KR980002892A - Airfoil Impeller Manufacturing Method and Airfoil Impeller - Google Patents

Airfoil Impeller Manufacturing Method and Airfoil Impeller Download PDF

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Publication number
KR980002892A
KR980002892A KR1019970051678A KR19970051678A KR980002892A KR 980002892 A KR980002892 A KR 980002892A KR 1019970051678 A KR1019970051678 A KR 1019970051678A KR 19970051678 A KR19970051678 A KR 19970051678A KR 980002892 A KR980002892 A KR 980002892A
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KR
South Korea
Prior art keywords
airfoil
upper plate
main plate
bent
groove
Prior art date
Application number
KR1019970051678A
Other languages
Korean (ko)
Other versions
KR100265648B1 (en
Inventor
정영교
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정영교
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Filing date
Publication date
Application filed by 정영교 filed Critical 정영교
Priority to KR1019970051678A priority Critical patent/KR100265648B1/en
Publication of KR980002892A publication Critical patent/KR980002892A/en
Application granted granted Critical
Publication of KR100265648B1 publication Critical patent/KR100265648B1/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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • F04D29/282Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
    • F04D29/283Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis rotors of the squirrel-cage type
    • 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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes
    • 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
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/601Mounting; Assembling; Disassembling specially adapted for elastic fluid pumps
    • 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
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/62Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/626Mounting or removal of fans

Landscapes

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

Abstract

본 발명은 용접열에 의해 익형의 날개(6)가 변형을 일으키거나 파손되는 것을 방지할 수 있는 익형 임펠러 제작방법 및 그 방법에 의한 익형 임펠러에 관한 것이다.The present invention relates to a method for manufacturing a airfoil impeller that can prevent deformation or breakage of the blade 6 of the airfoil by welding heat, and airfoil impeller according to the method.

본 발명에 따르면, 박판으로 구성된 다수개의 익형날개의 곡면부(12) 양단에 수평으로 플랜지부(16)을 형성하고, 상기 익형날개(6)의 평면부(14) 양단에 절곡편 (18)을 형성하여, 상기 절곡편(18)이 삽입결합되는 관통홈(20)이 소정의 위치에 형성된 주판(2)과 상판(4)을 상기 절곡편(18)이 관통홈(20)에 삽입되도록 상기 익형날개(6)의 양단에 결합하고, 상기 절곡편(18)을 절곡한 후, 상기 절곡편 ( 18)과 플랜지부(16)를 주판(2)과 상판(4)에 용접결합하는 것을 특징으로 하는 익형 임펠러 제작방법이 제공된다.According to the present invention, a flange 16 is formed horizontally at both ends of the curved portions 12 of the plurality of airfoil blades formed of thin plates, and the bent piece 18 is disposed at both ends of the flat portion 14 of the airfoil blade 6. To form the main plate 2 and the upper plate 4 in which the through groove 20 into which the bent piece 18 is inserted and coupled to the predetermined position is inserted into the through groove 20. After coupling to both ends of the airfoil (6), bending the bending piece 18, welding the bending piece 18 and the flange portion 16 to the main plate (2) and the upper plate (4) Provided is a method for manufacturing an airfoil impeller.

Description

익형 임펠러 제작방법 및 그에 의한 익형 임펠러Airfoil Impeller Manufacturing Method and Airfoil Impeller

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음Since this is an open matter, no full text was included.

제1도는 종래의 임펠러를 도시한 사시도.1 is a perspective view showing a conventional impeller.

제2도는 본 고안에 따른 임펠러의 제작방법을 도시한 분해사시도.Figure 2 is an exploded perspective view showing a manufacturing method of the impeller according to the present invention.

제3도는 익형날개의 단면도.3 is a cross-sectional view of the airfoil.

Claims (2)

박판으로 구성된 다수개의 익형날개의 곡면부(12) 양단에 수평으로 플랜지부 (16)을 형성하고, 상기 익형 날개(6)의 평면부(14) 양단에 절곡편(18)을 형성하여, 상기 절곡편(18)이 삽입결합되는 관통홈(20)이 소정의 위치에 형성된 주판(2)과 상판(4)을 상기 절곡편(18)이 관통홈(20)에 삽입되도록 상기 익형날개(6)의 양단에 결합하고, 상기 절곡편(18)을 절곡한 후, 상기 절곡편(18)과 플랜지부(16)를 주판 (2)과 상판(4)에 용접결합하는 것을 특징으로 하는 익형 임펠러 제작방법.The flanges 16 are horizontally formed at both ends of the curved portions 12 of the plurality of airfoil blades formed of thin plates, and bent pieces 18 are formed at both ends of the flat portion 14 of the airfoil blades 6. The airfoil wing 6 so that the bent piece 18 is inserted into the through groove 20 by inserting the main plate 2 and the upper plate 4 having the through groove 20 into which the bent piece 18 is inserted into a predetermined position. Air-conditioning impeller characterized in that it is coupled to both ends of the bent, the bending piece 18, and then the bending piece 18 and the flange portion 16 is welded to the main plate (2) and the upper plate (4) How to make. 소정의 위치에 관통홈(20)이 형성된 주판(2) 및 상판(4)과, 박판으로 제작되며 곡면부(12)와 이곡면부(12)보다 곡률반경이 작거나 거의 평면으로 구성된 둘레면인 평면부(14)로 구성되고 상기 주판(2)과 상판(4)의 사이에 원주를 따라 장착하는 다수개의 익형날개(6)을 포함하며, 상기 날개(6)는 곡면부(12)의 양단에 수평으로 플랜지부(16)가 형성되고, 평면부(14)의 양단에 상기 주판(2)과 상판(4)에 형성된 관통홈(20)에 삽입절곡되는 절곡편(18)이 형성되며, 상기 플랜지부(16)과 절곡편(18)은 상기 주판(2)과 상판(4)에 용접결합되는 것을 특징으로 하는 익형 임펠러.The main plate 2 and the upper plate 4 formed with the through groove 20 at a predetermined position, and a thin plate, the radius of curvature smaller than the curved portion 12 and the curved surface portion 12 is a peripheral surface composed of a substantially flat Comprising a flat portion 14 and includes a plurality of airfoil wings (6) mounted along the circumference between the main plate (2) and the upper plate (4), the blade (6) is both ends of the curved portion (12) The flange portion 16 is formed horizontally on the bent, and the bent piece 18 inserted into the through groove 20 formed in the main plate 2 and the upper plate 4 is formed at both ends of the flat portion 14, The flange portion (16) and the bent piece (18) is airfoil impeller, characterized in that the welded to the main plate (2) and the upper plate (4). ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019970051678A 1997-10-09 1997-10-09 Method for manufacturing blade impeller and blade impeller manufactured by such method KR100265648B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019970051678A KR100265648B1 (en) 1997-10-09 1997-10-09 Method for manufacturing blade impeller and blade impeller manufactured by such method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019970051678A KR100265648B1 (en) 1997-10-09 1997-10-09 Method for manufacturing blade impeller and blade impeller manufactured by such method

Publications (2)

Publication Number Publication Date
KR980002892A true KR980002892A (en) 1998-03-30
KR100265648B1 KR100265648B1 (en) 2001-01-15

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KR1019970051678A KR100265648B1 (en) 1997-10-09 1997-10-09 Method for manufacturing blade impeller and blade impeller manufactured by such method

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100438277B1 (en) * 2001-12-18 2004-07-02 엘지전자 주식회사 Manufacturing method of impeller
CN112483462A (en) * 2020-09-05 2021-03-12 佛山市顺德区涵一电器配件有限公司 Centrifugal wind wheel and manufacturing method thereof
KR20210105202A (en) * 2020-02-18 2021-08-26 엘지전자 주식회사 Impeller and method of manufacturing the same

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107642501A (en) * 2017-09-22 2018-01-30 山东美陵美力达风机有限公司 To impeller and its self-positioning welding fabrication technique after centrifugal fan
CN110285092A (en) * 2019-07-24 2019-09-27 佛山市鸿海风机有限公司 Large fan single blade chassis structure
CN111828377B (en) * 2020-07-13 2021-11-30 湖南鑫宏源高科有限公司 Centrifugal fan impeller

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100438277B1 (en) * 2001-12-18 2004-07-02 엘지전자 주식회사 Manufacturing method of impeller
KR20210105202A (en) * 2020-02-18 2021-08-26 엘지전자 주식회사 Impeller and method of manufacturing the same
US11578605B2 (en) 2020-02-18 2023-02-14 Lg Electronics Inc. Impeller and method of manufacturing the same
CN112483462A (en) * 2020-09-05 2021-03-12 佛山市顺德区涵一电器配件有限公司 Centrifugal wind wheel and manufacturing method thereof

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Publication number Publication date
KR100265648B1 (en) 2001-01-15

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