CN112879159B - Internal combustion engine with Tesla valve structure - Google Patents

Internal combustion engine with Tesla valve structure Download PDF

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Publication number
CN112879159B
CN112879159B CN202110229198.0A CN202110229198A CN112879159B CN 112879159 B CN112879159 B CN 112879159B CN 202110229198 A CN202110229198 A CN 202110229198A CN 112879159 B CN112879159 B CN 112879159B
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stator
tesla valve
rotor
tesla
internal combustion
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CN112879159A (en
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江晓东
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    • 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
    • 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
    • F01D1/36Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector

Abstract

Compared with the traditional internal combustion engine, the internal combustion engine has smaller volume, fewer parts, lower manufacturing and operating maintenance cost, reduced energy consumption, simple mechanical structure, lower manufacturing cost and maintenance cost and more energy conservation. The invention comprises a stator and a rotor, and is characterized in that the stator is in a disc cover body structure, the outer wall of the opening end of the stator is provided with a first Tesla valve channel extending from the inner side wall of the stator to the sealing end of the stator, the top end of the stator is provided with a combustion chamber and a sparking hole communicated with the first Tesla valve channel, the sparking hole is provided with a spark plug in a matching way, the stator is also provided with an exhaust port communicated with the first Tesla valve channel, and the sealing end of the stator is provided with a first connecting hole.

Description

Internal combustion engine with Tesla valve structure
Technical Field
The invention belongs to the technical field of internal combustion engines, and particularly relates to an internal combustion engine with a Tesla valve structure.
Background
An internal combustion engine is a common power supply device, and the currently popular internal combustion engine is a standard reciprocating four-stroke internal combustion engine or a gas turbine. The four-stroke internal combustion engine has to convert the reciprocating motion into the circular motion through a crankshaft, and has a complicated mechanical structure because the four-stroke internal combustion engine also needs to be provided with a gas inlet mechanism, a gas outlet mechanism and the like. The gas turbine requires a large volume of multi-stage blade driving and special manufacturing materials, and is very high in cost. Therefore, there is a need for a new energy-saving internal combustion engine that can replace the conventional internal combustion engine, and can bring lower manufacturing cost and maintenance cost with smaller volume, lighter weight and fewer parts, and can run smoothly and reduce energy consumption.
Disclosure of Invention
Aiming at the problems, the invention makes up the defects of the prior art and provides an internal combustion engine with a Tesla valve structure; compared with the traditional internal combustion engine, the internal combustion engine has smaller volume, fewer parts, lower manufacturing and operating maintenance cost, energy consumption reduction, simple mechanical structure, lower manufacturing cost and maintenance cost and more energy conservation.
In order to achieve the purpose, the invention adopts the following technical scheme.
The invention provides a tesla valve structure internal combustion engine which comprises a stator and a rotor and is characterized in that the stator is of a disc cover body structure, the outer wall of the opening end of the stator is provided with a first tesla valve channel extending from the inner side wall of the stator to the sealing end of the stator, the top end of the stator is provided with a combustion chamber and a sparking hole communicated with the first tesla valve channel, the sparking hole is provided with a spark plug in a matching manner, the stator is also provided with an exhaust port communicated with the first tesla valve channel, the sealing end of the stator is provided with a first connecting hole, the rotor is of a disc cover body structure, the sealing end of the rotor is provided with a second connecting hole, the stator is connected in a groove of the stator in a relatively rotating manner through a central shaft penetrating through the first connecting hole and the second connecting hole, the outer wall of the opening end of the rotor is provided with a second connecting hole extending from the outer side wall of the rotor to the sealing end of the rotor The tesla valve passage, first tesla valve passage with the second tesla valve passage is the same half tesla valve structure but the circumference direction of arranging is opposite, the open end detachably of stator is connected with the turbine lid, be provided with central air inlet on the turbine lid, the inboard cooperation of turbine lid is provided with the tesla valve ring, be provided with on the tesla valve ring with the valve ring gas outlet of combustion chamber UNICOM, still be provided with the valve ring air inlet on the tesla valve ring the valve ring gas outlet with be provided with tesla valve structure groove between the valve ring air inlet.
Furthermore, a bearing seat is arranged on the outer side of the sealing end of the stator, the central shaft penetrates through a bearing in the bearing seat, and the central shaft is fixed on the rotor through a shaft head nut.
Furthermore, a key groove is formed in the second connecting hole, and a key block is arranged at the corresponding position of the central shaft in a matched mode.
Furthermore, a sealing groove is formed in the rotor at the position of a friction pair with the stator, and a sealing ring is arranged in the sealing groove.
Furthermore, the sealing end of the rotor is provided with turbine blades which are circumferentially arranged.
Further, the forward direction of the Tesla structure groove is consistent with the rotation direction of the rotor.
Furthermore, the sealing end of the stator is provided with heat dissipation holes which are circumferentially arranged, the bottom of the sealing end of the stator is also provided with a lubricating oil inlet, and the lubricating oil inlet is communicated with the inside of the stator through a lubricating channel arranged inside the stator.
Further, the turbine cover is connected with the Tesla valve ring in an interference fit mode.
Further, the lower end of the stator is connected with a base, and a base threaded hole is formed in the base.
Furthermore, the opening end of the stator and the turbine cover are provided with corresponding buckling threaded holes, and the stator and the turbine cover penetrate through the bolts to be detachably connected with each other through the buckling threaded holes.
The invention has the beneficial effects.
The invention has the advantages of smaller volume, fewer parts and lower manufacturing and operation maintenance cost compared with the traditional four-stroke internal combustion engine because the valve mechanism is omitted and the connecting rod crankshaft part is not arranged. Compared with a gas turbine, the structure of the Tesla valve with the reverse annular arrangement ensures higher output power and fuel efficiency and more stable power output under the condition of a primary rotor. Through the Tesla one-way valve characteristic, the high-pressure gas in the combustion chamber is ensured not to flow back, an air inlet valve is replaced, and the energy consumption is reduced. And a torque difference is formed through a Tesla valve structure on a relative motion surface of the stator and the rotor, so that the rotor is driven to rotate. The crankshaft structure is not needed, the mechanical structure is simple, the manufacturing cost and the maintenance cost are lower, and more energy is saved.
Drawings
In order to make the technical problems, technical solutions and advantageous effects solved by the present invention more clearly apparent, the present invention is further described in detail below with reference to the accompanying drawings and the detailed description. It should be understood that the detailed description and specific examples, while indicating the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
FIG. 1 is a schematic side, half-section elevational view of the present invention.
Fig. 2 is a schematic side view in half section of the present invention.
Fig. 3 is an enlarged schematic view of the invention at a in fig. 2.
Fig. 4 is another side elevational schematic view of the present invention.
Fig. 5 is a schematic view of the stator and base of the present invention.
Fig. 6 is a schematic view of one side of a rotor of the present invention.
Fig. 7 is a schematic view of the other side of the rotor of the present invention.
Fig. 8 is a schematic view of a tesla valve ring of the present invention.
FIG. 9 is a schematic view of a turbine cover of the present invention.
Figure 10 is a cross-sectional view of another aspect of the present invention.
Fig. 11 is a schematic view of the movement and forces of the stator and rotor at the point of ignition and detonation of the present invention.
The labels in the figure are: the structure comprises a stator 1, a rotor 2, a first Tesla valve channel 3, a combustion chamber 4, a firing hole 5, a spark plug 6, an exhaust port 7, a first connecting hole 8, a second connecting hole 9, a central shaft 10, a second Tesla valve channel 11, a turbine cover 12, a central air inlet 13, a Tesla valve ring 14, a valve ring air outlet 15, a valve ring air inlet 16, a Tesla valve structure groove 17, a bearing seat 18, a spindle head nut 19, a key groove 20, a key block 21, a sealing groove 22, a sealing ring 23, a turbine fan blade 24, a heat dissipation hole 25, a lubricating oil inlet 26, a base 27, a base threaded hole 28, a lubricating channel 29 and a threaded fastening hole 30.
Detailed Description
As shown in the attached drawings, the present embodiment includes a stator 1 and a rotor 2, the stator 1 is a disk cover structure, the outer wall of the opening end of the stator 1 is provided with a first tesla valve channel 3 extending from the inner side wall of the stator 1 to the sealing end of the stator 1, the first tesla valve channel 3 is characterized in that a complete tesla valve structure is split by a central line and is uniformly distributed along the circumference by 360 degrees, the gas flow island in the first tesla valve channel 3 can also be effectively connected with the sealing end of the stator 1 and keeps the gas flow island relatively fixed.
The top of stator 1 is provided with combustion chamber 4 and the hole of striking sparks 5 with first tesla valve passageway 3 UNICOM, and the hole of striking sparks 5 department cooperation is provided with spark plug 6, still is provided with the gas vent 7 with first tesla valve passageway 3 UNICOM on the stator 1, strikes sparks through spark plug 6 and ignites the oil gas mixture who enters into the compression in the combustion chamber 4, and the oil gas after lighting can wind first tesla valve passageway 3 and second tesla valve passageway 11 and move to gas vent 7 and exhaust.
The end of sealing of stator 1 is provided with first connecting hole 8, and rotor 2 is the structure of the dish lid, and the end of sealing of rotor 2 is provided with second connecting hole 9, and stator 1 can connect in the recess of stator 1 relatively rotatoryly through the center pin 10 that passes first connecting hole 8 and second connecting hole 9, and second connecting hole 9 just and the external diameter cooperation of center pin 10. A bearing seat 18 is arranged on the outer side of the sealing end of the stator 1, the central shaft 10 penetrates through a bearing in the bearing seat 18 to ensure that the stator 1 and the rotor 2 move concentrically and fix the geometric relationship of the two parts, and the central shaft 10 is fixed on the rotor 2 through a shaft head nut 19.
The outer wall of the opening end of the rotor 2 is provided with a second tesla valve channel 11 which extends to the sealing end of the rotor 2 through the outer side wall of the rotor 2, the first tesla valve channel 3 and the second tesla valve channel 11 are of the same half tesla valve structure but are arranged in opposite circumferential directions, one is in a clockwise direction, and the other is in a counterclockwise direction. The rotation direction of the rotor 2 during working depends on the direction interchange of the tesla valve structures of the stator 1 and the rotor 2 (the direction of the tesla valve refers to that when fluid moves in the tesla valve, the direction with small resistance is forward, the direction with large resistance is reverse, and the period of the tesla valve is the minimum structure size of the same geometrical structure repeated. After the stator 1 and the rotor 2 are mounted together, a rotational gap of 0.2-0.5mm is left between the two in the relative rotational section.
The second connecting hole 9 is provided with a key groove 20, and a key block 21 is arranged at the corresponding position of the central shaft 10 in a matching way, so that the rotor 2 and the central shaft 10 can not rotate mutually, and simultaneously rotate and output circular motion torque.
The closed end of the rotor 2 is provided with circumferentially arranged turbine blades 24, which turbine blades 24 are rotated in synchronism when the rotor 2 is rotated.
A sealing groove 22 is arranged on the rotor 2 at the friction pair with the stator 1, and a sealing ring 23 is arranged in the sealing groove 22 to ensure that high-temperature and high-pressure gas in the combustion chamber 4 is not leaked.
All be provided with lock screw hole 30 on stator 1's the opening end and the turbine lid 12, stator 1 and turbine lid 12 pass lock screw hole 30 through the screw rod and can dismantle the connection, and stator 1 and the part of turbine lid 12 inlaying scribble sealed glue, prevent that the gas of burning from leaking. The turbine cover 12 is provided with a center intake port 13, and the external oil-gas mixture enters the internal combustion engine through the center intake port 13.
The inner side of the turbine cover 12 is provided with a tesla valve ring 14 in an interference fit connection mode, compressed oil-gas mixed gas can only flow in a channel specific to a tesla valve structure, the tesla valve ring 14 is provided with a valve ring gas outlet 15 communicated with the combustion chamber 4, the tesla valve ring 14 is further provided with a valve ring gas inlet 16, a tesla valve structure groove 17 is formed between the valve ring gas outlet 15 and the valve ring gas inlet 16, and when the rotor 2 rotates, the turbine fan blades 24 on the rotor 2 guide the oil-gas mixed gas into the tesla valve structure groove 17 of the tesla valve ring 14 through the valve ring gas inlet 16 and finally send the oil-gas mixed gas into the combustion chamber 4 from the valve ring gas outlet 15.
The circumferential direction of the tesla-structure groove coincides with the rotational direction of the rotor 2, so that the tesla valve ring 14 functions as an intake check valve. When the rotor 2 rotates, the turbine blades 24 on the rotor 2 guide the air-fuel mixture through the air inlet opening into the tesla valve ring 14 and finally into the combustion chamber 4 on the stator 1.
The sealing end of the stator 1 is provided with heat dissipation holes 25 which are circumferentially arranged, so that heat dissipation during working is facilitated.
The main lubrication surface is the relative movement of the friction pair between the rotor 2 and the stator 1. There is not mechanical friction between stator 1 and rotor 2, and the movement clearance that it formed is sealed by sealing ring 23, and similar to the piston ring in traditional internal-combustion engine, in order to increase the wear resistance of sealing ring 23, stator 1's sealing end bottom still is provided with lubricating oil inlet 26, and lubricating oil inlet 26 communicates with stator 1's inside through the lubricated passageway 29 that sets up in stator 1 inside, guarantees that machine oil can reach required position, and lubricated passageway 29 can guarantee the little and incessant supply of machine oil.
The lower end of the stator 1 is connected with a base 27, a base threaded hole 28 is formed in the base 27, and the stator can be fixed on a proper tool frame through the base 27.
As an internal combustion engine, the external attachment of the present invention further includes: starting a motor and a storage battery, a spark plug 6 ignition control device and the like. These devices are not essential to the use of conventional internal combustion engines and are not in the subject of the present patent, and are therefore not listed and discussed. In discussing the principles of operation of the present invention, however, it has been assumed that the devices described above are present and operating properly. If necessary, the device of the invention also considers the water-cooling pump and the heat exchanger thereof.
The invention relates to the working principle.
The turbine blades 24 are driven by the external starter to start circular motion with the rotor 2. This process also presses the mixture in the turbine cover 12 through the passages of the tesla valve ring 14 into the combustion chamber 4 of the stator 1 and continuously sucks the mixture from the outside through the central inlet 13 of the turbine cover 12.
When the oil-gas mixture reaches the combustion chamber 4, the spark plug 6 can discharge and ignite at a proper moment, and the gas is deflagrated to form high-pressure gas. Due to the one-way conduction function of the tesla valve ring 14, the high-pressure gas cannot flow back from the gas inlet and can only flow along the circumferential direction between the stator 1 and the rotor 2 through the tesla valve channels reserved on the stator 1 and the rotor 2.
As shown in fig. 11, after a tesla valve strip is divided into two parts, one of the two parts is turned 180 ° and replaced again, a new tesla valve with opposite directions is formed, i.e. the new tesla valve is formed by the first tesla valve channel 3 and the second tesla valve channel 11. In this new tesla valve, the upper and lower halves oppose each other in resistance to flow through the tesla valve.
In the vicinity of the combustion chamber 4, the flowing gas is not directional. However, because the stator 1 and the rotor 2 are of the novel tesla valve structure with opposite directions on both sides of the rotating gap (in the figure, the stator 1 is counterclockwise, and the rotor 2 is clockwise), the stator 1 can provide counterclockwise resistance to the airflow in the airflow flowing process, so that the airflow flows slowly along the clockwise direction, and even stops completely. Similarly, a counter-clockwise moving air stream will encounter a clockwise resistance on the rotor 2. However, since the rotor 2 can make a circular motion relative to the combustion chamber 4, the resistance exerted on the air flow by the rotor 2 becomes a moment that the air flow pushes the rotor 2 to rotate, and the rotor 2 is forced to make a counterclockwise rotation. Once the rotor 2 has been brought into a counter-clockwise rotation, all the air flow against the direction of rotation of the rotor 2 is almost equivalent to no resistance (viscous resistance) with respect to the rotation of the rotor 2. While all the counter-clockwise rotating gas flow lines can also have little resistance for the stator 1. The end result is that the exploding high pressure gas acts on the tesla valve passages of the stator 1 and rotor 2, respectively, creating a torque which forces the rotor 2 to rotate relative to the stator 1, i.e. as shown, the stator 1 (upper half) is subjected to a right force F1 and the rotor 2 (lower half) is subjected to a left force F2, which forces the upper and lower parts to move relative to each other, depending on the unidirectional conductance nature of the tesla valve. If this structure is distributed over a 360 deg. circumference, a relative rotational movement is generated.
In fact, the air flow moving against the direction of the rotor 2 also forms a great resistance to movement due to the viscous effect of the surface of the rotor 2 on the air flow. In the small circumferential direction from the combustion chamber 4 to the exhaust port 7, the combined force of the airflow obstruction of the reverse tesla valve on the stator 1 and the high-speed viscous action of the rotor 2 forces the airflow to hardly reach the exhaust port 7 in the clockwise direction, and the distance is 6-8 times the periodic arrangement of the single tesla valve bodies. Thus, 80% of the high-pressure gas exploded in all the combustion chambers 4 reaches the exhaust port 7 from the large circumferential direction counterclockwise (in the direction synchronized with the rotor 2), and the maximum thermal efficiency is satisfied.
It should be understood that the detailed description of the present invention is only for illustrating the present invention and is not limited by the technical solutions described in the embodiments of the present invention, and those skilled in the art should understand that the present invention can be modified or substituted equally to achieve the same technical effects; as long as the use requirements are met, the method is within the protection scope of the invention.

Claims (10)

1. The internal combustion engine with the Tesla valve structure comprises a stator (1) and a rotor (2), and is characterized in that the stator (1) is of a disc cover body structure, the outer wall of the opening end of the stator (1) is provided with a way, the inner side wall of the stator (1) extends to a first Tesla valve channel (3) of the sealing end of the stator (1), the top end of the stator (1) is provided with a combustion chamber (4) communicated with the first Tesla valve channel (3) and a sparking hole (5), the sparking hole (5) is provided with a spark plug (6) in a matching manner, the stator (1) is further provided with an exhaust port (7) communicated with the first Tesla valve channel (3), the sealing end of the stator (1) is provided with a first connecting hole (8), the rotor (2) is of a disc cover body structure, the sealing end of the rotor (2) is provided with a second connecting hole (9), the stator (1) is connected in a groove of the stator (1) in a relatively rotatable manner through a central shaft (10) penetrating through the first connecting hole (8) and the second connecting hole (9), the outer wall of the opening end of the rotor (2) is provided with a way, the outer wall of the rotor (2) extends to a second Tesla valve channel (11) at the sealing end of the rotor (2), the first Tesla valve channel (3) and the second Tesla valve channel (11) are of the same half Tesla valve structure but are opposite in circumferential arrangement direction, the opening end of the stator (1) is detachably connected with a turbine cover (12), a central air inlet (13) is arranged on the turbine cover (12), a Tesla valve ring (14) is arranged on the inner side of the turbine cover (12) in a matched manner, a valve ring air outlet (15) communicated with the combustion chamber (4) is arranged on the Tesla valve ring (14), the Tesla valve ring (14) is also provided with a valve ring air inlet (16), and a Tesla valve structure groove (17) is arranged between the valve ring air outlet (15) and the valve ring air inlet (16).
2. A tesla valve construction internal combustion engine according to claim 1, characterised in that a bearing seat (18) is provided outside the closed end of the stator (1), the central shaft (10) passing through a bearing in the bearing seat (18), the central shaft (10) being fixed to the rotor (2) by means of a spindle nose nut (19).
3. A internal combustion engine with tesla valve structure according to claim 1, characterized in that the second connecting hole (9) is provided with a key slot (20), and the central shaft (10) is provided with a key block (21) at a corresponding position.
4. A tesla-valve-structured internal combustion engine according to claim 1, characterized in that the rotor (2) is provided with a sealing groove (22) at the friction pair with the stator (1), the sealing groove (22) being provided with a sealing ring (23).
5. A engine according to claim 1, wherein the closed end of the rotor (2) is provided with circumferentially arranged turbine blades (24).
6. A tesla valve configuration internal combustion engine according to claim 1, characterised in that the direction of the tesla configuration grooves coincides with the direction of rotation of the rotor (2).
7. A internal combustion engine with tesla valve structure according to claim 1, characterized in that the sealing end of the stator (1) is provided with a circumferential array of heat dissipation holes (25), the bottom of the sealing end of the stator (1) is further provided with a lubricant inlet (26), and the lubricant inlet (26) is communicated with the inside of the stator (1) through a lubricant passage (29) arranged inside the stator (1).
8. A tesla valve configuration internal combustion engine according to claim 1, wherein the turbine cover (12) is connected with the tesla valve ring (14) in an interference fit.
9. A tesla valve construction internal combustion engine according to claim 1, characterised in that a base (27) is attached to the lower end of the stator (1), the base (27) being provided with a threaded base hole (28).
10. A tesla valve structure internal combustion engine according to claim 1, wherein the open end of the stator (1) and the turbine cover (12) are provided with corresponding fastening threaded holes (30), and the stator (1) and the turbine cover (12) are detachably connected by bolts passing through the fastening threaded holes (30).
CN202110229198.0A 2021-03-02 2021-03-02 Internal combustion engine with Tesla valve structure Active CN112879159B (en)

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CN113757725B (en) * 2021-06-26 2022-08-02 中国人民解放军空军工程大学 Rotary detonation combustion chamber modal control flow channel configuration
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改善CA6110ZLRA5车用柴油机经济性的试验研究;夏少华等;《现代车用动力》;20020515;4-6 *
航空二冲程直喷发动机电控润滑系统试验研究;武浩;《北京理工大学学报》;20190929;719-724 *

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