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KR960003204B1 - Manufacturing method of the rotor for the compressor motor - Google Patents

Manufacturing method of the rotor for the compressor motor Download PDF

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Publication number
KR960003204B1
KR960003204B1 KR1019890007852A KR890007852A KR960003204B1 KR 960003204 B1 KR960003204 B1 KR 960003204B1 KR 1019890007852 A KR1019890007852 A KR 1019890007852A KR 890007852 A KR890007852 A KR 890007852A KR 960003204 B1 KR960003204 B1 KR 960003204B1
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KR
South Korea
Prior art keywords
fixing pin
rotor
inner diameter
crankshaft
aluminum
Prior art date
Application number
KR1019890007852A
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Korean (ko)
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KR910002074A (en
Inventor
라상윤
Original Assignee
삼성전자주식회사
강진구
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Priority to KR1019890007852A priority Critical patent/KR960003204B1/en
Publication of KR910002074A publication Critical patent/KR910002074A/en
Application granted granted Critical
Publication of KR960003204B1 publication Critical patent/KR960003204B1/en

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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K17/00Asynchronous induction motors; Asynchronous induction generators
    • H02K17/02Asynchronous induction motors
    • H02K17/16Asynchronous induction motors having rotors with internally short-circuited windings, e.g. cage rotors
    • H02K17/20Asynchronous induction motors having rotors with internally short-circuited windings, e.g. cage rotors having deep-bar rotors
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K15/00Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
    • H02K15/02Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Abstract

The method for manufacturing a rotor in a compressor motor comprises the steps of: (1) inserting a predetermined size of hole formed at the center of a plurality of core plates to the circumference of a fixing pin; (2) filling an aluminium layer in the space limited by the minor diameter of the core plates and the fixing pin by aluminium die casting the structure obtained by the step (1); (3) removing the fixing pin from the structure obtained through the step (2) and finely working the aluminium layer and the circumference of the core plates; and (4) heating and expanding the structure obtained through the step (3), inserting a crank shaft of a compressor and then contracting the structure to stick the minor diameter of the aluminium layer fast to the crank shaft.

Description

압축기 모터의 로터(Rotor) 제조 방법Rotor manufacturing method of compressor motor

제1도는 본 발명의 고정핀과 코어의 분해 사시도.1 is an exploded perspective view of the fixing pin and the core of the present invention.

제2도는 결합된 고정핀과 코어에 알루미늄을 다이케스팅한 단면도.Figure 2 is a cross-sectional view of the die casting aluminum to the fixing pin and the core combined.

제3도는 제2도의 A-A선 단면도.3 is a cross-sectional view taken along the line A-A of FIG.

제4도는 본 발명으로 얻어진 로터를 장착한 압축기 모터의 단면도.4 is a sectional view of a compressor motor equipped with a rotor obtained in the present invention.

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

1 : 고정핀 2,3 : 공간돌기1: Fixing pin 2,3: Space protrusion

4 : 코어 5 : 구멍4: core 5: hole

6 : 소공 7 : 알루미늄층6: pore 7: aluminum layer

본 발명은 압축기 모터에 있어서, 회전자의 자속이 크랭크축을 통하여 상실되지 않도록 회전자의 코아 내경이 크랭크축에 직접 닿지 않고 삽착하게 된 압축기 모터의 로터 제조 방법에 관한 것이다.The present invention relates to a method for manufacturing a rotor of a compressor motor in which the core diameter of the rotor is inserted without directly contacting the crank shaft so that the magnetic flux of the rotor is not lost through the crank shaft.

종래 대부분의 로터는 수개의 코어를 고정핀에 적층되게 억지 압입끼운 다음 알루미늄 다이캐스팅 금형에 인써트(Wsert) 사출한 후 고정핀을 분리시켜 로터의 내경과 외경을 정밀 가공하여 크랭크축에 압입 삽착하였던 것으로써, 이는 코어의 내경이 크랭크축에 밀착되어 있는 관계로 로터의 자속이 크랭크축을 통하여 상실되는 결점이 있는 것이었으며, 또한 상기의 결점을 시정하여 효율을 상승시키기 위해 코어의 내경을 알루미늄으로 감싸주게 된 것은 크랭크축의 외경과 코어의 내경사이에 일정한 공간을 주도록 알루미늄 다이케스팅 금형에 설치하여 그 공간에 알루미늄이 충전되도록 한 것이므로 다이캐스팅 작업상 금형내에 크랭크축의 위치 설정이 용이하지 못한 결점이 있어 작업이 어려워 대부분 자속의 상실을 감수한채 상기의 로터를 사용하고 있는 것이었다.Conventionally, most rotors are press-fitted with several cores stacked on a fixed pin, and then inserted into an aluminum die casting mold, and then the fixed pins are separated to precisely process the inner and outer diameters of the rotor and press-inserted into the crankshaft. This is because the core of the core is in close contact with the crankshaft, so that the magnetic flux of the rotor is lost through the crankshaft. Also, the inner diameter of the core is wrapped in aluminum to correct the defect and increase the efficiency. What is given is that it is installed in the aluminum die casting mold to give a certain space between the outer diameter of the crankshaft and the inner diameter of the core, so that aluminum is filled in the space, which makes it difficult to position the crankshaft in the die. Most of them use the above rotor with loss of magnetic flux It was in.

본 발명은 이상과 같은 종래 로터중 코어의 내경에 알루미늄을 적층한 로터를 제작 과정에서 크랭크축과 무관시켜 알루미늄 다이케스팅 작업상 용이하도록 통상의 고정핀 외주면에 3개 이상의 돌기를 돌설하여 고정핀의 외경과 코어의 내경 사이에 알루미늄을 다이케스팅하도록 한 것으로써, 이하 도면 실시예에 따라 상세히 설명하면 다음과 같다.In the present invention, the rotor is laminated with aluminum to the inner diameter of the core of the conventional rotor as described above, regardless of the crankshaft in the manufacturing process, so that three or more projections on the outer circumferential surface of the conventional fixing pin to facilitate the aluminum die casting operation, the outer diameter of the fixing pin By die-casting aluminum between the inner diameter of the core, will be described in detail according to the following embodiments of the drawings.

제1도의 부호 1은 고정핀을 나타낸 것으로 이 고정핀(1)은 통상의 2단으로된 고정핀 외주면에 공간돌기 (2), (3)을 3방향으로 돌출하였으며, 부호 4는 통상의 코어를 가르킨 것으로 구멍(5)을 중심으로 수개의 소공(6)이 그 둘레에 천공되어 있다.In Fig. 1, reference numeral 1 denotes a fixing pin. The fixing pin 1 protrudes space projections (2) and (3) in three directions on an outer circumferential surface of a conventional two-stage fixing pin. As indicated by, several small holes 6 are drilled around the hole 5.

[실시예]EXAMPLE

[공정 1][Step 1]

상기의 코어(4)중 구멍(5)의 내경이 큰것 수개를 고정팬(1)의 직경이 굵은측에 끼워 공간돌기(3)가 구멍(5) 내경에 밀착되도록하고, 구멍(5)의 내경이 작은 코어(4) 수개는 직경이 가는측의 고정핀(1)에 끼워 구멍(5) 내경에 공간돌기(2)가 밀착되도록하되, 각기의 코어(4)에 천공된 소공(6)이 일치되도록 적층시켜 연통되도록하여 코어(4)와 고정핀(1)의 조립체를 형성한다.The inner diameter of the hole 5 of the above-mentioned cores 4 is inserted into the side of the fixing fan 1 having a large diameter so that the space projection 3 is in close contact with the inner diameter of the hole 5, and the Several cores (4) having a small inner diameter are inserted into the fixing pin (1) on the thin side so that the space projection (2) is in close contact with the inner diameter of the hole (5), and the small holes (6) perforated in the respective cores (4). It is stacked so as to be in communication with each other to form an assembly of the core (4) and the fixing pin (1).

[공정 2][Step 2]

상기 실시예 공정 1점에서 행한 조립체는 각 코어(4)의 내경과 공간돌기 (2), (3)을 제외한 고정핀(1)의 외주면과는 공간돌기(2), (3)에 의하여 3방향으로 공간이 형성되는 것으로써, 이를 알루미늄 다이케스팅 금형내에 장전시켜 알루미늄층(7)을 다이케스팅하여 단면상으로 제2도 및 제3도와 같이 되도록 한다.The assembly carried out in the first step of the above embodiment is the inner diameter of each core 4 and the outer circumferential surface of the fixing pin (1) except for the space projections (2), (3) by the space projections (2), (3) As the space is formed in the direction, it is loaded into the aluminum die casting mold to die cast the aluminum layer 7 so as to be in the cross-sectional view as shown in FIG. 2 and FIG.

[공정 3][Step 3]

상기 공정 2에서 행한 알루미늄 다이케스팅된 것에서 고정핀(1)을 빼내어 미완성의 로터를 형성한 다음 로터의 내경 즉 공간돌기 (2), (3)에 의하여 형성된 삼방향의 요흠 공간 이외의 고정핀(1)의 외주면으로 인하여 형성된 내주면과 로터의 외주면을 정밀 가공하여 완성품을 만든다.The fixing pin 1 is removed from the die-casted aluminum in the step 2 to form an unfinished rotor, and then the fixing pins other than the three-way recessed space formed by the inner diameter of the rotor, that is, the space protrusions 2 and 3 The inner peripheral surface formed by the outer peripheral surface of) and the outer peripheral surface of the rotor are processed precisely to make a finished product.

[공정 4][Step 4]

상기 공정 3점에서 만든 완성품 전체에 열을 가하여 정밀 가공된 내주면을 팽창 확대시켜 제4도에 표시된 압축기 모터(8) 크랭크축(9)에 끼운다음 냉각하면 팽창된 로터의 수축으로 인하여 그 내주면이 따라서 축되도록하여 크랭크축에 밀착시킨다.Applying heat to the entire finished product made in step 3 above, expand and expand the precision machined inner circumferential surface, insert it into the crankshaft 9 of the compressor motor 8 shown in FIG. 4, and then cool the inner circumferential surface due to shrinkage of the expanded rotor. Therefore, to be in close contact with the crank shaft.

이상과 같이된 본 발명은 제4도에 표현된 바와 같이 각 코어(4)의 내경을 알루미늄으로 덮어 씌웠으므로 덮어 씌운 알루미늄의 크랭크축(9)의 외주면에 밀착되어 크랭크축(9)에 로터가 연결된 것이기 때문에 로터의 자속이 크랭크축에 전달되지 않게 되므로 종래 크랭크축 외주면에 코어 내경이 직접 밀착된 것보다는 자성이 소멸되지 않고 회전율이 높으며, 또한 고정핀(1)의 외주면에 공간돌기(2), (3)을 형성시켜 고정핀(1)의 외주면에 수개의 코어(4)를 적층 삽착한 다음 알루미늄 다이케스팅 금형에 넣어 다이케스팅하는 것이므로 종래 금형내에 크랭크축의 외주면과 코어의 내경 사이에 일정한 공간이 유지되도록하여 그 공간에 알루미늄 다이케스팅한 것보다는 작업이 용이하여 다량 생산할 수 있게 되는 효과를 얻게 된 것이다.In the present invention as described above, since the inner diameter of each core 4 is covered with aluminum, as shown in FIG. 4, the rotor is in close contact with the outer circumferential surface of the crankshaft 9 of the overlaid aluminum. Since the magnetic flux of the rotor is not transmitted to the crankshaft because it is connected, the magnetism does not disappear and the rotation rate is higher than the inner diameter of the core directly contacting the outer circumference of the conventional crankshaft, and the space projection (2) on the outer circumferential surface of the fixing pin (1). , (3) is formed by stacking and inserting several cores (4) on the outer peripheral surface of the fixing pin (1), and then placing the die in an aluminum die casting mold, so that a constant space is maintained between the outer peripheral surface of the crankshaft and the inner diameter of the core in the conventional mold. As much as possible, rather than aluminum die-casting in the space, it is easy to work and can produce large quantities.

Claims (1)

(가) 중앙에는 소정크기의 구멍(5)이 형성되고 몸체의 둘레에는 다수의 소공들(6)이 형성된 다수의 코어판(4)의 상기 구멍(5)을 3방향으로 공간돌기(2), (3)가 돌설된 고정핀(1)의 외주면에 상기 각 소공들(6)을 일치시켜서 억지끼우는 단계 ; (나) 상기 단계(가)를 거친 중간물을 다이케스팅 금형에 장전하여 알루미늄 다이케스팅시켜서 상기 적층된 코어판(4)의 내경과 상기 고정핀(1)에 의해 한정되는 공간상에 알루미늄층(7)을 충진시키는 단계 ; (다) 상기 단계(나)를 거친 중간물에서 고정핀(1)을 제거하고 상기 적층된 코어판(4)의 내경에 충진된 알루미늄층(7) 및 적층된 코어판(4)의 외주면을 정밀가공하는 단계 및 (라) 상기 단계 (다)를 거친 중간물을 가열 팽창시켜서 압축기의 크랭크 샤프트(9)를 삽입한 후에 상기 중간물을 수축시켜 상기 알루미늄층(7)의 내경과 상기 크랭크샤프트(9)를 밀착시키는 단계를 구비하여 되는 압축기 모터의 로터제조방법.(A) Space projections 2 in the three directions of the holes 5 of the plurality of core plate 4 formed with a predetermined size of the hole (5) in the center and a plurality of small holes (6) around the body , (3) forcing the respective small holes (6) to the outer circumferential surface of the fixing pin (1) protrudingly fitted; (B) The aluminum layer 7 is loaded on the space defined by the inner diameter of the laminated core plate 4 and the fixing pins 1 by loading the intermediate material passed through step (a) into a die casting mold and aluminum die casting. Filling; (C) Remove the fixing pin (1) from the intermediate through the step (b) and the outer peripheral surface of the aluminum layer 7 and the laminated core plate 4 filled in the inner diameter of the laminated core plate 4 Precision machining and (D) heating and expanding the intermediate, which has undergone the above (C), to insert the crankshaft 9 of the compressor, and then contract the intermediate to shrink the inner diameter of the aluminum layer 7 and the crankshaft. The rotor manufacturing method of the compressor motor provided with the step of closely contacting (9).
KR1019890007852A 1989-06-08 1989-06-08 Manufacturing method of the rotor for the compressor motor KR960003204B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019890007852A KR960003204B1 (en) 1989-06-08 1989-06-08 Manufacturing method of the rotor for the compressor motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019890007852A KR960003204B1 (en) 1989-06-08 1989-06-08 Manufacturing method of the rotor for the compressor motor

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KR910002074A KR910002074A (en) 1991-01-31
KR960003204B1 true KR960003204B1 (en) 1996-03-06

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6848495B2 (en) 2003-05-19 2005-02-01 Bristol Compressors, Inc. Method of manufacturing a laminated rotor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100400451B1 (en) * 2001-01-04 2003-10-01 엘지전자 주식회사 Manufacturing rotor and method of line bar started permanent magnet motor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6848495B2 (en) 2003-05-19 2005-02-01 Bristol Compressors, Inc. Method of manufacturing a laminated rotor
US6900573B2 (en) 2003-05-19 2005-05-31 Bristol Compressors, Inc. Rotor core lamination for a laminated rotor

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