WO2014146521A1 - 一种空心转子能量转化装置 - Google Patents

一种空心转子能量转化装置 Download PDF

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Publication number
WO2014146521A1
WO2014146521A1 PCT/CN2014/071936 CN2014071936W WO2014146521A1 WO 2014146521 A1 WO2014146521 A1 WO 2014146521A1 CN 2014071936 W CN2014071936 W CN 2014071936W WO 2014146521 A1 WO2014146521 A1 WO 2014146521A1
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WO
WIPO (PCT)
Prior art keywords
wheel
rotor
fixed
ignition
stator
Prior art date
Application number
PCT/CN2014/071936
Other languages
English (en)
French (fr)
Inventor
王军
Original Assignee
Wang Jun
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wang Jun filed Critical Wang Jun
Publication of WO2014146521A1 publication Critical patent/WO2014146521A1/zh

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F01D1/38Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes of the screw type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/20Three-dimensional
    • F05D2250/25Three-dimensional helical

Definitions

  • the invention relates to a hollow rotor energy conversion device, and the invention relates to a hollow hollow heart rotor rotor energy energy conversion conversion device, and it relates to It is a Lily.. It uses a spiral spiral wheel structure with a hollow hollow core to rotate the rotor, so that the fuel mixture is mixed and driven in the jet jet drive device and
  • the ignition ignition drive device is equipped with no contactless contact action, and the four or four processes that have been sucked in, compressed and contracted, burned and burned, and discharged are discharged.
  • the actual implementation is not continuously interrupted by the circulation of the ring to continue to transform into a machine mechanical energy and electrical energy. .
  • the conversion efficiency of the conversion is much higher than that of the conventional piston-type and the rotor-shaft torsion-force engine. More, and at the same time, the lowering of the noise and noise is lower, and the balance of the rotation and balance is increased. .
  • the main stator is mainly the fuel supply for supply and control control point ignition time and the suction and intake parameters, so the wear loss is less, Safety and safety can be reliable, low maintenance and low maintenance, easy to clean and wash, and long life.
  • the main components of the fuel-fuel mixture and the gas mixture are divided into oxygen and oxygen gas, and at least the package includes diesel fuel, gasoline and gasoline, and coal kerosene. Oil, biomass, oil, and the like, and other
  • the prior art combustion chamber cooling and wear parts cooling also need to consume their own energy, at least 20% - 25% of the combustion energy is lost through the water circulation system, although the existing computer technology can effectively control the water circulation, but the combustor to the water temperature
  • the difference in thermal resistance of the sampling, the temperature control lag, and the abnormality of the coolant leakage result in the loss of effective heat of combustion and the incomplete combustion of the exhaust gas.
  • Reciprocating piston engines in addition to low speed, large volume, heavy weight and high vibration, this complex structure also forces inertia forces to each other, and at the same time it also develops its potential for high-speed and smooth development.
  • the crankshaft wears up and the vibration increases.
  • the efficiency can only be maintained within a certain range.
  • the current speed is up to 6500RPM and the efficiency is up to 40%.
  • the cylinder liner and piston wear more than 0. 19mm, and the gas leakage will be more serious, resulting in the efficiency falling below 35%.
  • the noise of the reciprocating crankshaft, at high speed not only consumes energy, but also brings great harm to the working environment.
  • the dynamic fluctuation of the piston reciprocates, causing obvious vibrational motion of the rotation, and as the speed increases, the frequency of the vibrational artery gradually increases, which consumes both power and noise.
  • the most dangerous is the logic abnormality of Quxin, flywheel, air intake and exhaust, which will cause the high-pressure gas in the combustion chamber to be released and instantaneously knocked.
  • the explosion will be caused by the spontaneous combustion of the fuel injection pipe through the combustion chamber. , that is, it may cause metal fragments to splash when it is serious.
  • the reciprocating piston-type exhaust valve is usually opened before the piston reaches the dead point. Since the volume of the fuel mixture is increased to 60-90 times before the original compression, if it cannot be fully utilized in an instant, Destructive forces are caused to damage other valves and cylinder walls. Therefore, at least 40% 45% of the combustion can be removed from the exhaust.
  • the turbine addition technology has a certain degree of reuse value, it can reuse up to 58% of the exhaust gas energy, but its operation requires the rotor to be more than 2000RPM to be effective, otherwise the surplus can only be exhausted by the friction of the turbine itself. However, less than 2000 RPM is currently the most commonly used speed segment of the engine, so a large amount of combustion can naturally disappear.
  • the angular piston rotary engine that is, the Wankel rotary engine has relatively few moving parts.
  • the rotor works three times per revolution, and has a high horsepower compared to the normal piston engine that rotates twice every two revolutions.
  • the advantage of volume ratio is relatively low, so that the combustion is not sufficient, the exhaust gas is severely discharged, and there is friction with the stator casing at the top corner of the triangle.
  • this wear increases, that is, the volume loss of the high pressure gas is increased, the shaft There is also wear and tear in the seal that causes volume leakage.
  • the friction between the apex angle and the friction of the piston structure is the same principle, and as the degree of rotation increases, the heat generated by the friction is larger, so the energy consumption of the heat dissipation system is greater.
  • the volume of the easy-coupled rotary engine is small and light, the volume of the same-power reciprocating engine is reduced and the weight is much reduced.
  • the wear between the shafts causes the loss of high pressure gas to remain severe.
  • the number of gears before and after the Ji has increased a lot, and the wear of the occlusal drive rotor has increased a lot, that is, it consumes more energy.
  • abnormalities often occur, that is, the overall abnormal frequency increases.
  • the existing shaft torque engine is a single mechanical energy that converts combustion energy into shaft torque. It cannot be directly converted into electric energy, and it must be connected through a shaft to realize the power generation effect of the generator. The efficiency of electrical energy is even lower.
  • the prior patent No. 021 ⁇ 3455 relates to a rolling screw engine, including a cylinder block, a cylinder head, a valve train, an energy conversion mechanism, a cold P mechanism, and a lubrication mechanism.
  • the energy conversion mechanism includes a screw conversion mechanism and continuous stepping.
  • the spiral converting mechanism is composed of a rolling spline and a rolling screw
  • the rolling spline is composed of a jacket, a middle sleeve, an inner sleeve and a steel ball
  • the rolling screw is provided by a spiral sleeve, a middle sleeve and an inner sleeve.
  • the steel ball composition, the rolling spline and the rolling screw are provided as a whole; one end or both ends of the inner sleeve are connected in series with the piston rod in one or more cylinder bodies;
  • the continuous stepping rotation mechanism includes a screw conversion mechanism
  • the two sets of reverse-rotating spiral-feeding and output gears are respectively connected by two spiral sleeves through the clutch and the output gear; the two sets of spiral-paid inner sleeves are integrated, and the two spiral sleeves are arranged between the two thrust bearings.
  • the prior patent No. 200910206243 relates to a rotary engine in which a compressed air buffer chamber, a combustion chamber and a rotor chamber are formed in an engine casing, and an air compressor outlet port is connected to the combustion chamber through a one-way valve through a compressed air buffer chamber, and the combustion chamber is connected.
  • a fuel injection device and a timing ignition device a gas injection port of the combustion chamber is connected to the rotor chamber, a rotor is installed in the rotor chamber, and the rotor is composed of a rotor shaft and a rotor blade.
  • the rotor blades are concentrically distributed on the upper rotor shaft, and the rotor shaft is mounted on the engine casing.
  • an air compressor is installed on the rotor shaft.
  • the invention has a simple structure, few parts, easy manufacture, stable performance, and simple maintenance, a variety of fuels can be used, but long-term wear between the rotor blades and the casing causes high-pressure gas loss, resulting in a decrease in efficiency. The higher the speed, the greater the wear.
  • the existing patent number 200910103789 is a ring cylinder rotor engine composed of a rotor and a stator.
  • the space between the rotor and the stator is an annular combustion chamber, and eight pistons are mounted on the rotor.
  • the two groups are divided into two groups to make a turn-by-turn alternate position rotation in the annular combustion chamber.
  • the annular combustion chamber is divided into eight cylinders by the piston.
  • the two cylinders have the same stroke, and the expansion tension is transmitted to the gear crankshaft through the connecting members in the rotor, and then the teeth are 3 ⁇ 4 teeth.
  • the wheel crankshaft is transmitted to the output shaft to continuously rotate the output shaft. Due to the presence of the crankshaft and the transmission of the gears, the wear is increased, and at the same time, the increase of the shaft clearance against the speed causes the gas leakage, that is, the efficiency to decrease.
  • the prior patent No. 201020170497 relates to a rotary engine.
  • the rotor is provided with a rotor in the inner cavity of the stator, and the end caps are fixed at both ends.
  • the central shaft of the rotor is connected to the end cover, and the rotor is provided with a through groove, and two blades are installed therein.
  • a spring is connected between the blades, and the exposed edges of the two blades are placed on the edge of the stator cavity, and the rotor sealing strip is embedded on the exposed sides of the two blades;
  • the inner cavity of the stator is two semicircles plus two straight transition sections;
  • the lower stator transition section of the stator is embedded with the stator lower sealing strip, and the air inlet and the exhaust port are opened on both sides;
  • the upper stator sealing strip is embedded on the upper straight transition section of the stator, and the connecting hole and the compressed air passage are opened on both sides.
  • a control valve is provided in the communication hole, and the upper port leads to the gas storage tank; a one-way helium gas valve is arranged in the compressed gas passage, and the upper port leads to the gas storage tank; a spark plug hole is opened beside the communication hole, and a spark plug is installed therein; .
  • the existing patent number 201010245132 is a new type of screw rotor engine, which is characterized in that there are two special ⁇ -shaped screws in the dumbbell-shaped casing, the small heads are opposite, riveted on the main shaft as a whole, and a gear on the side
  • the meshing acts as a diversion flow ffl, and the space surrounding the screw in the middle of the cylinder is close to the combustion chamber, and has a spark plug and a fuel injector.
  • the air is compressed by the helium screw into the combustion chamber, and the oil is continuously burned therein. And promote the work of the snails.
  • the gear connection increases the friction loss, and the gap of the combustion chamber gradually increases with the increase of the speed, that is, the volume energy loss increases the efficiency.
  • the product technology of the invention mainly relies on the radial component of the internal combustion energy expansion force of the hollow rotor to directly push the rotor to rotate, which not only improves the conversion efficiency, but also reduces the noise and improves the rotation speed. It also reduces the characteristics of faults, safety and reliability, low maintenance, easy cleaning and improved life. Its main structural features are as follows -
  • a hollow rotor energy conversion device is characterized by: at least, the rotor (12) has a hollow cone shape as a whole, a spiral wheel (1), a front cover (2), a back cover (4), and a heat dissipation ring (13)
  • the rotor of the shaft head U5) is fixed on the stator (6) under the support of two bearings ( ), and the fuel injection device (imposed on the stator is concentrically aligned with the front cover, and the inner wall of the middle portion of the spiral wheel is fixed at least
  • a set of ignition heads (3), at least one set of ignition driving devices (10) corresponding to the circumferential angle of the ignition head are fixed on the stator, and the rear part of the spiral wheel extends into the hollow center of the power generating device (5) to start the motor (9)
  • Concentrically fixed with the starting device (8) in the front section of the stator and the shaft head concentrically aligned the shaft head with inertia is separated and statically connected in series after the starting and starting devices are connected
  • the heat-dissipating ring is composed of a plurality of blades fixed around the outer wall of the high-temperature zone of the spiral wheel to rotate synchronously with the rotor, and the auxiliary component (16) is fixedly mounted at any position of the stator.
  • the spiral wheel (1) is characterized by: at least one from the front wheel cavity (] -. 2) to the rear wheel cavity (1.7).
  • the number of cavities is at least i and the spiral rotation angle exceeds 2 ⁇ .
  • the volume of the cavity gradually becomes smaller and smaller from front to back, while the volume of the rear wheel cavity remains unchanged.
  • the three-wheel wall (L 1 ) is continuously thickened from front to back without expectation, and the four front wheel (L 4) to the rear wall of the wheel (L 5) gradually thickening the interior without steps, the thickness of the five-wheel rear rib (L 6) is greater than the front rib of the wheel (1. 3), and the six ignition head mounting unit (L 9) is located on the inner wall of the spiral wheel without any leakage from the outer wall.
  • the ignition head mounting unit is sealed by a non-magnetic material to make the magnetic lines from the inner wall to the outer
  • the walls are completely conductive to each other.
  • the rear end side of the eight-helical wheel has an opening of the # ⁇ (1.8) and the number of holes corresponds to the number of the wheel chambers.
  • the front wheel cavity and the rear wheel cavity are transparent, and the number of the wheel cavity is one by one. correspond.
  • the front cover (2) is characterized by: at least: an opening having a suction port (2. 2) for fuel on a different circumference of the front cover radius, and corresponding to the position and number of the spiral wheel cavity, the second wheel Front rib seat (2.4) Wheel front wall seat (2.5) and wheel front rib (1.3) Wheel front wall (1.4) One-to-one sealing connection, _ ⁇ :
  • the door valve (2.3) is fixed on the front cover radius and the suction port corresponds , the closing area is larger than the suction port
  • the suction area, the four-valve valve is equivalent to the circumferential radius R of the injection nozzle (11.1) of the fuel injection device and the same circumferential angle, and maintains a certain axial rotation gap distance.
  • the five automatic switches (2.1) are fixed behind the front cover. It can only be opened from the outside and always closed inside.
  • the six automatic switch device controls the door valve to have a spring force greater than i. The external pressure can open the door valve.
  • the seven automatic switches are fixed in front of the suction port, that is, from the rear to the rear axle. If the rotor is turned clockwise, it will be fixed at the clockwise side of the suction port.
  • the fuel injection device (11) is characterized in that it comprises at least an outer cavity which is sealed by a casing (1L 5) and an inner casing (1L 6), and a nozzle which is fixed in the cavity (1 ⁇ 1)
  • One end is connected to the fuel mixing channel (ii.4), and the other end is opposite the front edge of the suction port (2.2) in the direction of rotation.
  • the three nozzles are mounted in one-to-one correspondence with the suction port of the front cover, and the four fuel delivery channels (11.2) and
  • the high-pressure air conveying passage (iL 3) communicates internally through the filter net.
  • the diameter of the five inner shells is larger than the diameter of the shaft head, that is, the rotor rotates without contact and friction.
  • the ignition head (3) is characterized in that: at least, a sensing surface (3.1) is fixed in the ignition mounting unit (L9), the second magnetic force can penetrate the closed wheel wall to reach the sensing surface, and the three ignition coils (3.2) are wound around On the inner conducting magnet (3.4), the four electrodes (3.3) are welded to the ignition coil end to end and a certain gap between the poles to ensure the energization fire.
  • the mounting angle of the five or more ignition heads is equal to 2 ⁇ divided by the number of wheel chambers n . ⁇ ⁇ 231 / ⁇ .
  • the ignition driving device (10) is characterized by: at least: a driving cable U0.1) - the first end is directly welded to the driving coil ⁇ .3), the other end is directly welded to the auxiliary part of the stator, and the second driving coil is wound around the outer guiding
  • the three drive coils are fixed on the outer wall of the non-magnetic ring (10.4), and the circumferential angle ⁇ is equal to the circumferential angle of the ignition head installation.
  • the four non-magnetic rings have a certain radial rotation gap with the outer wall of the spiral wheel. That is to ensure that the rotor rotates without contact and friction, but does not affect the magnetic transmission.
  • the rear cover (4) is characterized by: at least one round rear wall groove (4.1), the rear wheel groove (4.3) and the rear wheel wall (1.5) of the spiral wheel and the rear wheel rib (1.6) - a corresponding seal embedded Fixed, two back cover force surface (4.2) Fasten the drive shaft (4.4) to ensure the same torque as the rotor.
  • the power generating device (5) is characterized in that: at least, a rotor of the power generator is fixed to the outside of the rotor
  • the _ three power generation casing is fixed on the stator and has no contact with the rotor and no friction.
  • the stator coil is connected to the auxiliary component of the stator, that is, the induced current is turned on.
  • the auxiliary component (16) is characterized by: at least: a circuit module for rectifying and inverting the induced current, two fixed storage batteries connected to the inverter circuit and connected by the electric device, and three fixed fuel injection Device control port circuit and ignition drive control terminal circuit, four pressure sensors fixed on the stator, temperature sensor, rotor position sensor, gas sensor, suction port sensor, ignition coil sensor, and other sensors requiring control detection around the rotor No contact friction, five fixed CPU control circuit modules are connected with all sensors, power supply, and output control terminals, and six fixed other auxiliary components for function expansion.
  • the present invention also includes the following features:
  • the connection of the front and rear covers of the spiral wheel and the connection of the ignition head are relatively static and fixed without wear seals, and the internal high pressure during the suction compression expansion exhaust cycle The gas is not possible to expose the pool to the outside. Therefore, after the wheel chamber of the spiral wheel sucks in the fuel mixture, the compressed combustion expansion gas continues to push the work in the radial direction until the value of the flame energy is not increased, thereby achieving the highest conversion rate of combustion energy.
  • the volume of the front wheel cavity will gradually form a relative vacuum as the operation progresses. Below one atmosphere, the threshold of the suction port is automatically smashed by the external fuel mixture gas pressure, that is, the fuel mixture is ensured. The rapid entry of gas also saves the pressure energy consumption of the injector.
  • the shaft head has a certain inertia.
  • the wheel chamber performs work in the shortest interval of 31 /2, it can continue to rotate between 3 ⁇ /2 ⁇ ⁇ by the inertia of the shaft head, that is, the second work is performed.
  • the fuel injection device is not connected to the front cover suction port of the rotor, and the fuel mixture gas is docked in the air through the injection nozzle and the suction port of the suction port, so the fuel in the front wheel cavity of the rotor does not continue to inject fuel accumulation due to the abnormality of the injection valve. Excess, even if the ignition time is advanced, it will not ignite the upward oil circuit, so the possibility of spontaneous combustion or knocking is completely eliminated.
  • the same jet drive and rotor are non-contact and frictionless.
  • the ignition head inside the rotor does not contact the external ignition drive device, but the high-frequency magnetic force penetrates the wheel wall to obtain the ignition potential energy, which does not cause any friction to the rotor rotation, and completely eliminates the open flame to the oil passage leakage. The possibility of igniting knock.
  • Increasing the diameter of the spiral wheel is equivalent to increasing the torque of the rotor, that is, increasing the uranium output torque torque of the rotor.
  • the shortest cycle of inhalation to exhaust can be completed within 2 cycles of one rotor rotation. If one wheel cavity is used, the gas expansion in one rotation cycle is the same as only 4 wheel chambers, and the suction is completed one by one. The gas exhaust cycle, the expansion force work time reaches 2 ⁇ , that is, one turn.
  • the number of cycles and the ignition determine the frequency and period of the pulsation of the spiral wheel.
  • the number of wheel chambers is increased and the ignition time interval is reduced, the expansion force continues to be proud and the pulsation approaches 0.
  • the rotor is driven by the rotor to dissipate the heat-dissipating ring. Since the friction force of the blade and the air is far less than the lifting force of the gravity cycle and the frictional force in the circulation body, the residual heat dissipation effect can not be used. It also achieves the goal of improving overall efficiency.
  • This wind cooling method also eliminates the possibility of freezing of the winter water-cooled circulation system, and at the same time, the lower starting speed and lower heat-dissipating efficiency increase the starting temperature of the low-temperature environment, and consume energy without auxiliary heating.
  • the sensor includes real-time tracking of rotor speed, wheel cavity temperature, nozzle pressure, suction port position, fuel injection drive current, starting electric current, ignition drive current, ignition coil position, and other abnormal information. After that, it is immediately transferred to the CPU center of the computer on the stator, and the corresponding output is given through operation and processing, that is, each operating parameter is guaranteed in the established process. The sequence is also performed, which also reduces the possibility of abnormalities and failures.
  • the ignition drive device on the stator is installed in multiple groups along the spiral wheel axis. When starting at low speed, it is ignited farthest from the front cover. When it enters the medium speed after starting, it ignites closer to the front cover, when entering the high speed. When running, it ignites closest to the front cover.
  • the energy conversion of the stator coil and the rotor follows the principle of the induction generator, and the principle of the DC brushless generator, the principle of the high-efficiency permanent magnet generator, and the principle of the brushless excitation synchronous generator, that is, the conversion efficiency is the highest.
  • Figure 3 Axial section of the spiral wheel of the product of the present invention
  • Ignition head mounting unit Fig. 4 Radial sectional view of the spiral wheel of the product of the invention as seen from the small circle to the direction of the large circle.
  • Ignition head mounting unit Fig. 5 Rear view radial section of the front cover of the product of the invention
  • Inner Shell Figure 7 Combination of radial section view of the ignition head structure of the product of the present invention (inside) and radial section of the ignition drive structure (outer)
  • Non-magnetic conduction' Fig. 8 Axial sectional view of the back cover of the product of the invention (left) and front radial sectional view (right) Notes:
  • Fuel control terminal There are various valves and connection mechanisms that can recognize and receive signal commands from the CPU, and effectively close and open the injection nozzle, and the switching frequency meets the needs of the maximum rotor speed.
  • Output shaft rotation It has the ability to load and connect load torque.
  • Generator operation Complete the conversion process of kinetic energy from the rotor to electric energy, including at least two processes of induction and inverter, and follow the principle of induction generator, or the principle of DC brushless generator, the principle of high efficiency permanent magnet generator, Brush excitation field synchronous generator principle any kind of process.
  • CPU It can complete all the functions of the computer, including at least all signals identifying and receiving the sensor, can perform logical conversion and data storage, and can output effective commands to control all terminals.
  • FIG. 8 block diagram of the fuel injection driving process of the product of the invention
  • Gas sensing A sensor designed to detect the outflow pressure of the nozzle.
  • Position sensing It is specially used to detect the non-contact detection sensor before the arrival of the suction port.
  • CPU It can complete all the functions of the if computer, including at least all the signals of the identification and receiving sensors, logic conversion and data storage, and can output effective commands to control all terminals.
  • Battery storage It can absorb the power of the power generation unit and supply power to the starter motor, various drive units, sensors and CPU components.
  • the normally closed electromagnetic switch can meet the corresponding opening and closing of the maximum rotor speed.
  • Spray nozzle It is specially used for fuel mixed gas injection, and it is sprayed out with a gas sensor and can withstand the impact of high pressure gas.
  • Suction port The radius of the front cover of the rotor, and contains the detection point of the position sensor.
  • Figure 12 is a block diagram showing the working principle of the ignition driving process of the product of the present invention. Annotation
  • Position Sensing Dedicated to the detection of contactless detection sensors before the ignition coil.
  • CPU It can complete all functions of the computer, including at least all signals for identifying and receiving sensors, enabling logical conversion and data storage, and outputting effective commands to control all terminals.
  • Battery storage It can absorb the power of the power generation unit and provide power to the startup power, various drive units, sensors and CPU components.
  • Inverter conversion circuit A circuit that converts DC power into AC high frequency.
  • High-frequency coil It can convert high-frequency alternating current into magnetic force and have a certain direction.
  • Inductive coil capable of sensing magnetic force and forming an electromotive force at the beginning of the coil.
  • Electrode discharge Automatic current discharge after the accumulation of opposite charges.
  • the battery power supply of the auxiliary unit U6) turns on the starter motor (9), and then the starting device (8) drives the rotor (12) to start rotating, and the spiral wheel (1) also rotates with the same.
  • the front wheel chamber (L 2) forms a relative vacuum under the helical thrust due to the sealing of the front cover (2).
  • the front cover valve (2.3) is externally sprayed.
  • the front cover valve in the opposite direction is closed, so The expanded high-pressure gas can only continue to advance in the original direction, and the radial thrust continues to work as the expansion force moves toward the rear section of the spiral wheel, and is discharged from the exhaust port U. 8) until it is no longer usable.
  • the wheel wall receives the radial thrust transformed by the expansion force, that is, the speed of the radial rotation increases instantaneously, and the shaft head with the inertia continues to rotate, so that the vacuum of the front wheel cavity is formed for the second time, and the vacuum degree is increased a lot.
  • the fuel injector instantaneously injects the fuel mixture gas into the suction port in accordance with the calculation program set by the CPU on the stator.
  • the spiral wheel rotates, thereby driving the entire rotor to rotate.
  • the starting motor automatically opens the rotor and stops rotating.
  • the power generating rotor material (5.4) in the rear section is in the power generating device, and the surrounding induction stator coil (5.1) is induced according to the right-hand law, and the current is in the auxiliary component of the stator (16). Under the action of rectification, the battery is stored and stored.
  • the injection drive control port When the injection drive control port amplifies the injection capacity, the fuel mixture gas expansion force is enhanced and the rotor speed is increased.
  • the injection capacity is 0, the rear cover of the spiral wheel cannot absorb the fuel mixture, that is, the rotor stops by itself. After the rotor stops running, the shaft head and the starting device are connected in series to wait for the start.
  • the spiral wheel rotation process is completed by the cp computer.
  • the starter motor is commanded to drive the rotor to start rotating, and the position sensor near the rotor detects the correct position of the rotor.
  • the signal is passed to the CPU, and the CPU is analyzed by other signal data.
  • a command is given to the fuel control end of the fuel injection drive unit to cause the injection nozzle to open and align with the rotor intake ⁇ to inject the fuel mixture.
  • the CPU calculates and analyzes the signal provided by the rotor position sensor, it issues a command to the ignition control unit of the ignition drive to start ignition.
  • the rotor speed increases to a certain extent
  • the CPU passes the speed sensor to confirm that the spiral wheel has started to start, and each sensor enters the real-time monitoring state.
  • the sensor that starts the motor feeds back the signal to CPI].
  • the CPU After the CPU has been calculated and analyzed, it is necessary to turn off the starter motor. After the fault is removed, start again.
  • the gas sensor of the exhaust port detects the abnormality of the exhaust gas, the signal is transmitted to the CPI], and the CPU issues an instruction to the relevant output control terminal through operation and analysis, and adjusts accordingly to ensure the best.
  • the running state when the gas sensor of the exhaust port detects the abnormality of the exhaust gas, the signal is transmitted to the CPI], and the CPU issues an instruction to the relevant output control terminal through operation and analysis, and adjusts accordingly to ensure the best.
  • the running state when the gas sensor of the exhaust port detects the abnormality of the exhaust gas, the signal is transmitted to the CPI], and the CPU issues an instruction to the relevant output control terminal through operation and analysis, and adjusts accordingly to ensure the best.
  • the running state
  • the fuel injection driving process is completed by the CPU computer.
  • the sensor near the suction port detects the arrival of the rotor suction port, and the signal is transmitted to the CPU.
  • a command is given to the current operational amplifier circuit, so that the amplified current enters the normally-closed high-frequency electromagnetic valve.
  • the injection nozzle injects the fuel mixed gas at the suction port. If an abnormality occurs in the high-frequency electromagnetic valve, the signal is immediately transmitted to the CPU by the current sensor.
  • the CPU immediately performs calculation and processing on the information, and then issues a command to the current operational amplifier to stop the output, and then returns to normal after the fault is eliminated.
  • the ignition driving process is completed by the CPU calculation process.
  • the CPU As shown in the block diagram of Fig. 12, after the battery power switch is turned on, when the ignition coil sensor near the rotor detects the arrival of the rotor ignition coil, the signal is transmitted to the CPU, and the CPU passes through.
  • an instruction is sent to the inverter conversion circuit to convert the direct current into a high-frequency alternating current into the high-frequency coil, and the magnetic field generated by the high-frequency coil passes through the non-magnetic material into the sensing surface of the induction coil, and the induction coil is obtained.
  • the magnetic field generates an induced electromotive force, which ionizes the discharge immediately after the potential is accumulated at the electrode end, that is, ignites the fuel mixture.
  • the signal is immediately transmitted to the CPU by the near current sensor.
  • the CPU receives the information and immediately performs calculation and processing. It is necessary to issue a command to the inverter circuit to stop the output before the fault is removed. normal.
  • the fuel mixture is completed in a wheel chamber and divided into four states, namely, vacuum suction A, instantaneous compression B, and ignition expansion (:, exhaust gas discharge 0.
  • the four states must be at least in the spiral -
  • the circumference angle is completed within 2 ⁇ , and the ⁇ expansion ⁇ must be greater than then into the rear wheel cavity, otherwise the energy will be lost in advance.
  • the four cycle states are completed within a radius of 2 ⁇ of the circumference of the spiral, that is, the expansion force performs one rotation at a time.
  • the pressure is low and the pressure is insufficient. Therefore, it is necessary to adopt an extended spiral wheel lead to increase the compression force, that is, from the ⁇ state to the ⁇ state, the rotor needs to be rotated n times and then ignited. For this reason, when used in low speed applications, long lead driving force can be adopted, and high speed occasions can use short lead driving force.
  • the minimum lead length is equal to the diameter of the spiral wheel to meet the general rotor speed requirement. Otherwise, the lead is very good. The short corresponding speed is extremely high, which will lose its meaning for general use conditions.
  • the ignition drive device on the stator can be installed in multiple groups along the spiral wheel axis. When starting at low speed, it is ignited farthest from the front cover. When starting to enter the medium speed, it is ignited near the front cover, when entering high speed operation. , then ignites closest to the front cover.
  • a plurality of wheel chambers may be added in the radial direction of the spiral wheel, that is, the expansion force is increased to effectively work, and the corresponding suction port, fuel injection device, ignition head and ignition driving device are also added.
  • the number of wheel chambers needs to be evenly paired.
  • the four-state cycle of the plurality of wheel chambers can be successively performed, and the pulsation amplitude of the work, that is, the pulsation period is shortened, the pulsation frequency is increased, and the disturbance to the output and the periphery is reduced.
  • the spiral wheel lead can be appropriately lengthened, so that the radial component of the expansion force after combustion is continuously worked until it is not utilized, and then discharged from the helium port.
  • multi-wheel cavity and successive ignition mode are adopted, so that one wheel cavity first burns and the temperature is transmitted to the next wheel cavity temperature through the wheel wall, which also ensures that the compression interval is long enough, and the temperature rises fast, that is, the expansion force is effective. Longer cycles increase conversion efficiency.
  • the size or lining of the heat ring can be changed.
  • the number of turns of the heat-dissipating ring is reduced, and the diameter of the blade is increased. This reduces the difficulty of starting due to excessive heat dissipation and the loss of combustion energy. .
  • the heat-dissipating ring can be eliminated, and the outer wall of the rotor and the air can be used to dissipate heat.
  • the heat-dissipating ring can be made of superconducting material, and the number and diameter of the blades are large enough.
  • an oxide film may be formed on the inner wall of the spiral wheel. If the film is thickened, the gas passage will be narrowed and the work will be affected. It is necessary to stop the front cover and the back cover, and use the soft tool to enter the spiral wheel. Wheel cavity cleaning is simple and convenient.
  • the direction of rotation of the rotor is determined by the direction of the wheel wall of the spiral wheel, that is, the direction of the work of the high pressure gas from the front cover to the back cover is determined, so that the rotor of the working process is not allowed to reverse, otherwise the impact on the front cover is set in the starting device.
  • the mechanical device that rotates the rotor in the correct direction is set.
  • the starting device brakes and locks immediately, until the abnormal cancellation is made, and the normal starting can be started again.

Abstract

一种空心转子能量转化装置,该装置至少包括:转子(12),其整体呈空心锥体状,由螺旋轮(1)、前盖(2)、后盖(4)、散热环(13)、轴头(15)组成的转子在两个轴承(14)的支撑下固定在定子(6)上;利用空心转子的螺旋轮结构,使燃料混合物在燃料喷射装置(11)和点火驱动装置(10)的无接触作用下完成吸入、压缩、燃烧、排出四个过程,实现不断循环持续转化成机械能和电能,其转化效率优于活塞式和转子式结构的轴扭力发动机,同时降低了噪音和提高了旋转平衡度。

Description

种空心转子能量转化装置 所所属属技技术术领领域域 本本发发明明型型专专利利是是涉涉及及一一种种空空心心转转子子能能量量转转化化装装置置,, 它它是是利利..用用空空心心转转子子的的螺螺 旋旋轮轮结结构构,, 使使燃燃料料混混合合物物在在喷喷射射驱驱动动装装置置和和点点火火驱驱动动装装置置无无接接触触作作用用下下完完成成吸吸 入入、、 压压缩缩、、 燃燃烧烧、、 排排出出的的四四个个过过程程,, 实实现现不不断断循循环环持持续续转转化化成成机机械械能能和和电电能能。。其其 转转化化效效率率比比传传统统的的活活塞塞式式和和转转子子式式结结构构技技术术的的轴轴扭扭力力发发动动机机提提高高很很多多,,同同时时降降低低 了了噪噪音音和和提提高高了了旋旋转转平平衡衡度度。。 由由于于燃燃烧烧循循环环过过程程是是在在空空心心转转子子内内部部完完成成,, 而而且且膨膨 胀胀力力直直接接驱驱动动转转子子运运转转,, 而而定定子子主主要要是是燃燃料料供供给给和和控控制制点点火火时时间间和和吸吸入入参参数数,,所所 以以磨磨损损较较少少、、 安安全全可可靠靠、、 维维护护较较低低、、 清清洗洗方方便便、、 寿寿命命较较长长。。 这这里里燃燃料料混混合合气气体体的的 主主要要成成分分除除了了氧氧气气外外,, 至至少少还还包包括括柴柴油油、、 汽汽油油、、 煤煤油油、、 生生物物油油以以及及其其它它可可以以燃燃烧烧
Figure imgf000002_0001
背景技术 目前用于轴扭力的发动机技术主要是活塞式结构和转子式结构。 而这两种 结构据统 if只有 30%- 40%的燃烧能转化为动能, 其它都是以热能散发和废气排放 散失。这种结构都是在定子燃烧室里面燃烧, ϋ转子在定子里面的铀上进行相对 运动, 所以至少有轴摩擦和密封件摩擦。 这些摩擦损耗, 和固有密封随着运行磨 损的加大导致高压气体泄漏, 即效率低下。 同时, 为了减少泄漏损耗, 还增加了 很多润滑油系统, 这些辅助系统除了消耗自身的能量外,还要耗用材料资源和人 力维护资源。
同 , 现有技术的燃烧室降温和磨损件降温也需要消耗自身能量, 至少燃 烧能的 20%- 25%通过水循环系统散失, 尽管利用现有计算机技术可有效控制水循 环, 但是丛燃烧室到水温采样的热阻差异、 温控滞后、冷却液泄漏异常, 即带来 燃烧有效热量散失和燃烧不彻底尾气危害环境的结果。
往复活塞发动机, 除了转速低、 体积大、 重量重、 震动大, 这种复杂结构 还对惯性力相互拟制, 同时也拟制了它向高速平稳方向发展的可能。当高速运转 时, 曲轴的磨损加大, 震动加大, 其效率只能维持在一定的范围, 目前转速最高 6500RPM , 效率最高 40%。 工作 2000小时后, 缸套与活塞磨损超过 0. 19mm, 气体泄 漏就会更加严重, 导致效率下降到 35%以下。 而且往复曲轴的噪音在高速下, 除 了消耗能量外, 还给工作环境带来了很大的危害。 活塞往复形成的动力波动,使 转动有明显的震动脉动, 而且随着速度的增加, 这种震动脉动频率逐渐增加,它 既消耗了动力, 也增加了噪音。最危险的是曲辛由、 飞轮、 进气阔、 排气阔逻辑异 常 ,会导致燃烧室高压气体无法释放而瞬间爆震,有时也会因为喷油管道直通 燃烧室关闭泄露自燃引起瞬间爆震, 即严重时可能造成金属碎片飞溅。
特别是往复活塞式发动 的排气阀, 通常是在活塞做功到达死点前就已经 打开, 由于燃料混合气体燃烧后体积增加到原来压缩前的 60- 90倍, 若瞬间不能 全部利用, 就会使膨胀力产生破坏力对其它阀门和缸壁破坏。 因此, 至少有 40% 45%燃烧能从废气口排除。 尽管涡轮增加技术在一定程度上对之有再利用价 值, 最多再利用 5 8%的排出废气能, 但是其运行要求转子超过 2000RPM才有效, 否则剩只能被涡轮自身的摩擦消耗殆尽。 然而, 低于 2000RPM是目前发动机最常 用的转速段, 因此大量的燃烧能自然消失。
Ξ:角活塞旋转式发动机, 也就是汪克尔转子发动机 运动零件相对较少, 转 子每旋转一圈就作功三次, 与一般的活塞发动机每旋转两圈才作功一次相比,具 有高马力容积比的优点。但是压缩比较低, 使得燃烧不能够很充分, 尾气排放严 重, 而且在三角的顶角处有与定子外壳的摩擦, 长时间工作, 这个磨损增大,即 导致高压气体的容积损耗加大, 轴封间也有的磨损导致容积泄露。 同时这个顶角 的摩擦与活塞式结构的摩擦是同样的原理, 而且随转度增加,摩擦产生的热量更 大, 所以采.用散热系统的能量消耗更大。
易理偶式转子发动机虽然整体积小、 重量较轻, 同功率比往复式发动机的 体积减少, 重量也减轻很多。 但是, 轴间的磨损导致高压气体损失依然严重。而 Ji前后的齿轮数量增加了很多, 咬合驱动转子产生磨损增加了很多, 即消耗能量 多。 同时, 也由于固有的润滑油泵系统的维护经常出现异常, 即整体异常频率增 加。
· 另外, 现有轴扭力发动机都是单一的将燃烧能转化为轴扭力的 械能, 不 能直接将之转化成电能, 而且必须通过一段轴连接才能实现发电机的发电效果, 而使燃烧能转电能的效率更加低下。 现有专利号 021Λ3455是涉及一种滚动螺旋发动机, 包括汽缸体、 汽缸盖, 配气机构, 能量转换 构, 冷 P机构, 润滑机构; 其特征在于: 能量转换机构包 括螺旋转换机构和连续步进旋转机构: 其中, 螺旋转换机构由滚动花键付及滚动 螺旋付串行排列组成, 滚动花键付 外套、 中套、 内套、 钢球组成, 滚动螺旋付 由螺旋套、 中套、 内套、 钢球组成, 滚动花键付和滚动螺旋付的内套为一整体; 内套的一端或两端与一个或多个汽缸体内的活塞杆串接;连续步进旋转机构包括 螺旋转换机构中的两套旋向相反滚动螺旋付和输出齿轮,由两个螺旋套分别通过 离合器与输出齿轮连接; 两套螺旋付的内套为一整体, 两个螺旋套装在两个止推 轴承中间。尽管改变了曲轴连接为螺旋套结构,但是推力的活塞杆的原动力没有 改变, 而 Ji增加的部件之间依然有相对磨损, 即消耗自身能量。
现有专利号 200910206243是涉及一种转子发动机, 在发动机壳体内形成压 缩空气缓冲室、燃烧室和转子室, 空气压缩机出气口通压缩空气缓冲室经单向气 门连通燃烧室,燃烧室上连接燃料喷射装置和正时点火装置,燃烧室的喷气口连 通转子室, 转子室内安装转子, 转子由转子轴和转子叶片组成, 转子叶片同心圆 形分布上转子轴上, 转子轴安装在发动机壳体上, 转子轴上安装空气压缩机。尽 管该发明结构简单, 零件少, 制造容易, 性能稳定, 维护简单, 可以使.用多种燃 料, 但是其转子叶片与壳体间长期磨损会导致高压气体损失, 导致效率下降。而 ϋ速度越高, 磨损越大。
现有专利号 200910103789 是一种环缸转子发动机, 由转子与定子组成。转 子与定子之间的空间为环形燃烧室,转子上安装有 8个活塞 ϋ分为 2组在环形燃 烧室内做逐歩交替换位转动, 环形燃烧室被活塞分割成 8个汽缸, 运转时, 当一 组活塞前进 另一组活塞静止。 使环形燃烧室内一组汽缸容积在减小, 另一组 汽缸容积在增大。彼此间容积发生变化从而实现 4个冲程。 8个汽缸中, 对置的
2个汽缸冲程相同,膨张力是通过转子内的连接构件传递给齿轮曲轴的, 再¾齿 轮曲轴传递给输出轴从而使输出轴不断的旋转。 由于曲轴存在和齿轮传递, 就会 加大磨损, 同时轴间隙对着速度的增加, 会使气体泄漏即效率下降。
现有专利号 201020170497 是涉及一种转子发动机, 在定子内腔中设有转 子,两端固定端盖, 转子中心轴穿接在端盖上,转子上开有通槽, 内装两个叶片, 两叶片之间接有弹簧, 两叶片的外露边顶在定子内腔边沿,在两叶片的外露边上 嵌接转子密封条; 定子的内腔为两个半圆加上、 下两个直线过渡段; 在定子的下 直线过渡段上嵌接定子下密封条, 两边开有进气口和排气口; 在定子的上直线过 渡段上嵌接有定子上密封条, 两边开有连通孔和压缩气通道; 连通孔中设有控制 阀, 上口通向储气罐; 在压缩气通道中装有单向迸气阀, 上口通向储气罐; 在连 通孔旁开有火花塞孔, 内装有火花塞。 尽管该发明产品体积小, 马力大, 省油, 运转平稳, 噪音低, 但是转子中心轴穿接在端盖上, 而 ϋ这种固有嵌接转子密封 条隨着运行 间和速度的加快, 磨损加大, 即原能量泄漏加大效率下降。
现有专利号 201010245132 是-一种新型螺杆转子发动机, 其特点是在哑铃形 的壳体中有两个特制的嚷 ^形螺杆, 小头相对, 铆接在主轴上成为整体, 并与侧 面一齿轮啮合起到导流作 ffl , 四周与缸体密合缸体中部螺杆相对的空间为燃烧 室, 有火花塞和喷油嘴, 运行时, 由迸气螺杆压缩空气进入燃烧室, 油料在其中 连续燃烧并推动做功螺秆运转傲功。但齿轮连接增加摩檫损耗, 同^燃烧室的间 隙随着速度的增加会逐渐增加, 即容积能量损耗加大效率下降。 发明内容 为了弥补现有发动机技术缺陷,本发明产品技术主要依靠空心转子内部自身 燃烧能膨胀力的径向分量直接推动转子旋转, 既提高了转化效率, 同时也降低了 噪音, 提升了旋转速度, 又减少故障、 安全可靠、 维护较低、 清洗方便、 提高寿 命的特点。 其主要结构特征如下-
K 一种空心转子能量转化装置结构特征在于: 至少包括, 转子 (12) 整体呈空 心椎体状, ώ螺旋轮(1 )、前盖(2)、后盖(4)、 散热环(13)、轴头 U5) 组成的转子在两个轴承( )的支撑下固定在定子(6)上,燃料喷射装置(ι υ 固定在定子上与前盖同心对准, 螺旋轮中段内壁固定装有至少一组点火头 ( 3) , 与点火头圆周角径向对应的点火驱动装置(10) 至少一组固定在定子 上, 螺旋轮后段伸入发电装置 (5) 的空心中央, 启动电机 (9) 与启动装置 (8)同心固定在定子前段与轴头同心对准, 具有惯量的轴头在启动^与启动 装置串接启动后分离而静止 又串接, 传感器(7 )固定安装在定子上而且非 接触地靠近在转子前中后各段外围, 散热环由多个叶片组成固定在螺旋轮高 温区的外壁周围可隨转子同步转动, 辅助部件 (16 ) 固定装在定子的任意位 置。
2、 螺旋轮 (1 ) 结构特征在于: 至少包括, 一从前轮腔 (]—. 2 ) 到后轮腔 (1. 7) 腔数至少 i个且螺旋旋转角超过 2 π , 二前轮腔容积从前到后逐渐平滑变小, 而后轮腔的容积保持不变, ―三轮墙 (L 1 )从前到后连续增厚无台盼, 四从轮 前壁(L 4) 到轮后壁(L 5)逐渐加厚内部无台阶, 五轮后筋(L 6) 厚度大 于轮前筋 (1. 3) , 六点火头安装单元 (L 9) 位于螺旋轮内壁且与外壁无任 何泄露, 七点火头安装单元处是 非导磁材料密封即可使磁力线从内壁到外 壁相互完全导通, 八螺旋轮的后端侧面有 #气口 (1.8)的开孔且孔数量与轮 腔数对应, 九前轮腔和后轮腔通透, 而 ϋ轮腔数前后一一对应。
、 前盖(2) 结构特征在于: 至少包括, 一在前盖半径不同圆周上有燃料的吸入 口 (2。 2)的开口, 且与螺旋轮腔体位置和数量-一一对应, 二轮前筋座 (2.4) 轮前壁座 (2.5) 与轮前筋 (1.3) 轮前壁 (1.4) 一一对应密封固定连接, _Ξ: 在前盖半径上固定着门阀 (2.3) 和吸入口对应, ϋ其关闭面积大于吸入口
(2.2)的吸入面积, 四门阀与燃料喷射装置的喷射嘴(11.1)所在圆周半径 R和同圆周角等同, 且保持一定的轴向转动间隙距离, 五自动开关 (2.1) 固 定在前盖后面只能从外部打开而内部向外始终关闭, 六自动开关装置控制门 阀的弹力大于 i个大气压差时外部压力才可打开门阀 ,七自动开关固定在吸入 口转动方向的前方, 即从前往后轴向看转子若顺时针则自动幵关就在吸入口 的顺时针方前方处固定。
、 燃料喷射装置(11)结构特征在于:至少包括,一由外壳(1L 5)和内壳(1L 6) 组成对外密闭的内部空腔, 二在空腔里固定着的喷射嘴 (1丄 1) 一端连接燃 料混合通道(ii.4) , 另一端对着吸入口 (2.2) 的旋转方向前方边沿, 三喷 射嘴安装方位与前盖的吸入口一一对应, 四燃料输送通道 (11.2) 和高压空 气输送通道 (iL 3) 通过过滤网在内部相通, 五内壳直径大于轴头直径即转 子转动无接触无摩擦。
、 点火头 (3) 结构特征在于: 至少包括, 一感应面 (3.1) 固定在点火安装单 元 (L 9) 里, 二磁力可穿透密闭轮壁抵达感应面, 三点火线圈 (3.2) 缠绕 在内导磁体 (3.4) 上, 四电极 (3.3) 与点火线圈首尾焊接且极间有一定的 间隙可保证通电 火, 五多个点火头安装圆周角《等于 2 π除以轮腔数 n, 即 ω ~231 /η。
、 点火驱动装置 (10) 结构特征在于: 至少包括, 一驱动电缆 U0.1) —端首 尾直接与驱动线圈 αο.3) 焊接, 另一端与定子的辅助部件直接焊接, 二驱 动线圈缠绕在外导磁体 (10.2) 上, 三驱动线圈固定在非导磁环 (10.4) 外 壁上, 其圆周角 ω等于点火头安装的圆周角《, 四非导磁环与螺旋轮外壁有 一定的径向旋转间隙即保证转子转动无接触无摩擦, 但不影响磁力传递。 、 后盖 (4) 结构特征在于: 至少包括, 一轮后壁槽 (4.1) 轮后筋槽 (4.3)与 螺旋轮的轮后壁 (1.5) 和轮后筋 (1.6) —一对应密封嵌入固定, 二后盖受 力面 (4。 2) 紧固着驱动轴 (4.4) 保证与转子有同等转矩同步转动。
、 发电装置(5) 结构特征在于: 至少包括, 一转子的外部固定着发电转子材料
(5.4) , 二感应定子线圈 (5.1)和位置传感器(5.2) 围绕着发电转子材料 被包涵在发电外壳(5.3)里面, _三发电外壳固定在定子上且与转子无接触无 摩擦, 四感应定子线圈的与定子的辅助部件相连接, 即接通感应电流。
、 辅助部件 (16) 结构特征在于: 至少包括, 一用于对感应电流进行整流和逆 变的电路模块, 二固定装有蓄电瓶与逆变电路连接和用电设备连接, 三固定 着燃料喷射装置控制端口电路和点火驱动控制端□电路, 四固定在定子上的 压力传感器、 温度传感器、 转子位置传感器、 气体传感器、 吸入口传感器、 点火线圈传感器、和其它需要控制检测的传感器围绕着转子周围无接触摩檫, 五固定有 CPU控制电路模块与所有传感器、 电源、和输出控制端连接, 六固定 其它 ffl于功能扩展的辅助部件。 本发明技术除了上述的结构特征外, 还包括如下内容特点: 螺旋轮前后盖的连接和点火头的连接是相对静止固定没有磨损密封件, 在吸气压縮膨膨排气循环过程中内部高压气体是没有可能池露到外面。 所 以, 螺旋轮的轮腔吸入燃料混合物后, 压缩燃烧膨胀气体持续的径向推动做 功, 直到没有再利 ffl价值为止, 从而实现燃烧能转化率最高的效果。
2、 由于螺旋轮转动后, 前轮腔容积随着运转的进行, 必然形成相对真空, 低于一个大气压时, 吸气口的门闺自动被外部的燃料混合气体气压打幵, 即 保证燃料混合气体的快速进入, 也节约了喷油嘴的压力能耗。
3、 轴头具有一定惯量,当轮腔在最短 间 31 /2内做功,则可依靠轴头惯性持 续转动 3 π /2ίΗ'间, 即进入第二次做功。
4、 燃料喷射装置没有和转子的前盖吸入口连接, 而燃料混合气体是通过喷 射嘴的喷射和吸入口的吸入空中对接, 所以转子前轮腔的燃料不会因为喷射 阀门异常持续喷射燃料堆积过剩, 即便点火时间提前也不会引燃上行油路, 所以彻底杜绝了自燃或爆震的可能。 同 喷射驱动装置与转子是无接触无摩 擦。
5、 转子内部的点火头没有接触外部的点火驱动装置, 而是通过高频磁力穿 透轮壁感应获得点火电势能, 不会对转子转动造成任何摩擦, 同时也彻底杜 绝了明火对油道泄露引燃爆震的可能。
6、 加长螺旋轮的导程和螺旋数, 使高压气体的膨胀力得到充分释放, 直到 剩余能量无法利用后丛排气口排出, 即保证了在低速度 自行加大压缩力彻 底燃烧的效果。
7、 加大螺旋轮的直径, 相当于加大了转子的转矩, 即提高了转子的铀输出 扭力力矩。
8、 一次吸气到排气的循环最短可以在一个转子旋转一周 2 周期内完成,若 采用一个轮腔, 则一个旋转周期内气体膨胀做功 间是 同样仅需 4个 轮腔, 而且逐次完成吸气排气循环, 则膨胀力做功时间达到 2 π即一圈。
9、 轮腔数和点火 间决定螺旋轮做功脉动的频次和周期, 当增加轮腔数和 减少点火时间间隔, 则膨胀力持续傲功, 脉动随之趋近于 0。
10、 利用转子带动散热环的叶片进行散热,由于叶片与空气的摩檫力远远小 于水循环需要的克服重力的提升力和循环体内的摩檫力, 既达到无法利.用的 余热散发效果, 也达到提^整体效率的目的。 这种风力散热方式, 也排除了 冬季水冷循环系统被冻裂的可能, 同时 于启动 速度较低散热效率较低即 提高了低温环境的启动温度, 无需辅助加热而消耗能量。
1 除了前后支撑轴承固定需少量润滑油外, 无需其它特意的润滑系统,即 减少了润滑油系统引发的整机故障, 和节约了材料资源。
12、 由于排气口在静止时, 与前轮腔完全导通,所以减速或停止后会使高压 气体完全释放, 不存在尾气残留导致气道积碳自燃危险隐患。
13、 由于螺旋轮只有前后的支撑轴承在磨损, 其它部件都相对固定没有磨 损, 即噪音源只在轴承上, 所以整体运行噪音很低, 同 ^整 寿命增加。
14、 传感器包括对转子速度、轮腔温度、 喷射嘴压力、 吸入口位置、 燃油喷 射驱动装置电流、 启动电 电流、 点火驱动装置电流、 点火线圈位置、 以及 其它异常信息进行实时跟踪, 得知异常后, 立即传递给定子上的计算机 CPU 中心, 经过运算与处理给出对应的输出, 即保证了各个运行参数在既定的程 序下进行, 也减少了异常和故障的可能。
15、 通过加大螺旋轮前后直径的缩小比飼, 或增加点火头到前盖的压缩距 离, 则对低燃点燃料无需点火就可以完成燃烧膨胀, 使膨张力直接产生径向 推力做功, 这样整体结构更加简单。
16、 采用多组点火头和点火驱动装置,在不同的位置点火以适应不同的转子 速度, 可以最大的满足燃烧能的转化和释放。 即在定子上的点火驱动装置沿 螺旋轮轴向多组安装, 低速启动时, 则在距离前盖最远处点火, 当启动后进 入中速, 则在距离前盖较近处点火, 当进入高速运转时, 则在距离前盖最近 处点火。
17、 若输出轴上不加机械负载, 而 ϋ加大发电装置的功率, 那么就可以当成 燃烧能发电装置, 无需轴连接, 和无轴磨损带来的能量消耗。 同时定子线圈 和转子的能量转换, 遵循感应型发电机原理, 和直流无刷发电机原理、 高效 永磁发电机原理、 无刷励磁同步发电机原理, 即转化效率最高。
18、 由于吸入到排气整个循环通道是平滑流畅, 没有直角拐弯, 也没有齿轮 转化机构, 而 ϋ吸入后到排气口是通透, 所以不会有积碳产生。 即便长 ^间 工作, 在内壁上形成氧化薄膜, 则需要打开前后盖子, 用软偉工具进入螺旋 轮的轮腔即可清理, 即簡单方便。
19、 在启动装置里设定了转子转动正确方向的机械装置,当出现倒转时立即 刹车并锁定, 直到异常取消, 才可以再次正常启动。
^图说明 图 1 : 本发明产品结构立体示意图
注解;
i、 螺旋轮
3. 点火头
4. 后盖
5. 发电装置
6. 定子
7. 传感器
8. 启动装置
9. 启动电机
10. 点火驱动装置
1 L 燃料喷射装置
12. 转子
13. 散热环
14. 轴承
15. 轴头
16. 辅助部件
1.8、 #气口 图 2: 本发明产品轴向剖面图
注解;
1、 螺旋轮
2、 前盖
3、 点火头
4、 后盖
5、 发电装置
6、 定子
7、 传感器
8、 启动装置
9、 启动电机
10、 点火驱动装置
IU 燃料喷射装置
12、 转子
13、 散 叶环
14、 轴承
15、 轴头
16、 辅助部件
1.8、 排气口
44、 驱动轴
图 3: 本发明产品的螺旋轮轴向剖面图
注解;
1.1、 轮墙
1.2、 前轮腔
1.3、 轮前筋
14、 轮前壁
1.5、 轮后壁
16、 轮后筋
1.7、 后轮腔
1.8、 排气口
1.9、 点火头安装单元 图 4: 本发明产品的螺旋轮从小圆往大圆方向看的径向剖面图 注解:
11、 轮墙
1.2、 前轮腔
1.3、 轮前筋
1.4、 轮前壁
1.5、 轮后壁
1.6、 轮后筋 1.7、 后轮腔
1.8、 排气口
1.9、 点火头安装单元 图 5: 本发明产品的前盖后视径向剖面图
注解:
2.1、 自动开关
2。 2、 吸入口
2.3、 门阀
2.4、 轮前筋座
2.5、 轮前壁座
R、 多个吸入口围成圆周的半径 图 6: 本发明产品的燃油喷射装置径向剖面图
注解:
11. I, 喷射嘴
11。 2、 燃料输送通道
11.3、 高压空气输送通道
11.4, 燃料混合通道
11.5, 外壳
11.6、 内壳 图 7: 本发明产品的点火头结构安装径向剖面图 (内) , 和点火驱动装置结构安 装径向剖面图 (外) 的组合图
注解:
3.1、 感应面
3.2、 点火线圈
3.3、 电极
3.4、 内导磁体
10.1、 驱动电缆
10.2、 外导磁体
10.3、 驱动线圈
10.4、 非导磁 ' 图 8: 本发明产品的后盖的轴向剖面图 (左) 和前视径向剖面图 (右) 注解:
4.1、 轮后壁槽
4.2、 受力面
4.3、 轮后筋槽
4。 4、 驱动轴 图 9: 本发明产品的发电装置轴向剖面图
注解:
5.1、 感应定子线圈和发电励磁线圈 5. 2、 位置传感器
5. 3 发电外壳
5. 4、 发电转子^料
1. 1、 轮墙
1 . 5、 轮后壁 图 10: 本发明产品工作原理框图
注解:
1、 燃料控制端: 有各种阀门和连接机构能够识别和接收来自 CPU的信号指令, 并对喷射嘴进行有效的关闭和打开, 而且开关频率满足最大转子转速的需 要。
2、 螺旋轮工作: 按照真空吸入 A-瞬间压缩 B -点燃膨胀 C-废气 #出0四种状态 进行持续的循环过程。
3、 输出轴转动: 具有承载和连接负荷力矩的能力。
4、 发电机工作: 完成转子的动能向电能的转化过程, 至少包括感应和逆变两个 过程, 且遵循感应型发电机原理, 或直流无刷发电机原理、 高效永磁发电机 原理、 无刷励磁同步发电机原理任意一种过程。
5、 启动电机: 能够接收蓄电瓶电源使其转动力矩带动转子旋转起来。
6、 传感器: 对转子和定子运行的所有程参数进行确认和跟进, 包括转子转动角 度、 转子速度、 转子温度、 吸入口位置、 点火线圈位置、 排出口气压, 喷射 嘴气压、 所有驱动电流电压、 以及对转子和定子正常运行有帮助的其它参数 的探测与感应。
7、 CPU: 能够完成 i 算机的所有功能, 至少包括识别和接收传感器的所有信号, 能够进行逻辑换算和数据储存, 能够输出有效指令对所有终端进行控制。
8、 蓄电瓶: 能够吸收发电装置的电能, 同时向启动电机、 各种驱动装置、 传感 器和 CPU部件提供电源。 图 1 1 ; 本发明产品的燃料喷射驱动过程工作原理框图
注解:
6 1、 电流传感: 专用于检测门阀的输入电流的传感器。
6.2、 气体传感: 专用于检测喷射嘴的气体流出压力的传感器。
6 3、 位置传感: 专用于检测吸入口来临前的无接触检测传感器。
7、 CPU: 能够完成 if算机的所有功能, 至少包括识别和接收传感器的所有信号, 能够进行逻辑换算和数据储存, 能够输出有效指令对所有终端迸行控制。
8、 蓄电瓶: 能够吸收发电装置的电能, 同时可以向启动电机、 各种驱动装置、 传感器和 CPU部件提供电源。
10, 电流运放; 将控制信号进行运算放大至电流具有打开控制电磁阀的能力,该 电磁阀是专门用于控制喷射嘴开关。
11 , 电磁阀门: 常态闭合的电磁开关, 可满足转子最高转速的对应打开和关闭。
12、喷射嘴: 专用于燃油混合气体喷射, 出口出含有气体传感器, 且能承受高压 气体的冲击的喷射。
13、 吸入口: 转子的前盖半径处, 并含有位置传感器的检测感应点。 图 12; 本发明产品的点火驱动过程工作原理框图 注解;
6.4、 位置传感: 专用于检测点火线圈来临前的无接触检测传感器。
6.5、 电流传感: 专用于高频线圈电流的检测传感器。
7、 CPU: 能够完成计'算机的所有功能, 至少包括识别和接收传感器的所有信号, 能够进行逻辑换算和数据储存, 能够输出有效指令对所有终端进行控制。
8、 蓄电瓶: 能够吸收发电装置的电能, 同时可以向启动电 、 各种驱动装置、 传感器和 CPU部件提供电源。
14、 逆变转化电路: 将直流电源转化成交流高频的电路。
15、 高频线圈: 能够将高频交流电转成磁力并有一定的方向。
16、 感应线圈; 能够感应磁力并在线圈的出头位形成电动势。
17、 电极放电: 在异性电荷累计后自动电流放电。
具体实施方式 下面结合^图对实施本发明型产品的进一步说明。 依照附图所示, 辅助部件 U6) 的蓄电瓶电源开通使启动电机 (9) 启动, 接着启动装置 (8) 带动转子 (12 ) 开始转动, 螺旋轮 (1 ) 也跟着同歩转动。当 螺旋轮被转动后, 由于前盖 (2)密闭, 所以前轮腔 (L 2)在螺旋推力下, 形成 相对真空。 当真空压差大于 1个大气压时, 即前盖的门阀 (2. 3) 被外部喷射嘴
( I I. 1 ) 的喷射气体压力 开, 燃料混合气体通过吸入口 (2. 2) 喷入前轮腔。 螺旋轮被继续带动转动,燃料混合气体从前段被压缩至中段达到一定的压力和温 度, 此刻点火头 (3)按照 CPU设定好的运算程序即刻点火引燃, 即前轮腔瞬间产 生膨胀力, 于轮墙 (1. 1 ) 在外力带动作用下一直旋转, 此时膨胀力加大了原 方向的轮墙推力, 尽管也有部分反方向的膨胀力, 但反方向的前盖门阀关闭,于 是膨胀的高压气体只能按照原来方向继续前进,而旦膨胀力随着向螺旋轮后段移 动过程中, 径向推力持续做功, 直到不能再利用即从排气口 U. 8) 排出。 当轮 墙得到膨胀力转化的径向推力后, 即径向转动的速度瞬间增加, 带动具有惯量的 轴头继续转动, 于是前轮腔的真空第二次形成, 且真空度增加了很多, 此时喷油 嘴按照定子上 CPU设定好的运算程序瞬间将燃料混合气体第二次喷入吸入口。 依 次循环,螺旋轮转动起来,从而带动整个转子转动起来。此时, 由于启动装置(8) 具有自动分离作用, 转子自行转动后, 启动电机便自动来开转子而停止转动。同 时转子转动后, 其后段的发电转子材料 (5. 4) 在发电装置里, 依照右手定律使 周围的感应定子线圈 (5. 1 ) 产生感应电流, 该电流在定子的辅助部件 (16) 整 流作用下, 对蓄电瓶充电保存。 喷射驱动控制端口放大喷射容量, 则燃料混合气 体膨胀力做功加强, 转子转速提升。 当喷射容量为 0时, 則螺旋轮的后盖无法吸 入燃料混合气体, 即转子自行停止。转子停止运转后轴头与启动装置串接等待下 )启动。
螺旋轮转动过程由 cp †算机处理完成, 如附图 io原理框图所示, 蓄电瓶电 源开关接通后, 启动电机得到指令带动转子开始转动, 同时靠近转子的位置传感 器检测到转子正确位置后, 则将该信号传递给 CPU, CPU再经过其它信号数据分析 处理后发出指令给燃料喷射驱动装置的燃料控制端,使喷射嘴打开对准转子吸入 □射入燃料混合气体。同时 CPU对转子位置传感器提供的信号进行运算和分析后, 发出指令给点火驱动装置点火控制端开始点火。 当转子速度增加到一定程度后,
CPU通过速度传感器, 确认螺旋轮已经开始启动,各个传感器进入实时监测状态。 在启动过程中, 启动电机若发生异常, 則启动电机的传感器反馈该信号给 CPI], CPU经过运算和分析后必要关闭启动电机, 待故障排除后, 再次启动。 转子正常 运转过程中, 当排气口的气体传感器检测到废气异常后, 将该信号传递给 CPI], CPU经过运算和分析发出指令给相关的输出控制端, 进行相应的调整, 以保证最 佳的运行状态。
燃料喷射驱动过程由 CPU计算机处理完成, 如 ^图 l i原理框图所示, 蓄电瓶 电源开关接通后,靠近吸入口的传感器检测到转子吸入口到来, 则将该信号传递 给 CPU, CPU再经过其它信号数据分析处理后发出指令给电流运放电路, 使放大后 的电流进入常闭态的高频电磁阀门, 高频电磁阀门被打幵后, 喷射嘴对准吸入口 喷射燃料混合气体。若在高频电磁阀门出现异常, 则立即由 it近的电流传感器将 信号传递给 CPU, CPU对该信息立即进行运算和处理必要时发出指令给电流运放停 止输出, 待故障排除后恢复正常。
点火驱动过程由 CPU计算 处理完成, 如 图 12原理框图所示, 蓄电瓶电源 开关接通后,靠近转子的点火线圈传感器检测到转子点火线圈到来时, 则将该信 号传递给 CPU, CPU再经过与其它信号数据分析处理后发出指令给逆变转化电路, 使直流转化成高频的交流进入高频线圈,高频线圈产生的磁场透过非导磁材料进 入感应线圈的感应面, 感应线圈得到磁场即产生感生电动势, 当电势在电极端积 累后立即电离放电, 即点燃燃料混合气体。 若在逆变电路输出端出现异常, 则立 即由 '近的电流传感器将信号传递给 CPU , CPU接到该信息立即进行运算和处理必 要 发出指令给逆变电路前段停止输出, 待故障排除后恢复正常。
燃料混合气偉循环在一个轮腔里完成, 并分四个状态, 即真空吸入 A、 瞬间 压缩 B、 点燃膨胀 (:、 废气排出0。 但采用一个轮腔时, 四个状态必须至少在螺旋 -个圆周角 2 π内完成, ϋ膨胀^间必须大于 后再进入后轮腔, 否则能量会 提前散失。
螺旋轮的螺旋极角 Θ大小是反应螺旋轮导程不变情况下螺旋的数量和螺旋 线长的长度。若螺旋直径 一定, 则 Θ越大, 螺旋数量越少螺旋线约短, 反之数 量越多线越长。即当 Θ增加^膨胀力在径向的余弦分量减少, 轴向的正弦分量在 增加, 反之径向力增加轴向力减少。但是膨胀气体与腔体内壁的实际摩擦力随着 螺旋线的加长而在增加, 所以 9 =45度^近是有效做功最高的理论角度。
若转子的转速要求较高, 则这四个循环状态最少在一个螺旋圆周 2 ^内完成, 即膨胀力做功一次转动一圈。 在转子要求低速时, 由于压缩程度较低压力不足, 所以必须采取加长螺旋轮导程来实现增加压縮力, 即从 Α状态到 Β状态, 需要转子 转动 n圈后再点燃。 为此, 当在低速场合使用, 可采取长导程的驱动力, 高速场 合可采用短导程的驱动力,最低导程长度等于螺旋轮的直径即可满足一般转子转 速要求, 否则导程很短对应转速极高, 对一般的使用工况将失去意义。
由于多组轴向点火头和点火驱动装置, 可在不同的位置点火以适应不同的转 子速度需要, 以最大的满足燃烧能的转化和释放。即可在定子上的点火驱动装置 沿螺旋轮轴向多组安装,低速启动时在距离前盖最远处点火,当启动进入中速后, 在距离前盖较近处点火, 当进入高速运转时, 则在距离前盖最近处点火。 为了提高转子的动能, 可以在螺旋轮径向增加多个轮腔, 即增加膨张力有效 做功强度,同时也要增加相应的吸入口、燃料喷射装置、点火头和点火驱动装置。 但为了保证转速的平衡性, 需要轮腔个数采取偶数成对出现。
为了减少转子的脉动, 可以将多个轮腔的四状态循环逐次进行, 点火依次进 行即做功的脉动幅度下降, 脉动周期缩短, 脉动频率增加, 对输出和周边的干扰 减少。
为了提高低速的能量转化效率, 可以适当的加长螺旋轮导程, 使燃烧后的膨 胀力径向分量持续做功, 直到没有利用价值后再从棑气口排出。 同时, 采用多轮 腔和逐次点火方式, 使一个轮腔先燃烧将温度通过轮墙传递给下一个轮腔温度, 这样也保证了压缩的 间足够长,而且温度上升快,即膨胀力有效做功周期更长 从而提高了转化效率。
为了适应不同燃料在不同的环境的正常使用, 可以改变散热环尺寸或衬质。 当环境温度较低而旦燃料的热当量偏低, 则散热环的叶 i†数减少直径减少, 反之 叶片 ·数增加直径增加, 这样以减少因散热过大导致的启动困难和燃烧能的损失。 若环境长期处在低于常温下, 可以取消散热环,利用转子外壁自行和空气摩檫散 热。 若环境长期处在高于常温下, 可釆用超导材料制作散热环, 并且叶片数量和 直径足够大。
转子经过长时间工作后, 在螺旋轮内壁上可能会形成氧化薄膜, 该薄膜加厚 则会使气体通道变窄而影响做功, 则需要停车打开前盖和后盖, 用软体工具进入 螺旋轮的轮腔清理, 即简单方便。
由于转子转动的方向由螺旋轮的轮墙转角方向决定, 即 前盖到后盖高压气 体做功的方向被确定, 所以不允许工作过程转子倒转, 否则会对前盖造成冲击 即在启动装置里设定了转子转动正确方向的机械装置,当倒转时启动装置立即刹 车并锁定, 直到异常取消, 才可以再次正常启动。
在体积受限的超低速工况下,采用立式安装,即螺旋轮的前盖朝上后盖超下。 燃料混合气体被吸入前轮腔后, 由于受到自身重力朝下的作 )¾ , 压缩过程在低速 向下压缩效率自然增加, 同时也使膨胀的高压气体逆向做功减少, 即膨胀力有效 做功强度增加, 即效率得到提升。 在此已经涉及到的和未来涉及到本发明产品的各种应用, 其改进、接近或类 似装置, 则视为与本发明雷同。也包括联想到类似结构和不同用途而产生的其它 结构产品, 则也视为与本发明雷同。

Claims

、 一种空心转子能量转化装置结构特征在于: 至少包括, 转子 (12) 整体呈空心椎体状, 由螺旋轮 (i) 、 前盖 (2) 、 后盖 (4) 、 散热环 (13) 、 轴头 (15) 组成的转子在两 个轴承 (14) 的支撑下固定在定子 (6) 上, 燃料喷射装置 (11) 固定在定子上与前盖 同心对准, 螺旋轮中段内壁固定装有至少一组点火头 (3) , 与点火头圆周角径向对应 的点火驱动装置 αο)至少一组固定在定子上, 螺旋轮后段伸入发电装置 (5) 的空心 中央, 启动电机 (9) 与启动装置 (8) 同心固定在定子前段与轴头同心对准, 具有惯量 的轴头在启动时与启动装置串接启动后分离而静止时又串接, 传感器 (7) 固定安装在 定子上而且非接触地靠近在转子前中后各段外围, 散热环由多个叶片组成固定在螺旋轮 高温区的外壁周围可随转子同步转动, 辅助部件 (16) 固定装在定子的任意位置。 、 根据权利 1所述的一种空心转子能量转化装置中的螺旋轮 α) , 其结构特征在于: 至少 包括, 一从前轮腔 (1.2) 到后轮腔 (1.7) 腔数至少 i个且螺旋旋转角超过 2 π, 二前轮 腔容积从前到后逐渐平滑变小, 而后轮腔的容积保持不变, ―三轮墙 (1.1) 前到后连 续增厚无台阶,四从轮前壁 (丄 4)到轮后壁(1.5)逐渐加厚内部无台阶,五轮后筋(1。 6) 厚度大于轮前筋 (1.3) , 六点火头安装单元(L9) 位于螺旋轮内壁且与外壁无任何泄 露, 七点火头安装单元处是由 导磁材料密封即可使磁力线从内壁到外壁相互完全导 通, 八螺旋轮的后端侧面有排气口 (L8) 的开孔且孔数量与轮腔数对应, 九前轮腔和 后轮腔通透, 而且轮腔数前后一一对应。
、 根据权利 1所述的一种空心转子能量转化装置中的前盖 (2) 结构特征在于: 至少包括, 一在前盖半径不同圆周上有燃料的吸入□ (2.2) 的开口, 且与螺旋轮腔体位置和数量 一一对应, 二轮前筋座 (2.4) 轮前壁座 (2.5) 与轮前筋 (L3) 轮前壁 (1.4) 一一对 应密封固定连接, ―三在前盖半径上固定着门阀 (2.3) 和吸入口对应, ϋ其关闭面积大 于吸入口 (2.2) 的吸入面积, 四门阀与燃料喷射装置的喷射嘴 (ii.l) 所在圆周半径 R 和同圆周角等同, ϋ保持一定的轴向转动间隙距离, 五自动开关 (2.1) 固定在前盖后 面只能从外部打开而内部向外始终关闭, 六自动开关装置关闭门阀的弹力至少支撑大于 1个大气压差时外部压力才可打开门阀, 七自动开关固定在吸入口转动方向的前方, 即 从前往后轴向看转子若顺^针则自动开关就在吸入□的顺时针方向前方处固定。
、 根据权利 1所述的一种空心转子能量转化装置中的燃料喷射装置 (U) , 其结构特征在 于: 至少包括, 一由外壳 (11.5) 和内壳 (11.6)组成对外密闭的内部空腔, 二在空腔 里固定着的喷射嘴 (1丄 1) 一端连接燃料混合通道 (ii.4) , 另一端对着吸入口 (2。 2) 的旋转方向前方边沿, :三喷射嘴安装方位与前盖的吸入口一一对应, 四燃料输送通道
(11.2)和高压空气输送通道 (11.3) 通过过滤网在内部相通, 五内壳直径大于轴头直 径即转子转动无接触无摩擦。
、 根据权利 1所述的一种空心转子能量转化装置中的点火头 (3) , 其结构特征在于: 至少 包括, 一感应面 (3。 i) 固定在点火安装单元 (L9) 里, 二磁力可穿透密闭轮壁抵达感 应面, :三点火线圈 (3.2) 缠绕在内导磁体 (3.4) 上, 四电极 (3.3) 与点火线圈首尾 焊接且极间有一定的间隙可保证通电打火, 五多个点火头安装圆周角《等于 2 π除以轮 腔数 η, 即 ω=2κ/η。
、 根据权利 1所述的一种空心转子能量转化装置中的点火驱动装置 (10) , 其结构特征在 于: 至少包括, 一驱动电缆 (1(11) 一端首尾直接与驱动线圈 (10.3)焊接, 另一端与 定子的辅助部件直接焊接, 二驱动线圈缠绕在外导磁体 (10.2) 上, Ξ:驱动线圈固定在 非导磁环 U0.4) 外壁上, 其圆周角 ω等于点火头安装的圆周角 ω, 四非导磁环与螺旋 轮外壁有一定的径向旋转间隙即保证转子转动无接触无摩擦, 但不影响磁力传递。 、 根据权利 1所述的一种空心转子能量转化装置中的后盖 (4) , 其结构特征在于: 至少包 括, 一轮后壁槽 (4.1) 轮后筋槽 (4.3) 与螺旋轮的轮后壁 (1.5) 和轮后筋 (1.6)— 一对应密封嵌入固定, 二后盖受力面 (4.2) 紧固着驱动轴 (4.4) 保证与转子有同等转 矩同歩转动。 、 根据权利 1所述的一种空心转子能量转化装置中的发电装置 (5) , 其结构特征在于: 至 少包括, 一转子的外部固定围绕着发电转子材料 (5. 4) , 二感应定子线圈 (5. 1 )和位 置传感器(5. 2) 围绕着发电转子材料被包涵在发电外壳 (5. 3)里面, 发电外壳固定 在定子上且与转子无接触无摩擦, 四感应定子线圈的与定子的辅助部件相连接, 即接通 感应电流。
、 根据权利 1所述的一种空心转子能量转化装置中的辅助部件 (16 ) , 其结构特征在于: 至少包括, 一固定装着用于对感应电流进行整流和逆变的电路模块, 二固定装有蓄电瓶 与逆变电路连接和用电设备连接, ≡固定着燃料喷射装置和控制端口电路以及点火驱动 装置和控制端口电路, 四固定在定子上的压力传感器、 温度传感器、 转子位置传感器、 气体传感器、 吸入口传感器、 点火线圈传感器、 和其它需要控制检测的传感器围绕着转 子周围无接触摩擦, 五固定有 CPU控制电路模块与所有传感器、 电源、 和输出控制端连 接, 六固定其它用于功能扩展的辅助部件。
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