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KR950001983Y1 - Swirling apparatus for air intake - Google Patents

Swirling apparatus for air intake Download PDF

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Publication number
KR950001983Y1
KR950001983Y1 KR92013507U KR920013507U KR950001983Y1 KR 950001983 Y1 KR950001983 Y1 KR 950001983Y1 KR 92013507 U KR92013507 U KR 92013507U KR 920013507 U KR920013507 U KR 920013507U KR 950001983 Y1 KR950001983 Y1 KR 950001983Y1
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South Korea
Prior art keywords
air
vortex
pack
internal combustion
exhaust
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KR92013507U
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Korean (ko)
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KR940003688U (en
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조병민
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조병민
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Priority to KR92013507U priority Critical patent/KR950001983Y1/en
Priority to EP93916261A priority patent/EP0604634A1/en
Priority to AU45870/93A priority patent/AU4587093A/en
Priority to PCT/KR1993/000060 priority patent/WO1994002735A1/en
Publication of KR940003688U publication Critical patent/KR940003688U/en
Application granted granted Critical
Publication of KR950001983Y1 publication Critical patent/KR950001983Y1/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
    • 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
    • F02M29/00Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture
    • F02M29/04Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having screens, gratings, baffles or the like
    • F02M29/06Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having screens, gratings, baffles or the like generating whirling motion of mixture
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/18DOHC [Double overhead camshaft]
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Processes For Solid Components From Exhaust (AREA)

Abstract

내용 없음.No content.

Description

내연기관용 공기와류 발생기Air Vortex Generator for Internal Combustion Engines

제1도는 본고안의 전체사시도.1 is a perspective view of the present article.

제2도는 본 고안의 주요요부인 공기와류 유도팩을 평면상에서 본 상세도.Figure 2 is a detailed view of the air vortex induction pack is a principal part of the subject innovation in plan view.

제3도는 본 고안을 자동차 및 내연기관의 공기 정화통을 통과한 연소공기 흡입호스(또는 배기구)에 고정 장착된 상태를 보여주는 일예시도.3 is an exemplary view showing a state in which the present invention is fixedly mounted to a combustion air intake hose (or exhaust port) that has passed through an air purifier of an automobile and an internal combustion engine.

제4도는 본 고안을 내연기관의 엔진에 설치한 실시예시도.Figure 4 is an embodiment of the present invention installed in the engine of the internal combustion engine.

* 도면의 주요부분에 대한부호의 설명* Explanation of the symbols for the main parts of the drawings

1 : 흡입호스(및 배기구) 10 : 공기유입소경제한판1: Suction hose (and exhaust port) 10: Air inlet station

11 : 공기유입구 12 : 간격지지핀11: air inlet 12: spacing support pin

20 : 공기와류유도팩 21 : 유입날개20: air vortex induction pack 21: inlet wing

22 : 원심력와류 유도날개 25 : 구심력와류발사구멍22: centrifugal vortex induction wing 25: centripetal vortex firing hole

24 : 공기저지판(원심와류의 구시와류의 공기 분리판)24: air blocking plate (air separation plate of old vortex of centrifugal vortex)

본 고안은 자동차 및 내연기관의 공기정화통을 통과한 연소공기의 흡기 호소중도 및 머플러의 배기구에 장착사용하는 것으로 엔진에 흡기되는 연소 공기가 벤튜리작용과 소용돌이 와류작용에 의해 보다 빠르게 소용돌이 흡기될 수 있도록 하여 ,연료(휘발유, 디젤유, LPG, 외)와 공기의 혼합효유를 높여 혼합가스의 연소폭발효율을 증대시켜 주고, 엔진의 배기구에서는 배기가스를 고속 와류시켜 배출하여 엔진의 연소성능을 향상토록 한 내연기관용의 공기 와류발생기에 관한 것이다.The present invention is used in the intake appeal of the combustion air passed through the air purifying cylinder of automobiles and internal combustion engines and the exhaust port of the muffler, so that the combustion air intake of the engine can be vortexed intake more rapidly by the venturi action and the vortex vortex action. Increase the combustion explosive efficiency of the mixed gas by increasing the mixed effective oil of fuel (petrol, diesel, LPG, etc.) and air, and improve the combustion performance of the engine by vortexing and exhausting the exhaust gas at the exhaust of the engine at high speed. An air vortex generator for internal combustion engines.

이를 좀더 상세히 설명하면, 흡입공기 또는 배기가스를 벤튜리 효과를 발생시키는 공기유입소경 제한판에 의하여 순간 유속을 일차적으로 증대시킨 다음 유속이 증대된 흡입공기 또는 배기가스가 공기 유입 소경제한판과 일정간격을 유지하고 있는 공과류 유도팩에 유도되면서 와류 현상으로 변환된 흡입공기 또는 배기가스가 급속히 소용도리 흡입되고 송요돌이 배출되므로서, 흡기시에는 연료와 공기의 혼합효율을 높여주며 시린더내의 공기 충진 비율을 높여 연료 절감의 효과와 엔진의 연소성능을 향상시켜 주고, 배기시에는 배기불량을 배제하도록 고안된 내연기관용의 공기와류 발생기이다.To explain this in more detail, the instantaneous flow rate is primarily increased by the air inlet diameter limiting plate that generates the intake air or exhaust gas, and then the intake air or exhaust gas having the increased flow rate is consistent with the inflow limiting economy. Intake air or exhaust gas which is converted into vortex phenomena is rapidly sucked up and exhausted by the turbulence while maintaining the gap. Therefore, during intake, the mixing efficiency of fuel and air is increased and the air in the cylinder is increased. It is an air vortex generator for internal combustion engines designed to increase the filling ratio, improve fuel efficiency and improve the combustion performance of the engine, and eliminate exhaust failures when exhausting.

각종의 연료(휘발유, 경유, LPG, 수소가스외)를 사용하는 내연기관의 연소공기의 흡기 및 배기에 와류를 발생시켜 연료와 공기의 소용돌이 혼합 비율을 급속히 향상시키므로서 일정한 용량의 시린더조건내에서의 연소폭발반응속도를 높여 주게되면 보다 높은 효율의 엔진 출력(상대성이 이론인 E-mc2의 원리적용)을 얻을 수 있으며 불완전연소의 매연공해를 감소시키고, 또한 소용돌이 배기로 엔진의 배기 성능을 향상 시킬 수 있다는 것은 과학적 사실로 알려져 있다.Vortex is generated in the intake and exhaust of the combustion air of the internal combustion engine using various fuels (petrol, diesel, LPG, hydrogen gas, etc.) to rapidly improve the vortex mixing ratio of fuel and air, while maintaining a constant capacity in the cylinder condition. Increasing the combustion explosive reaction rate at will result in higher efficiency engine output (applied to the principle of relativity, E-mc 2 ), reducing the soot pollution of incomplete combustion, and vortex exhaust. It is known to be a scientific fact that it can improve.

이분양의 배경기술로서 과거에는 와류실식 엔진(TURBULENCE CHAMBER ENGINE)등이 있었으며, 현재는 더욱 발전되어 내연기관의 시린더 본체에 소용돌이 흡기 및 배기의 구조를 채택한 시린더내의 수평 와류발생형인 DOHC 앤진등이 있다.In the past, as a background technology of this predecessor, there were TURBULENCE CHAMBER ENGINE, etc., and now, DOHC ENGINE, which is a horizontal vortex generation type in the cylinder, which is further developed and adopts the structure of swirl intake and exhaust in the cylinder body of the internal combustion engine. There is this.

또한, 각종의 종래 내연기관 및 자동차 엔진의 흡기부(에어크리너, 카브레이터, 또는 흡기관)와 배기부(배기관)에 동력 회전식 또는 고정장치식의 방법으로된 여러형태의 공기와류발생장치를 설치하여 엔진의 연소성능개선을 목적으로 하는 국외 및 국내의 여러 특허고안 등이 이미 실용화 사용되고 있다.In addition, various types of air vortex generators are provided in the intake part (air cleaner, carburetor or intake pipe) and exhaust part (exhaust pipe) of various conventional internal combustion engines and automobile engines by the method of power rotation or fixed device type. In order to improve the combustion performance of the engine, a number of foreign and domestic patent proposals have already been put into practical use.

이러한 내연기관의 와류발생장치에 관한 고안들로서 미국특허 제2,017,043호 미국특허 제3,877,907호, 미국 특허 제4,962,642호, 일본공개특허공보 번호 소58-13,122호 한국실용신안공보공고번호 76-1369호, 한국특허공부 91-444호, 한국공개특허공보 88-14,235호, 일본공개실용신안공보 소60-30, 322호등이 공지된다 있다.Designs related to the vortex generator of such an internal combustion engine include US Patent No. 2,017,043 US Patent No. 3,877,907, US Patent No. 4,962,642, and Japanese Patent Application Publication No. So 58-13,122, Korean Utility Model Publication No. 76-1369, Korea Japanese Patent Application Laid-Open No. 91-444, Korean Laid-Open Patent Publication No. 88-14,235, Japanese Laid-Open Utility Model Publication No. 60-30, 322 and the like are known.

이상의 고안등에서 채택한 와류발생장치의 구조형태로서는 십자(+)형의 와류발생장치 프로펠러(PROPELLER)형의 와류발생장치, 방사상팬(RADLIAL FAN)형이 와류 발생장치, 나선형 파이프(SPIRALPIPE)형의 와류발생장치, 방사상 판체 배열을 이용한 와류발생장치등이 있으나, 나선형 또는 방사상 판체 배열식의 와류구조형태에서는 나선 또는 방사선을 따라 공기가 흐르도록 형성된 구조로 공기의 와류 유도 효율이 빈약한 결함이 있었으며, 방사상 팬(방사사와류 날개)형으로 된것은 와류팬의 중앙저면부에 저기압이 생성 흡착되어 급기 속도가 빠르지 못한 결함이 있었다.As the structure of the vortex generator which is adopted in the above, etc., the vortex generator of the cross type (PROPELLER), the vortex generator of the radial fan type, the vortex generator of the radial fan type, the vortex of the spiral pipe type (SPIRALPIPE) There are generators and vortex generators using radial plate arrays. However, in the spiral or radial plate array vortex structure, air flows along spirals or radiation, and the vortex induction efficiency of air is poor. The radial fan type had a defect in which the air supply speed was not high due to the low pressure generated and adsorbed on the central bottom of the vortex fan.

본 고안은 이같은 구조적 결함을 해소하기 위해 흡입공기와 배기가스가 흡기관 및 배기관에 고정밀착 설치된 본 고안의 공기와류발생기의 공기와류 유도팩을 거쳐 소용돌이 와류로 변환될때, 원심력 와류와 저기압 중심의 구심력 와류로 순간 분리되며 통과하도록 하여 한층 급기속도를 빠르게 개량한 고안으로 기존의 여러 고안들과 다른 특징을 원심력과 구심력의 와류로 분리되는 복합와류를 이용하는 기술로서 상세히 설명하면 다음과 같다.In order to solve such a structural defect, the centrifugal vortex and the low pressure centered centripetal force when the intake air and exhaust gas are converted into the vortex vortex through the air vortex induction pack of the air vortex generator of the present invention installed in close contact with the intake pipe and the exhaust pipe The instantaneous separation by passing through the vortex as a design to improve the air supply speed is further improved as a technology using a complex vortex separated from the existing several designs and vortices of centrifugal force and centripetal force in detail as follows.

공기정화기를 통과한 흡입공기 또는 배기가스의 호스(또는 배기구)에 순간 유속을 증가시켜주는 벤튜리 효과를 내는 공기유입소경 제한판과 지지핀으로 일정 간격을 유지하게 된 원심력 소용돌이를 발생시키는 외측구조의 와류유도 날개부와 중심에 구심력 소용돌이를 발생키는 저기압 구멍이 있는 공기분리판(공지 저지판)의 내측 구조로된 공기와류유도팩을 연결한 공기와류 발생기를 장착하여 보다 강력한 저기압중심의 구심력 소용돌이를 얻도록 한 2중의 복합 와류발생 고안인 것이다.Outer structure that generates centrifugal force vortex that maintains a certain distance with air inlet diameter limiting plate and support pin which has venturi effect to increase instantaneous flow rate in the intake air or exhaust hose (or exhaust port) that passed through air purifier More powerful low pressure centered centripetal force by installing an air vortex generator connected to an air vortex induction pack that has an inner structure of an air separation plate (notice blocking plate) with a low pressure hole that generates a vortex vortex in the center It is a double complex vortex generation design to obtain a vortex.

본 고안의 이러한 원리는 마치 M16총열강선 역활의 원심력 소용돌이 발생작용으로, 저기압 중심의 구심력 소용돌이 실탄을 고속발사 하는 것과 유사한방법으로 구심력 중심의 강력한 소용돌이 와류를 얻어 내연기관의 연소성능향상에 사용토록 고안한 것으로 첨부 도면에 의거 상세히 설명하면 다음과 같다.This principle is designed to be used for improving the combustion performance of internal combustion engines by obtaining a strong vortex vortex centered on the centripetal force in a similar way to the high-speed firing of low pressure centered centripetal vortex shells. When described in detail based on the accompanying drawings as follows.

제1도는 본 고안의 전체 사시도이다.1 is an overall perspective view of the present invention.

공기유입공(110이 통공된 벤튜리(VENTURi) 효과를 내는 공기유입 소경제한판(10)을 지지판(12)에 의하여 공기와류 유도팩(20)과 적정한 간격을 유지하도록 하되, 공기와류유도팩(20)은 중심에 적정 규격의 저기압 구멍(25)를 갖는 공기저지판 (또는 공기분리판)(24)의 외주에 평면 및 저면 16면 (또는 다수의 면)을 갖는 유입날개(21)가 경사지게 입설되고, 그와 연장되는 유도날개(22)와 외향으로 경사지게 형성되는 공기 배출공간(23)을 형성하여서 된 것이다.The air inlet hole (110) through the vent inlet (VENTURi) effect is to maintain a proper distance from the air vortex induction pack 20 by the support plate 12, but the air vortex induction pack 10 20 is an inlet blade 21 having a flat surface and a bottom face 16 (or a plurality of faces) on the outer circumference of the air blocking plate (or air separation plate) 24 having a low-pressure hole 25 of a suitable standard in the center. It is made by forming the air discharge space 23 formed inclined inclined, and the induction wing 22 extending therefrom and inclined outward.

이와같이 구성된 본 고안의 작용효과를 설명하면 다음과 같다.Referring to the effect of the present invention configured as described above are as follows.

제3에는 본 고안이 흡입호스(1)에 장착된 상태를 예시하고 있으며, 제2도는 공기와류 유도팩(20)을 평면상에서 본 것이다.The third embodiment illustrates a state in which the present invention is mounted on the suction hose 1, and FIG. 2 shows the air vortex induction pack 20 in a plan view.

공기가 흡입호스(1)의 선단에 인입되면, 인입된 공기는 벤튜리(VENTuRi)효과를 내는 공기유입소경 제한판(10)에 의해 일단 저지되어 축소된 공기 유입공(11)을 통과하면서 유속이 빨라진 상태에서 공기와류 유도팩(20) 내에 유입되는데, 여기에 유입된 공기는 중심에 저기압 소용돌이 구멍(25)를 갖는 공기저지판(24)에 저지되어 유입날개(21) 사이에 공존하면서, 유도날개(22)에 유도되어 원심력의 와류(소용돌이)현상을 발생시키면서 공기 배출공간(23)을 통해 유입호스(1)의 후단으로 유속이 급속히 빨라진 와류현상으로 변환되어 급기되고, 공기 저지판(24)의 중심구멍(25)에서는 고속의 저기압 중심의 구심력 와류가 발생되어 유입호스(1)의 후단으로 발사되어 내연기관내의 연료(휘발유, 디젤유, LPG 외)와 소용돌이 혼합 유입하게 된다.When the air enters the front end of the suction hose 1, the drawn air is blocked by the air inlet diameter limiting plate 10 having the Venturi (VENTuRi) effect and passes through the reduced air inlet hole 11 to flow velocity. In this accelerated state is introduced into the air vortex induction pack 20, the air introduced therein is blocked by the air blocking plate 24 having a low pressure vortex hole 25 in the center and coexists between the inlet vanes 21, Induced by the guide vane 22, while generating a vortex (swirl) phenomenon of centrifugal force is converted into the vortex phenomenon, the flow velocity is rapidly accelerated to the rear end of the inlet hose (1) through the air discharge space 23, the air blocking plate ( In the center hole 25 of 24, a high-speed, low-pressure central centripetal vortex is generated, which is fired to the rear end of the inlet hose 1, and vortex-mixed with the fuel (petrol, diesel, LPG, etc.) in the internal combustion engine.

이와 같이 하여 내연기관내에 유입된 와류공기는 연료와 높은 혼합비율로 혼합되어 시린더 내에서 빠른 반응속도로 폭발하므로 엔진의 연소성능 개선과 출력에너지 향상의 효과를 얻게된다.In this way, the vortex air introduced into the internal combustion engine is mixed with fuel at a high mixing ratio to explode at a high reaction rate in the cylinder, thereby improving the combustion performance and output energy of the engine.

또, 머플러의 배기구에 설치하였을 경우에는 시린더내의 배기가스를 급속히 와류시켜 배제하도록 하므로서 배기불량과 배기소음을 줄일 수 있도록 고안된 것이다.In addition, when installed in the exhaust port of the muffler, it is designed to reduce the exhaust failure and exhaust noise by vortexing to remove the exhaust gas in the cylinder rapidly.

Claims (1)

공기유입공(11)이 통공된 벤튜리(VENTuRi)효과를 내는 공기유입소경 제한판(10)을 간격 지지핀(12)에 의하여 공기와류 유도팩(2)과, 적정한 간격을 유지하도록 하되, 공기와류 유도팩(20)은 중심부에 적정 구경의 저기압구멍(25)를 갖는 공기저지판(공기분리판)(24)의 외주에 평면 및 저면의 16면(또는 다수의 면)을 갖는 유입날개(21)가 경사지게 입설되고 그와 연장되는 유도날개(22)가 외향으로 경사지게 형성되어 공기배출공간(23)을 형성하여서 된 원심과 구심의 2종 복합와류를 발생시키는 내연기관용 공기와류 발생기.The air inlet hole limiting plate 10 having the venturi (VENTuRi) effect through the air inlet hole (11) by the spacing support pin 12 to maintain the proper space between the air vortex induction pack (2), The air vortex induction pack 20 has an inlet vane having 16 planes (or a plurality of planes) of a flat surface and a bottom surface on the outer circumference of the air blocking plate (air separation plate) 24 having a low pressure hole 25 having an appropriate diameter in the center thereof. An air vortex generator for an internal combustion engine which generates two kinds of vortices of centrifugal and centripetal by forming an air discharge space 23 by inclined outwardly and inducing wings 22 extending therefrom.
KR92013507U 1992-07-22 1992-07-22 Swirling apparatus for air intake KR950001983Y1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
KR92013507U KR950001983Y1 (en) 1992-07-22 1992-07-22 Swirling apparatus for air intake
EP93916261A EP0604634A1 (en) 1992-07-22 1993-07-21 Air whirlpool generator for an internal combustion engine
AU45870/93A AU4587093A (en) 1992-07-22 1993-07-21 Air whirlpool generator for an internal combustion engine
PCT/KR1993/000060 WO1994002735A1 (en) 1992-07-22 1993-07-21 Air whirlpool generator for an internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR92013507U KR950001983Y1 (en) 1992-07-22 1992-07-22 Swirling apparatus for air intake

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KR940003688U KR940003688U (en) 1994-02-21
KR950001983Y1 true KR950001983Y1 (en) 1995-03-23

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KR20010025656A (en) * 2001-01-15 2001-04-06 지정현 The rapid eddy device for inhaled air of automobile
CN1539058A (en) 2001-06-29 2004-10-20 赫罗・普拉桑塔・维贾亚 Air-stirring blade for internal combustion engine
KR200268794Y1 (en) 2001-10-23 2002-03-18 김세영 Wing structure of air swirling device for internal combustion engine
US7055512B2 (en) 2002-08-16 2006-06-06 The Fuel Genie Corporation Device and method for changing angular velocity of airflow

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GB645812A (en) * 1948-10-21 1950-11-08 William George Thompson Improvements in or relating to charge mixing devices for internal combustion engines
CH284184A (en) * 1950-08-22 1952-07-15 Kuhn Emil Device for mixing the fuel-air mixture in the intake line of an internal combustion engine.
FR2265997A1 (en) * 1974-03-29 1975-10-24 Reissmueller Anton
US4094291A (en) * 1976-02-23 1978-06-13 Ford Motor Company Apparatus for mixing a vaporized liquid fuel with air
US4222456A (en) * 1977-04-25 1980-09-16 Kasper Witold A Sound-suppressing and back pressure-reducing apparatus and method

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KR940003688U (en) 1994-02-21
WO1994002735A1 (en) 1994-02-03
AU4587093A (en) 1994-02-14

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