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WO2011016619A2 - Centrifugal pump having an improved impeller - Google Patents

Centrifugal pump having an improved impeller Download PDF

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Publication number
WO2011016619A2
WO2011016619A2 PCT/KR2010/004363 KR2010004363W WO2011016619A2 WO 2011016619 A2 WO2011016619 A2 WO 2011016619A2 KR 2010004363 W KR2010004363 W KR 2010004363W WO 2011016619 A2 WO2011016619 A2 WO 2011016619A2
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WO
WIPO (PCT)
Prior art keywords
blade
impeller
centrifugal pump
rotation
feather
Prior art date
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PCT/KR2010/004363
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French (fr)
Korean (ko)
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WO2011016619A3 (en
Inventor
안병무
Original Assignee
(주)안국밸브
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Publication of WO2011016619A2 publication Critical patent/WO2011016619A2/en
Publication of WO2011016619A3 publication Critical patent/WO2011016619A3/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/2261Rotors specially for centrifugal pumps with special measures
    • F04D29/2288Rotors specially for centrifugal pumps with special measures for comminuting, mixing or separating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2210/00Working fluids
    • F05D2210/10Kind or type
    • F05D2210/11Kind or type liquid, i.e. incompressible
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/60Fluid transfer
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00Rotary kinetic fluid motors or pumps
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S417/00Pumps
    • Y10S417/90Slurry pumps, e.g. concrete

Definitions

  • the present invention relates to a centrifugal pump having improved efficiency, and improves the pumping efficiency and performance by improving the shape of an impeller provided in the housing of the centrifugal pump.
  • Pumps for sucking and transporting fluids are broadly classified according to their principle structure or power source, and are related to centrifugal pumps which are cost-effective pumps by structural classification.
  • impellers for centrifugal pumps are radial type impellers and mixed type impellers with side plates on the suction side, and semi open impellers for slurry transfer. Impellers with only side plates on the boss side) and open impellers (without suction side plates or with minimal side plates on the boss side).
  • Hermetic impeller is suitable for the transfer of solids-free water (general fluid), semi-open impeller is turbid sewage, water transfer (turbid fluid) for drainage, open impeller is sewage, sludge, slurry ( Suitable for the transfer of fluids (solid fluids) containing slurries).
  • Impeller is a configuration that functions to pump the liquid by generating a centrifugal force while rotating inside the casing, the most important part to act as a pump, and also has the greatest impact on the characteristics of the pump. Therefore, depending on the structure of the impeller, its use is different and the effect will be enormous.
  • volute pump A pump with no guide vane on the outer perimeter of the impeller and a vortex chamber directly adjacent to the outer circumference is called a volute pump, which is generally used for low heads.
  • the impeller 20a (hereinafter, referred to as 'prior art 1') provided in the conventional centrifugal pump, as shown in FIG.
  • liquids containing solids in the form of vanes of one vane body, two or more outer curves or spiral shapes, or more than 10% The liquid is also worn out so that the air outlet 14, which is spaced apart from the impeller 20a, the vane blade 22a and the inner wall of the casing 12a, is blocked, damaged, or entangled, and is fixed to the fixed cavitation.
  • the suction action becomes impossible and at the same time wears out and eventually damages the impeller 20a.
  • the casing (12a) to the inner wall is correlated with damage to the suction and discharge of the fluid.
  • the blade feather (22a) is embossed to be easily worn, there is a problem that the pump efficiency is low, the use is limited only in the case of low lift.
  • Korean Patent No. 732196 (filed in 2005) (hereinafter referred to as 'Prior Technology 2') solves the problems of the existing centrifugal pumps, such as wear, reduced suction force, low efficiency, and durability of parts. 2 and 3, an impeller 20b for a slurry pump, in which a groove 24b is formed in a lengthwise direction on an upper surface of a radially protruding wing feather 22b. ) has been disclosed.
  • Figure 2 shows a cross-sectional view of a centrifugal pump with an impeller 20b
  • Figure 3 is a perspective view showing an impeller according to the prior art 2.
  • the present invention has been made to solve the problems of the prior art as described above, impellers particularly suitable for the transport of fluids (solid fluid) containing sewage, sludge, slurry (slurry), etc. It is an object to propose a centrifugal pump having.
  • an object of the present invention is to propose a centrifugal pump that can improve the suction force and efficiency compared to the prior art.
  • the centrifugal pump according to the present invention is characterized by having an impeller of an improved structure. That is, the impeller wing of the present invention is formed with a concave groove 124 is formed long in the longitudinal direction on the front surface thereof, based on the concave groove 124, the height of the blade feather in the rotational direction (Ha) ) Is formed low, and the wing feather height (Hb) in the opposite direction of rotation is formed high.
  • a recess 132 and a protrusion 133 are formed on the side surface in the rotational direction of the vane 122 to easily grind or cut the solids into which the vane is introduced. It is characterized by having.
  • the centrifugal pump according to the present invention is a centrifugal pump particularly suitable for transporting fluids (solid fluids) containing sewage, sludge, slurry, etc., with much lower initial starting power than the prior art. It is possible to start the drive, high efficiency, it is possible to obtain the effect of increasing the suction force of the fluid.
  • the centrifugal pump according to the present invention has a characteristic effect that can form an uneven portion 132, 133 on the front side of the wing feather, effectively crush the solid.
  • FIG. 1 is a cross-sectional view of the main part showing an embodiment of a conventional centrifugal pump
  • Figure 4 is a perspective view showing a schematic shape of the centrifugal pump impeller according to the present invention
  • FIG. 5 is a cross-sectional view taken along the line A-A in FIG.
  • FIG. 6 is a cross-sectional view taken along the line B-B in FIG.
  • Figure 7 is a perspective view showing the auxiliary feather formed on the back of the impeller according to the present invention.
  • Figure 4 is a perspective view showing a schematic shape of the centrifugal pump impeller according to the present invention
  • Figure 5 is a cross-sectional view taken along the line A-A in Figure 4
  • Figure 6 is a cross-sectional view taken along the line B-B in FIG.
  • a centrifugal pump includes a housing having a suction port and a discharge port, and an impeller 120 provided inside the housing and rotating by a driving means.
  • the impeller 120 includes a plurality of wing feathers 122 extending radially at the same angle from the center of rotation, and the shaft hole 130 at the center thereof.
  • the drive shaft is exposed to the inside of the housing, the shaft hole of the impeller is fitted to the drive shaft is coupled.
  • the housing is an annular half-volute type, and in the low pressure part, the clearance between the inner diameter of the housing and the outer diameter (end feather end surface) of the impeller 120, that is, the vortex casing is Although it is very narrow, it is a semivolute type in which the size of the vortex chamber becomes larger as the inner diameter of the housing gradually increases toward the high pressure part.
  • the concave groove 124 is formed in the front surface (surface) of the impeller wing feathers long along the longitudinal direction of the wing feathers.
  • the concave groove 124 is configured to be gradually deeper as it moves away from the center of rotation, so that the fluid introduced through the suction port can be easily transferred to the vortex chamber through the concave groove 124, this concave groove 124 Has a function as an induction furnace.
  • the blade feather 122 is divided into the front portion 123a and the rear portion 123b by the concave groove 124, and the impeller based on the concave groove 124 in one wing feather.
  • the portion located on the side in which the direction of rotation is referred to as the front portion 123a, and the portion located on the opposite side of the front portion with respect to the concave groove will be referred to as the rear portion 123b.
  • the height Ha (also referred to as 'thickness') of the front part (the rotational direction) of the vane is formed to be lower than the height of the feather tip Hb of the rear part.
  • the centrifugal pump according to the present invention configured as described above has a torque at the moment when the pump starts operation as compared with the case where the height of the vane blade of the front part (the rotational direction) and the height of the vane blade of the rear part (the opposite direction) are the same. It can mitigate and lower the starting power required to start a stationary pump, especially when used in high viscosity liquids.
  • the impeller 120 is formed through the suction port.
  • the solids introduced into the center portion are crushed or cut by the uneven parts 132 and 133 formed on the front side of the wing feathers while being transferred to the vortex chamber along the wing feathers.
  • the recess 132 and the protrusion 133 are preferably formed on the side surface of the wing feather front part. If the concave-convex portion is formed on the front side of the wing feather rear part, the fluid may be disturbed by the concave-convex portion while the fluid introduced through the suction port is transferred to the vortex chamber through the concave groove 124. In this case, the suction force may be a cause of deterioration, which is not preferable.
  • the protrusion 133 is formed at the end of the blade feather, by using a strong centrifugal force acting on the blade feather tip and the impact force of the protrusion 133, the solids that are not crushed by the recess 132 to strongly The effect of grinding can be obtained.
  • the auxiliary feather 131 is further provided on the back of the wing feather.
  • the back of the impeller is made of a flat plane, so that the contact area with the inner surface of the casing is large, which not only causes a large torque for initial start-up, but also acts as a cause of output loss due to frictional force, resulting in low efficiency.
  • the auxiliary collar in the present invention can achieve the effect of increasing the suction force of the fluid while solving the above problems.
  • the auxiliary feather 131 in the present invention the width and thickness is formed to be constant is provided on the back of each wing feather 122, respectively, the further away from the rotation center, the opposite the rotation It consists of a shape that curves gently toward the direction.
  • the auxiliary feather 131 having such a configuration can minimize the gap between the impeller and the casing wall, and reduce the friction area with the casing wall. Furthermore, the fluid flowing between the wing feathers and the wing feathers effectively flows into the vortex chamber. It will be pushed out.
  • the centrifugal pump according to the present invention configured as described above has the characteristic effect of effectively forming the uneven parts 132 and 133 on the front side of the blade feather, which can effectively crush the solids, and improve the suction force and efficiency compared to the prior art. It is particularly useful as a pump for conveying a fluid (solid fluid) containing sewage, sludge, slurry, and the like.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The centrifugal pump of the present invention has an impeller of an improved construction. More specifically, the impeller of the present invention has a blade wherein the front surface comprises a sunken recess (124) formed extending in the length direction, and, with respect to the sunken recess (124), the height (Ha) of the blade on the side in the direction of rotation is formed so as to be low while the height (Hb) of the blade on the opposite side to the direction of rotation is formed so as to be high, and wherein the face of the blade (122) on the side in the direction of rotation is formed with a concave part (132) and a convex part (133), such that the blade has a function whereby solid matter which has flowed in can easily be ground up or cut. The centrifugal impeller of the present invention, which is constituted in this way, has the concavo-convex parts (132)(133) formed in the front face of the blade and has a characteristic effect whereby it can effectively grind solid matter, and thus it is particularly useful as a pump for conveying fluids (solids-laden fluids) containing dirty water, sludge, slurry and the like.

Description

개선된 임펠러를 구비한 원심펌프Centrifugal pumps with improved impeller
본 발명은 효율을 향상시킨 원심펌프(Centrifugal Pump)에 관한 것으로서, 원심펌프의 하우징 내부에 구비되는 임펠러(impeller)의 형상을 개선하여 펌핑 효율과 성능을 개선시킨 것이다.The present invention relates to a centrifugal pump having improved efficiency, and improves the pumping efficiency and performance by improving the shape of an impeller provided in the housing of the centrifugal pump.
유체를 흡입하여 이송하는 펌프는, 그 원리 구조에 따라 또는 동력원에 따라 크게 분류되는데, 여기서는 구조상 분류에 의한 비용적식 펌프인 원심펌프에 관한 것이다.Pumps for sucking and transporting fluids are broadly classified according to their principle structure or power source, and are related to centrifugal pumps which are cost-effective pumps by structural classification.
원심펌프의 가장 일반적인 임펠러는 용도별 형식에 따라, 레이디얼 임펠러와 혼류(Mixed)형 임펠러가 흡입측에 측판이 있는 구조로 사용되고 있는 밀폐형 임펠러와, 슬러리 이송에 사용되고 있는 세미 오픈 임펠러(Semi Open impeller : 보스측의 측판만 완전히 있는 임펠러)와, 오픈 임펠러(Open impeller :흡입측의 측판이 없는, 또는 보스측의 측판도 최소한으로 한 임펠러)가 있다.The most common impellers for centrifugal pumps are radial type impellers and mixed type impellers with side plates on the suction side, and semi open impellers for slurry transfer. Impellers with only side plates on the boss side) and open impellers (without suction side plates or with minimal side plates on the boss side).
밀폐형 임펠러는 고형물이 없는 물(일반유체)의 이송에 적합하고, 세미 오픈 임펠러는 혼탁한 오수, 배수용의 물이송(혼탁유체), 오픈 임펠러는 오수(汚水), 오니(汚泥), 슬러리(Slurry) 등이 함유한 유체(고형물 유체)의 이송에 적합하다.Hermetic impeller is suitable for the transfer of solids-free water (general fluid), semi-open impeller is turbid sewage, water transfer (turbid fluid) for drainage, open impeller is sewage, sludge, slurry ( Suitable for the transfer of fluids (solid fluids) containing slurries).
임펠러는 케이싱 내부에서 회전하면서 원심력을 발생하여 액체를 압송하는 기능을 하는 구성으로서, 펌프 작용을 하는 가장 중요한 부분이며 또한 펌프의 특성에 가장 큰 영향을 미친다. 그러므로 임펠러의 구조에 따라 그 용도가 달라지게 마련이며 그 효과는 엄청나다 할 것이다.Impeller is a configuration that functions to pump the liquid by generating a centrifugal force while rotating inside the casing, the most important part to act as a pump, and also has the greatest impact on the characteristics of the pump. Therefore, depending on the structure of the impeller, its use is different and the effect will be enormous.
임펠러의 바깥 둘레에 안내깃이 없고 바깥둘레에 바로 접하여 와류실이 있는 펌프를 볼류트 펌프(Volute Pump)라 하는데, 일반적으로 양정이 낮은 것에 사용된다.A pump with no guide vane on the outer perimeter of the impeller and a vortex chamber directly adjacent to the outer circumference is called a volute pump, which is generally used for low heads.
그러나, 종래의 원심펌프에 구비되는 임펠러(20a)(이하 '종래기술1'이라 한다)는, 도 1에 도시된 바와 같이, 유체의 마찰을 받는 바깥 곡선(베인 곡선) 날개가 각기 이송유체와 특성에 따라 1개의 베인(vane) 몸체에 360°의 깃을 형성하고 있는 것부터 2개 혹은 다수의 바깥 곡선을 가진 날개이거나 혹은 나선형의 곡선을 가진 형태들로 고형물이 혼입된 액체나 10% 이상의 혼기액도 이에 대한 마모가 심하여 임펠러(20a) 날개 깃(22a)과 케이싱(12a) 내벽과의 이격 공간인 흡출구(14)가 막히거나, 파손되며 엉겨붙은 뿐만 아니라 고정 공동현상(Fixed cavitation)에 의하여 흡입작용이 불가능하게 되는 동시에 마모되고 결국 임펠러(20a)를 파손시킨다. 그와 상관된 케이싱(12a) 내벽까지 파손되어 유체의 흡입과 토출에 악영향을 미치는 문제점이 있었다.However, the impeller 20a (hereinafter, referred to as 'prior art 1') provided in the conventional centrifugal pump, as shown in FIG. Depending on the characteristics, liquids containing solids in the form of vanes of one vane body, two or more outer curves or spiral shapes, or more than 10% The liquid is also worn out so that the air outlet 14, which is spaced apart from the impeller 20a, the vane blade 22a and the inner wall of the casing 12a, is blocked, damaged, or entangled, and is fixed to the fixed cavitation. As a result, the suction action becomes impossible and at the same time wears out and eventually damages the impeller 20a. There was a problem in that the casing (12a) to the inner wall is correlated with damage to the suction and discharge of the fluid.
즉, 상기 날개 깃(22a)이 양각으로 형성되어 쉽게 마모되며, 펌프 효율이 낮고, 저양정의 경우에만 사용이 한정되는 문제점이 있었다.That is, the blade feather (22a) is embossed to be easily worn, there is a problem that the pump efficiency is low, the use is limited only in the case of low lift.
이러한 문제를 해결하기 위해, 한국 등록특허 제732196호(2005년 출원)(이하 '종래기술2'라 한다)에서는 기존의 원심 펌프의 문제점인 마모와 흡인력 저하, 저효율성 문제를 해결하고 부품의 내구성을 향상시키기 위해, 도 2 및 도 3에 도시된 바와 같이, 방사상으로 돌출되는 날개 깃(22b)의 상부면에 길이방향으로 음각 형성된 홈부(24b)가 형성된 슬러리 펌프(Slurry pump)용 임펠러(20b)가 개시된 바 있다. In order to solve this problem, Korean Patent No. 732196 (filed in 2005) (hereinafter referred to as 'Prior Technology 2') solves the problems of the existing centrifugal pumps, such as wear, reduced suction force, low efficiency, and durability of parts. 2 and 3, an impeller 20b for a slurry pump, in which a groove 24b is formed in a lengthwise direction on an upper surface of a radially protruding wing feather 22b. ) Has been disclosed.
도 2는 임펠러(20b)가 구비된 원심펌프의 단면도를 도시한 것이며, 도 3은 상기 종래기술2에 의한 임펠러를 도시한 사시도면이다.Figure 2 shows a cross-sectional view of a centrifugal pump with an impeller 20b, Figure 3 is a perspective view showing an impeller according to the prior art 2.
그러나, 종래기술2의 경우에도 양정이 별로 증가되지 않는 단점이 있을 뿐만 아니라, 원심펌프의 동작 개시에서부터 정상 회전속도에 도달하기까지 걸리는 시간이 길고, 날개 깃(22b)과 케이싱(12b) 내벽 사이의 밀착면적이 커서 초기 운전에 큰 소비전력이 요구되는 등의 단점이 지적되고 있다.However, in the case of the related art 2, not only does the head not increase much, but also it takes a long time from the start of the operation of the centrifugal pump to reach the normal rotational speed, and between the blade vane 22b and the inner wall of the casing 12b Its disadvantage is that large power consumption is required for the initial operation due to its large contact area.
특히, 오수(汚水), 오니(汚泥), 슬러리(Slurry) 등이 함유된 유체(고형물 유체)의 이송용으로 사용되는 원심펌프의 경우에는 고형물이 임펠러(20b)의 날개 깃(22b)과 날개 깃(22b)의 사이 또는 날개 깃(22b)의 뒷면(25b)과 케이싱 내벽(112b) 사이에 끼여 흡인력 저하의 원인이 되기도 하며, 심지어 펌프 고장을 야기하기도 하는 문제가 많다.In particular, in the case of a centrifugal pump used for transporting a fluid (solid fluid) containing sewage, sludge, slurry, and the like, solids are contained in the vane blades 22b and the wings of the impeller 20b. There are many problems that can be caught between the feather 22b or between the back surface 25b of the wing feather 22b and the casing inner wall 112b, causing a decrease in suction force, and even causing a pump failure.
본 발명은 상기와 같은 종래기술들의 문제점을 해결하기 위해 안출된 것으로서, 오수(汚水), 오니(汚泥), 슬러리(Slurry) 등이 함유된 유체(고형물 유체)의 이송용에 특히 적합한 임펄러를 갖는 원심펌프를 제안하는 것을 목적으로 한다.The present invention has been made to solve the problems of the prior art as described above, impellers particularly suitable for the transport of fluids (solid fluid) containing sewage, sludge, slurry (slurry), etc. It is an object to propose a centrifugal pump having.
또한, 본 발명은 종래기술에 비해 흡인력과 효율성을 향상시킬 수 있는 원심펌프를 제안하는 것을 목적으로 한다.In addition, an object of the present invention is to propose a centrifugal pump that can improve the suction force and efficiency compared to the prior art.
상기와 같은 목적을 구현하기 위해, 본 발명에 의한 원심펌프는 개선된 구조의 임펠러를 구비함을 특징으로 한다. 즉, 본 발명에 의한 임펠러의 날개 깃에는 그 앞면에 오목홈(124)이 그 길이방향으로 길게 형성되어 이루어지는데, 상기 오목홈(124)을 기준으로 하여, 회전방향 쪽의 날개 깃 높이(Ha)를 낮게 형성하고, 회전 반대방향 쪽의 날개 깃 높이(Hb)를 높게 형성한 것을 특징으로 한다.In order to achieve the above object, the centrifugal pump according to the present invention is characterized by having an impeller of an improved structure. That is, the impeller wing of the present invention is formed with a concave groove 124 is formed long in the longitudinal direction on the front surface thereof, based on the concave groove 124, the height of the blade feather in the rotational direction (Ha) ) Is formed low, and the wing feather height (Hb) in the opposite direction of rotation is formed high.
또한, 상기 날개 깃(122)의 회전방향 쪽 측면에는 요부(凹部)(132) 및 돌출부(凸部)(133)를 형성하여, 이 날개 깃이 유입된 고형물을 용이하게 분쇄 또는 절단하는 기능을 갖도록 한 것을 특징으로 한다.In addition, a recess 132 and a protrusion 133 are formed on the side surface in the rotational direction of the vane 122 to easily grind or cut the solids into which the vane is introduced. It is characterized by having.
이 외에도 본 발명의 목적을 달성하기 위한 구체적인 수단들이 발명의 상세한 설명에서 제시될 것이다.In addition, specific means for achieving the object of the present invention will be presented in the detailed description of the invention.
본 발명에 의한 원심펌프는 오수(汚水), 오니(汚泥), 슬러리(Slurry) 등이 함유된 유체(고형물 유체)의 이송용에 특히 적합한 원심펌프로서, 종래기술에 비해 훨씬 적은 초기 기동전력으로도 구동개시가 가능하며, 효율성이 높고, 유체의 흡입력을 증대시키는 효과를 얻을 수 있다.The centrifugal pump according to the present invention is a centrifugal pump particularly suitable for transporting fluids (solid fluids) containing sewage, sludge, slurry, etc., with much lower initial starting power than the prior art. It is possible to start the drive, high efficiency, it is possible to obtain the effect of increasing the suction force of the fluid.
특히, 본 발명에 의한 원심펌프는 날개 깃의 전방 측면에 요철부(132)(133)를 형성하여, 고형물을 효과적으로 분쇄할 수 있는 특징적 효과를 갖는다.In particular, the centrifugal pump according to the present invention has a characteristic effect that can form an uneven portion 132, 133 on the front side of the wing feather, effectively crush the solid.
도 1은 종래 원심펌프의 실시예를 도시한 요부 단면도1 is a cross-sectional view of the main part showing an embodiment of a conventional centrifugal pump
도 2 및 도 3은 종래기술(한국특허 제732196호)에 개시된 원심펌프의 요부 단면도 및 임펠러의 사시도2 and 3 are a sectional view of the main portion and the impeller of the centrifugal pump disclosed in the prior art (Korean Patent No. 732196)
도 4는 본 발명에 의한 원심펌프 임펠러의 개략적인 형상을 도시한 사시도Figure 4 is a perspective view showing a schematic shape of the centrifugal pump impeller according to the present invention
도 5는 도 4에서의 A-A선 단면도5 is a cross-sectional view taken along the line A-A in FIG.
도 6은 도 4에서의 B-B선 단면도6 is a cross-sectional view taken along the line B-B in FIG.
도 7은 본 발명에 의한 임펠러의 배면에 형성된 보조 깃을 도시한 사시도Figure 7 is a perspective view showing the auxiliary feather formed on the back of the impeller according to the present invention
이하에서는 첨부된 도면을 참고하여 본 발명을 상세히 설명하도록 한다.Hereinafter, with reference to the accompanying drawings to describe the present invention in detail.
도 4는 본 발명에 의한 원심펌프 임펠러의 개략적인 형상을 도시한 사시도이며, 도 5는 도 4에서의 A-A선 단면도를 도시한 것이며, 도 6은 도 4에서의 B-B선 단면도를 도시한 것이다.Figure 4 is a perspective view showing a schematic shape of the centrifugal pump impeller according to the present invention, Figure 5 is a cross-sectional view taken along the line A-A in Figure 4, Figure 6 is a cross-sectional view taken along the line B-B in FIG.
본 발명의 바람직한 실시 예에 따른 원심펌프는, 흡입구와 토출구를 가지는 하우징과, 상기 하우징의 내부에 구비되어, 구동수단에 의해 회전하는 임펠러(120)를 포함하여 구성된다. A centrifugal pump according to a preferred embodiment of the present invention includes a housing having a suction port and a discharge port, and an impeller 120 provided inside the housing and rotating by a driving means.
상기 임펠러(120)는 도 4에 도시된 바와 같이, 회전 중심에서부터 동일 각도로 방사상으로 연장된 다수 개의 날개 깃(122)과, 중심부의 축공(130)으로 이루어진다.As shown in FIG. 4, the impeller 120 includes a plurality of wing feathers 122 extending radially at the same angle from the center of rotation, and the shaft hole 130 at the center thereof.
여기서, 상기 하우징의 내부에는 구동축이 노출되어 있어서, 이 구동축에 임펠러의 축공이 끼워져 결합된다. 그리고, 상기 하우징은 환형의 반(半)볼류트(Volute)형으로서, 저압부에서는 하우징의 내경과 임펠러(120)의 외경(날개 깃 끝단면) 사이의 틈새 즉, 와류실(volute casing)은 매우 좁으나, 고압부 쪽으로 갈수록 점점 하우징의 내경이 커짐으로써 와류실의 크기가 커지는 형태의 반볼류트 형이다.Here, the drive shaft is exposed to the inside of the housing, the shaft hole of the impeller is fitted to the drive shaft is coupled. In addition, the housing is an annular half-volute type, and in the low pressure part, the clearance between the inner diameter of the housing and the outer diameter (end feather end surface) of the impeller 120, that is, the vortex casing is Although it is very narrow, it is a semivolute type in which the size of the vortex chamber becomes larger as the inner diameter of the housing gradually increases toward the high pressure part.
특히, 본 발명에서 임펠러의 날개 깃의 앞면(표면)에는 오목홈(124)이 날개 깃의 길이방향을 따라 길게 형성되어 이루어진다. 상기 오목홈(124)은 회전중심에서 멀어질수록 완만하게 깊어지도록 구성됨으로써, 흡입구를 통해 유입된 유체가 이 오목홈(124)을 통해 용이하게 와류실로 이송될 수 있게 하므로, 이 오목홈(124)은 유도로(誘導路)로서의 기능을 갖는다.In particular, in the present invention, the concave groove 124 is formed in the front surface (surface) of the impeller wing feathers long along the longitudinal direction of the wing feathers. The concave groove 124 is configured to be gradually deeper as it moves away from the center of rotation, so that the fluid introduced through the suction port can be easily transferred to the vortex chamber through the concave groove 124, this concave groove 124 Has a function as an induction furnace.
본 발명에서의 날개 깃(122)은, 상기 오목홈(124)에 의해 전방부(123a)와 후방부(123b)로 나뉘게 되는데, 하나의 날개 깃에 있어서 상기 오목홈(124)을 기준으로 임펠러가 회전하는 방향 쪽에 위치한 부분을 전방부(123a)로, 상기 오목홈을 기준으로 하여 상기 전방부의 반대 쪽에 위치한 부분을 후방부(123b)로 부르기로 한다.In the present invention, the blade feather 122 is divided into the front portion 123a and the rear portion 123b by the concave groove 124, and the impeller based on the concave groove 124 in one wing feather. The portion located on the side in which the direction of rotation is referred to as the front portion 123a, and the portion located on the opposite side of the front portion with respect to the concave groove will be referred to as the rear portion 123b.
본 발명에서는 날개 깃의 전방부(회전방향 쪽) 높이(Ha)('두께'라고도 함)를 후방부의 날개 깃 높이(Hb)에 비해 낮게 형성한 것을 특징으로 한다.In the present invention, the height Ha (also referred to as 'thickness') of the front part (the rotational direction) of the vane is formed to be lower than the height of the feather tip Hb of the rear part.
이와 같이 구성되는 본 발명에 의한 원심펌프는, 전방부(회전방향 쪽)의 날개 깃 높이와 후방부(반대방향 쪽)의 날개 깃의 높이가 동일한 경우에 비해, 펌프가 동작 개시되는 순간 토오크를 완화시킬 수 있으며, 특히 점도가 높은 액체에서 사용되는 경우 정지된 펌프를 동작 개시하는 데 요구되는 기동전력을 낮출 수 있다.The centrifugal pump according to the present invention configured as described above has a torque at the moment when the pump starts operation as compared with the case where the height of the vane blade of the front part (the rotational direction) and the height of the vane blade of the rear part (the opposite direction) are the same. It can mitigate and lower the starting power required to start a stationary pump, especially when used in high viscosity liquids.
또한, 본 발명에서 상기 날개 깃(122) 전방부의 회전방향 쪽(전방쪽) 측면에는 요부(凹部)(132) 및 돌출부(凸部)(133)를 형성함으로써, 흡입구를 통해 임펠러(120)의 중앙부로 유입된 고형물들이 날개 깃을 따라 와류실로 이송되는 동안에, 상기 날개 깃의 전방 측면에 형성된 요철부(凹凸部)(132)(133)에 의해 분쇄되거나 절단되도록 한 것을 특징으로 한다.Further, in the present invention, by forming the recess 132 and the protrusion 133 on the side of the front side of the wing blade 122 in the rotational direction (front side), the impeller 120 is formed through the suction port. The solids introduced into the center portion are crushed or cut by the uneven parts 132 and 133 formed on the front side of the wing feathers while being transferred to the vortex chamber along the wing feathers.
상기한 요부(132) 및 돌출부(133)는 날개 깃 전방부의 측면에 형성하는 것이 매우 바람직하다. 만약, 날개 깃 후방부의 전방 측면에 요철부(凹凸部)를 구성할 경우에는 흡입구를 통해 유입된 유체가 오목홈(124)을 통해 와류실로 이송되는 동안에 상기 요철부에 의해 유체이송을 방해할 수 있어서, 흡입력을 저하시키는 요인이 될 수 있으므로 바람직하지 못하게 된다.The recess 132 and the protrusion 133 are preferably formed on the side surface of the wing feather front part. If the concave-convex portion is formed on the front side of the wing feather rear part, the fluid may be disturbed by the concave-convex portion while the fluid introduced through the suction port is transferred to the vortex chamber through the concave groove 124. In this case, the suction force may be a cause of deterioration, which is not preferable.
특히, 상기 돌출부(133)는 상기 날개 깃의 끝단에 형성함으로써, 날개 깃 끝단에 작용하는 강한 원심력과 상기 돌출부(133)의 충격력을 이용하여, 요부(132)에 의해 분쇄되지 못한 고형물들을 강력하게 분쇄시키는 효과를 얻을 수 있다.In particular, the protrusion 133 is formed at the end of the blade feather, by using a strong centrifugal force acting on the blade feather tip and the impact force of the protrusion 133, the solids that are not crushed by the recess 132 to strongly The effect of grinding can be obtained.
더 나아가, 본 발명에서는 상기 날개 깃의 뒷면에 보조 깃(131)이 더 구비된다. 종래기술2에서는 임펠러의 배면은 편평한 평면으로 이루어져 있어, 케이싱 내면과의 접촉면적이 커서, 초기 기동에 큰 토오크가 요구되는 원인이 될 뿐만 아니라, 마찰력에 의한 출력손실의 원인으로 작용하여 효율성이 낮아질 수밖에 없었다. 본 발명에서의 보조 깃은 상기한 문제를 해결하면서도 유체의 흡입력을 증대시키는 효과를 얻을 수 있다.Furthermore, in the present invention, the auxiliary feather 131 is further provided on the back of the wing feather. In the prior art 2, the back of the impeller is made of a flat plane, so that the contact area with the inner surface of the casing is large, which not only causes a large torque for initial start-up, but also acts as a cause of output loss due to frictional force, resulting in low efficiency. There was no choice but to. The auxiliary collar in the present invention can achieve the effect of increasing the suction force of the fluid while solving the above problems.
본 발명에서의 보조 깃(131)은 도 7에 도시한 바와 같이, 그 폭과 두께는 일정하게 형성되어 각 날개 깃(122)의 뒷면에 각각 구비되어 이루어지되, 회전 중심에서 멀어질수록 회전 반대방향 쪽으로 완만하게 만곡되는 형상으로 구성된다. As shown in FIG. 7, the auxiliary feather 131 in the present invention, the width and thickness is formed to be constant is provided on the back of each wing feather 122, respectively, the further away from the rotation center, the opposite the rotation It consists of a shape that curves gently toward the direction.
이와 같은 구성으로 된 보조 깃(131)은 임펠러와 케이싱 벽면 사이의 틈새를 최소화하면서도, 케이싱 벽면과의 미찰면적을 줄이는 효과를 얻을 수 있으며, 더 나아가 날개 깃과 날개 깃 사이로 흐르는 유체를 효과적으로 와류실로 밀어내는 작용을 하게 되는 것이다.The auxiliary feather 131 having such a configuration can minimize the gap between the impeller and the casing wall, and reduce the friction area with the casing wall. Furthermore, the fluid flowing between the wing feathers and the wing feathers effectively flows into the vortex chamber. It will be pushed out.
이와 같이 구성된 본 발명에 의한 원심펌프는 날개 깃의 전방 측면에 요철부(132)(133)를 형성하여, 고형물을 효과적으로 분쇄할 수 있는 특징적 효과를 가지며, 종래기술에 비해 흡인력과 효율성을 향상시킬 수 있어, 오수(汚水), 오니(汚泥), 슬러리(Slurry) 등이 함유된 유체(고형물 유체)의 이송용 펌프로서 특히 유용하다.The centrifugal pump according to the present invention configured as described above has the characteristic effect of effectively forming the uneven parts 132 and 133 on the front side of the blade feather, which can effectively crush the solids, and improve the suction force and efficiency compared to the prior art. It is particularly useful as a pump for conveying a fluid (solid fluid) containing sewage, sludge, slurry, and the like.
이상에서 본 발명을 설명함에 있어 첨부된 도면을 참조하여 특정 형상과 구조를 갖는 임펠러를 구비한 원심펌프를 위주로 설명하였으나, 본 발명은 당업자에 의하여 다양한 변형 및 변경이 가능하고, 이러한 변형 및 변경은 본 발명의 보호범위에 속하는 것으로 해석되어야 한다.In the above description of the present invention, the centrifugal pump having an impeller having a specific shape and structure has been described with reference to the accompanying drawings, but the present invention can be variously modified and changed by those skilled in the art. It should be interpreted as falling within the protection scope of the present invention.

Claims (4)

  1. 흡입구와 토출구를 가지는 하우징과;A housing having a suction port and a discharge port;
    상기 하우징의 내부에 구비되며, 회전 중심에서부터 동일 각도로 방사상으로 연장된 다수 개의 날개 깃(122)으로 이루어지며, 구동수단에 의해 회전하는 임펠러(120)를 포함하는 원심펌프에 있어서,In the centrifugal pump which is provided in the housing, consisting of a plurality of blade feathers 122 extending radially at the same angle from the center of rotation, comprising an impeller 120 rotated by a driving means,
    상기 날개 깃(122)의 표면에는 오목홈(124)이 그 길이방향을 따라 길게 형성되어 이루어지되, Concave groove 124 is formed on the surface of the wing feather 122 is formed long along its longitudinal direction,
    상기 오목홈(124)을 기준으로 하여, 회전방향 쪽의 날개 깃 높이(Ha)는 회전 반대방향 쪽의 날개 깃 높이(Hb)보다 낮게 구성되어 이루어지는 것을 특징으로 하는 원심펌프.Based on the concave groove 124, the vane blade height (Ha) in the rotational direction is lower than the vane blade height (Hb) in the opposite direction of rotation is made of a centrifugal pump.
  2. 제1항에 있어서,The method of claim 1,
    상기 날개 깃(122)의 회전방향 쪽 전방 측면에는 요부(凹部)(132) 및 돌출부(凸部)(133)가 형성되어 이루어지되, 상기 돌출부(133)는 상기 날개 깃의 끝단에 구비되는 것을 특징으로 하는 원심펌프.Concave portions 132 and protrusions 133 are formed on the front side of the wing blade 122 in the rotational direction, and the protrusions 133 are provided at the ends of the wing feathers. Centrifugal pump characterized in that.
  3. 제2항에 있어서, The method of claim 2,
    상기 날개 깃의 뒷면에 보조 깃(131)이 더 구비되어 이루어지되,The auxiliary feather 131 is further provided on the back of the wing feather,
    상기 보조 깃은 회전 중심에서 멀어질수록 회전 반대방향 쪽으로 완만하게 만곡되는 것을 특징으로 하는 원심펌프.Centrifugal pump is characterized in that the auxiliary feather is gently curved toward the opposite direction of rotation as it moves away from the center of rotation.
  4. 제1항 내지 제3항 중의 어느 한 항에 있어서,The method according to any one of claims 1 to 3,
    상기 오목홈(124)은 날개 깃의 길이방향을 따라 길게 형성되어 이루어지되, 그 깊이는 회전중심에서 멀어질수록 완만하게 깊어지는 것을 특징으로 하는 원심펌프.The concave groove 124 is formed long along the longitudinal direction of the blade feather, the depth of the centrifugal pump characterized in that the deeper the further away from the center of rotation.
PCT/KR2010/004363 2009-08-06 2010-07-05 Centrifugal pump having an improved impeller WO2011016619A2 (en)

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KR101404578B1 (en) * 2012-08-13 2014-06-09 주식회사 대영파워펌프 Impeller of centrifugal pump
KR101775587B1 (en) * 2016-02-05 2017-09-08 주식회사 지트리비앤티 Circulation pump
WO2018052190A1 (en) * 2016-09-13 2018-03-22 서울대학교산학협력단 Centrifugal pump impeller including ridge structure
KR20180079505A (en) * 2016-12-30 2018-07-11 명화공업주식회사 Waterpump impeller
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