressurized air with certain pressure sprays into the fuel mix that sprays with fuel injector 13 in the front chamber 10 through fumarole 12 and forms inflammable mixture, inflammable mixture is generated high-temperature high-pressure fuel gas by ignition mechanism 22 ignition combustions, little camshaft 24 that opens on the suction port is opened acting rotor suction port 21 simultaneously, high-temperature high-pressure fuel gas sprays to acting rotor 3 through acting rotor suction port 21, the tongue piece 39 of acting on the rotor 3 under the pressure of high-pressure gas promotes to lower slider, the blade 19 that high-temperature high-pressure fuel gas promotes on the acting rotor 3 makes acting rotor 3 rotate acting, described acting rotor 3 drives rotor 2 rotations of calming the anger through planetary gear set 32, air is in the rotor suction port 4 of calming the anger enters the centrifugal rotor 2 of calming the anger, 18 formation have the pressurized air of certain pressure in the air outlet through the centrifugal rotor 2 pressurization back of calming the anger, described gas storage valve 19 cuts out caisson 20 and opens the rotor air outlet 18 of calming the anger, open air valve 37 simultaneously, the pressurized air that described 18 places, rotor air outlet of calming the anger have a certain pressure through air outlet 18 enter firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' in, the pressurized air with certain pressure from fumarole 12 spray people firing chamber front chamber 10 and the second firing chamber front chamber 10 ' with the fuel mix burning of fuel injector 11 ejections promote acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 rotate acting.Advantage: owing to adopted two firing chambers at present embodiment, three acting rotors, and all connected by planetary gear set 32 between three acting rotors, through planetary gear set control gear 33 can regulate and control arbitrarily respectively to do work between the rotor and and the rotating ratio between the rotor 2 of calming the anger, regulate and control more flexible, can also between rotor air outlet 18 and the firing chamber rear chamber 11 air valve 37 be set calming the anger, can close or open in two firing chambers any arbitrarily according to different power output needs in the work and can make and have only a job also can make in three acting rotors to have only two work that three acting rotors are all worked in three acting rotors, its power output accommodation is broader.

Figure 17, Figure 18 shows the 7th specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and the non-turbine-type acting rotor formation of calming the anger, described acting rotor is by acting rotor 3 and the second acting rotor 3 ' constitute, the described rotor 2 of calming the anger, acting rotor 3 and the second acting rotor 3 ' in body 1, be installed in rotor 2 chambeies of calming the anger in the body 1 respectively on same axis, in acting rotor 3 chambeies and the second acting rotor, the 3 ' chamber, the described rotor 2 of calming the anger is contained on the rotor shaft 5 of calming the anger, described second acting rotor 3 ' the be contained in acting rotor shaft 6 ' on, a firing chamber of described acting rotor 3 and the second acting rotor 3 ' share is in acting rotor 3 chambeies with above the second acting rotor, 3 ' chamber in the body 1, described firing chamber is identical with the firing chamber of narrating among first embodiment, described rotor 2 air outlets 18 of calming the anger are communicated with firing chamber rear chamber 11 rear ends, on the described air outlet 18 gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described firing chamber front chamber 10 front ends are respectively through acting rotor suction port 21 and the second acting rotor suction port 21 ' with acting rotor 3 and second acting rotor 3 ' connection, described acting rotor suction port 21 and the second acting rotor suction port 21 ' on camshaft 24 is housed respectively, the described rotor shaft 5 of calming the anger is followed second acting rotor shaft 6 ' connection through planetary gear set 32, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described planetary gear set 32 and planetary gear set control gear 33 all are installed in acting rotor 3 wheel bodys, described acting rotor 3 wheel bodys can directly be connected on the bull gear 48 in the planetary gear set 32, also can directly substitute the bull gear 48 in the planetary gear set 32, can also directly connect with planetary carrier 49 centers in the planetary gear set 32, save acting rotor shaft 6, make overall structure compacter, volume is littler, the described second acting rotor shaft 6 ' directly connect with the rotor shaft 5 of calming the anger through planetary gear set 32, Placement one: when acting rotor 3 wheel bodys substitute bull gear 48 in the planetary gear set 32, the second acting rotor shaft 6 ' and the rotor shaft 5 of calming the anger can be connected in planetary carrier 49 centers in the planetary gear set 32 and the sun gear 50 in the heart, Placement two: when acting rotor 3 wheel bodys are connected in the planetary carrier 49 in the planetary gear set 32 in the heart, the second acting rotor shaft 6 ' and the rotor shaft 5 of calming the anger can be connected in bull gear 48 in the planetary gear set 32 and the sun gear 50 in the heart, at work, when acting rotor 3 lockings, the described second acting rotor 3 ' with the default planetary gear set 32 rotating ratio transmissions of rotor 2 peaces of calming the anger, when 3 runnings of acting rotor, the described second acting rotor 3 ' will change with the rotation speed change of acting rotor 3 with the rotating ratio of calming the anger between the rotor 2, other operation mode is described in detail in a second embodiment, the described rotor 2 of calming the anger, acting rotor 3, the second acting rotor 3 ' and basic structure and the working principle thereof of firing chamber are all identical with what narrate among the 4th embodiment, are not repeated.

Figure 19, Figure 20 shows the 8th specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by the previous stage vane pump formula rotor 52 of calming the anger, calm the anger rotor 51 and non-turbine-type acting rotor 3 and body 1 of vane pump formula constitutes, described vane pump formula rotor 51 and the previous stage vane pump formula rotor 52 of calming the anger of calming the anger is installed in the body 1 calm the anger rotor 51 chambeies and previous stage vane pump formula of oval-shaped vane pump formula respectively and calms the anger in rotor 52 chambeies, described acting rotor 3 is installed in body 1 inner cylindrical acting rotor 3 chambeies, calm the anger rotor 51 and previous stage vane pump formula of described vane pump formula calmed the anger rotor 52 and acting rotor 3 all in body 1 on the same axis line, the described vane pump formula rotor 51 of calming the anger is installed on the rotor shaft 5 of calming the anger for the final stage rotor of calming the anger, the described previous stage vane pump formula rotor 52 of calming the anger is installed in previous stage and calms the anger on the rotor shaft 55, described acting rotor 3 is installed on the acting rotor shaft 6, described calm the anger rotor shaft 5 and the previous stage rotor shaft 55 of calming the anger is coaxial connections with acting rotor shaft 6, described body 1 front has the previous stage rotor suction port 53 front one-level vane pump formulas rotor 52 of calming the anger of calming the anger to communicate, described previous stage is calmed the anger rotor air outlet 54 with rotor suction port 4 connections of calming the anger, described suction port 4 is communicated with the vane pump formula rotor 51 of calming the anger, on the described rotor air outlet 18 of calming the anger gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described acting rotor 3 is unshrouded impeller structures, described impeller upper blade 28 is fixed on the wheel body not with the contact of chamber wall, the described previous stage rotor shaft 55 of calming the anger, calm the anger and bearing 7 is housed in body 1 spacing wall on rotor shaft 5 and the acting rotor shaft 6, in the body 1 throat less chamber is arranged above described acting rotor 3 chambeies, the cylindrical piston 8 that is complementary with circle in the firing chamber is arranged in the described throat less chamber, on described cylindrical piston 8 peripheries sealed piston ring 9 is arranged, described cylindrical piston 8 is divided into firing chamber front chamber 10 and firing chamber rear chamber 11 to the firing chamber, described cylindrical piston 8 can slide in firing chamber front chamber 10 and firing chamber rear chamber 11, there is fumarole 12 at described piston 8 centers, described fumarole 12 centers be equipped with can antero posterior axis to the fuel injector 13 of activity, on the described fumarole 12 guiding piece 27 is arranged, in the described cylindrical piston 8 rear end firing chamber rear chamber 11 spring 14 is arranged, in the described spring 14 rear end firing chamber rear chamber 11 piston position controller 15 is arranged, in described spring 14 circles telescopic pipe 16 is arranged, described telescopic pipe 16 front ends are communicated with fuel injector 13, the rear end is through piston position controller 15, body 1 is communicated with fuel supplying device 17, described firing chamber rear chamber 11 rear ends communicate with the rotor air outlet 18 of calming the anger, described firing chamber front chamber 10 front ends are communicated with acting rotor 3 suction ports 21, on described firing chamber front chamber 10 front ends acting rotor, 3 suction ports 21 ignition mechanism 22 and flameholder 23 are installed, there is rotatable cam axle 24 at described acting rotor 3 suction ports 21 places, described acting rotor 3 air outlets 25 communicate with air outlet flue 26, have with blade 28 with wide tongue piece 39 between adjacent two blades 28 on described acting rotor 3 impellers, a limit of described tongue piece 39 connects through 40 one-tenth activity of movable axis with blade 28 top margins in adjacent two blades 28, described movable axis 40 is on acting rotor 3 blades 28 counterclockwise blade face top margins, described tongue piece 39 is to slide up and down in the scope of blade face between the 0-90 degree of its adjacent another blade 28 in another edge of axle center with movable axis 40, its top dead center be no more than corresponding blade 28 top margins that slide, the slip radian on 28 its radians of camber of the corresponding blade in described tongue piece 39 slip limits and tongue piece 39 slip limits is complementary, when tongue piece 39 active edges adjacent two blades 28 during at top dead center, form a rotor cavity 41 of sealing relatively between the wheel sheet 31 on tongue piece 39 and wheel week and blade 28 both sides, there is the sub-cavity of annular gas tank 34 transfers 41 corresponding on the described acting rotor 3 chamber sidewalls, described annular gas tank 34 communicates with acting rotor air outlet 25 through air flue 36, on the described air flue 36 air valve 37 is arranged, described rotor cavity 41 bottoms communicate with corresponding annular gas tank 34 on the acting rotor 3 chamber sidewalls, and there is gas exhausting valve 38 acting rotor air outlet 25 with on the outer air outlet flue 26 in air flue 36 places of communicating of annular gas tank 34.Basic functional principle: caisson 20 is opened in described gas storage valve 19 occlusion pressure air rotor air outlets 18, the pressurized air that has certain pressure in the described caisson 20 promotes piston 8 and strengthens fumarole 12 apertures to front chamber's 10 slips in gas storage valve 19 enters firing chamber rear chamber 11, pressurized air sprays into firing chamber front chamber 10 from fumarole 12, fuel injector 13 ejection fuel mix the formation inflammable mixture with pressurized air simultaneously, an inflammable mixture part enters in the flameholder 23 inflammable mixture that does not enter flameholder 23 with another part through flameholders 23 and converges and lighted the burning of expanding by igniter 22 and generate high-temperature high-pressure fuel gas, high-pressure gas promotion piston 8 reduces the simultaneously little camshaft 24 that opens on the acting rotor suction port 21 of fumarole 12 apertures to rear chamber's 11 sliding compression springs 14 and opens acting rotor suction port 21, high-pressure gas sprays to acting rotor 3 through acting rotor suction port 21, tongue piece 39 on described acting rotor 3 blades 28 slides in rotor cavity 41 under the pressure of high-pressure gas promotes, high-pressure gas promotes blade 28 rotates acting rotor 3, acting rotor 3 drives calm the anger rotor shaft 5 and the previous stage rotor shaft 55 of calming the anger through acting rotor shaft 6 and makes rotor 51 and previous stage vane pump formula rotor 52 rotations of calming the anger of calming the anger of vane pump formula, air enters previous stage vane pump formula and calms the anger in the rotor 52 and to form pressurized air with certain pressure and directly enter the vane pump formula and calm the anger in the rotor 51 and to compress the pressurized air that the formation of pressurizeing has elevated pressures again through the vane pump formula rotor 51 of calming the anger through calm the anger rotor air outlet 54 and the rotor suction port 4 of calming the anger of previous stage through the previous stage vane pump formula rotor 52 pressurization backs of calming the anger through the previous stage rotor suction port 53 of calming the anger, described gas storage valve 19 cuts out caisson 20 and opens the rotor air outlet 18 of calming the anger simultaneously, pressurized air with elevated pressures enters through the rotor air outlet 18 of calming the anger in the firing chamber rear chamber 11 and becomes inflammable mixture through fumarole 12 spray people firing chamber front chamber 10 with the fuel mix that fuel injector 13 sprays, inflammable mixture is with rotor 3 rotations that further promote to do work of high-temperature high-pressure fuel gas in the firing chamber front chamber 10 burning expansion together, described acting rotor shaft 6 terminal output powers.The formula of vane pump described in present embodiment rotor 51 and the previous stage vane pump formula rotor 52 of calming the anger of calming the anger constitutes the two-stage vane pump formulas rotor of calming the anger, improve the rotor of calming the anger and exported compressed-air actuated compression ratio, further improve pressurized gas pressure in the firing chamber rear chamber 7, further improve the gaseous-pressure in the firing chamber front chamber 6, be conducive to the abundant burning of fuel.

Figure 20, Figure 21 shows the 9th specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, the centrifugal rotor 2 of calming the anger, vane pump formula rotor 51 and the non-turbine-type acting rotor 3 of calming the anger constitutes, described non-turbine-type acting rotor 3 is unshrouded impeller structures, the described vane pump formula rotor 51 of calming the anger is installed in the body 1 oval-shaped vane pump formula and calms the anger in rotor 51 chambeies, described centrifugal rotor 2 and the impeller type acting rotor 3 of calming the anger is installed in body 1 inner cylindrical acting rotor 3 chambeies, described vane pump formula is calmed the anger rotor 51 and centrifugal rotor 2 and the impeller type acting rotor 3 of calming the anger all in body 1 on the same axis line, the described vane pump formula rotor 51 of calming the anger is installed on the rotor shaft 5 of calming the anger for the final stage rotor of calming the anger, the described centrifugal rotor 2 of calming the anger is installed in previous stage and calms the anger on the rotor shaft 55, described acting rotor 3 is installed on the acting rotor shaft 6, described calm the anger rotor shaft 5 and the previous stage rotor shaft 55 of calming the anger is coaxial connections, the described rotor shaft 5 of calming the anger connects with acting rotor shaft 6 through planetary gear set 32, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described body 1 front has calm the anger rotor suction port 53 of previous stage to communicate with the centrifugal rotor 2 of calming the anger, described previous stage is calmed the anger rotor air outlet 54 with rotor suction port 4 connections of calming the anger, described suction port 4 is communicated with the vane pump formula rotor 51 of calming the anger, on the described rotor air outlet 18 of calming the anger gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described acting rotor 3 impeller upper blades 28 are fixed on the wheel body not with the contact of chamber wall, the described previous stage rotor shaft 55 of calming the anger, calm the anger and bearing 7 is housed in body 1 spacing wall on rotor shaft 5 and the acting rotor shaft 6, in the body 1 throat less chamber is arranged above described acting rotor 3 chambeies, described firing chamber front chamber 10 front ends are communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, described air outlet 25 is with on the air flue 36 outer air outlet flues 36 that annular gas tank 34 is communicated with on the acting rotor 3 chamber sidewalls gas exhausting valve 38 being arranged, on the described air flue 36 air valve 37 is arranged, described planetary gear set 32 is identical with planetary gear set control gear 33 with planetary gear set 32 described in second embodiment with planetary gear set control gear 33, described acting rotor 3 is identical with the firing chamber with the acting rotor of narrating among the 8th embodiment 3 with basic structure and the working principle of firing chamber, no longer describe in detail, the rotor of calming the anger in the present embodiment is to be constituted and mixed the coaxial gas pressure mechanism of two-stage by centrifugal calm the anger rotor 2 and the vane type oil pump formula rotor 51 of calming the anger, mix the two stage compressor structure and can utilize the performance characteristic of the various forms of rotors of calming the anger further to improve the working rotor efficient of calming the anger better, effectively improve the pressurized gas pressure of the rotor air outlet 18 of calming the anger.

Figure 20, Figure 22 shows the tenth specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, the centrifugal rotor 2 of calming the anger, vane pump formula rotor 51 and the non-turbine-type acting rotor 3 of calming the anger constitutes, described non-turbine-type acting rotor 3 is unshrouded impeller structures, the described vane pump formula rotor 51 of calming the anger is installed in the body 1 oval-shaped vane pump formula and calms the anger in rotor 51 chambeies, described centrifugal rotor 2 and the impeller type acting rotor 3 of calming the anger is installed in body 1 inner cylindrical acting rotor 3 chambeies, described vane pump formula is calmed the anger rotor 51 and centrifugal rotor 2 and the impeller type acting rotor 3 of calming the anger all in body 1 on the same axis line, the described vane pump formula rotor 51 of calming the anger is installed on the rotor shaft 5 of calming the anger for the final stage rotor of calming the anger, the described centrifugal rotor 2 of calming the anger is installed in previous stage and calms the anger on the rotor shaft 55, described acting rotor 3 is installed on the acting rotor shaft 6, the described rotor shaft 5 of calming the anger connects through calm the anger rotor shaft 55 of planetary gear set 32 front one-levels, the described rotor shaft 5 of calming the anger connects with acting rotor shaft 6 through planetary gear set 32, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described body 1 front has calm the anger rotor suction port 53 of previous stage to communicate with the centrifugal rotor 2 of calming the anger, described previous stage is calmed the anger rotor air outlet 54 with rotor suction port 4 connections of calming the anger, described suction port 4 is communicated with the vane pump formula rotor 51 of calming the anger, on the described rotor air outlet 18 of calming the anger gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described acting rotor 3 impeller upper blades 28 are fixed on the wheel body not with the contact of chamber wall, the described previous stage rotor shaft 55 of calming the anger, calm the anger and bearing 7 is housed in body 1 spacing wall on rotor shaft 5 and the acting rotor shaft 6, in the body 1 throat less chamber is arranged above described acting rotor 3 chambeies, described firing chamber front chamber 10 front ends are communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, described air outlet 25 is with on the air flue 36 outer air outlet flues 36 that annular gas tank 34 is communicated with on the acting rotor 3 chamber sidewalls gas exhausting valve 38 being arranged, on the described air flue 36 air valve 37 is arranged, described planetary gear set 32 is identical with planetary gear set control gear 33 with planetary gear set 32 described in second embodiment with planetary gear set control gear 33, described acting rotor 3 is identical with the firing chamber with the acting rotor of narrating among the 8th embodiment 3 with basic structure and the working principle of firing chamber, here no longer describe in detail, the rotor of calming the anger in the present embodiment is to be constituted and mixed the two stage compressor structure by centrifugal calm the anger rotor 2 and the vane type oil pump formula rotor 51 of calming the anger, mix the two stage compressor structure and under the flexible allotment of 32 pairs of rotating speeds of planetary gear set, can utilize the performance characteristic of the various forms of rotors of calming the anger further to improve the working rotor efficient of calming the anger better, effectively improve the pressurized gas pressure of the rotor air outlet 18 of calming the anger.

Figure 20, Figure 23 shows the 11 specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ', before calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 and body 1 of secondary turbine-type constitute, the described turbine-type rotor 56 of calming the anger is installed on the rotor shaft 5 of calming the anger for the final stage rotor of calming the anger, previous stage turbine-type rotor 56 ' the be installed in previous stage of calming the anger is calmed the anger on the rotor shaft 55, before described the secondary turbine-type calm the anger rotor 56 〞 be installed in before secondary calm the anger on the rotor shaft 57, described acting rotor 3 is installed on the acting rotor shaft 6, the described turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ', before secondary turbine-type rotor 56 〞 and the non-turbine-type acting rotor 3 of calming the anger all in body 1, be installed in rotor 56 chambeies of calming the anger respectively on same axis, the previous stage rotor 56 ' chamber of calming the anger, preceding secondary is calmed the anger in rotor 56 〞 chambeies and acting rotor 3 chambeies, described acting rotor shaft 6 is with calming the anger between the rotor shaft 5, the rotor shaft 5 front one-levels of calming the anger are calmed the anger between the rotor shaft 55, it all is to connect with planetary gear set 32 that previous stage calms the anger that rotor shaft 55 front secondarys calm the anger between the rotor shaft 57, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described acting rotor 3 is unshrouded impeller structures, described impeller blade 28 is fixed on the wheel body, combuster in the body 1 above described acting rotor 3 chambeies, described firing chamber is identical with acting rotor 3 with the firing chamber of narrating among the 8th embodiment with acting rotor 3, described body 1 front end has preceding secondary rotor suction port 59 front secondarys rotor 56 〞 that calm the anger that calm the anger to communicate, secondary the calm the anger rotor suction port 53 of rotor air outlet 58 front one-levels of calming the anger is communicated with before described, calm the anger rotor air outlet 54 of described previous stage is communicated with the final stage rotor suction port 4 of calming the anger, described final stage is calmed the anger rotor air outlet 18 with the 11 rear ends connection of firing chamber rear chamber, on the described air outlet 18 gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described firing chamber front chamber 10 front ends are communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, described air outlet 25 is with on the air flue 36 outer air outlet flues 36 that annular gas tank 34 is communicated with on the acting rotor 3 chamber sidewalls gas exhausting valve 38 being arranged, on the described air flue 36 air valve 37 is arranged, in the present embodiment by the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ', before secondary turbine-type rotor 56 〞 that calm the anger constitute the multistage turbine formula rotor of calming the anger, utilize planetary gear set 32 and planetary gear set control gear 33 can regulate and control flexibly the multistage turbine formula calm the anger rotor at different levels between and final stage calm the anger rotor 56 with the rotating ratio between the acting rotor 3, further performance utilizes the calm the anger advantage of rotor of multistage turbine formula.

Figure 20, Figure 24 shows the 12 specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by the centrifugal rotor 2 of calming the anger, the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ', before calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 and body 1 of secondary turbine-type constitute, the described centrifugal rotor 2 of calming the anger is installed on the rotor shaft 5 of calming the anger for the final stage rotor of calming the anger, the turbine-type rotor 56 of calming the anger is installed in previous stage and calms the anger on the rotor shaft 55, the described previous stage turbine-type secondary of calming the anger before the rotor 56 ' be installed in is calmed the anger on the rotor shaft 57, secondary turbine-type rotor 56 〞 that calm the anger are installed in first three level and calm the anger on the rotor shaft 60 before described, described acting rotor 3 is installed on the acting rotor shaft 6, the described centrifugal rotor 2 of calming the anger, the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ', before secondary turbine-type rotor 56 〞 and the non-turbine-type acting rotor 3 of calming the anger all in body 1, be installed in centrifugal rotor 2 chambeies of calming the anger respectively on same axis, rotor 56 chambeies of calming the anger, the previous stage rotor 56 ' chamber of calming the anger, preceding secondary is calmed the anger in rotor 56 〞 chambeies and acting rotor 3 chambeies, described acting rotor shaft 6 is with calming the anger between the rotor shaft 5, the rotor shaft 5 front one-levels of calming the anger are calmed the anger between the rotor shaft 55, previous stage calm the anger rotor shaft 55 front secondarys calm the anger between the rotor shaft 57 and preceding secondary to calm the anger that rotor shaft 57 fronts calm the anger between the rotor shaft 60 for three grades all be to connect with planetary gear set 32, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described acting rotor 3 is unshrouded impeller structures, described impeller blade 28 is fixed on the wheel body, combuster in the body 1 above described acting rotor 3 chambeies, described firing chamber is identical with acting rotor 3 with the firing chamber of narrating among the 8th embodiment with acting rotor 3, described body 1 front end has first three level rotor suction port 61 front secondary turbine-types rotor 56 〞 that calm the anger that calm the anger to communicate, described first three level calm the anger rotor suction port 59 of rotor air outlet 62 front secondary turbine-types of calming the anger is communicated with, calm the anger rotor air outlet 58 of secondary turbine-type is communicated with the turbine-type rotor suction port 53 of calming the anger before described, described turbine-type is calmed the anger rotor 56 air outlets 54 with centrifugal rotor 2 suction ports 4 connections of calming the anger, described final stage is calmed the anger rotor air outlet 18 with the 11 rear ends connection of firing chamber rear chamber, on the described air outlet 18 gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described firing chamber front chamber 10 front ends are communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, described air outlet 25 is with on the air flue 36 outer air outlet flues 36 that annular gas tank 34 is communicated with on the acting rotor 3 chamber sidewalls gas exhausting valve 38 being arranged, on the described air flue 36 air valve 37 is arranged, in the present embodiment by the centrifugal rotor 2 of calming the anger, the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ' and preceding secondary turbine-type rotor 56 〞 that calm the anger constitute the hybrid multi-stage rotor of calming the anger jointly, utilize 33 pairs of hybrid multi-stages of planetary gear set 32 and planetary gear set control gear to calm the anger between each rotor of rotor and the hybrid multi-stage rotor of calming the anger connects between the rotor 3 with acting, can regulate and control more flexibly that hybrid multi-stage is calmed the anger between the rotor rotors at different levels and with the rotating ratio between the acting rotor 3, it is better that pressures-combustion is mated.

Figure 20, Figure 25 shows the 13 specific embodiment of this programme, by accompanying drawing as can be seen, internal combustion engine shown in the present embodiment is by body 1, preceding secondary turbine-type acting rotor 56 〞, the previous stage turbine-type calm the anger rotor 56 ', the turbine-type rotor 56 of calming the anger, calm the anger rotor 51 and non-turbine-type acting rotor 3 of centrifugal calm the anger rotor 2 and vane pump formula constitutes, the described vane pump formula rotor 51 of calming the anger is installed on the rotor shaft 5 of calming the anger for the final stage rotor of calming the anger, the described centrifugal rotor 2 of calming the anger is installed in previous stage and calms the anger on the rotor shaft 55, described turbine-type calm the anger rotor 56 be installed in before secondary calm the anger on the rotor shaft 57, previous stage turbine-type first three level of rotor 56 ' be installed in of calming the anger is calmed the anger on the rotor shaft 60, before described the secondary turbine-type calm the anger rotor 56 〞 be installed in before level Four calm the anger on the rotor shaft 63, described acting rotor 3 is installed on the acting rotor shaft 6, the described vane pump formula rotor 51 of calming the anger, the centrifugal rotor 2 of calming the anger, the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ', before secondary turbine-type rotor 56 〞 and the non-turbine-type acting rotor 3 of calming the anger all in body 1, be installed in vane pump formula rotor 51 chambeies of calming the anger on same axis respectively, centrifugal rotor 2 chambeies of calming the anger, rotor 56 chambeies of calming the anger, the previous stage rotor 56 ' chamber of calming the anger, preceding secondary is calmed the anger in rotor 56 〞 chambeies and acting rotor 3 chambeies, described acting rotor shaft 6 is with calming the anger between the rotor shaft 5, the rotor shaft 5 front one-levels of calming the anger are calmed the anger between the rotor shaft 55, the previous stage rotor shaft 55 front secondarys of calming the anger are calmed the anger between the rotor shaft 57, before secondary calm the anger three grades of rotor shaft 57 fronts calm the anger between the rotor shaft 60 and first three level to calm the anger that rotor shaft 60 front level Four calm the anger between the rotor shaft 63 all be to connect with planetary gear set 32, on the described planetary gear set 32 planetary gear set control gear 33 is arranged, described acting rotor 3 is unshrouded impeller structures, described impeller blade 28 is fixed on the wheel body, combuster in the body 1 above described acting rotor 3 chambeies, described firing chamber is identical with acting rotor 3 with the firing chamber of narrating among the 8th embodiment with acting rotor 3, described body 1 front end has preceding level Four rotor suction port 64 front secondary turbine-types rotor 56 〞 that calm the anger that calm the anger to communicate, level Four three grades of 65 fronts, the rotor air outlet rotor suction ports 61 of calming the anger of calming the anger are communicated with before described, described first three level calm the anger rotor suction port 59 of rotor air outlet 62 front secondarys of calming the anger is communicated with, before secondary the calm the anger rotor suction port 53 of rotor air outlet 58 front one-levels of calming the anger be communicated with, described previous stage is calmed the anger rotor air outlet 54 with rotor suction port 4 connections of calming the anger, described final stage is calmed the anger rotor air outlet 18 with the 11 rear ends connection of firing chamber rear chamber, on the described rotor air outlet 18 of calming the anger gas storage valve 19 is arranged, described gas storage valve 19 is communicated with body 1 outer caisson 20, described firing chamber front chamber 10 front ends are communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, described air outlet 25 is with on the air flue 36 outer air outlet flues 36 that annular gas tank 34 is communicated with on the acting rotor 3 chamber sidewalls gas exhausting valve 38 being arranged, on the described air flue 36 air valve 37 is arranged, in this specific embodiment by the vane pump formula rotor 51 of calming the anger, the centrifugal rotor 2 of calming the anger, the turbine-type rotor 56 of calming the anger, the previous stage turbine-type calm the anger rotor 56 ' and preceding secondary turbine-type rotor 56 〞 that calm the anger constitute the hybrid multi-stage rotor of calming the anger jointly, utilize 33 pairs of hybrid multi-stages of planetary gear set 32 and planetary gear set control gear to calm the anger between each rotor of rotor and the hybrid multi-stage rotor of calming the anger connects between the rotor 3 with acting, can regulate and control more flexibly that hybrid multi-stage is calmed the anger between the rotor rotors at different levels and with the rotating ratio between the acting rotor 3, make pressure-combustion coupling better, the more pressurized air of high compression ratio can enough be provided, suitably adjust the position of piston 8 in the firing chamber by firing chamber rear chamber 7 inner carrier position controllers 10 and adapt to the needed different conditional request of various fuel combustions, reach many fuel of machine purpose.

By to the narration of above 13 specific embodiments as can be seen, the application can have many variations to be not limited only to above 13 specific embodiments, more than can exchange between 13 specific embodiments and have or not, exchange mutually, as can be with first, second, the 3rd, the 4th, the 5th, the 6th, acting rotor among the 7th embodiment is with the 8th, the 9th, the tenth, the 11, the 12, the acting rotor exchanges among the 13 embodiment, can also reconfigure, also having described acting rotor can be one, two, or a plurality of acting rotors more than two, also have, it also can be the firing chamber of can also dividing into groups to use, each acting rotor private firing chamber that described a plurality of acting rotor can share a firing chamber, the described rotor of calming the anger can be centrifugal turbocompressor, vane pump formula gas compressor, turbine-type page or leaf sheet gas compressor, it also can be other form of being applicable to this programme rotor of calming the anger, the described rotor of calming the anger can be one-level, the above multistage compressor structure of two-stage and two-stage, as the multistage turbine gas compressor, multistage blade compressor etc., the hybrid multi-stage gas pressure mechanism that the gas compressor that the described rotor of calming the anger can also be various ways constitutes, be final stage as making elementary centrifugal turbocompressor with turbine page or leaf chip gas compressor, centrifugal turbocompressor is that elementary vane pump formula gas compressor is mixed construction such as middle final stage, can be that coaxial pattern also can be can also be that selectively to use planetary gear set to connect coaxial with the split axle pattern that planetary gear set connects between described multistage compressor structure or hybrid multi-stage gas pressure mechanism at different levels, the split axle mixed mode, described planetary gear set can be that single planetary gear set structure also can be two or more a plurality of planetary gear set structures, described camshaft, the gas storage control valve, caisson, flameholder and gas exhausting valve can save.Above all changes are all within the application's protection domain.

Claims (9)

1. internal combustion engine, by body, the rotor of calming the anger, acting rotor and fuel supplying device, ignition mechanism constitutes, the rotor of calming the anger is installed in respectively in calm the anger rotor chamber and the acting rotor chamber with the acting rotor, acting rotor and calming the anger has body wall and spring bearing at interval between the rotor, the body front has suction port to follow to calm the anger rotor to communicate, it is characterized in that: the described rotor of calming the anger links to each other with acting rotor diaxon on same axis, described acting rotor is non-turbine-type blade wheel structure, described firing chamber is cylindrical shape on the acting rotor in the body, the cylindrical piston that is complementary with circular diameter in the firing chamber is arranged in the firing chamber, on the described cylindrical piston periphery seal ring is arranged, described cylindrical piston is divided into former and later two chambers to the firing chamber, described cylindrical piston can slide in the chamber of the front and back of firing chamber, there is fumarole at described cylindrical piston center, the intracardiac fuel injector that is equipped with in the described fumarole, described fuel injector can be axially movable in fumarole, in the firing chamber rear chamber of described cylindrical piston rear end spring is arranged, described spring rear end has the piston position controller, in the described spring ring telescopic pipe is arranged, described telescopic pipe front end communicates with fuel injector, the telescopic pipe rear end is through the piston position controller, body communicates with fuel supplying device, described firing chamber rear chamber rear end is communicated with the rotor air outlet of calming the anger, described firing chamber front chamber front end is communicated with acting rotor suction port, on the described acting rotor suction port ignition mechanism is installed, described acting rotor air outlet communicates with air outlet flue at the another side of suction port correspondence.

2. according to the described a kind of internal combustion engine of claim 1, it is characterized in that: described acting rotor chamber is circular, have with blade with wide tongue piece between adjacent two blades on the impeller in the described acting rotor chamber, a limit of described tongue piece becomes active with a blade top margin in adjacent two blades through movable axis and connects, described tongue piece is that the blade face of its another adjacent another blade in edge of axle center slides up and down in the scope between the 0-90 degree with the movable axis, its top dead center be no more than the corresponding blade top margin that slides, the slip radian on corresponding its radian of blade face camber in described tongue piece slip limit and tongue piece slip limit is complementary, described tongue piece active edges is adjacent two blades when top dead center, tongue piece, form a rotor cavity between the wheel body, there is annular gas tank the sub-cavity bottom of transfer corresponding part on the described acting rotor chamber sidewall, described annular gas tank communicates with acting rotor air outlet through air flue, on the described air flue air valve is arranged, described rotor cavity bottom communicates with corresponding annular gas tank on the acting rotor chamber sidewall.

3. according to the described a kind of internal combustion engine of claim 1, it is characterized in that: described acting rotor chamber is oval, blade on the non-turbine-type impeller of described acting rotor can slide in the wheel body axial notch from inside to outside, in the described blade vane hole is arranged, there is roller to follow the contact of oval acting rotor chamber inner headed face in the described blade end face groove, have with blade with wide tongue piece between adjacent two blades on the non-turbine-type impeller of described acting rotor, described tongue piece is to be in active string by concave volume and convex body to insert and constitute, on the convex body top end spring is arranged in the described concave volume, a limit of described tongue piece becomes active with a blade top margin in adjacent two blades through movable axis and connects, described tongue piece is that the blade face of its another adjacent another blade in edge of axle center slides up and down in the scope between the 0-90 degree with the movable axis, its top dead center be no more than the corresponding blade top margin that slides, the slip radian on corresponding its radian of blade face camber in described tongue piece slip limit and tongue piece slip limit is complementary, described tongue piece active edges is adjacent two blades when top dead center, tongue piece, form a rotor cavity between the wheel body, described vane hole one end communicates with the impeller cavity bottom with the axial notch bottom the other end that communicates, with corresponding part, axial notch bottom annular gas tank is arranged on the described acting rotor chamber sidewall, described annular gas tank communicates with acting rotor air outlet through air flue, on the described air flue air valve is arranged, described axial notch bottom communicates with corresponding annular gas tank on the acting rotor chamber sidewall, and described rotor cavity communicates with the axial notch bottom through vane hole.

4. according to claim 1,2,3 each described a kind of internal combustion engines, it is characterized in that: described acting rotor is two.

5. according to claim 1,2,3 each described a kind of internal combustion engines, it is characterized in that: described acting rotor is a plurality of.

6. according to claim 1,2,3 each described a kind of internal combustion engines, it is characterized in that: the described rotor of calming the anger is the two stage compressor structure that two rotors constitute.

7. according to claim 1,2,3 each described a kind of internal combustion engines, it is characterized in that: the described rotor of calming the anger is the multistage compressor structure that a plurality of rotors constitute.

8. according to claim 1,2,3 each described a kind of internal combustion engines, it is characterized in that: the hybrid multi-stage gas pressure mechanism that the rotor that the described rotor of calming the anger is various ways constitutes.

9. according to each described a kind of internal combustion engine in the claim 1,2,3, it is characterized in that: on the described rotor air outlet of calming the anger the gas storage control valve is arranged, the gas storage control valve connects with the outer caisson of body, in the puff prot of described piston center guiding piece is arranged, on the described acting rotor suction port flameholder is arranged, there is camshaft at the suction port place, on the described air outlet flue gas exhausting valve is arranged, on the axle between described acting rotor is at different levels with calm the anger rotor and do work rotor and the rotor of calming the anger planetary gear set and planetary gear set control gear are arranged.

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