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KR100953454B1 - Intake pressure elimination backflow prevention device for internal combustion engine - Google Patents

Intake pressure elimination backflow prevention device for internal combustion engine Download PDF

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Publication number
KR100953454B1
KR100953454B1 KR1020080017224A KR20080017224A KR100953454B1 KR 100953454 B1 KR100953454 B1 KR 100953454B1 KR 1020080017224 A KR1020080017224 A KR 1020080017224A KR 20080017224 A KR20080017224 A KR 20080017224A KR 100953454 B1 KR100953454 B1 KR 100953454B1
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South Korea
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intake
internal combustion
fixed tube
combustion engine
fixed
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KR20090091976A (en
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박현순
손춘남
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이지엘(주)
주식회사 제트플러스
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Priority to KR1020080017224A priority Critical patent/KR100953454B1/en
Priority to PCT/KR2008/001614 priority patent/WO2009066836A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10242Devices or means connected to or integrated into air intakes; Air intakes combined with other engine or vehicle parts
    • F02M35/10275Means to avoid a change in direction of incoming fluid, e.g. all intake ducts diverging from plenum chamber at acute angles; Check valves; Flame arrestors for backfire prevention
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10091Air intakes; Induction systems characterised by details of intake ducts: shapes; connections; arrangements
    • F02M35/10118Air intakes; Induction systems characterised by details of intake ducts: shapes; connections; arrangements with variable cross-sections of intake ducts along their length; Venturis; Diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10242Devices or means connected to or integrated into air intakes; Air intakes combined with other engine or vehicle parts
    • F02M35/10262Flow guides, obstructions, deflectors or the like
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

본 발명은 내연기관용 흡기압력제거 역류방지 장치에 관한 것으로, 더욱 상세하게는 내부가 통공되고, 다수의 고정공이 통공된 고정턱이 외주면을 따라 돌출 형성된 2차흡기관 및 2차흡기관 사이에 벤츄리관 원리의 역기류통로를 형성시키도록 일단이 2차흡기관 내주면에 고정되고, 타단으로 갈수록 2차흡기관의 중심부로 절곡되며, 원주면을 따라 다수의 고정관유동구가 형성된 벤츄리관 구조의 고정관을 구비하여 공기흡입관과 스로틀바디, 스로틀바디와 서지탱크의 연결부 및 흡기매니폴더와 내연기관의 연결부 중 어느 하나 이상에 설치된다.The present invention relates to an intake pressure removing backflow prevention device for an internal combustion engine, and more particularly, a venturi pipe principle between a secondary intake pipe and a secondary intake pipe formed with a plurality of fixed holes through which a fixed jaw protrudes along an outer circumferential surface thereof. One end is fixed to the inner circumferential surface of the secondary intake pipe so as to form a reverse air flow path of the air inlet, bent to the center of the secondary intake pipe toward the other end, and the air suction pipe is provided with a fixed tube of venturi tube structure in which a plurality of fixed pipe flow holes are formed along the circumferential surface. And the throttle body, the connection between the throttle body and the surge tank, and the connection between the intake manifold and the internal combustion engine.

상기와 같은 구성에 의하면, 혼합기체의 유입을 신속하게 함은 물론, 역류되는 역기류기체를 용이하게 재유입 순환시킬 수 있어 완전 연소를 유도함에 따라 내연기관의 성능을 향상시킬 수 있고, 연비개선과 출력향상 및 매연을 감소시키며, 열에너지 효율을 극대화시킬 수 있고, 내연기관 흡기관구조 내부에 다수 개를 설치하여 흡기를 더욱 신속하고 원활하게 유입시킴과 동시에 역기류기체 역시, 신속하게 재유입 순환시킬 수 있다.According to the configuration as described above, it is possible to facilitate the inflow of the mixed gas, as well as to easily re-inflow and circulate backflow gas back flow can improve the performance of the internal combustion engine by inducing complete combustion, improve fuel efficiency It also improves power output, reduces smoke, maximizes thermal energy efficiency, and installs a plurality of internal combustion engine intake pipes to intake air more quickly and smoothly. You can.

내연기관, 흡기관구조, 흡기압력제거, 역류, 방지 Internal combustion engine, intake pipe structure, intake pressure elimination, backflow prevention

Description

내연기관용 흡기압력제거 역류방지 장치{The inhalation pressure removal backward preventing apparatus for the internal combustion engine}The inhalation pressure removal backward preventing apparatus for the internal combustion engine

본 발명은 흡기압력제거 역류방지 장치에 관한 것으로, 더욱 상세하게는 내부가 통공되고, 다수의 고정공이 통공된 고정턱이 외주면을 따라 돌출 형성된 2차흡기관 및 2차흡기관 사이에 벤츄리관 원리의 역기류통로를 형성시키도록 일단이 2차흡기관 내주면에 고정되고, 타단으로 갈수록 2차흡기관의 중심부로 절곡되며, 원주면을 따라 다수의 고정관유동구가 형성된 벤츄리관 구조의 고정관을 구비한다.The present invention relates to an intake pressure removing backflow prevention device, and more particularly, the inside of the vent hole, and a plurality of fixing holes through which the fixing jaw protrudes along the outer circumferential surface between the secondary intake pipe and the secondary intake pipe. One end is fixed to the inner circumferential surface of the secondary intake pipe to form an airflow passage, and is bent to the center of the secondary intake pipe toward the other end, and has a fixed tube having a venturi tube structure in which a plurality of fixed pipe flow holes are formed along the circumferential surface.

이 2차흡기관과 고정관은 공기흡입관과 스로틀바디, 스로틀바디와 서지탱크의 연결부 및 흡기매니폴더와 내연기관의 연결부 중 어느 하나 이상에 설치된다.The secondary intake pipe and the fixed pipe are installed in at least one of the air intake pipe and the throttle body, the connection of the throttle body and the surge tank, and the connection of the intake manifold and the internal combustion engine.

상기와 같은 구성에 의하면, 혼합기체의 유입을 신속하게 함은 물론, 역류되는 역기류기체를 용이하게 재유입 순환시켜 완전 연소를 유도함에 따라 내연기관의 성능을 향상시킬 수 있고, 연비개선과 출력향상 및 매연을 감소시키며, 열에너지 효율을 극대화시킬 수 있다.According to the configuration as described above, it is possible to improve the performance of the internal combustion engine as well as to speed up the inflow of the mixed gas, as well as to easily re-introduce the reverse flow of backflow gas to induce complete combustion, improve fuel economy and output It can improve and reduce soot and maximize thermal energy efficiency.

그리고 내연기관 흡기관구조 내부에 다수 개를 설치하여 흡기를 더욱 신속하고 원활하게 유입시킴과 동시에 역기류기체 역시, 신속하게 재유입 순환시키는 내연기관용 흡기압력제거 역류방지 장치에 관한 것이다.Further, the present invention relates to an intake pressure removing backflow prevention device for an internal combustion engine, in which a plurality of internal combustion engines are installed inside the intake pipe structure to intake air more quickly and smoothly, and at the same time, the reverse airflow gas is also rapidly re-introduced and circulated.

일반적으로, 내연기관 엔진은 흡입, 압축, 폭발, 배기의 순서로 4 행정으로 이루어져 출력을 발생시키고, 이 출력은 구동축을 회전시켜 기계장치를 작동시키게 된다.In general, an internal combustion engine generates four outputs in the order of intake, compression, explosion, and exhaust, and this output causes the drive shaft to rotate to operate the mechanism.

이와 같은, 4 행정 중 흡입은 외부공기를 유입시켜 이동중 미립화된 연료와 혼합시켜 실린더의 연소실에 공급하는 것이다.In this four-stroke intake, the external air is introduced, mixed with the atomized fuel during movement, and supplied to the combustion chamber of the cylinder.

연소실에 혼합기체가 흡입되면, 실린더가 상승하여 혼합기체를 압축시킨 후, 점화플러그에서 불꽃이 발생되어 압축된 혼합기체가 폭발하게 되며, 이 폭발에 의해 실린더가 하측으로 이동하면서 출력이 발생된다.When the mixed gas is sucked into the combustion chamber, the cylinder rises to compress the mixed gas, and then sparks are generated in the spark plug, causing the compressed mixed gas to explode. The explosion causes the cylinder to move downward to generate power.

그리고 폭발한 배기가스는 배기관을 통해 외부로 배출되는 과정 중 다시 혼합기체가 연소실을 채우게 된다.In addition, the exploded exhaust gas is discharged to the outside through the exhaust pipe, and the mixed gas again fills the combustion chamber.

이와 같은, 4 행정이 연속 반복되어 출력이 지속적으로 발생되며, 출력을 높이기 위해 4 행정 시간을 단축시키게 된다.As such, four strokes are repeated in succession, and output is continuously generated, and the four stroke time is shortened to increase the output.

그러나, 4 행정중 배기와 흡입단계에서 연소된 배기가스 배출후 흡입되는 혼합기체가 연소실로 공급되어야 하나 배출되지 못한 연소실의 연소 잔류가스 및 배기가스가 역류하여 연소실내로 재 유입되고, 유입된 연소가스와 혼합기체가 함께 채워진 후, 압축 및 폭발이 이루어짐으로 출력이 저하되는 문제점이 있다.However, the mixed gas sucked after exhausting the exhaust gas combusted in the exhaust and intake stages during the 4th stroke should be supplied to the combustion chamber, but the combustion residual gas and the exhaust gas of the unvented combustion chamber flow back to the combustion chamber, and the introduced combustion After the gas and the mixed gas are filled together, there is a problem that the output is reduced by compression and explosion.

이는 공기흡입관 및 스로틀바디를 통과한 혼합기체가 연소실에서 연소되어 배출되는 과정에서 배기압력과 밸브 오버랩에 의해 배기가스가 역류되어 연소실로 재유입됨에 따라 배기가스가 역류되는 현상이 발생되고, 이 역기류기체에 의해 혼합기체의 유입이 방해되는 것이며, 불완전연소가 유도되는 것이다.This is because when the mixed gas passing through the air suction pipe and the throttle body is combusted and discharged in the combustion chamber, the exhaust gas flows back as the exhaust gas flows back into the combustion chamber due to the exhaust pressure and the valve overlap, and the exhaust gas flows back into the combustion chamber. Inflow of the mixed gas is prevented by the airflow gas, and incomplete combustion is induced.

또한, 혼합기체의 흡입시, 실린더의 연소실에 흡입되는 혼합기체의 량이 공급되는 혼합기체 량보다 적기 때문에 스로틀바디를 통해 지속적으로 공급되는 혼합기체에 의해 흡기매니폴더에 잔류한 혼합기체가 역류하게 되어 흡기를 방해하는 문제가 발생되는 것이다.In addition, when the mixed gas is inhaled, the amount of the mixed gas sucked into the combustion chamber of the cylinder is less than the amount of the mixed gas supplied, so that the mixed gas remaining in the intake manifold is flowed back by the mixed gas continuously supplied through the throttle body. Problems that interfere with inspiration occur.

이에 본 발명은 상기와 같은 문제점들을 해소하기 위해 안출된 것으로써, 내부가 통공되고, 다수의 고정공이 통공된 고정턱이 외주면을 따라 돌출 형성된 2차흡기관 및 2차흡기관 사이에 벤츄리관 원리의 역기류통로를 형성시키도록 일단이 2차흡기관 내주면에 고정되고, 타단으로 갈수록 2차흡기관의 중심부로 절곡되며, 원주면을 따라 다수의 고정관유동구가 형성된 벤츄리관 구조의 고정관을 구비한다.Accordingly, the present invention has been devised to solve the above problems, the inside of the vent hole, and a plurality of fixing holes through the fixing jaw between the secondary intake pipe and the secondary intake pipe formed along the outer circumferential surface of the principle of the venturi tube principle One end is fixed to the inner circumferential surface of the secondary intake pipe to form an airflow passage, and is bent to the center of the secondary intake pipe toward the other end, and has a fixed tube having a venturi tube structure in which a plurality of fixed pipe flow holes are formed along the circumferential surface.

이 2차흡기관과 고정관은 공기흡입관과 스로틀바디, 스로틀바디와 서지탱크의 연결부 및 흡기매니폴더와 내연기관의 연결부 중 어느 하나 이상에 설치된다.The secondary intake pipe and the fixed pipe are installed in at least one of the air intake pipe and the throttle body, the connection of the throttle body and the surge tank, and the connection of the intake manifold and the internal combustion engine.

상기와 같은 구성에 의하면, 혼합기체의 유입을 신속하게 함은 물론, 역류되는 역기류기체를 용이하게 재유입 순환시켜 완전 연소를 유도함에 따라 내연기관의 성능을 향상시킬 수 있고, 연비개선과 출력향상 및 매연을 감소시키며, 열에너지 효율을 극대화시킬 수 있다.According to the configuration as described above, it is possible to improve the performance of the internal combustion engine as well as to speed up the inflow of the mixed gas, as well as to easily re-introduce the reverse flow of backflow gas to induce complete combustion, improve fuel economy and output It can improve and reduce soot and maximize thermal energy efficiency.

그리고 내연기관 흡기관구조 내부에 다수 개를 설치하여 흡기를 더욱 신속하고 원활하게 유입시킴과 동시에 역기류기체 역시, 신속하게 재유입 순환시키는 내연기관용 흡기압력제거 역류방지 장치를 제공하는 것이 목적이다.In addition, it is an object of the present invention to provide an intake pressure removing backflow prevention device for an internal combustion engine, in which a plurality of internal combustion engines are installed inside the intake pipe structure to intake air more quickly and smoothly, and at the same time, the reverse air flow is also quickly re-introduced and circulated.

상기 목적을 이루기 위한 본 발명은, 흡입되는 외기와 별도로 공급되는 연료가 혼합된 혼합기체를 내연기관에 공급하도록 공기흡입관과 스로틀바디, 서지탱크, 흡기매니폴더 등을 갖는 내연기관의 흡기관구조에 위치되어 상기 혼합기체가 유입되도록 내부가 통공되고, 다수의 고정공이 통공된 고정턱이 외주면을 따라 돌출 형성된 2차흡기관, 및 상기 2차흡기관 내주면에 일단이 고정되고, 타단으로 갈수록 2차흡기관의 중심부로 절곡되며, 원주면을 따라 다수의 고정관유동구가 형성된 벤츄리관 구조의 고정관을 포함하여 이루어지고, 상기 고정관과 2차흡기관 사이에는, 유입되는 혼합기체 중 연소실에 유입되지 않아 역류되는 역기류기체가 유입되는 벤츄리관 원리의 역기류통로를 형성시켜 유입된 역기류기체를 상기 고정관유동구를 통해 고정관 내부로 유도하여 지속적으로 흡입되는 혼합기체를 따라 다시 연소실로 재유입 순환시키도록, 상기 2차흡기관과 고정관이 공기흡입관과 스로틀바디, 스로틀바디와 서지탱크의 연결부 및 흡기매니폴더와 내연기관의 연결부 중 어느 하나 이상에 설치된다.In order to achieve the above object, the present invention provides an intake pipe structure of an internal combustion engine having an air suction pipe, a throttle body, a surge tank, an intake manifold, and the like to supply a mixed gas mixed with fuel supplied separately from the outside air to be sucked to the internal combustion engine. It is located inside the through-hole so that the mixed gas is introduced, the fixed jaw through which a plurality of fixing holes are protruded along the outer circumferential surface, and one end is fixed to the inner circumferential surface of the secondary intake pipe, the other end of the secondary intake pipe It is bent to the center, and comprises a fixed tube of the venturi tube structure formed with a plurality of fixed tube flow holes along the circumferential surface, and between the fixed tube and the secondary intake pipe, the reverse air flow flowing back to the combustion chamber does not flow into the combustion chamber The inlet air flow path formed by the venturi pipe principle in which the inlet gas flows into the inlet air stream is fixed through the fixed pipe flow port. The secondary intake pipe and the fixed pipe are connected to the air intake pipe and the throttle body, the throttle body and the surge tank, and the connection between the intake manifold and the internal combustion engine so that the secondary intake pipe and the fixed pipe are circulated back to the combustion chamber along with the continuously inhaled mixed gas. It is installed on any one or more.

바람직하게, 상기 고정관의 타단부에는 허니콤(honeycomb) 구조를 갖는 내부연통이 더 구비된다.Preferably, the other end of the fixed tube is further provided with internal communication having a honeycomb (honeycomb) structure.

그리고 상기 고정관의 내측에 설치되어 고정관유동구에서 나오는 역기류기체가 흡기와 충돌되는 것을 최소화시키며, 흡기의 유입속도를 증가시켜 흡기를 신속하고 원활하게 유입시키는 고정관날개가 더 구비된다.And it is installed on the inside of the fixed tube to minimize the impact of the backflow gas from the fixed tube flow port with the intake, the inlet tube wings for increasing the intake rate of intake quickly and smoothly is further provided.

또한, 상기 고정관날개는, 다수의 고정관유동구 사이인 상기 고정관의 내주면을 따라 일정한 간격으로 설치된 다수의 날개, 및 상기 다수의 날개가 상호 접하는 고정관의 중심부에 위치되는 원추형의 날개몸체를 포함하여 이루어진다.The fixed tube wing may include a plurality of wings installed at regular intervals along an inner circumferential surface of the fixed tube between the plurality of fixed tube flow ports, and a conical wing body positioned at the center of the fixed tube in which the plurality of wings contact each other.

그리고 상기 날개는 유입방향을 기준선으로 일정경사지게 절곡 형성된다.The blade is bent to be inclined at a baseline in the inflow direction.

또한, 상기 고정관의 타단부에는 허니콤(honeycomb) 구조를 갖는 날개연통이 더 구비된다.In addition, the other end of the fixed tube is further provided with a wing communication having a honeycomb (honeycomb) structure.

그리고 상기 고정관 내부에 설치되고, 흡기의 유입방향으로 갈수록 단면적이 감소되도록 중심방향으로 경사지게 절곡되어 흡기의 속도를 증가시키며, 상기 고정관의 내주면과의 사이에 고정관유동구와 연통되는 제2역기류통로를 형성시키는 고정관날개가 더 구비된다.And installed inside the fixed tube, bent inclined toward the center so as to decrease the cross-sectional area toward the inlet direction of the intake to increase the speed of the intake, the second backflow flow passage communicating with the fixed tube flow port between the inner peripheral surface of the fixed tube Fixing tube wings to form are further provided.

또한, 상기 고정관날개의 흡기 유입방향 끝단 내부에 허니콤(honeycomb) 구조를 갖는 날개연통이 더 구비된다.In addition, the wing communication having a honeycomb (honeycomb) structure is further provided inside the intake inlet end of the fixed tube wing.

상기한 바와 같이, 본 발명에 의한 내연기관용 흡기압력제거 역류방지 장치에 의하면, 유입되는 흡기중 역류되는 역기류기체를 2차흡기관과 고정관 사이에 형성된 벤츄리관 원리의 역기류통로로 유도하고, 유도된 역기류기체는 고정관유동구를 통해 벤츄리관인 고정관 내부로 이동되어 새로 유입되는 흡기와 함께 엔진의 연소실로 신속하고 원활하게 유입될 수 있기 때문에 역기류기체가 흡기의 유입을 방해하는 것을 방지할 수 있다.As described above, according to the intake pressure removing backflow prevention device for the internal combustion engine according to the present invention, the inflow backflow gas flowing back in the intake air induction into the backflow passage of the principle of the venturi tube formed between the secondary intake pipe and the fixed pipe, The reversed airflow can be prevented from interfering with the inflow of the intake air because the inflow airflow can be moved to the inside of the fixed pipe which is the venturi pipe through the fixed pipe flow port, and can be introduced into the combustion chamber of the engine quickly and smoothly with the newly introduced intake air. .

이와 같이, 역기류기체의 유입을 방지하여 흡기압력이 제거되면, 신속하고 원할한 혼합기체의 유입으로 완전 연소를 유도함에 따라 내연기관의 성능을 향상시킬 수 있어 연비개선과 출력향상 및 매연을 감소시키고 열에너지 효율을 극대화시킬 수 있다.As such, when the intake pressure is removed by preventing the inflow of backflow gas, the performance of the internal combustion engine can be improved by inducing complete combustion with the inflow of a fast and smooth mixture gas, thereby improving fuel efficiency, improving output and reducing smoke. And maximize thermal energy efficiency.

또한, 2차흡기관과 고정관을 흡기관구조 내부에 다수 개를 설치하여 흡기를 더욱 신속하고 원활하게 유입시킴과 동시에 역기류기체를 신속하게 재유입 순환시킬 수 있게 하는 매우 유용하고 효과적인 발명이다.In addition, by installing a plurality of secondary intake pipe and a fixed tube inside the intake pipe structure, it is a very useful and effective invention that allows the intake air more quickly and smoothly inflow and at the same time to re-introduce the reverse air flow.

이하, 본 발명의 바람직한 실시 예를 첨부된 도면을 참조하여 설명한다.Hereinafter, preferred embodiments of the present invention will be described with reference to the accompanying drawings.

또한, 본 실시 예는 본 발명의 권리범위를 한정하는 것은 아니고 단지 예시로 제시된 것이며, 그 기술적 요지를 이탈하지 않는 범위 내에서 다양한 변경이 가능하다.In addition, the present embodiment is not intended to limit the scope of the present invention, but is presented by way of example only, and various modifications may be made without departing from the technical gist of the present invention.

도 1은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치를 도시한 도면이고, 도 2는 도 1의 A-A' 선을 따라 절단한 부분 단면사시도를 도시한 도면이며, 도 3은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치의 측단면도를 도시한 도면이고, 도 4는 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치의 공기 유입상태를 도시한 도면이며, 도 5는 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 내부연통이 더 구비된 상태를 도시한 도면이고, 도 6은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 고정관날개가 더 구비된 실시 예를 도시한 도면이며, 도 7은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 고정관날개가 더 구비된 다른 실시 예를 도시한 도면이고, 도 8은 도 7에 날개연통이 더 구비된 실시 예를 도시한 도면이며, 도 9는 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 고정관날개가 더 구비된 또 다른 실시 예를 도시한 도면이고, 도 10은 도 10에 날개연통이 더 구비된 실시 예를 도시한 도면이며, 도 11은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치의 설치상태를 도시한 도면이다.1 is a view showing an intake pressure removing backflow prevention device for an internal combustion engine according to the present invention, Figure 2 is a view showing a partial cross-sectional perspective view taken along the line AA 'of Figure 1, Figure 3 according to the present invention 4 is a side cross-sectional view of the intake pressure removing backflow preventing device for an internal combustion engine, and FIG. 4 is a view illustrating an air inflow state of the intake pressure removing backflow preventing device for an internal combustion engine according to the present invention, and FIG. FIG. 6 is a view illustrating a state in which internal communication is further provided in the intake pressure removing backflow prevention device for an engine, and FIG. FIG. 7 is a view illustrating another embodiment in which an intake pressure removing backflow prevention device for an internal combustion engine is further provided with a fixed tube blade, and FIG. 8 is a seal further provided with a wing communication in FIG. 7. 9 is a view showing an example, Figure 9 is a view showing another embodiment in which a fixed tube wing is further provided in the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention, Figure 10 is a wing communication in Figure 10 11 is a view showing an embodiment provided, Figure 11 is a view showing an installation state of the intake pressure removing backflow prevention device for the internal combustion engine according to the present invention.

도면에서 도시한 바와 같이, 내연기관용 흡기압력제거 역류방지 장치(10)는 2차흡기관(100) 및 고정관(110)으로 구성되는 것으로, 2차흡기관(100)과 고정관(110)은 동심원을 갖는 상호 다른 직경으로 이루어진다.As shown in the figure, the intake pressure removing backflow prevention device 10 for the internal combustion engine is composed of a secondary intake pipe 100 and the fixed pipe 110, the secondary intake pipe 100 and the fixed pipe 110 has a concentric circle. It is made of different diameters.

2차흡기관(100)은 내연기관에 공기를 유입시키는 흡기관구조(1) 내부에 고정되는 것으로, 흡기관구조(1) 중 각 부품이 연결되는 부분에 고정된다.The secondary intake pipe 100 is fixed inside the intake pipe structure 1 for introducing air to the internal combustion engine, and is fixed to a portion to which each component of the intake pipe structure 1 is connected.

다시 말해, 공기흡입관(2)과 스로틀바디(3), 스로틀바디(3)와 서지탱크(4) 및 흡기매니폴더(5)와 엔진(6) 연결부 중 어느 하나 이상에 설치되어 흡기압력을 제거하여 신속하고 원활하게 역기류기체를 새로운 흡기와 함께 재유입 순환시킴으로, 신속하게 연소실로 유입시키게 된다.In other words, the air intake pipe (2) and the throttle body (3), the throttle body (3) and the surge tank (4), and the intake manifold (5) and the engine (6) is connected to any one or more of the connection to remove the intake pressure As a result, the backflow gas is quickly and smoothly flowed back into the combustion chamber with the new intake air.

2차흡기관(100)은 내부가 통공되고, 외주면을 따라 고정턱(102)이 돌출형성되며, 고정턱(102)을 따라 다수의 고정공(104)이 일정간격으로 형성된다.Inside the secondary intake pipe 100, the fixing jaw 102 is formed to protrude along the outer circumferential surface, a plurality of fixing holes 104 are formed at regular intervals along the fixing jaw 102.

이 2차흡기관(100)의 고정턱(102)이 공기흡입관(2)과 스로틀바디(3), 스로틀바디(3)와 서지탱크(4) 및 흡기매니폴더(5)와 엔진(6) 연결부에 끼워져 별도의 고정부재(미 도시)에 의해 고정되게 된다.The fixing jaw 102 of the secondary intake pipe 100 is connected to the air suction pipe 2, the throttle body 3, the throttle body 3, the surge tank 4, the intake manifold 5 and the engine 6. It is fitted to be fixed by a separate fixing member (not shown).

그리고 2차흡기관(100)의 내측에는 외주면을 따라 다수의 고정관유동구(112)가 형성된 고정관(110)이 설치되어 2차흡기관(100)에 의해 보호되고, 고정관(110)과 2차흡기관(100) 사이에 일측으로 개방된 역기류통로(120)를 형성시킨다.And inside the secondary intake pipe 100, a fixed tube 110 formed with a plurality of fixed tube flow openings 112 are installed along the outer circumferential surface and protected by the secondary intake pipe 100, and the fixed pipe 110 and the secondary intake pipe 100 Between the) to form an open air flow passage 120 to one side.

다시 말해, 고정관(110)은 일단이 2차흡기관(100)의 내측에 고정되고, 타단으로 갈수록 중심방향으로 절곡되어 타단으로 개방된 역기류통로(120)가 형성되는 것으로, 이 역기류통로(120)는 고정관유동구(112)와 개방된 타단이 연통되도록 형성된다.In other words, the fixed pipe 110 is one end is fixed to the inside of the secondary intake pipe 100, the other end is bent toward the center to form a reverse air flow passage 120 is opened to the other end, the reverse air flow passage ( 120 is formed to communicate with the other end of the fixed tube flow opening 112 is open.

이는, 내연기관의 구조상 4 행정의 흡기시, 실린더의 연소실에 흡기압력이 발생되어 혼합기체의 유입을 방해하게 되고, 이 혼합기체의 역류에 의해 유입되는 흡기도 역류되는 현상이 발생되기 때문에, 이 역기류기체를 역기류통로(120)로 유입시켜 순환될 수 있도록 이동시키는 것이다.This is because, due to the structure of the internal combustion engine, the intake pressure is generated in the combustion chamber of the cylinder to hinder the inflow of the mixed gas, and the intake air flowing back due to the reverse flow of the mixed gas occurs. It is to move the reverse air flow to the reverse air flow path 120 to be circulated.

상기와 같이, 역기류기체가 역기류통로(120)를 따라 이동하게 되면, 고정관(110)에 형성된 고정관유동구(112)를 통해 고정관(110) 내측으로 이동하게 되고, 이동된 역기류기체는 유입되는 새로운 외부공기와 함께 엔진(6) 연소실로 신속하게 유입되어 완전연소를 유도하게 된다.As described above, when the backflow gas moves along the backflow passage 120, the backflow gas moves to the inside of the fixed pipe 110 through the fixed pipe flow port 112 formed in the fixed pipe 110, and the moved backflow gas flows in. The new external air is rapidly introduced into the combustion chamber of the engine 6 to induce complete combustion.

이때, 고정관(110)은 2차흡기관(100)과 결합된 일단부에서 타단으로 갈수록 중앙방향으로 경사지게 형성되어 깔대기 형상으로 이루어지기 때문에 혼합기체의 유입속도를 증가시킴과 동시에, 2차흡기관(100)과의 이격거리를 변화시켜 역기류통로(120)의 양단부 단면적이 다르게 형성시키게 된다.At this time, the fixed tube 110 is formed inclined toward the center from one end coupled to the second intake pipe 100 toward the other end to increase the inflow rate of the mixed gas and at the same time, the secondary intake pipe 100 The cross-sectional area of both ends of the backflow passage 120 is differently formed by changing the separation distance from the backplane.

이와 같이, 역기류통로(120)의 단면적을 고정관유동구(112)와 연통된 일단부에서 타단으로 갈수록 점차적으로 크게 형성시키면, 타단으로 유입되는 역기류기체의 속도를 증가시켜 역기류기체의 유입을 신속하고 원활하게 유도하고, 고정관유동구(112)를 용이하게 통과시키기 위한 것이다.As such, if the cross-sectional area of the reverse air flow passage 120 is gradually increased from one end communicated with the fixed pipe flow port 112 to the other end, the speed of the reverse air flow flowing into the other end is increased to increase the inflow of the reverse air flow gas. It is to guide quickly and smoothly, and to easily pass through the fixed tube flow port (112).

그리고 도 5에서 도시한 바와 같이, 고정관(110)의 타단부에는 내부연통(130)이 설치되며, 내부연통(130)은 허니콤(honeycomb) 구조로 이루어져 고정관(110) 가장자리에서 발생되는 흡기의 확산을 방지하여 더욱 신속하고 원활하게 유입시킬 수 있게 된다.And as shown in Figure 5, the other end of the fixed tube 110, the internal communication 130 is installed, the internal communication 130 is made of a honeycomb (honeycomb) structure of the intake air generated at the edge of the fixed tube 110 Prevents diffusion and allows for faster and smoother inflow.

도 6 내지 도 8에서 도시한 바와 같이, 고정관(110)의 내측에 고정관날개(140)가 설치되어 유입되는 흡기를 더욱 신속하게 유입시킬 수 있고, 흡기의 원활한 유입에 의해 고정관유동구(112)를 통해 고정관(110) 내부로 유입된 역기류기체를 신속하게 유입시킬 수 있다.As shown in Figure 6 to 8, the fixed tube wing 140 is installed inside the fixed tube 110 can be introduced to the intake air more quickly, the inlet tube flow opening 112 by the smooth inlet of the intake Through the backflow gas introduced into the fixed tube 110 can be quickly introduced.

고정관날개(140)는 날개몸체와 다수의 날개로 구성되며, 날개는 다수의 고정관유동구(112) 사이인 고정관(110)의 내측에 각각 설치되고, 날개몸체는 원추형상으로 이루어져 다수의 날개가 상호 접하는 중심부에 설치된다.The fixed tube wing 140 is composed of a wing body and a plurality of wings, the wings are respectively installed inside the fixed tube 110 between the plurality of fixed tube flow openings 112, the wing body is made of a conical shape, the plurality of wings are mutually It is installed in the center of contact.

이때, 날개몸체는 본 발명에서 원추형상으로 이루어지지만, 고정관(110) 내측에서 흡기의 흐름을 신속하고 원활하게 이루어지게 할 수 있는 구조라면 다른 형상으로 변경되어 설치될 수 있는 것이다.At this time, the wing body is made of a conical shape in the present invention, if the structure that can make the flow of intake quickly and smoothly inside the fixed tube 110 can be installed in a different shape.

한편, 도 8에서 도시한 바와 같이, 고정관날개(140')의 다른 실시 예로, 날개를 유입방향을 기준선으로 일정경사지게 절곡 형성되어 유입되는 흡기를 신속하게 유입시킬 수 있고, 이에 따라 고정관유동구(112)을 통과한 역기류기체를 신속하게 재유입 순환시킬 수 있다.On the other hand, as shown in Figure 8, in another embodiment of the fixed tube wing 140 ', the blade is bent to be inclined in a predetermined line in the inflow direction can be introduced into the intake air inlet quickly, accordingly fixed tube flow port 112 It is possible to quickly recirculate the backflow gas passed through).

그리고 고정관(110)의 고정되지 않은 단부(타단)에는 허니콤(honeycomb) 구조의 날개연통(150)이 구비되어 흡기를 더욱 신속하게 유입시킬 수 있고, 흡기의 원활한 유입에 의해 고정관유동구(112)를 통해 유입된 역기류기체를 신속하게 이동시킬 수 있는 것이다.And the non-fixed end (the other end) of the fixed tube 110 is provided with a wing communication 150 of the honeycomb (honeycomb) structure to intake the intake more quickly, the inlet tube flow opening 112 by the smooth inlet of the intake It is possible to quickly move the backflow gas introduced through.

또한, 도 10에서 도시한 바와 같이, 고정관(110)의 내측에 고정관날개(140")가 설치되는 것으로, 일단이 고정관(110)의 내주면과 연결되고, 타단으로 갈수록 중심방향으로 절곡된다.In addition, as shown in Figure 10, the fixed tube wing 140 "is installed inside the fixed tube 110, one end is connected to the inner circumferential surface of the fixed tube 110, the other end is bent toward the center direction.

다시 말해, 고정관날개(140")는 흡기의 유입방향(타단)으로 갈수록 단면적이 감소되도록 중심방향으로 경사지게 형성되어 고정관(110)과의 사이에 제2역기류통로(160")를 형성하게 된다.In other words, the fixed tube wing 140 "is formed to be inclined toward the center so that the cross-sectional area decreases toward the inflow direction (the other end) of the intake air, thereby forming a second reverse air flow path 160" between the fixed pipe 110 and the fixed pipe 110. .

고정관날개(140")의 타단이 중심방향으로 경사를 이루면, 흡기관구조(1)로 유입된 흡기의 유입속도가 증가되어 용이하게 유입될 수 있다.When the other end of the fixed tube wing 140 ″ is inclined toward the center direction, the inflow rate of the intake air flowing into the intake pipe structure 1 is increased and thus can be easily introduced.

그리고 제2역기류통로(160")는 역기류통로(120)로 유입된 역기류기체가 고정관유동구(112)를 통과하면서, 흡기관구조(1)의 역방향으로 혹시 역류하는 것을 방지하기 위한 것으로, 역기류기체를 더욱 신속하게 유입시킬 수 있다.In addition, the second backflow passage 160 ″ prevents backflow in the reverse direction of the intake pipe structure 1 while the backflow gas flowing into the backflow passage 120 passes through the fixed pipe flow port 112. As a result, the backflow gas can be introduced more quickly.

또한, 고정관날개(140")의 타단에는 허니콤(honeycomb) 구조의 날개연통(150")이 구비되어 흡기를 더욱 용이하게 유입시킬 수 있고, 흡기의 원활한 유입에 의해 고정관유동구(112)를 통해 유입된 역기류기체를 신속하게 유입시키는 것이 바람직하다.In addition, the other end of the fixed tube wing (140 ") is provided with a wing communication (150") of the honeycomb (honeycomb) structure to facilitate intake more easily, through the fixed tube flow opening 112 by the smooth inlet of the intake It is desirable to quickly introduce the introduced backflow gas.

그리고 도 11에서 도시한 바와 같이, 2차흡기관(100)과 고정관(110)으로 구성된 흡기압력제거 역류방지 장치(10)는 흡기관구조(1)의 공기흡입관(2)과 스로틀바디(3), 스로틀바디(3)와 서지탱크(4) 및 흡기매니폴더(5)와 엔진(6) 연결부 중 어느 하나 이상에 설치된다.11, the intake pressure removing backflow prevention device 10 including the secondary intake pipe 100 and the fixed pipe 110 includes an air intake pipe 2 and a throttle body 3 of the intake pipe structure 1. And at least one of a throttle body 3, a surge tank 4, and an intake manifold 5 and an engine 6 connection portion.

이와 같이, 흡기압력제거 역류방지 장치(10)가 공기흡입관(2)과 스로틀바디(3), 스로틀바디(3)와 서지탱크(4) 및 흡기매니폴더(5)와 엔진(6) 연결부 중 어느 하나 이상에 설치되면, 각 구간에서 발생되는 역기류기체를 각각 재유입 순환시켜 유입되는 새로운 혼합기체와 함께 신속하게 연소실로 유입되는 것이다.As such, the intake pressure removing backflow prevention device 10 includes an air intake pipe 2, a throttle body 3, a throttle body 3, a surge tank 4, an intake manifold 5, and an engine 6 connection part. If installed in any one or more, the backflow gas generated in each section is introduced to the combustion chamber quickly with the new mixed gas introduced by the re-introduced circulation.

도 1은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치를 도시한 도면이고,1 is a view showing an intake pressure removing backflow prevention device for an internal combustion engine according to the present invention,

도 2는 도 1의 A-A' 선을 따라 절단한 부분 단면사시도를 도시한 도면이며,FIG. 2 is a partial cross-sectional perspective view taken along the line AA ′ of FIG. 1;

도 3은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치의 측단면도를 도시한 도면이고,3 is a side cross-sectional view of the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention;

도 4는 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치의 공기 유입상태를 도시한 도면이며,4 is a view showing an air inlet state of the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention,

도 5는 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 내부연통이 더 구비된 상태를 도시한 도면이고,5 is a view showing a state in which the internal communication is further provided in the intake pressure removing backflow prevention device for the internal combustion engine according to the present invention,

도 6은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 고정관날개가 더 구비된 실시 예를 도시한 도면이며,6 is a view showing an embodiment further provided with a fixed tube blade in the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention,

도 7은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 고정관날개가 더 구비된 다른 실시 예를 도시한 도면이고,7 is a view showing another embodiment further provided with a fixed tube blade in the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention,

도 8은 도 7에 날개연통이 더 구비된 실시 예를 도시한 도면이며,8 is a view showing an embodiment in which the wing communication is further provided in FIG.

도 9는 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치에 고정관날개가 더 구비된 또 다른 실시 예를 도시한 도면이고,9 is a view showing another embodiment further provided with a fixed tube blade in the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention,

도 10은 도 10에 날개연통이 더 구비된 실시 예를 도시한 도면이며,FIG. 10 is a view illustrating an embodiment in which wing communication is further provided in FIG. 10.

도 11은 본 발명에 따른 내연기관용 흡기압력제거 역류방지 장치의 설치상태를 도시한 도면이다.11 is a view showing an installation state of the intake pressure removing backflow prevention device for an internal combustion engine according to the present invention.

< 도면의 주요 부분에 대한 부호의 설명 ><Description of Symbols for Main Parts of Drawings>

1 : 흡기관구조 10 : 흡기압력제거 역류방지 장치1: Intake pipe structure 10: Intake pressure removing backflow prevention device

100 : 2차흡기관 102 : 고정턱100: secondary intake pipe 102: fixed jaw

104 : 고정공 110 : 고정관104: fixing hole 110: fixing tube

112 : 고정관유동구 120 : 역기류통로112: fixed pipe flow opening 120: backflow passage

130 : 내부연통 140, 140', 140" : 고정관날개130: internal communication 140, 140 ', 140 ": fixed tube wing

150, 150" : 날개연통 160" :제2역기류통로150, 150 ": wing communication 160": second reverse air flow path

Claims (8)

흡입되는 외기와 별도로 공급되는 연료가 혼합된 혼합기체를 내연기관에 공급하도록 공기흡입관과 스로틀바디, 서지탱크, 흡기매니폴더 등을 갖는 내연기관의 흡기관구조(1)에 위치되어 상기 혼합기체가 유입되도록 내부가 통공되고, 다수의 고정공(104)이 통공된 고정턱(102)이 외주면을 따라 돌출 형성된 2차흡기관(100); 및The mixed gas is located in the intake pipe structure (1) of the internal combustion engine having an air intake pipe, a throttle body, a surge tank, an intake manifold, and the like to supply a mixed gas mixed with the supplied outside air and the fuel supplied to the internal combustion engine. A second intake pipe 100 through which an inside is introduced so as to be introduced, and a fixing jaw 102 through which a plurality of fixing holes 104 are formed protrudes along an outer circumferential surface thereof; And 상기 2차흡기관(100) 내주면에 일단이 고정되고, 타단으로 갈수록 2차흡기관(100)의 중심부로 절곡되며, 원주면을 따라 다수의 고정관유동구(112)가 형성된 벤츄리관 구조의 고정관(110)을 포함하여 이루어지고,One end is fixed to the inner circumferential surface of the secondary intake pipe 100, the other end is bent to the center of the secondary intake pipe 100, the fixed tube 110 of the venturi tube structure formed with a plurality of fixed pipe flow holes 112 along the circumferential surface It is made, including 상기 고정관(110)과 2차흡기관(100) 사이에는, 유입되는 혼합기체 중 연소실에 유입되지 않아 역류되는 역기류기체가 유입되는 벤츄리관 원리의 역기류통로(120)를 형성시켜 유입된 역기류기체를 상기 고정관유동구(112)를 통해 고정관(110) 내부로 유도하여 지속적으로 흡입되는 혼합기체를 따라 다시 연소실로 재유입 순환시키도록,Between the fixed pipe 110 and the secondary intake pipe 100, backflow flow introduced by forming a backflow passage 120 of the venturi tube principle in which a backflow gas flows back because it does not flow into the combustion chamber among the inflowing mixed gases. To guide the gas through the fixed tube flow port 112 into the fixed tube 110 to circulate back to the combustion chamber along the continuously inhaled mixed gas, 상기 2차흡기관(100)과 고정관(110)이 공기흡입관과 스로틀바디, 스로틀바디와 서지탱크의 연결부 및 흡기매니폴더와 내연기관의 연결부 중 어느 하나 이상에 설치되며,The secondary intake pipe 100 and the fixed pipe 110 is installed in any one or more of the air intake pipe and the throttle body, the connection of the throttle body and the surge tank and the connection of the intake manifold and the internal combustion engine, 상기 고정관(110)의 내측에 설치되어 고정관유동구(112)에서 나오는 역기류기체가 흡기와 충돌되는 것을 최소화시키며, 흡기의 유입속도를 증가시켜 흡기를 신속하고 원활하게 유입시키는 고정관날개(140)가 더 구비되고,The fixed tube 110 is installed inside the fixed tube 110 to minimize the backflow gas from the fixed tube flow port 112 collides with the intake, and the fixed tube wing 140 to quickly and smoothly introduce the intake by increasing the intake rate of the intake More equipped, 상기 고정관날개(140)는,The fixed tube wing 140, 다수의 고정관유동구(112) 사이인 상기 고정관(110)의 내주면을 따라 일정한 간격으로 설치된 다수의 날개; 및A plurality of wings installed at regular intervals along the inner circumferential surface of the fixed tube 110 between the plurality of fixed tube flow holes 112; And 상기 다수의 날개가 상호 접하는 고정관(110)의 중심부에 위치되는 원추형의 날개몸체를 포함하여 이루어지는 내연기관용 흡기압력제거 역류방지 장치.Intake pressure removing backflow prevention device for an internal combustion engine comprising a conical wing body located in the center of the fixed tube 110 which the plurality of wings are in contact with each other. 제1항에 있어서,The method of claim 1, 상기 고정관의 타단부에는 허니콤(honeycomb) 구조를 갖는 내부연통이 더 구 비되는 것을 특징으로 하는 내연기관용 흡기압력제거 역류방지 장치.The other end of the fixed tube is provided with an internal communication having a honeycomb (honeycomb) structure further characterized in that the intake pressure removal backflow prevention device for the internal combustion engine. 삭제delete 삭제delete 제1항에 있어서,The method of claim 1, 상기 날개는 유입방향을 기준선으로 일정경사지게 절곡 형성되는 것을 특징으로 하는 내연기관용 흡기압력제거 역류방지 장치.The blade is formed to be bent at a predetermined inclination with respect to the inflow direction, the intake pressure removal backflow prevention device for an internal combustion engine. 제1항에 있어서,The method of claim 1, 상기 고정관(110)의 타단부에는 허니콤(honeycomb) 구조를 갖는 날개연통(150)이 더 구비되는 것을 특징으로 하는 내연기관용 흡기압력제거 역류방지 장치.At the other end of the fixed tube 110, the wing communication (150) having a honeycomb (honeycomb) structure is further provided, characterized in that the intake pressure removal backflow prevention device for an internal combustion engine. 제1항에 있어서,The method of claim 1, 상기 고정관(110) 내부에 설치되고, 흡기의 유입방향으로 갈수록 단면적이 감소되도록 중심방향으로 경사지게 절곡되어 흡기의 속도를 증가시키며, 상기 고정관(110)의 내주면과의 사이에 고정관유동구(112)와 연통되는 제2역기류통로를 형성시키는 고정관날개(140")가 더 구비되는 것을 특징으로 하는 내연기관용 흡기압력제거 역류방지 장치.It is installed inside the fixed tube 110, bent inclined toward the center to reduce the cross-sectional area toward the inflow direction of the intake to increase the speed of the intake, between the fixed tube flow port 112 and the inner peripheral surface of the fixed tube 110 Intake pressure removing backflow prevention device for an internal combustion engine, characterized in that the fixed tube wing (140 ") is further provided to form a second backflow passage communicating. 제7항에 있어서,The method of claim 7, wherein 상기 고정관날개의 흡기 유입방향 끝단 내부에 허니콤(honeycomb) 구조를 갖는 날개연통이 더 구비되는 것을 특징으로 하는 내연기관용 흡기압력제거 역류방지 장치.Intake pressure removing backflow prevention device for an internal combustion engine, characterized in that the wing communication having a honeycomb (honeycomb) structure is further provided inside the end of the intake inlet direction of the fixed tube blade.
KR1020080017224A 2007-11-22 2008-02-26 Intake pressure elimination backflow prevention device for internal combustion engine Expired - Fee Related KR100953454B1 (en)

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PCT/KR2008/001614 WO2009066836A1 (en) 2007-11-22 2008-03-21 Apparatus for removing intake pressure and preventing backflow for internal combustion engines

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Publication number Priority date Publication date Assignee Title
JP2003002292A (en) * 2001-06-27 2003-01-08 Sanshin Ind Co Ltd Intake device of engine for water jet propulsion boat
KR100769700B1 (en) * 2007-06-15 2007-10-23 손춘남 Back pressure removal backflow prevention device
KR100878256B1 (en) 2007-11-22 2009-01-14 이지엘(주) Intake pressure elimination backflow prevention device for internal combustion engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003002292A (en) * 2001-06-27 2003-01-08 Sanshin Ind Co Ltd Intake device of engine for water jet propulsion boat
KR100769700B1 (en) * 2007-06-15 2007-10-23 손춘남 Back pressure removal backflow prevention device
KR100878256B1 (en) 2007-11-22 2009-01-14 이지엘(주) Intake pressure elimination backflow prevention device for internal combustion engine

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