WO2019203437A1 - Dispositif d'admission à réduction de bruit pour augmenter la sortie d'un moteur à combustion interne - Google Patents
Dispositif d'admission à réduction de bruit pour augmenter la sortie d'un moteur à combustion interne Download PDFInfo
- Publication number
- WO2019203437A1 WO2019203437A1 PCT/KR2019/002480 KR2019002480W WO2019203437A1 WO 2019203437 A1 WO2019203437 A1 WO 2019203437A1 KR 2019002480 W KR2019002480 W KR 2019002480W WO 2019203437 A1 WO2019203437 A1 WO 2019203437A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- vortex
- air
- internal combustion
- combustion engine
- inner diameter
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 47
- 230000001965 increasing effect Effects 0.000 title claims abstract description 12
- 238000000926 separation method Methods 0.000 claims abstract description 20
- 238000009751 slip forming Methods 0.000 claims abstract description 4
- 230000001603 reducing effect Effects 0.000 claims description 16
- 230000009467 reduction Effects 0.000 claims description 9
- 230000002708 enhancing effect Effects 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 4
- 238000009499 grossing Methods 0.000 claims description 2
- 239000000446 fuel Substances 0.000 abstract description 11
- 239000000779 smoke Substances 0.000 abstract description 5
- MWUXSHHQAYIFBG-UHFFFAOYSA-N Nitric oxide Chemical compound O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 6
- 239000007789 gas Substances 0.000 description 5
- 238000009434 installation Methods 0.000 description 4
- 239000004071 soot Substances 0.000 description 4
- 230000008569 process Effects 0.000 description 3
- 230000033228 biological regulation Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N1/00—Silencing apparatus characterised by method of silencing
- F01N1/08—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling
- F01N1/12—Silencing apparatus characterised by method of silencing by reducing exhaust energy by throttling or whirling using spirally or helically shaped channels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B31/00—Modifying induction systems for imparting a rotation to the charge in the cylinder
- F02B31/04—Modifying induction systems for imparting a rotation to the charge in the cylinder by means within the induction channel, e.g. deflectors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to a noise reduction intake apparatus for enhancing the output of an internal combustion engine, and more particularly, is installed in the intake portion of an internal combustion engine such as an automobile to install an air vortex generator to make the air intake and exhaust into a rotating vortex Noise for enhancing the output of the internal combustion engine that improves the flow of fuel and improves the fuel efficiency by improving the output according to the intake and exhaust efficiency, reduces the noise caused by the flow separation phenomenon, reduces the smoke and extends the engine life. It relates to a reduced type intake apparatus.
- a diesel engine is basically provided with a turbo charger and an intercooler in order to provide high-speed driving ease by supercharging intake air at high speed, and to cope with exhaust gas regulation and CO 2 regulation.
- the turbocharger is a kind of blower and utilizes the flow energy of the exhaust gas exiting the exhaust manifold of the engine.
- the turbine of the turbocharger rotates, and at the same time, the compressor installed while being coaxially opposite is rotated, so that the intake air is sucked and pressed by the compressor to supercharge the combustion chamber of the engine cylinder. Is supplied.
- the pressure of the intake air can be increased, but due to the problem that the temperature of the air increases in the process of compressing the air, the combustion temperature and the exhaust temperature are increased, and the actual filling efficiency is improved. Is a problem.
- the supercharged intake air is cooled in the intercooler, thereby preventing heat generation of intake air due to supercharging and supplying the cooled intake air to the combustion chamber, thereby improving the filling efficiency of the combustion chamber.
- the intake system of a diesel engine using a turbocharger and an intercooler increases the amount of intake air, thereby reducing the exhaust gas, improving fuel efficiency, reducing engine noise, and improving fuel efficiency.
- the air vortex generator is installed in the intake and exhaust pipe of the vehicle, such as Korean Patent Registration No. 17564042, to extend the life by increasing the suction power and discharge power of the air through the vortex generator which induces the flow of air at high speed.
- the conventional technologies are disadvantageous in that the flow of the intake and exhaust air is not fast, and the flow separation phenomenon that separates the wing and the wind occurs because the vortex is generated and supplied to the left direction in which the structure is complicated or the vortex does not occur smoothly.
- This phenomenon of flow separation causes irregular air flow, generates noise, causes loss in suction force, and has a disadvantage of vibration.
- the problem to be solved by the present invention is to solve the above-mentioned drawbacks.
- the problem of the present invention is that the bend of the wing installed on the inlet side of the vehicle generates the vortex, thereby reducing the flow separation phenomenon and improving the combustion efficiency by smoothing the flow of air. To improve fuel economy, reduce soot and reduce engine life and noise.
- Another object of the present invention is to adjust the size of the inlet and outlet of the inner diameter tube to form a vortex due to the role of the supercharger according to the Bernoulli principle and the protrusion of the vortex protrusion installed on the inner diameter of the inner diameter tube.
- the present invention forms an inner diameter tube having a hollow in the inner diameter of the cylindrical tube installed between the outside of the internal combustion engine and the engine, and inclined so that three to six in a space between the cylindrical tube and the inner diameter tube have a spiral shape in one direction.
- the noise reduction intake apparatus for increasing the output of the internal combustion engine is installed so that the vortex blades are formed at regular intervals to supply air in one direction to form a vortex,
- the vortex wing is such that the wave pattern is continuously formed in the first entry portion where the air to be sucked first contact;
- the wave pattern is characterized in that to smooth the flow of air by reducing the flow separation phenomenon to install the bent portion formed in the form of irregularities in the form of semi-circular curved and elliptic curved.
- the present invention forms an outer diameter pipe having a space in the inner diameter of the exhaust pipe installed between the engine and the outside of the internal combustion engine, and 4 to 10 vortices in the inner diameter direction from the tip portion of the inclined surface of the outer diameter pipe and the inner diameter inlet to the entire surface thereof.
- the protrusion protrudes helically;
- the vortex protrusion protrudes in a spiral shape in the same direction as the vortex wing, and the hollow is formed to be in the same position as the tip of the hollow.
- the noise reduction type intake / exhaust device for enhancing the output of an internal combustion engine which is provided with vortex vanes at intervals so that air is supplied in one direction to form vortices.
- the vortex wing includes an inlet side wing bend to smooth the flow of air by reducing the flow separation phenomenon on the starting inclined surface from the outside to the inside relative to the spiral direction;
- the wing bent portion is formed of any one of a wave pattern, a sawtooth, a triangle and a quadrangle to have a concave-convex shape so as to have any one of a circular and a semicircular shape, and the entrance side has an inclined surface starting from the outside from the outside in the helical direction. It is formed to be formed on the starting inclined surface, the rear end of the vortex wing is characterized in that the rear inclined surface is formed from the inner side to the outer side on the basis of the spiral direction and is formed to be inclined and inclined as a whole.
- the present invention is installed on the intake side of the car to generate the vortex through the vortex blades to generate the vortex and supply is made, to catch the air due to the bent portion of the vortex wing to reduce the flow peeling phenomenon to smooth the flow of air combustion efficiency To improve fuel economy, reduce soot and extend engine life and reduce noise.
- the present invention has the effect of forming a vortex protrusion at regular intervals in the inner diameter of the inner diameter pipe to form a vortex when exhausted by the intake of air to smooth the flow of air, and the inlet of the inner diameter pipe is formed large and the outlet is small Bernoulli It is to provide the role of a supercharger according to the principle.
- FIG. 1 is a perspective view showing a preferred embodiment of the present invention
- Figure 2 is a plan view showing the installation state of the present invention
- Figure 3 is a front sectional view showing an installation state of the present invention
- Figure 4 is an enlarged view of the main portion of the bent portion for the vortex wing of the present invention
- Figure 5 is an enlarged view of the main portion showing another embodiment of the bent portion for the vortex wing of the present invention
- Figure 6 is an enlarged view of the main portion showing another embodiment of the bent portion for the vortex wing of the present invention
- FIG. 7 is a perspective view showing another embodiment of the present invention.
- Figure 8 is a plan view showing the whole surface of another embodiment of the present invention.
- FIG. 9 is a front view showing the whole surface of another embodiment of the present invention.
- FIG. 10 is a front sectional view showing another embodiment of the present invention installed state
- FIG. 11 is an enlarged cross-sectional view showing main parts of another embodiment of the present invention.
- FIG. 1 is a perspective view showing a preferred embodiment of the present invention
- Figure 2 is a plan view showing an installation state of the present invention
- Figure 3 is a front sectional view showing an installation state of the present invention
- Figure 4 is a bent portion for the vortex wing of the present invention It shows the enlarged part of the main part.
- an intake device 10 to be installed in a part of the intake pipe 20 which functions as an innet pipe for guiding air sucked from the outside, so that the air sucked by an internal combustion engine such as a car forms a vortex. .
- the intake apparatus 10 is preferably installed by selecting a variety of positions between the engine in the portion where the internal combustion engine intakes air.
- the intake apparatus 10 is to prevent the charging efficiency is lowered or the mixer temperature is increased after the end of the engine compression and knocking because the temperature is increased by the compression.
- the intake apparatus 10 has an inner diameter tube 12 is installed to have a circular hollow 13 in the center of the inner diameter of the cylindrical tube 11 formed in a circular shape, the inner diameter tube 12 and the cylindrical tube 11 It connects three to six vortex vanes 15 at regular intervals to the space 14 between them.
- the vortex wing 15 is formed to be inclined to have a spiral shape in one direction and is connected to have a certain height, and the bent portion 16 is formed in a wave pattern at the tip of the entry portion of the vortex wing 15 to reduce the flow separation phenomenon. It is to smooth air flow and reduce noise.
- the wave pattern is formed to have a semi-circular curve or an elliptic curve in an uneven form to be installed so that the intake air collides first.
- FIG. 5 is an enlarged main part showing another embodiment of the bent portion for the vortex wing of the present invention
- Figure 6 is an enlarged main view showing another embodiment of the bent portion for the vortex wing of the present invention.
- the bent portion 16 formed in the vortex wing 15 is formed such that the serrated or triangular irregularities are formed continuously like the bent portions 16a and 16b instead of the wavy pattern, or the quadrangles are continuously formed in the irregular shape.
- Figure 7 is a perspective view showing another embodiment of the present invention
- Figure 8 is a plan view showing a whole surface of another embodiment of the present invention
- Figure 9 is a front view showing a whole surface of another embodiment of the present invention
- Figure 10 is the present invention 11 is a front enlarged cross-sectional view showing another embodiment of the present invention
- Figure 11 is a main portion enlarged cross-sectional view of another embodiment of the present invention vortex wing
- Figure 12 shows a main portion enlarged cross-sectional view for another embodiment of the inner diameter of the present invention.
- Intake air is installed in one part of the intake / exhaust pipe which supplies one part sucked from the outside or the air sucked in and then is discharged to the exhaust pipe through the engine room, so that the air exhausted by the internal combustion engines such as automobiles forms the vortex It is to install the device 10.
- the intake apparatus 10 selects and installs various positions between the engine of the part which an internal combustion engine takes in air, and the part which exhausts.
- the intake apparatus 10 has an inner diameter tube 12 is installed to have a hollow 13 formed in the center in the center, between the outer diameter tube 11 having a space 14 as the outer diameter of the inner diameter tube 12.
- Vortex vanes 15 are connected at three to six at regular intervals.
- the vortex wing 15 is formed to be inclined to have a spiral shape in one direction and is connected to have a predetermined height, and the bend portion 23 is formed in a wave pattern at the tip of the entry portion of the vortex wing 15 to form a flow separation phenomenon. Reducing airflow and reducing noise.
- the wave pattern is formed to have a semi-circular curve or an elliptic curve to have an uneven shape so that the air sucked in collides first.
- the outer diameter pipe 11 is formed with a hollow inclined surface (11a) is formed to be inclined toward the inside from the inlet side, it is preferable to install the vortex wing (15) in the portion where the hollow inclined surface (11a) ends.
- the vortex wing 15 has a starting inclined surface 21 formed at an inlet side from the outside in the spiral direction so that the wing bent portion 23 is formed at the starting inclined surface 21, and the vortex wing 15 is formed.
- the rear inclined surface 22 is formed from the inner side to the outer side with respect to the spiral direction, and is formed to be inclined at the same time as a spiral as a whole.
- the vortex wing 15 is formed to start at the end of the hollow inclined surface (11a) to reach the tip of the outer diameter tube 11, or to be formed so that the end portion ends slightly ahead of the tip of the outer diameter tube (11). desirable.
- the inner tube 12 is preferably formed to start at the end portion of the hollow inclined surface (11a) to the end of the outer diameter tube 11, the end portion is formed a little ahead of the tip of the outer diameter tube 11, the start The outer diameter of the tip and the end is the same or the outer diameter of the end is formed to be smaller.
- the inner diameter of the inner diameter pipe 12 is formed with a circular hollow 13, the inner diameter inlet inclined surface 32 is formed to be inclined so as to decrease in diameter from the starting point to the inside from the starting point, the inner diameter of the inclined surface 32 It is formed so that the supercharging phenomenon according to Bernoulli principle occurs by forming the diameter smaller toward the inner diameter outlet 33 than the inner diameter.
- the vortex protrusion 40 is protruded to be spiral in the same direction as the vortex wing 15, and the tip is formed to be in the same position as the tip of the hollow 13.
- one side of the air intakes in the process of supplying the outside air through the intake pipe 20 and supplied through the intake device 10. It is rotated in the direction to generate the vortex to improve the flow of air to improve the intake efficiency.
- the flow of air is rotated in one direction through the vortex vanes 15 of the intake apparatus 10 to generate vortices so that the flow of air is improved, and the vortex air is rotated and supplied to the engine of the internal combustion engine.
- the temperature of the supplied air is maintained at the most suitable temperature, thereby improving output and reducing noise.
- the vortex wing 15 is connected to the cylindrical tube 11 and the inner diameter tube 12 in a spiral at regular intervals in one direction to the space 14, so that the air supplied to the space 14 forms a vortex
- the bent portions 16, 16a, and 16b of the wing blade 15 are installed at the inlet for sucking the outside air to generate the vortex, and then reduce the flow separation phenomenon to smooth the flow of air to improve the combustion efficiency. To reduce noise and reduce vibration through the ability to reduce soot and extend engine life while reducing flow separation.
- the bent portions 16, 16a, and 16b may be formed in a wavy pattern, or may be any one of a sawtooth, a triangle, and a quadrangle formed in the form of irregularities so that the curved portions may move in the same direction as the air flow.
- it can provide a reduction effect of the flow separation phenomenon to prevent the loss of suction power of the internal combustion engine.
- the air is rotated in one direction in the process of being sucked and exhausted through the intake apparatus 10 that is sucked from the outside air through the internal combustion engine and exhausted to the outside to generate a vortex
- the exhaust efficiency is improved.
- the flow of air is rotated in one direction through the vortex vanes 15 of the intake apparatus 10 to generate vortices so that the flow of air is improved, and the vortex air is discharged to the outside after passing through the internal combustion engine.
- vortices are generated and discharged, thereby improving output and reducing noise.
- the vortex wing 15 is installed in the internal combustion engine of the vehicle in a spiral at regular intervals in one direction in the space 14 so that the air supplied to the space 14 is supplied to form a vortex, the vortex wing 15
- the wing bend 23 of the air is installed in the inner diameter to generate the vortex by the air intake, reduce the flow separation phenomenon to smooth the flow of air to improve the combustion efficiency to improve fuel efficiency, reduce the smoke and life of the engine It also reduces noise and reduces vibration through its ability to reduce flow separation.
- the wing bent portion 23 is formed in a wave pattern, or by applying any one of the serrated, triangular and square is formed in the uneven shape to make the same as the direction of the flow of air to move quickly to help the flow peeling It is possible to provide a reducing effect of the phenomenon to prevent the loss of suction power of the internal combustion engine.
- the vortex wing 15 has a starting inclined surface 11a formed at a starting point and a rear inclined surface 22 formed at an end thereof, and is formed to form a screw while forming an overall inclined surface in one direction, thereby separating the flow through the generation of vortices. It is effective in reducing the phenomenon.
- the inner diameter pipe 12 formed in the center of the space 14 is to allow the air flow smoothly through the inner diameter inlet slope 32, the vortex projection 40 of a constant interval formed in the hollow 13 of the inner diameter.
- the hollow 13 is formed so as to decrease in diameter toward the inner diameter exit 33 starting from the inner diameter inclined surface 32 to perform the role of the supercharger through the bottleneck of the incoming air, and at the same time Since it has been converted into energy, the air can flow out so that it can perform the role of a turbocharger without installing a separate turbo.
- the present invention is to generate the vortex by rotating the air in one direction through the vortex wing installed in the space and the vortex projection installed in the hollow in venting the air sucked in between the engine and the outside of the internal combustion engine
- the turbocharger according to the Bernoulli principle allows the air energy to be supplied farther, which is a very useful invention to extend the life of the engine and reduce the noise.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Abstract
La présente invention concerne un dispositif d'admission à réduction de bruit pour augmenter la sortie d'un moteur à combustion interne et, plus spécifiquement, un dispositif d'admission à réduction de bruit, pour augmenter la sortie d'un moteur à combustion interne, qui est disposé sur une unité d'admission d'un moteur à combustion interne d'un véhicule ou similaire, est pourvu d'un générateur de vortex d'air et améliore le flux d'air au moyen de la rotation de l'air qui est aspiré ou évacué dans un tourbillon rotatif, et améliore ainsi l'efficacité de combustion au moyen d'une sortie améliorée en fonction de l'efficacité d'admission/échappement et augmente ainsi l'efficacité du carburant, réduit le bruit dû à la séparation d'écoulement, réduit la fumée et prolonge la durée de vie d'un moteur. Le dispositif d'admission à réduction de bruit pour augmenter la sortie d'un moteur à combustion interne comprend un tuyau intérieur (12), ayant un creux (13), à l'intérieur d'un tuyau cylindrique (11) disposé entre l'extérieur du moteur à combustion interne et le moteur, a, à des intervalles fixes, 3 à 6 pales de vortex (15) formé de manière inclinée de manière à avoir une forme de spirale dans une direction dans un espace (14) entre le tuyau cylindrique (11) et le tuyau interne (12), et permet ainsi à l'air d'être fourni dans une direction et de former un tourbillon. Les pales de tourbillon (15) ont des motifs ondulés formés en continu sur la partie d'entrée avec laquelle l'air aspiré entre en contact au départ. Les motifs ondulés ont des parties incurvées (16, 16a, 16b), formées de manière concave et convexe sous la forme d'une courbe semi-circulaire ou d'une courbe elliptique, ce qui réduit la séparation des flux et facilite l'écoulement de l'air.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR10-2018-0044419 | 2018-04-17 | ||
KR1020180044419A KR101882834B1 (ko) | 2018-04-17 | 2018-04-17 | 내연기관의 출력 증강을 위한 소음 저감형 흡기 장치 |
KR10-2018-0063212 | 2018-06-01 | ||
KR1020180063212A KR101907139B1 (ko) | 2018-06-01 | 2018-06-01 | 내연기관의 출력 증강을 위한 소음 저감형 흡·배기 장치 |
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WO2019203437A1 true WO2019203437A1 (fr) | 2019-10-24 |
Family
ID=68239651
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/KR2019/002480 WO2019203437A1 (fr) | 2018-04-17 | 2019-03-05 | Dispositif d'admission à réduction de bruit pour augmenter la sortie d'un moteur à combustion interne |
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WO (1) | WO2019203437A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111140721A (zh) * | 2020-01-17 | 2020-05-12 | 浙江大学 | 一种螺旋式降噪装置及其方法 |
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KR20090107719A (ko) * | 2008-04-10 | 2009-10-14 | 박노진 | 내연기관 흡기 효율 개선장치 |
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KR20150118437A (ko) * | 2014-04-14 | 2015-10-22 | 박상호 | 내연기관의 연소효율 향상장치 |
KR101771384B1 (ko) * | 2017-05-25 | 2017-08-24 | 남준현 | 내연기관용 와류 발생기 |
KR20170111940A (ko) * | 2016-03-30 | 2017-10-12 | 유병남 | 내연기관용 유체가속장치 |
-
2019
- 2019-03-05 WO PCT/KR2019/002480 patent/WO2019203437A1/fr active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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KR20090107719A (ko) * | 2008-04-10 | 2009-10-14 | 박노진 | 내연기관 흡기 효율 개선장치 |
KR20130075874A (ko) * | 2011-12-28 | 2013-07-08 | 정병일 | 내연기관의 난류 형성 장치 |
KR20150118437A (ko) * | 2014-04-14 | 2015-10-22 | 박상호 | 내연기관의 연소효율 향상장치 |
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Publication number | Priority date | Publication date | Assignee | Title |
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CN111140721A (zh) * | 2020-01-17 | 2020-05-12 | 浙江大学 | 一种螺旋式降噪装置及其方法 |
CN111140721B (zh) * | 2020-01-17 | 2021-01-01 | 浙江大学 | 一种螺旋式降噪装置及其方法 |
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