CN103016205A - Flywheel engine - Google Patents
Flywheel engine Download PDFInfo
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- CN103016205A CN103016205A CN2012105262177A CN201210526217A CN103016205A CN 103016205 A CN103016205 A CN 103016205A CN 2012105262177 A CN2012105262177 A CN 2012105262177A CN 201210526217 A CN201210526217 A CN 201210526217A CN 103016205 A CN103016205 A CN 103016205A
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Abstract
The invention discloses a flywheel engine. The flywheel engine comprises a shell, a fuel supplying device, an igniting device, a starting device and a rotation stabilizing device, wherein a flywheel shaft is arranged on the shell and is connected with the starting device; at least one flywheel is arranged on the flywheel shaft; at least one combustion chamber is arranged on the flywheel and is provided with an igniter; the igniter is communicated with the igniting device through a circuit; the combustion chamber is provided with a combustion chamber air inlet and a combustion chamber air outlet; the combustion chamber air outlet is communicated with an air injecting chamber; the inner cavity of the air injecting chamber is opened and expanded towards the outer edge of the flywheel; an inclined angle is formed between the air injecting direction of the air injecting chamber and the radius of the flywheel; a pressurizing device is arranged at the place, corresponding to the combustion chamber air inlet, on the flywheel; the pressurizing device is provided with a pressurizing device air inlet; and the fuel supplying device is arranged by corresponding to the combustion chamber. The flywheel engine can output both torsion as well as push force, so that the thermal work efficiency can be greatly improved, various kinds of fuel can be used, and the flywheel engine can serve as a jet engine as well as a conventional engine, and can be widely applied to fields, such as vehicle and ship power, aviation and spaceflight power and thermal power.
Description
Technical field
The present invention relates to power equipment, engine art, specifically a kind of flywheel motor.
Background technique
Existing heat energy method for transformation, the method complex structure of conversion of heat into kinetic energy, the energy loss that medium tache causes is too many, and energy transformation ratio is too low, and device fabrication is very complicated, and equipment manufacturing cost is high, and capacity usage ratio is low.
Existing motor mainly contains internal-combustion engine and jet engine, and there are the defectives such as weight is large, rotating speed is low, energy consumption is high, discharge amount is large, noise is high, cost is high, maintenance cost is high, working life is short in internal-combustion engine; There are the defectives such as thrust is little, jet velocity is low, cost is high, energy consumption is high, harmful gas emission is large, maintenance cost is high, working life is short in jet engine.
Summary of the invention
The invention provides a kind of flywheel motor, adopt brand-new heat energy transform mode.Overcome the problems that exist with front engine, capacity usage ratio is high, and fuel combustion is abundant, and more environmental protection has improved greatly the power of motor and exported, and has greatly simplified the structure of motor.The present invention can make flywheel motor get final product outputting torsion also exportable flywheel end thrust or flywheel axial tension by adjusting jet direction.
Flywheel motor disclosed by the invention, of many uses: can be directly as motor, get final product also exportable thrust of outputting torsion, namely can be used as various conventional engines uses, also can be used as the Aeronautics and Astronautics motor and use, can be widely used in the fields such as car and boat power, thermal power generation, machinery power, aircraft, airship, rocket.
The present invention is achieved through the following technical solutions for achieving the above object:
Flywheel motor, comprise housing, fuel supplying device, ignition mechanism, starting drive and spin stabilization device, Flywheel axle on the housing, flywheel shaft connects starting drive, a flywheel is installed on the flywheel shaft at least, a firing chamber is set on the flywheel at least, set-point, firing chamber firearm, igniter is by the circuit communication ignition mechanism, air inlet of combustion chamber and air outlet, firing chamber are established in the firing chamber, the air outlet, firing chamber is communicated with nozzle chamber, nozzle chamber's inner chamber is to the expansion of flywheel outer rim direction opening, and the jet direction of nozzle chamber and flywheel radius are the angle of inclination, and the respective combustion chamber suction port arranges supercharging device on the flywheel, supercharging device arranges the supercharging device suction port, and the fuel supplying device respective combustion chamber arranges.
A plurality of blades are set in the supercharging device, blade and flywheel shaft cross section are the angle of inclination, supercharging device outer installment supercharging cover, supercharging cover inner chamber is expanded gradually to the air inlet of combustion chamber direction, the supercharging device middle part arranges the baffle cover, and baffle cover outer radial air inlet of combustion chamber direction is expanded gradually, and the expansion angle of baffle cover external diameter is greater than the expansion angle of supercharging cover inner chamber, the blade outer rim is arranged on the supercharging cover inwall, and the blade inner edge is arranged on the baffle cover outer wall.
Nozzle chamber's inner chamber cross-sectional circumference is circular, and the air outlet, firing chamber is arranged on nozzle chamber's inner chamber circumference.
The supercharging device axis central part arranges fuel and carries cavity, and fuel conveyor chamber road outlet end is communicated with the firing chamber, and fuel is carried cavity entrance point middle part that fuel is set and carried the cavity import, and the corresponding fuel of fuel supplying device is carried cavity import setting.
Housing is provided with a plurality of heat recovering devices.
The flywheel periphery arranges a plurality of firing chambers, firing chamber central axis and flywheel shaft central axis are and intersect angle, firing chamber inner chamber cross-sectional circumference is circular, air inlet of combustion chamber is located on the inner chamber circumference of firing chamber, the air outlet, firing chamber is located on the central axis of firing chamber, and air outlet, firing chamber cross sectional area is less than maximum cross section, firing chamber area.
The central axis cross section is set on the central axis in the firing chamber is circular obturator, obturator is arranged on the bottom interior wall of firing chamber.
A plurality of flywheels are installed on the flywheel shaft.
The jet direction of nozzle chamber and flywheel shaft cross section are the angle of inclination, and flywheel shaft passes supercharging device, and flywheel shaft passes the supercharging device suction port.
The jet direction of nozzle chamber and flywheel shaft cross section are the angle of inclination, flywheel shaft and supercharging device are in respectively the flywheel both sides, the flywheel shaft 5 interior fuel that arrange are carried cavity, and fuel is carried cavity axle head middle part that fuel is set and carried the cavity import, and the corresponding fuel of fuel supplying device is carried cavity import setting.
The invention has the advantages that: utilize brand-new heat energy method for transformation, take full advantage of circular movement and fluid motion, greatly simplified structure.The energy loss that its medium tache causes is few, and capacity usage ratio is high.It can use multiple gases, liquid, powdered fuel.Its thermal efficiency is high, and energy transforms more fully.This motor is the eddy current sustained combustion, sufficient combustion, and more environmental protection continues acting, has greatly improved power output, and greatly improve working life, and cost reduces greatly, can realize higher rotating speed.
This flywheel motor is by adjusting jet direction, can make flywheel motor outputting torsion or output flywheel end thrust or flywheel axial tension, can be widely used in the power equipment fields such as car, ship, Aeronautics and Astronautics, thermal power generation, can greatly reduce energy consumption, can use pluralities of fuel.Can directly use coal dust when being used for thermal power generation, can realize the dry type generating, can greatly improve generating efficiency, greatly save energy and reduce the cost, greatly reduce environmental pollution.
This flywheel motor can be used for various Aeronautics and Astronautics aircraft, and energy consumption can reduce greatly, and cost also reduces greatly, and performance is more reliable, can greatly improve flying power, greatly improves flying speed, greatly reduces the flight noise, greatly reduces equipment manufacturing cost.It can make aircraft speed improve constantly, and makes aircraft realize ultra high speed.The energy that advances the interior numerous particles of air-flow to carry can be converted into the thrust to aircraft fully, can make aircraft more energy-conservation, and it can make aircraft realize lower energy consumption.
It can be used for various car and boat power, and the jet thrust promotion car and boat that can utilize flywheel motor to produce advance or retreat, and produce brand-new jet power car and boat, can reequip existing car and boat.Can cancel the machine driven systems such as clutch, speed changer, transmission shaft, drive wheel, propeller cavitation, can bring simplify manipulative procedure, improve handling, improve car and boat speed, alleviate tire wear, reduce car body weight, reduce energy consumption, balancing vehicle antero posterior axis weight distribution, save interior space, alleviate wheel and rail wear, the plurality of advantages such as balance hull.
The present invention has the working life of cheap user cost, overlength, super wide fuel Applicable scope, super wide using scope, energy-conserving and environment-protective, lightweight, noise is low, ultralow vibrations, power is large, power range is wide, speed range is wide, moment of torsion is large, little etc. the advantage of volume, the present invention can solve Motor Vehicle substantially, aircraft noise pollutes and atmospheric pollution.
Description of drawings
Accompanying drawing 1 is agent structure schematic representation of the present invention;
Accompanying drawing 2 is that the A-A of accompanying drawing 1 is to the sectional structure schematic representation;
Accompanying drawing 3 is main TV structure schematic representation of one of embodiment of the invention;
Accompanying drawing 4 is main TV structure schematic representation of two of the embodiment of the invention;
Accompanying drawing 5 is main TV structure schematic representation of three of the embodiment of the invention;
Accompanying drawing 6 is main TV structure schematic representation of four of the embodiment of the invention;
Accompanying drawing 7 is main TV structure schematic representation of five of the embodiment of the invention;
Accompanying drawing 8 is flywheel face sectional structure schematic representation of five of the embodiment of the invention;
Accompanying drawing 9 is main TV structure schematic representation of six of the embodiment of the invention;
Accompanying drawing 10 is main TV structure schematic representation of seven of the embodiment of the invention;
Accompanying drawing 11 is main TV structure schematic representation of eight of the embodiment of the invention;
Accompanying drawing 12 is main TV structure schematic representation of nine of the embodiment of the invention;
Embodiment
Agent structure of the present invention comprises housing 1, fuel supplying device 2, ignition mechanism 3, starting drive 4 and spin stabilization device 20, Flywheel axle 5 on the housing 1, flywheel shaft 5 connects starting drive 4, a flywheel 6 is installed on the flywheel shaft 5 at least, a firing chamber 7 is set on the flywheel 6 at least, firing chamber 7 set-point firearms 8, igniter 8 is communicated with ignition mechanism 3 by circuit 9, air inlet of combustion chamber 10 and air outlet, firing chamber 11 are established in firing chamber 7, air outlet, firing chamber 11 is communicated with nozzle chamber 12, nozzle chamber's 12 inner chambers are expanded to flywheel 6 outer rim direction openings, nozzle chamber's 12 jet directions and flywheel 6 radiuses are the angle of inclination, respective combustion chamber suction port 10 arranges supercharging device 13 on the flywheel 6, and supercharging device 13 arranges supercharging device suction port 14, and fuel supplying device 2 respective combustion chamber 7 arrange.
Starting drive 4 comprises power supply, switch, circuit, starter motor, transmission device etc., when flywheel motor uses, need to start by starting drive, obtains initial rotational speed.Also can utilize starting drive to generate electricity simultaneously.
Flywheel shaft 5 connects starting drive 4.Starting drive 4 can be installed on the flywheel shaft 5, and 5 rotations of starting drive 4 flywheel driven axles are for flywheel motor provides initial speed.Starting drive 4 can pass through multiple transmission device flywheel driven axle 5 rotations such as belt, gear or coupling.
A flywheel 6 is installed on the flywheel shaft 5 at least.But simplified structure when on the flywheel shaft 5 flywheel being installed; Can better improve power when on the flywheel shaft 5 a plurality of flywheel 6 being installed, can two flywheels 6 be one group for saving the space, and two flywheels 6 can lean against together or be fabricated directly in together mutually.In order to prevent that waste gas from entering flywheel motor, can isolating plate be set at housing, isolating plate, is close to flywheel 6 and is not contacted with flywheel 6 with inner region near flywheel 6 edges.Can utilize the rotation of flywheel 6 that waste gas is thrown away, waste gas can not entered in flywheel 6 edges.Flywheel 6 can be made with multiple material, generally, can use the multiple heat-resistant, high strength materials such as multiple alloy material (tungsten-molybdenum alloy, titanium alloy, silicon alloy, zircaloy etc.), foamed material, refractory material (silicon carbide, silicon nitride, aluminium oxide etc.), can adopt the casting technique once-through, also can use the means of a powder metallurgy technique manufacturing, also can adopt Split type structure to be installed together and get final product, also can form by a firing with stupalith is disposable, can improve working life.When flywheel 6 adopts foamed materials to make, can adopt novel foam glass, foamed ceramics, foamed alloy etc., experimental results show that this material has the multiple excellent results such as high strength, high tenacity, high-temperature resistant, high heat insulation, ultra lightweighting.When flywheel 6 adopted alloy material, flywheel 6 surfaces also can arrange radiating fin and improve radiating effect, can reduce the requirement of material heatproof.Can spin stabilization device 20 be set in flywheel one side, for increasing stability, also can spin stabilization device 20 all be set in the flywheel both sides.
A firing chamber 7 is set on the flywheel 6 at least.It is circle or cirque structure that cross section can be arranged in firing chamber 7, and it is smooth and easy to be conducive to firing chamber 7 interior air motions, can make firing chamber 7 interior formation swirl combustions, can make sufficient combustion.When on the flywheel 6 firing chamber 7 being set, ring can be arranged in firing chamber 7, firing chamber 7 and flywheel 6 are located on the same spin axis, make firing chamber 7 and flywheel 6 coaxial rotatings, utilize rotation to make firing chamber 7 interior formation swirl combustions, firing chamber 7 inwalls are done to such an extent that the lines flow smoothly as far as possible, can make air motion more smooth and easy, can avoid in the firing chamber forming redundant space, tempering or cause hot plugging in the time of can avoiding lighting a fire better can easier igniting as far as possible.When on the flywheel 6 firing chamber 7 being set, also firing chamber 7 can be arranged on flywheel 6 peripheries, firing chamber 7 can be arranged to cross section is the columnar structured of circle, during flywheel motor work, flywheel shaft 5 is swung along certain limit, can be used as special-purpose applications in the occasion of some special requirements, flywheel 6 peripheries also can arrange a plurality of firing chambers 7, can realize that the flywheel axial rotary is stable.Also refractory masses can be set in the firing chamber, can improve firing chamber working life.
Igniter 8 is communicated with ignition mechanism 3 by circuit 9.One, an a plurality of or circle electrode can be installed near igniter 8 wiring terminal positions, electrode connecting circuit 9, circuit 9 is communicated with ignition mechanism 3.Make igniter 8 wiring terminals near electrode during mounting points firearm 8, reserve certain interval, high-tension electricity punctures the gap, realizes circuit 9 connections.Along with the flywheel rotation, igniter 8 moves near the electrode, and high-tension electricity punctures air and realizes that circuit 9 is communicated with, and realizes igniter 8 igniting.Also can brush be set at flywheel shaft, at flywheel electric wire be set, realize that by brush circuit 9 is communicated with.
Air inlet of combustion chamber 10 and air outlet, firing chamber 11 are established in firing chamber 7.When on the flywheel 6 firing chamber 7 being set, air inlet of combustion chamber 10 can be opened in firing chamber 7 one ends, and fuel mixture is directly entered in the firing chamber 7, and air outlet, firing chamber 11 can be located on 7 peripheries of firing chamber, and air outlet, a plurality of firing chamber 11 can be set; When on the flywheel 6 a plurality of firing chamber 7 being set, air inlet of combustion chamber 10 can be opened on the circular side wall of firing chamber 7, can make better firing chamber 7 interior formation eddy current, eddy current can improve the holdup time of air-flow in firing chamber 7, can better keep burning, air outlet, firing chamber 11 can be located on 7 medial axis, firing chamber, and each firing chamber 7 can arrange air outlet, a firing chamber 11.Air inlet of combustion chamber 10 areas are during greater than air outlet, firing chamber 11 area, throw away from air outlet, firing chamber 11 after can making air-flow in firing chamber 7, be pressurized better the formation pressurized gas, after in a single day fuel mixture is lighted, 11 ejections form jet thrust from the air outlet, firing chamber can to form high temperature and high pressure gas, promote the flywheel rotation.The ratio of air inlet of combustion chamber 10 areas and air outlet, firing chamber 11 areas can be debugged with reference to the ratio of existing air breathing engine air inlet of combustion chamber area and air outlet, firing chamber area and be got final product.
Air outlet, firing chamber 11 is communicated with nozzle chamber 12, and nozzle chamber's 12 inner chambers are expanded to flywheel 6 outer rim direction openings.Air outlet, firing chamber 11 is communicated with nozzle chamber 12, make the high temperature and high pressure gas of air outlet, firing chamber 11 ejections enter nozzle chamber 12, nozzle chamber's 12 inner chambers can better improve jet velocity to the expansion of flywheel 6 outer rim direction openings, better utilize energy, can improve flywheel motor efficient.Air outlet, firing chamber 11 place nozzle chamber inwalls will make that the lines flow smoothly, form the streamline shape, make air motion smooth and easy, alleviate wearing and tearing.Nozzle chamber's 12 lumen centers axis can be done and be in line, and also can make camber line or curve, and nozzle chamber's 12 lumen centers axis are made curve can better comply with jet moving direction, can raise the efficiency.
Nozzle chamber's 12 jet directions and flywheel 6 radiuses are the angle of inclination.Nozzle chamber's 12 jet directions and flywheel 6 radiuses can be with reference to the angles of inclination between centrifugal impellers blades and the radius, theoretical calculating: during 30 ° of left and right sides, angle of inclination, can utilize jet thrust to help flywheel to offset a part of centrifugal force, more High Rotation Speed of flywheel can be realized, the requirement to the flywheel material can be reduced.Adjust the angle of inclination of nozzle chamber's 12 jet directions and flywheel radius, can change flywheel motor to the adaptive capacity of rotating speed.Nozzle chamber's 12 jet directions and flywheel shaft cross section angle are 0 when spending, flywheel motor can only outputting torsion, when nozzle chamber's 12 jet directions and flywheel shaft cross section were the angle of inclination, flywheel motor got final product outputting torsion also exportable flywheel end thrust or flywheel axial tension.
Respective combustion chamber suction port 10 arranges supercharging device 13 on the flywheel 6.Supercharging device 13 can adopt multiple supercharging device, mixed flow centrifugal impeller or the centrifugal impeller of available various structures, available existing multiple mixed flow centrifugal impeller, impeller outlet is towards axial rotary, and impeller outlet is communicated with air inlet of combustion chamber 10, impeller and flywheel 7 synchronous rotaries, air-flow is pressurizeed, can improve suction pressure, can lengthen the impeller axial length, blade-shaped curl on the impeller is distributed, multiple layers of vanes also can axially be set form the multi-stage impeller structure.Supercharging device 13 is available existing multiple centrifugal impeller also, and advantage is: can reduce the impeller axial length, shortcoming is: need higher rotating speed just can reach the supercharging requirement.Centrifugal impeller inner chamber axial height can be dwindled from the center to the periphery gradually, increase blade, the blade number can be increased from the center to the periphery gradually, can improve pressure.Supercharging device 13 also can adopt on-bladed taper supercharging core structure, the taper core structure can be made in supercharging device 13 outsides, cone structure is made in supercharging device 13 inside, externally the conically shaped cone tip part arranges suction port, the conically shaped bottom is communicated with air inlet of combustion chamber 10 and gets final product, drive supercharging device 13 synchronous rotaries after flywheel 6 rotations, after the outside conically shaped inwall rotation, air-flow is thrown away to air inlet of combustion chamber 10 directions along outside conically shaped inwall, shortcoming is: when needing flywheel 6 rotating speeds to reach very high, just can reach the supercharging requirement, generally not adopt.Supercharging device 13 inner chamber maximum radius less than air outlet, firing chamber 11 to flywheel 6 axle center apart from the time, can utilize better centrifugal force to avoid tempering, can utilize centrifugal force to realize the supercharging working effect of pressed engine.Supercharging device 13 can be made one with flywheel 6, also can make Split type structure with flywheel 6 and be installed together and get final product.
The motor that the flywheel motor of this agent structure can be used as torsion output uses, the motor that also can be used as thrust output uses, the flywheel rotation sucks in the supercharging device suction port 14 fuel and air automatically, mix after in supercharging device 13, finishing supercharging, fuel mixture is pressed into firing chamber 7, throw away from air outlet, firing chamber 11,7 form the fuel under high pressure mixed gas in the firing chamber, igniter 8 igniting make the fuel under high pressure mixture combustion form high temperature and high pressure gas, and 11 ejections enter nozzle chamber 12 from the air outlet, firing chamber, at nozzle chamber's 12 interior jet-stream winds with certain jet direction that high-pressure injection gas is integrated into, form jet thrust, promote the flywheel rotation.Nozzle chamber's 12 jet directions and flywheel shaft cross section angle are 0 when spending, flywheel motor can only outputting torsion, when nozzle chamber's 12 jet directions and flywheel shaft cross section were the angle of inclination, flywheel motor got final product outputting torsion also exportable flywheel end thrust or flywheel axial tension.Flywheel motor can be used as equipment powered by conventional energy and uses, and can be widely used in the fields such as car, ship, aircraft, machinery power, thermal power generation, heat supply.The heat-conducting mediums such as exhaust-gas heated water that can utilize flywheel motor to discharge during heat supply can take full advantage of waste heat.
The structure of one of embodiment of the invention: on the agent structure basis, supercharging device 13 is interior to arrange a plurality of blades 16, blade 16 is the angle of inclination with flywheel shaft 5 cross sections, supercharging device 13 outer installment supercharging covers 17, supercharging cover 17 inner chambers are expanded gradually to air inlet of combustion chamber 10 directions, supercharging device 13 middle parts arrange baffle cover 18, baffle cover 18 outer radial air inlet of combustion chamber 10 directions are expanded gradually, the expansion angle of baffle cover 18 external diameters is greater than the expansion angle of supercharging cover 17 inner chambers, blade 16 outer rims are arranged on supercharging cover 17 inwalls, and blade 16 inner edges are arranged on baffle cover 18 outer walls.A plurality of blades 16 are arranged on the supercharging device 13, blade 16 and flywheel shaft 5 cross sections are certain angle of inclination, the angle of inclination can be selected to get final product about 30 degree generally speaking, can improve the axial motion speed of fluid, the axial acting ability of blade 16 convection cells be can improve, the better supercharging of blade convection cell and axially speed-raising made.Supercharging cover 17 is enclosed within baffle cover 18 outsides, blade 16 is arranged between the supercharging cover 17 baffle covers 18 gets final product, blade 16 and supercharging cover 17, baffle cover 18 can be made one.Also flywheel 6 and blade 16, supercharging cover 17, baffle cover 18 can be made one.Also can thicken impeller, make the blade 16 on the impeller form spiral distribution, multiple layers of vanes 16 also can axially be set form the multi-stage impeller structure.Blade 16 forms runner each other, supercharging device 13 is interior can be increased gradually to air inlet of combustion chamber 10 direction blades 16 quantity, and runner is shunk gradually to the outlet side, can further improve hydrodynamic pressure, can better avoid high-pressure liquid to reflux, capable of reducing energy consumption.Although runner shrinks gradually to the outlet side, Flow area dwindles gradually, and fluid motion speed improves gradually to the outlet side, under the same Flow area, fluid motion speed is higher, and flow is larger, does not affect fluid flow so runner shrinks gradually to the outlet side.The degree that runner shrinks gradually to the outlet side is larger, more can realize higher pressure, more can improve fluid and runner friction.Under suitable shrinkage degree, the relation between tunable friction energy loss and pressure improve.
Present embodiment has all functions of agent structure, can better improve suction pressure, raises the efficiency.
Two structure of the embodiment of the invention is: on above embodiment's architecture basics, nozzle chamber's 12 inner chamber cross-sectional circumference are circular, and air outlet, firing chamber 11 is arranged on nozzle chamber's 12 inner chamber circumference.Nozzle chamber's 12 inner chambers can be made cross-sectional circumference and be circular cylindrical shape, tubaeform, taper shape or ring etc. are multiple, air outlet, firing chamber 11 is arranged on nozzle chamber's 12 inner chamber circumference, the jet rotation under the effect of inertia that rotatablely moves that produces at flywheel that the firing chamber is produced rushed in the nozzle chamber 12 along nozzle chamber's 12 inner chamber cross section tangent directions, at screw propulsion eddy flow that increases progressively to the center rotating speed from the periphery of nozzle chamber's 12 interior formation, form the screw propulsion jet-stream wind from nozzle chamber's 12 interior ejections, the screw propulsion jet-stream wind can have special propelling effect, the interior numerous particles of screw propulsion air-flow each other movement velocity there are differences, the fltting speed of zones of different particle there are differences in the screw propulsion air-flow cross section, the slow particle of movement velocity is slower away from the speed of nozzle chamber, the fast particle of movement velocity is faster away from the speed of nozzle chamber, the fast particle of movement velocity can run into the slow particle of movement velocity, cause numerous particles to form each other the chain type transmission, they are higher to the transmission capacity of jet reaction.The screw propulsion air-flow provides the particle basically identical with flywheel sense of rotation and speed continuously, and these particles have better transmitted reaction force, and they are irrelevant to transmission capacity and the Speed of Reaction Wheels of reaction force.These particles finally have been delivered to screw propulsion air-flow center with reaction force, make screw propulsion air-flow center produce all the time the propelling force that a speed and screw propulsion air-flow center fltting speed equate substantially, all the time greater than flywheel edge rotation forward velocity, it can make flywheel produce higher rotating speed to this propelling force speed.Numerous Particles Movings are orderly in the screw propulsion air-flow that increases progressively from the periphery to the center rotating speed, make the reaction force transmission orderly, reaction force is collided mutually cause energy loss, the energy that numerous particles carry in the screw propulsion air-flow can be converted into the thrust to flywheel more fully, can be more energy-conservation.
Present embodiment has all functions of agent structure, can better improve Speed of Reaction Wheels, can greatly raise the efficiency.
Three structure of the embodiment of the invention is: on above embodiment's architecture basics, supercharging device 13 axis central parts arrange fuel and carry cavity 15, fuel carries cavity 15 outlet end to be communicated with firing chamber 7, fuel is carried cavity entrance point middle part that fuel is set and is carried cavity import 19, and fuel supplying device 2 corresponding fuel carry cavity import 19 to arrange.Can fuel be set at supercharging device 13 axis central parts and carry cavity 15, carry cavity entrance point middle part that fuel is set at the fuel of supercharging device suction port 14 ends and carry cavity import 19, the outlet of the fuel pipe of fuel supplying device 2 is located at fuel carries near the cavity import 19 or probe into fuel and carry cavity import 19 get final product, the centrifugal force that can utilize the flywheel rotation to produce axially directly is delivered into fuel in the firing chamber 7 along fuel conveying cavity 15.Fuel directly is delivered into when firing chamber 7 is interior can avoid fuel conveyor chamber channel temp too high and causes fuel to carry the cavity internal combustion at fuel.
Present embodiment has all functions of agent structure, causes fuel to carry the cavity internal combustion at fuel in the time of can avoiding fuel conveyor chamber channel temp too high, and shortcoming is: fuel lacks mixing, causes easily burning insufficient, does not generally adopt.
Four structure of the embodiment of the invention is: on above embodiment's architecture basics, housing 1 is provided with a plurality of heat recovering devices 21.A plurality of heat recovering devices 21 can adopt hot channel, heat supply sheet etc., can can be arranged on a plurality of heat recovering devices 21 on the housing, can be when cast housing direct casting, can make on the housing and to form many and adopt hot channel, adopting the hot channel inlet end gets final product as shell air inlet, also can adopt the hot channel inlet end with many and be communicated as one, unification is offered a suction port as shell air inlet, can more convenient installation air inlet supplementary equipment.A plurality of heat recovering devices 21 are also available adopts the heat pipe manufacturing, can adopt heat pipe with many and be installed on the housing or on the inner walls and get final product, and can improve and adopt hot side, improves and adopts thermal effect.A plurality of heat recovering device 21 imports also can connect the air-flow conveying equipment, utilize the air-flow conveying equipment that air-flow is flowed to flywheel motor by a plurality of heat recovering devices 21 and get final product.Large-scale flywheel motor can be with hydromining warm, utilize a plurality of heat recovering devices 21 as heat supply source to extraneous heat supply.Mini flywheel motor available air is adopted heat, improves the flywheel motor intake temperature.
Present embodiment has all functions of agent structure, can gather waste heat, reduces case temperature, simplifies engine structure, improves intake temperature, improves engine efficiency.
Five structure of the embodiment of the invention is: on above embodiment's architecture basics, flywheel 6 peripheries arrange a plurality of firing chambers 7, firing chamber 7 central axis and flywheel shaft 5 central axis are and intersect angle, firing chamber 7 inner chamber cross sections are circular, air inlet of combustion chamber 10 is located on the 7 inner chamber circumference of firing chamber, air outlet, firing chamber 11 is located on 7 central axis of firing chamber, and air outlet, firing chamber 11 cross sectional areas are less than firing chamber 7 maximum cross section areas.In order to improve space availability ratio, improve power, improve firing effect, the flywheel periphery can arrange a plurality of firing chambers 7.A plurality of firing chambers 7 and flywheel 6 can be made one, also a plurality of firing chambers 7 and flywheel 6 can be made Split type structure and be installed together and get final product.Firing chamber 7 central axis and flywheel shaft 5 central axis are and intersect angle, firing chamber 7 inner chamber cross sections are circular, air inlet of combustion chamber 10 is located on the 7 inner chamber circumference of firing chamber, air outlet, firing chamber 11 is located on 7 central axis of firing chamber, can utilize fluid motion inertia, fuel mixture after tangentially pouring eddy current that increases progressively from the periphery to the center rotating speed of firing chamber 7 interior formation, is gone out from air outlet, firing chamber 11 firing chamber 7 cross sections, can make fuel mixture under effect of inertia, be cut in the firing chamber 7 more swimmingly eddy current that increases progressively to the center rotating speed from the periphery of 7 interior formation in the firing chamber.The more high firing chamber 7 interior formation eddy current that more are conducive to of Speed of Reaction Wheels more can improve the rotational speed of firing chamber 7 interior eddy current.The low structure of the high side of a side also can be arranged in air inlet of combustion chamber 10 outers, and the lower structure of a side towards flywheel 6 sense of rotation the place aheads can further improve firing chamber 7 interior rotational speed of eddy current.Air outlet, firing chamber 11 is located on the 7 lumen centers axis of firing chamber, can better form from the periphery the jet of screw propulsion that the center rotating speed increases progressively.The line of firing chamber 7 lumen centers axis and nozzle chamber's 12 lumen centers axis is arranged to circular arc line, and the radian of circular arc line can equate with the radian at flywheel edge, can make firing chamber 7 and nozzle chamber's 12 fluid movement more smooth and easy.Air outlet, firing chamber 11 cross sectional areas are conducive to improve firing chamber 7 internal pressures less than firing chamber 7 maximum cross section areas, improve firing chamber 7 heat storage capacities, can make better firing chamber 7 keep burning.Firing chamber 7 also can arrange communicating passage each other, can be in the firing chamber middle and lower part of 7 lumen centers axis offer communicating passage, communicating passage can be arranged to pipe-like, communicating passage can make each firing chamber 7 be interconnected, ignition difficulties or the dead fiery phenomenon that can avoid better indivedual firing chambers to cause because of igniter failure.Communicating passage can better make the firing chamber keep burning, can play the effect that keeps in a fire, and causes flame-outly in the time of can avoiding motor significantly to reduce throttle, and flywheel motor is worked more normally.Communicating passage can be regarded the part of firing chamber as, and big-block engine also can be arranged on the ignition mechanisms such as spark plug, igniter in the communicating passage.Also the multiple tracks air-flow path can be set in the flywheel 6.The air-flow path inlet end is opened in the central region on flywheel 6 planes, to flywheel 6 outer rims expansion opening, can make flywheel 6 as draught fan impeller, make cooled gas interior to the motion of flywheel 6 outer rims from flywheel 6, air-flow path can play the effect of cooling combustion locular wall, jet locular wall, flywheel.Air-flow path also can be complied with flywheel 6 sense of rotation and tilt to pass the flywheel face, can play the effect of delivery air, air-flow can be transported to flywheel 6 another sides, and specific use can be arranged, and can be used on the aircraft, can guarantee that flywheel motor obtains live gas.Also can block body be set firing chamber 7 inwalls around igniter 8, utilize block body that igniter 8 is blocked, block body is reserved certain interval, makes the mixed gas can inlet point firearm 8 zones.Also can around existing spark plug, a cylinder be set as block body, spark plug is installed in the cylinder, bottom of cylinder arranges an intake grill, and intake grill is met to air-flow, makes air-flow constantly enter in the cylinder, behind the plug ignition, in cylinder, form a fireball, make cylinder form a small furnace, can play the kindling material effect, can be conducive to form sustained combustion in the firing chamber, make the firing chamber be not easy to stop working.Also above-mentioned cylinder and existing spark plug can be made one, make a kind of spark plug, can more conveniently use.Block body can make near the air-flow reduction of speed the igniter 8, avoids high velocity air that kindling material is taken away fast, can realize better igniting.Flame has diffusion velocity, and when airspeed was too fast, flame had little time diffusion, is namely taken out of firing chamber 7, causes ignition difficulties, and block body can address this problem well.
Present embodiment has all functions of agent structure, and efficient is higher, and is more energy-conservation, can reduce the Inner Wall of Combustion Chamber temperature, can make the higher temperature of formation in the firing chamber, can further improve flywheel motor efficient, and it is more obvious to be applied on the big-block engine effect.Rotating speed and flywheel 6 synchronization of the eddy current that increases progressively from the periphery to the center rotating speed in the firing chamber 7 improve, eddy current prolonged fuel in the firing chamber holdup time of 7, better guaranteed the abundant burning of fuel.The material that enters firing chamber 7 is involved in the eddy current center automatically, and the fuel combustion reaction occurs in the eddy current centre area, and the eddy-current screen energy has reduced direct the contacting of thermal response with firing chamber 7 inwalls, has reduced the temperatures involved of firing chamber 7 inwalls.Eddy current greatly prolonged fuel in the firing chamber 7 move distance and residence time, all there is relative movement each other in particle in the eddy current, fuel particle and oxygen particle are better reacted, in the eddy current center region, the speed of related movement that particle exists each other is faster, and friction pressure each other is larger, can make faster, the more fully reaction of fuel, make fast fully burning of fuel, can realize the fuel lean combustion, can better keep burning.Exergonic speed and what movement velocity and move distance have determined, jet screw propulsion has improved jet move distance and jet velocity greatly, make jetly better to release energy, and delivery temperature is reduced greatly.The High Temperature High Pressure that the eddy current centre area produces has improved the temperature difference with the external world greatly, can greatly improve thermal technology's transformation efficiency of flywheel motor, makes the flywheel motor thermal efficiency very high, makes flywheel motor very energy-conservation.Swirl combustion is burnt fuel more fully, makes very environmental protection of flywheel motor.
Six structure of the embodiment of the invention is: on embodiment's five architecture basics, the central axis cross section is set on the 7 interior central axis of firing chamber is circular obturator 22, obturator 22 is arranged on 7 bottom interior wall of firing chamber.Can be in the firing chamber 7 interior central axis the central axis cross section is set be circular obturator 22, the various shape such as obturator 22 can do coning, tubaeform, obturator 22 is arranged on 7 bottom interior wall of firing chamber and gets final product.Obturator 22 can be with firing chamber 7 bottom interior wall area fillings, can avoid this zone to produce causes fuel mixture too much to accumulate in the firing chamber more than the space, fuel mixture too much when causing igniting participates in instantaneous burst, cause the firing chamber to cause hot plugging or tempering, cause ignition difficulties or igniting idling too high.
Present embodiment has all functions of agent structure, can more convenient realization igniting.
Seven structure of the embodiment of the invention is: on above embodiment's architecture basics, a plurality of flywheels 6 are installed on the flywheel shaft 5.A plurality of flywheels 6 being installed on the flywheel shaft 5 can better being improved power, can two flywheels 6 be one group, and two flywheels 6 can lean against together or be fabricated directly in together mutually.
Present embodiment can improve the power of flywheel motor greatly, greatly improves power, can be used as large-sized power plant and uses.Can extensively be used in steamer, train, racing car, thermal power generation etc. needs on the powerful equipment, and its power can substantially exceed existing any superpower motors such as gas turbine.
Eight structure of the embodiment of the invention is: on above embodiment's architecture basics, nozzle chamber's 12 jet directions and flywheel shaft 5 cross sections are the angle of inclination, and flywheel shaft 5 passes supercharging device 13, and flywheel shaft 5 passes supercharging device suction port 14.Nozzle chamber's 12 jet directions and flywheel shaft 5 cross sections are the angle of inclination, can make flywheel motor get final product also exportable flywheel end thrust of outputting torsion, nozzle chamber's 12 jet directions and flywheel shaft 5 cross sections can be with reference to the angles of inclination of axial flow impeller blade and flywheel shaft cross section, the angle of inclination should not be too large, too conference hinders the rotating speed of flywheel motor, the angle of inclination also should not be too little, and the higher Speed of Reaction Wheels of too little requirement just can be exported larger thrust.The angle of inclination is less to make the easier raising of flywheel motor rotating speed, and the screw propulsion of formation jet has higher rotating speed, can make its thrust acceleration larger.Theoretical calculating: when 30 ° of left and right sides were selected at the angle of inclination, effect was better.For making the better bearing axial pushing force of flywheel, improving Speed of Reaction Wheels, can thicken flywheel.Flywheel shaft 5 passes supercharging device 13, and flywheel shaft 5 passes supercharging device suction port 14, and flywheel shaft 5 is passed supercharging device 13, passes supercharging device suction port 14 and get final product.During use, flywheel shaft is installed on cabin body or the car and boat body, nozzle chamber's 12 jet directions to the face tilt of flywheel shaft 5 cross sections away from flywheel shaft, can be produced the thrust to cabin body or car and boat body; Nozzle chamber's 12 jet directions to the face tilt of flywheel shaft 5 cross sections near flywheel shaft, can be produced the pulling force to cabin body or car and boat body.Can outputting torsion also the flywheel motor of exportable thrust can be used for various cars, ship, space flight, aviation aircraft, can utilize thrust to promote the traffic tool and advance, utilize the torsion generating supply traffic tool.The vortex air-flow that the peripheral rotating speed of individual therefrom mind-set of its ejection successively decreases, the eddy airstream sharp side forms a taper, and the cone tip part High Rotation Speed makes energy more concentrate on the center region, sharp side of eddy airstream, has greatly improved jet thrust and jet velocity.Therefrom the vortex air-flow that successively decreases of the peripheral rotating speed of mind-set greatly reduces the friction with surrounding atmosphere, greatly reduces jet noise.Can be at flywheel outer installment protective housing for increasing Security, protective housing outlet end edge and flywheel planar registration or just over the flywheel plane can not affect the jet-stream wind propelling, and protective housing can be avoided causing fragment to fly out and hurting sb.'s feelings because accident causes Flywheel Disintegration.Protective housing can arrange a plurality of heat recovering devices 21 and gather waste heat as the part of housing 1 in protective housing, can improve the thermal efficiency.Heat recovering device 21 imports also can connect the air-flow conveying equipment, utilize the air-flow conveying equipment that air-flow is flowed to flywheel motor by heat recovering device 21 and get final product.
Present embodiment is used for various space flight, aviation aircraft, comprise rocket, aircraft, airship, can replace various Aeronautics and Astronautics air breathing engines, its safer, more energy-conservation, cheap, longer service life, can greatly improve the aircraft flying power, reduce the flight noise, improve flying speed, improve thrust weight ratio.
Present embodiment is used for various car and boat power, and the thrust promotion car and boat that can utilize flywheel motor to produce advance or retreat, and produce brand-new jet power car and boat, can reequip existing car and boat.Can cancel the machine driven systems such as clutch, speed changer, transmission shaft, drive wheel, propeller cavitation, can bring simplify the chassis facility, simplify manipulative procedure, improve handling, improve accelerating ability, improve car and boat speed, alleviate tire wear, reduce car body weight, reduce energy consumption, balancing vehicle antero posterior axis weight distribution, save interior space, can cancel electric railway, alleviate wheel and rail wear, the plurality of advantages such as balance hull.One or more flywheel motor can be installed, can realize by the jet direction of rotary flyweights motor the car and boat tune, also can utilize the flywheel motor jet power to help vehicle descending, braking.The jet direction of flywheel motor is parallel with horizontal plane jet, can utilize more fully jet power, avoids energy loss.When the present embodiment flywheel motor is used on the motorcycle, directly flywheel motor is contained in the motorcycle rear portion and gets final product.
When the present embodiment flywheel motor is used on the car, flywheel motor can be contained in automobile rear, can vacate original engine compartment as trunk and energy-absorbing district, can make more coordinated balance of vehicle antero posterior axis center of gravity, more be conducive to vehicle performance.The controlled horizontal rotation apparatus of Flywheel motor can be set on automobile rear roof, trunk lid or chassis, realize the jet direction tune of flywheel motor with the rotation of Electric Machine Control horizontal rotation apparatus.Make flywheel motor jet obliquely upward, can utilize the adhesion between jet power raising wheel and the ground, make automobile safer, can make automobile realize higher speed.The controlled horizontal rotation apparatus turn inside diameter followup system of Flywheel motor is set, can utilizes jet power to assist vehicle to keep balance, alleviate vehicle roll, sideslip, whipping, greatly improve vehicle and cross curved ability.Horizontal rotation apparatus vehicle heavy braking 180 degree rotary systems are set, can utilize the flywheel motor jet power to help vehicle better to realize emergency braking, long distance braking, shorten stopping distance.When flywheel motor is installed on the automobile chassis, can make the controlled horizontal rotation apparatus running shaft of Flywheel motor become certain angle of inclination with gravity vertical, flywheel motor is jet to oblique below when making rolling-back of car, and bottom of car is affected by high-temperature gas when alleviating reversing.The present embodiment flywheel motor is used for racing car will create limit high speed on the motor racing history.
When the present embodiment flywheel motor is used aboard, the controlled horizontal rotation apparatus of a plurality of Flywheel motors can be set in the inner both sides of locomotive engine, make the jet position of flywheel motor not exceed the train both sides, make the jet direction of flywheel motor and train direction of advance be certain angle of inclination, it is jet to tilt to the train both sides, can realize locomotive propelling and retreat; When the present embodiment flywheel motor is used on the rail motor set, the controlled horizontal rotation apparatus of a plurality of Flywheel motors can all be set in every joint carriage chassis both sides, many flywheel motors are installed, make the jet direction of flywheel motor and train direction of advance be certain angle of inclination, it is jet to tilt to the train both sides, can realize advancing and retreating of rail motor set, make flywheel motor jet obliquely upward, can utilize the adhesion between jet power raising wheel and the rail, can avoid that the train was derailed, overturn, can make train safer, can make rail motor set can realize the limit high speed of ground motion.
When the present embodiment flywheel motor is used on speedboat, warship, the steamer etc., can cancel propeller cavitation, can be more energy-conservation, improve the speed of a ship or plane, can be more than the waterline of hull both sides or the deck controllable rotating device of a plurality of Flywheel motors is set, many flywheel motors are installed, when flywheel motor is installed in the hull both sides, can pass through the size and Orientation of the flywheel motor outputting power of change hull both sides, directly utilize jet power to realize that hull is turned, tune.The jet direction of flywheel motor is horizontal by the angle of inclination, and is jet to oblique below, can utilize the better balance hull of jet power, alleviates hull and jolted by Lidar Equation to rock, and makes the ship operation safer.Can reduce the hull draft, reduce the surface friction drag between hull and the current, improve the hull motion speed, even ship is close to fly away from the water surface, ship is close to flies up, form the water surface flying ship, can greatly improve ship's speed.Can utilize computer technology, the automatic rotation controlling device is set, automatically regulate the angle of inclination of jet direction and horizontal plane according to ship's speed, can utilize more fully jet energy.Controllable rotating device running shaft is parallel with horizontal plane, can make the controllable rotating device do the facade rotation, and when making flywheel motor be installed in the hull both sides, flywheel motor does not take up room too much to the hull both sides during rotation of controllable rotating device;
When the present embodiment flywheel motor is used on the submersible, propeller cavitation can be cancelled, the noise that advances can be reduced, can be more energy-conservation, improve the speed of a ship or plane, improve flying power.The controlled facade whirligig of the jet cylinder of a plurality of installations can be set in the submersible both sides, and controlled facade whirligig running shaft is parallel with horizontal plane, can make controlled facade whirligig do the facade rotation.Flywheel motor is installed in the jet cylinder, and jet cylinder inlet end arranges suction tude, during engine misses,, injects pressurized gas with jet jet direction down in jet cylinder, can utilize the interior gas of jet cylinder all the time water to be arranged, and can avoid water inlet in the motor.Motor is water inlet in a single day, and with the jet direction of jet cylinder down, opening high pressure gas utilizes pressurized gas that water inlet in the motor is discharged and gets final product.
Present embodiment is used for helicopter, can replace propeller cavitation, can be used for multiple vertically taking off and landing flyer, flying saucer etc.Can many playscripts with stage directions embodiment flywheel motor be installed as large-scale means of transportation at helicopter, vertically taking off and landing flyer, flying saucer etc., can deliver or lift by crane large cargo.The present embodiment flywheel motor can be used for specific use more; can realize easily vertical takeoff and landing of aircraft; vortex air-flow protection cabin body, the friction of dissolving cabin body and air that the peripheral rotating speed of the therefrom mind-set that can utilize flywheel motor to spray successively decreases, the moving direction that changes the cabin body, shielding gravity field etc. can be developed more course of new aircraft.The vortex air-flow that the peripheral rotating speed of the therefrom mind-set of flywheel motor ejection successively decreases can bring beyond thought flight effect.During use, flywheel motor can be arranged on body top, cabin, nozzle chamber's 12 jet directions are tilted to flywheel shaft 5 cross sections below, supercharging device suction port 14 is arranged on below, flywheel plane, at the flywheel 6 interior multiple tracks air-flow paths that arrange, utilize air-flow path that fresh air is inputted below, flywheel plane, can constantly supply with supercharging device suction port 14 fresh airs.Also can a plurality of heat recovering devices 21 be set in the cabin external body and gather waste heat, can improve the thermal efficiency.Heat recovering device 21 imports also can connect the air-flow conveying equipment, utilize the air-flow conveying equipment that air-flow is flowed to flywheel motor by a plurality of heat recovering devices 21 and get final product.
Eight structure of the embodiment of the invention is: on above embodiment's architecture basics, nozzle chamber's 12 jet directions and flywheel shaft 5 cross sections are the angle of inclination, flywheel shaft 5 is in respectively flywheel 6 both sides with supercharging device 13, the flywheel shaft 5 interior fuel that arrange are carried cavity 15, fuel is carried cavity 15 axle heads middle part that fuel is set and is carried cavity import 19, and fuel supplying device 2 corresponding fuel carry cavity import 19 to arrange.During use, flywheel motor can be arranged on body top, cabin, nozzle chamber's 12 jet directions are tilted to flywheel shaft 5 cross sections below, supercharging device suction port 14 is arranged on top, flywheel plane, carry cavity 15 at the flywheel shaft 5 interior fuel that arrange, carry cavity 15 axle heads middle part that fuel is set at fuel and carry cavity import 19, the fuel pipe of fuel supplying device 2 exports corresponding fuel and carries cavity import 19 settings to get final product, flywheel shaft 5 can adopt hollow shaft, carry cavity 15 1 ends to be arranged on the flywheel axle head fuel, fuel is carried cavity 15 axle heads middle part that fuel is set and is carried cavity import 19, fuel pipe outlet is located at fuel carries near the cavity import 19 or probe into fuel and carry cavity import 19 get final product, it is neighbouring or directly be delivered in the firing chamber 7 to utilize centrifugal force that the flywheel shaft rotation produces that fuel axially is transported to supercharging device suction port 14 along flywheel shaft 5.Also the multiple tracks air-flow path can be set in the flywheel 6, air-flow path can be complied with flywheel 6 sense of rotation and tilt to pass the flywheel face, can play the effect of delivery air, air-flow can be transported to the flywheel face at body place, cabin from the flywheel face at supercharging device 13 places, can reduce better the gas flow temperature of cabin external body, can make the gas of cabin external body keep fresh.
Present embodiment is used for helicopter, can replace propeller cavitation, can be used for multiple vertically taking off and landing flyer, flying saucer etc.Can many playscripts with stage directions embodiment flywheel motor be installed as large-scale means of transportation at helicopter, vertically taking off and landing flyer, flying saucer etc., can deliver or lift by crane large cargo.The present embodiment flywheel motor can be used for specific use more; can realize easily vertical takeoff and landing of aircraft; vortex air-flow protection cabin body, the friction of dissolving cabin body and air that the peripheral rotating speed of the therefrom mind-set that can utilize flywheel motor to spray successively decreases, the moving direction that changes the cabin body, shielding gravity field etc. can be developed more course of new aircraft.The vortex air-flow that the peripheral rotating speed of the therefrom mind-set of flywheel motor ejection successively decreases can bring beyond thought flight effect.
Working principle: flywheel motor of the present invention has an idling speed, during use, at first utilize starting drive to make the flywheel motor rotation, along with the flywheel rotation, in the air intake supercharging device suction port 14, after flywheel reaches idling speed, fuel supplying device begins transfer the fuel, fuel and combustion-supporting gas or air are sucked in the supercharging device 13 automatically, gas is even with fuel mix in supercharging device 13, realize supercharging, under pressure, fuel mixture enters the firing chamber, ignition device takes fire the fuel under high pressure mixed gas, make and produce high temperature and high pressure gas in the firing chamber, high temperature and high pressure gas is under the effect of the pressure of flywheel rotary centrifugal force and supercharging device 13 generations, can't be from air inlet of combustion chamber 10 ejections, can only be from the air outlet, firing chamber 11 ejections, pressurized gas are converted into the jet-stream wind that jet direction and flywheel 6 radiuses are the angle of inclination by nozzle chamber 12, the reaction force of jet thrust promotes the flywheel rotation, makes flywheel keep rotation, and gas is constantly sucked from supercharging device suction port 14,11 ejections form continual air-flow path from the air outlet, firing chamber.The prerequisite of flywheel motor maintenance work is to have a flywheel rotation idling, and the flywheel rotation is lower than idling, and flywheel motor can not maintenance work.Theoretical calculating: flywheel rotation idling generally turns 2000/gets final product more than the min.Pressurized gas are discharged from nozzle chamber, form thrust, promote the flywheel rotation, and the flywheel outer rim forms the from the center to the periphery eddy current that successively decreases of rotating speed, and this can reduce the noise of flywheel motor greatly.Whole flywheel motor works together does not have boom, spin stabilization as gyro, almost not vibration, shake etc.Flywheel motor is in case igniting can be closed ignition mechanism and starting drive, and cancellation external force boosting realizes self-High Rotation Speed, outputting power.
During flywheel motor outputting torsion pattern, utilize the flywheel rotation directly thrust to be converted into torsion, the energy loss of having avoided medium tache to cause improves mechanical efficiency greatly, and the capacity usage ratio of whole flywheel motor is improved greatly.
Flywheel motor is that outputting torsion is when also exporting flywheel end thrust or flywheel axial tension pattern, the screw propulsion frontal upcurrent that the from the center to the periphery rotating speed of a flywheel axial motion of generation successively decreases, reduced the friction of air-flow edge and outside air, greatly improve movement velocity and the thrust of central gas stream, greatly improved fltting speed.Jet screw propulsion has improved the move distance of particle in the air-flow, has improved energy release rate and the energy releasing amount of whole air-flow, has reduced the temperature of jet end, has improved capacity usage ratio.
Object is from static to high-speed motion, and speed all promotes gradually, and the reaction force acts of the jet power of air breathing engine makes aircraft obtain thrust in aircraft.Thrust from numerous particles in the jet-stream wind each other to the transmission of reaction force and the frictional force of jet-stream wind and ambient air.Aircraft movements speed is during near jet velocity, take aircraft as reference system: the air in the aircraft external world advances with aircraft movements speed to the opposite direction of aircraft direction of advance, cause the frictional force of jet-stream wind and ambient air very little, finally cause not producing thrust, make the accelerating ability of aircraft worse and worse, cause aircraft speed under the effect of resistance of air, to be difficult to improve again.If jet-stream wind can run into the air basically identical with aircraft movements direction and speed all the time, jet-stream wind will remain the thrust to aircraft.
The air-flow of tradition air breathing engine ejection is straight-line jet-stream wind, numerous particles substantially all are the speed propellings with uniformity in the jet-stream wind cross section, numerous particles are very poor to the transmission capacity of reaction force each other in the jet-stream wind, when this just causes aircraft to use traditional air breathing engine, after speed reaches a critical velocity, be subjected to drag effects speed to be difficult to promote, speed also is difficult to improve again in the situation of not considering propelling resistance again.
Therefrom the vortex that successively decreases of the peripheral rotating speed of mind-set advance in the air-flow numerous particles each other movement velocity have greatest differences, vortex advances the fltting speed of zones of different particle in the air-flow cross section to have greatest differences, vortex advances in the air-flow cross section from the center to the periphery, and the fltting speed of particle successively decreases, the slow particle of movement velocity is slower away from the speed of aircraft, the fast particle of movement velocity is faster away from the speed of aircraft, the fast particle of movement velocity can run into the slow particle of movement velocity, cause numerous particles to form each other the chain type transmission, they are high to the transmission capacity of jet reaction.Therefrom the vortex that successively decreases of the peripheral rotating speed of mind-set advances air-flow that the particle basically identical with aircraft movements direction and speed is provided continuously, and these particles have better transmitted reaction force, and they have nothing to do with aircraft speed to the transmission capacity of reaction force.These particles finally have been delivered to vortex with reaction force and have advanced the air-flow center, make vortex advance the air-flow center to produce all the time the propelling force that a speed and vortex propelling air-flow center fltting speed equate substantially, this propelling force speed is all the time greater than the aircraft forward velocity, and this propelling force speed deducts the aircraft forward velocity and substantially equals vortex propelling air-flow center jet velocity.
Object is affected by gravitation during from falling from high altitude, and the object speed of falling can be accelerated gradually, and objects at high speed is fallen.Vortex advances air-flow that thrust and the gravitation that aircraft produces is had the effect that plays the same tune on different musical instruments, even vortex advances the air-flow fltting speed not high, aircraft speed is improved gradually, make final high speed, the ultra high speed that it can make the existing air breathing engine of aircraft generation realize of forming of aircraft.
Therefrom the vortex that successively decreases of the peripheral rotating speed of mind-set advances in the air-flow numerous Particles Movings orderly, make the reaction force transmission orderly, reaction force is collided mutually cause energy loss, the energy that vortex advances the interior numerous particles of air-flow to carry can be converted into the thrust to aircraft more fully, can make aircraft more energy-conservation.It can make aircraft produce the super low energy consumption that existing air breathing engine can't be realized, can greatly improve the aircraft flying power simultaneously.The advance resistance of aircraft is mainly from resistance of air, the advance resistance of automobile, train, steamer except from the resistance of air also more from ground friction or current friction, so the advance resistance of aircraft is less, propulsion method can make the aircraft energy consumption greatly reduce as long as adopt more effectively.
Motor is exactly the instrument of conversion of heat into kinetic energy that fuel combustion is produced, and a perfect motor need have two primary conditions: 1, make as far as possible fully burning of fuel, 2, energy is fully transformed as far as possible.It also will have in addition: simple structure, simple conditions of manufacture, cheap cost, cheap user cost, the working life of overlength, super wide fuel Applicable scope, super wide Applicable scope, energy-conserving and environment-protective, lightweight, noise is low, low vibrations, power range is wide, speed range is wide, moment of torsion is large, little etc. the condition of volume.This flywheel motor has possessed these conditions, and it has realized fuel combustion better, the conversion of heat into kinetic energy that fuel combustion is produced.
Technological scheme of the present invention is not restricted in the embodiment's of the present invention scope.The present invention not technology contents of detailed description is known technology.
Claims (10)
1. flywheel motor, comprise housing (1), fuel supplying device (2), ignition mechanism (3), starting drive (4) and spin stabilization device (20), it is characterized in that: the upper Flywheel axle (5) of housing (1), flywheel shaft (5) connects starting drive (4), a flywheel (6) is installed on the flywheel shaft (5) at least, a firing chamber (7) is set on the flywheel (6) at least, firing chamber (7) set-point firearm (8), igniter (8) is communicated with ignition mechanism (3) by circuit (9), air inlet of combustion chamber (10) and air outlet, firing chamber (11) are established in firing chamber (7), air outlet, firing chamber (11) is communicated with nozzle chamber (12), nozzle chamber (12) inner chamber is expanded to flywheel (6) outer rim direction opening, the jet direction of nozzle chamber (12) and flywheel (6) radius are the angle of inclination, the upper respective combustion chamber suction port (10) of flywheel (6) arranges supercharging device (13), supercharging device (13) arranges supercharging device suction port (14), and fuel supplying device (2) respective combustion chamber (7) arranges.
2. flywheel motor according to claim 1, it is characterized in that: a plurality of blades (16) are set in the supercharging device (13), blade (16) is the angle of inclination with flywheel shaft (5) cross section, supercharging device (13) outer installment supercharging cover (17), supercharging cover (17) inner chamber is expanded gradually to air inlet of combustion chamber (10) direction, supercharging device (13) middle part arranges baffle cover (18), baffle cover (18) outer radial air inlet of combustion chamber (10) direction is expanded gradually, the expansion angle of baffle cover (18) external diameter is greater than the expansion angle of supercharging cover (17) inner chamber, blade (16) outer rim is arranged on supercharging cover (17) inwall, and blade (16) inner edge is arranged on baffle cover (18) outer wall.
3. flywheel motor according to claim 1 is characterized in that: nozzle chamber (12) inner chamber cross-sectional circumference is for circular, and air outlet, firing chamber (11) are arranged on nozzle chamber (12) the inner chamber circumference.
4. flywheel motor according to claim 1, it is characterized in that: supercharging device (13) axis central part arranges fuel and carries cavity (15), fuel carries cavity (15) outlet end to be communicated with firing chamber (7), fuel is carried cavity entrance point middle part that fuel is set and is carried cavity import (19), and the corresponding fuel of fuel supplying device (2) is carried cavity import (19) setting.
5. flywheel motor according to claim 1, it is characterized in that: housing (1) is provided with a plurality of heat recovering devices (21).
6. flywheel motor according to claim 1, it is characterized in that: flywheel (6) periphery arranges a plurality of firing chambers (7), firing chamber (7) central axis and flywheel shaft (5) central axis are and intersect angle, firing chamber (7) inner chamber cross-sectional circumference is circular, air inlet of combustion chamber (10) is located on the inner chamber circumference of firing chamber (7), air outlet, firing chamber (11) is located on the central axis of firing chamber (7), and air outlet, firing chamber (11) cross sectional area is less than maximum cross section, firing chamber (7) area.
7. flywheel motor according to claim 6 is characterized in that: the central axis cross section is set on the interior central axis in firing chamber (7) is circular obturator (22), obturator (22) is arranged on the bottom interior wall of firing chamber (7).
8. according to claim 1,2,3,4,5,6 or 7 each described flywheel motors, it is characterized in that: the upper a plurality of flywheels (6) of installing of flywheel shaft (5).
9. according to claim 1,2,3,4,5,6 or 7 each described flywheel motors, it is characterized in that: the jet direction of nozzle chamber (12) and flywheel shaft (5) cross section are the angle of inclination, flywheel shaft (5) passes supercharging device (13), and flywheel shaft (5) passes supercharging device suction port (14).
10. according to claim 1,2,3,4,5,6 or 7 each described flywheel motors, it is characterized in that: the jet direction of nozzle chamber (12) and flywheel shaft (5) cross section are the angle of inclination, flywheel shaft (5) is in respectively flywheel (6) both sides with supercharging device (13), fuel is set in the flywheel shaft (5) carries cavity (15), fuel is carried cavity (15) axle head middle part that fuel is set and is carried cavity import (19), and the corresponding fuel of fuel supplying device (2) is carried cavity import (19) setting.
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| CN104564423A (en) * | 2013-10-21 | 2015-04-29 | 王秋林 | Run-off ramjet engine |
| CN110552813A (en) * | 2019-08-28 | 2019-12-10 | 中南大学 | Rotary cutting type powder supply system and powder fuel ramjet engine thereof |
| CN116714783A (en) * | 2023-08-10 | 2023-09-08 | 北京航空航天大学 | Flywheel fan engine type aerospace carrier |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103016205A (en) * | 2012-09-09 | 2013-04-03 | 陈久斌 | Flywheel engine |
| CN115183276A (en) * | 2022-07-25 | 2022-10-14 | 清航空天(北京)科技有限公司 | Fuel supply assembly, engine combustion chamber structure and engine |
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| CN102588144A (en) * | 2011-07-19 | 2012-07-18 | 陈久斌 | Flywheel turbine |
| CN203067127U (en) * | 2012-09-09 | 2013-07-17 | 陈久斌 | Flywheel engine |
-
2012
- 2012-12-07 CN CN2012105262177A patent/CN103016205A/en active Pending
- 2012-12-07 CN CN 201220676719 patent/CN203067127U/en not_active Expired - Fee Related
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| US4332520A (en) * | 1979-11-29 | 1982-06-01 | The United States Of America As Represented By The United States Department Of Energy | Velocity pump reaction turbine |
| US5408824A (en) * | 1993-12-15 | 1995-04-25 | Schlote; Andrew | Rotary heat engine |
| CN1354322A (en) * | 2000-11-17 | 2002-06-19 | 祝长宇 | Jet rotary engine |
| CN101389849A (en) * | 2006-01-03 | 2009-03-18 | 创新能量公司 | Rotary heat engine |
| CN102278233A (en) * | 2010-07-07 | 2011-12-14 | 靳北彪 | Supersonic rotor engine |
| CN102588144A (en) * | 2011-07-19 | 2012-07-18 | 陈久斌 | Flywheel turbine |
| CN203067127U (en) * | 2012-09-09 | 2013-07-17 | 陈久斌 | Flywheel engine |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104564423A (en) * | 2013-10-21 | 2015-04-29 | 王秋林 | Run-off ramjet engine |
| CN110552813A (en) * | 2019-08-28 | 2019-12-10 | 中南大学 | Rotary cutting type powder supply system and powder fuel ramjet engine thereof |
| CN110552813B (en) * | 2019-08-28 | 2024-05-03 | 中南大学 | Rotary cutting type powder supply system and powder fuel ramjet engine thereof |
| CN116714783A (en) * | 2023-08-10 | 2023-09-08 | 北京航空航天大学 | Flywheel fan engine type aerospace carrier |
| CN116714783B (en) * | 2023-08-10 | 2023-10-10 | 北京航空航天大学 | Flywheel fan engine type aerospace carrier |
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| Publication number | Publication date |
|---|---|
| CN203067127U (en) | 2013-07-17 |
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Application publication date: 20130403 |