IP Library Granted Patent US 8,402,658
Granted Patent B2
US 8,402,658 · App. 12/595,968 · Granted Mar 26, 2013

Manufacturing method of compressor pulley

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Quick Facts
Patent No.
US 8,402,658
App. No.
12/595,968
Granted
Mar 26, 2013
Kind
B2
Abstract

A compressor pulley having a partially cold forged base of improved strength and a bridge of improved strength is easily manufactured. Metal is heated to a predetermined temp and then hot forged into a pulley shape. A piercing step then forms a through hold in a center portion of the pulley. The heated pulley is then cooled to room temperature. Then the pulley is rough guided. A partial cold-forging step forges the base at room temperature. A slot is then pierced in the base portion. During a finishing step, groove working and grinding are performed on a surface of the pulley.

Claims (32)

1. A method of manufacturing a compressor pulley which comprises a plate-shaped base portion, and an internal ring portion and an external ring portion that are each integrally formed with the base portion and protrude in a length direction of the compressor pulley, said method comprising:

heating a metallic material to at least a predetermined temperature;

hot-forging the metallic material into a pulley shape having the base portion, the internal ring portion and the external ring portion;

piercing a center portion of the metallic material to form a through-hole at a connecting portion connecting with an inner surface of the internal ring portion;

cooling the heated metallic material to a room temperature;

grinding inner and outer surfaces of the cooled metallic material;

partially cold-forging the base portion at the room temperature;

forming slots at the base portion; and

performing groove working and grinding on a surface of the pulley-shaped metallic material,

wherein

a thickness of a bridge portion that is formed between the slots after the grinding is larger than a standard thickness of the base portion, and

the partial cold-forging is performed only on the bridge portion that has the thickness larger than the standard thickness of the base portion.

2. The method according to claim 1 , further comprising forward extruding the metallic material to form the connecting portion that extends, in a direction substantially perpendicular to the length direction of the compressor pulley, on an upper side of the internal ring portion through the hot-forging.

3. The method according to claim 2 , wherein said upper side of the internal ring portion is opposite to the bridge portion in the length direction of the compressor.

4. The method according to claim 1 , wherein the predetermined temperature is higher than the room temperature.

5. The method according to claim 1 , wherein the slots are spaced away from each other in a circumferential direction of the through hole, and the bridge portion is formed between slots that are adjacent to each other in the circumferential direction.

6. A method of manufacturing a compressor pulley which comprises a plate-shaped base portion, and an internal ring portion and an external ring portion that are each integrally formed with the base portion and protrude in a length direction of the compressor pulley, said method comprising:

heating a metallic material to a predetermined temperature;

hot-forging the metallic material into a pulley shape having the base portion, the internal ring portion and the external ring portion;

forming a through-hole at the metallic material at a connecting portion;

cooling the heated metallic material to a room temperature;

grinding inner and outer surfaces of the cooled metallic material;

partially cold-forging the base portion at the room temperature;

forming a slot at the base portion; and

performing groove working and grinding on a surface of the pulley-shaped metallic material,

wherein

a thickness of the base portion after the grinding is larger than a standard thickness of the base portion, and

the partial cold-forging is performed only on the base portion which has the thickness larger than the standard thickness of the base portion.

7. The method according to claim 6 , further comprising forward extruding the metallic material to form the connecting portion that extends, in a direction substantially perpendicular to the length direction of the compressor pulley, on an upper side of the internal ring portion through the hot-forging.

8. The method according to claim 7 , wherein said upper side of the internal ring portion is opposite to the bridge portion in the length direction of the compressor.

9. The method according to claim 6 , wherein the predetermined temperature is higher than the room temperature.

10. The method according to claim 6 , wherein the slots are spaced away from each other in a circumferential direction of the through hole, and the bridge portion is formed between slots that are adjacent to each other in the circumferential direction.

Assignments (3)
CHANGE OF NAME Recorded Oct 30, 2015
From: HALLA VISTEON CLIMATE CONTROL CORPORATION
To: HANON SYSTEMS
Reel/Frame 037007/0103 →
CHANGE OF NAME Recorded Jun 28, 2013
From: HALLA CLIMATE CONTROL CORPORATION
To: HALLA VISTEON CLIMATE CONTROL CORPORATION
Reel/Frame 030704/0554 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 15, 2009
From: LEE, HEON SANG; JEONG, SEOK JE; KIM, GYEONG MIN; KIM, JONG MOK
To: HALLA CLIMATE CONTROL CORP.
Reel/Frame 023374/0621 →