US2104979A - Die block - Google Patents

Die block Download PDF

Info

Publication number
US2104979A
US2104979A US35104A US3510435A US2104979A US 2104979 A US2104979 A US 2104979A US 35104 A US35104 A US 35104A US 3510435 A US3510435 A US 3510435A US 2104979 A US2104979 A US 2104979A
Authority
US
United States
Prior art keywords
die block
chromium
molybdenum
steel
copper
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US35104A
Inventor
William F Finkl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Finkl A and Sons Co
Original Assignee
Finkl A and Sons Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Finkl A and Sons Co filed Critical Finkl A and Sons Co
Priority to US35104A priority Critical patent/US2104979A/en
Application granted granted Critical
Publication of US2104979A publication Critical patent/US2104979A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/22Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten

Definitions

  • This invention relates to steel alloys which are particularly adapted for use in die blocks used for hot work forging processes, and steel items requiring great hardness, durability and strength, and has for its principal object to provide an alloy of the class described, having desirable characteristics approximating those of the nickel, chromium, molybdenum type such as described in my prior Patent No. 1,464,174 and my copending application Serial No. 33,331, filed July 26, 1935, but more economical to manufacture, due to the use of less expensive alloying elements.
  • the alloy forming the subject of this application is, therefore, sufiicient to meet usual commercial requirements which are not so severe as to demand more expensive alloys such as my pr
  • the preferred ranges of the principal alloying elements are as follows:
  • chromium-copper-molybdenum steels are particularly characterized by uniformity of hardness penetration.
  • a block 11 inch cube of this alloy having .50% carbon, .75% chromium, 35% molybdenum and 2.85% copper was hardened and tempered to a surface hardness of 364 Brinell.
  • this block showed a center hardness of 352 Brinell, with a corresponding uniformity of hardness throughout the block section.
  • Such uniformity of hardness penetration in large sections is unusual, and is not obtainable in steels in common usage.
  • the steel is readily machinable when annealed by heating above the critical range, and allowing it to cool slowly. To harden, this steel is heated to above the critical range and cooled rapidly by quenching in a suitable medium, and temper- ,ing is done in the usual manner by reheating after quenching to the desired point. It is also machinable in hardened and tempered condition for many commercial purposes up to approximately 450 Brinell hardness.
  • a die block for hot forging made of steel alloy consisting of carbon ranging from .25 to 1.10%, chromium .25 to 1.50%, molybdenum .05 to 2.00%, copper .25 to 6.00%, and the balance essentially all iron.
  • a die block for hot forging made of steel alloy consisting of carbon ranging from .25 to .60%, chromium from .25 to 1.00%, molybdenum from .05 to 1.00%, copper from .25 to 4.00%, and the balance essentially all iron.
  • a tempered die block for hot forging made of steel alloy consisting of carbon ranging from .25 to 1.10%, chromium .25 to 1.50%, molybdenum .05 to 2.00%, copper .25 to 6.00%, and the balance essentially all iron.
  • a tempered die block for hot forging made of steel, alloy consisting of carbon ranging from .25 to .60%, chromium from .25 to 1.00%, molybdenum from .05 to 1.00%, copper from .25 to 4.00%, and the balance essentially all iron.

Description

Patented Jan. 11, 1938 UNITED STATES DIE BLOCK William F. Fink], Chicago, Finkl & Sons Company,
ration of Illinois 111., assignor to A. Chicago, 11]., a. corpo- No Drawing. Application August 7, 1935, Serial No. 35,104
4 Claims. This invention relates to steel alloys which are particularly adapted for use in die blocks used for hot work forging processes, and steel items requiring great hardness, durability and strength, and has for its principal object to provide an alloy of the class described, having desirable characteristics approximating those of the nickel, chromium, molybdenum type such as described in my prior Patent No. 1,464,174 and my copending application Serial No. 33,331, filed July 26, 1935, but more economical to manufacture, due to the use of less expensive alloying elements.
The alloy forming the subject of this application is, therefore, sufiicient to meet usual commercial requirements which are not so severe as to demand more expensive alloys such as my pr The preferred ranges of the principal alloying elements are as follows:
Per cent Carbon .25 to 1.10 Chromium .25 to 1.50 Molybdenum .05 to 2.00 Copper .25 to 6.00
I Per cent Carbon .25 to .65 Chromium .25 to 1.00 Molybdenum .05 to 1.00 Copper .25 to 4.00
These. chromium-copper-molybdenum steels are particularly characterized by uniformity of hardness penetration. For example, a block 11 inch cube of this alloy having .50% carbon, .75% chromium, 35% molybdenum and 2.85% copper, was hardened and tempered to a surface hardness of 364 Brinell. When out in half, this block showed a center hardness of 352 Brinell, with a corresponding uniformity of hardness throughout the block section. Such uniformity of hardness penetration in large sections is unusual, and is not obtainable in steels in common usage.
These steels are quite free from internal and thermal ruptures, thereby requiring less careful handling in manufacturingand processing. As a hot work steel, such as in a die block, this steel can be used at its higher hardnesses without danger from heat checking.
The steel is readily machinable when annealed by heating above the critical range, and allowing it to cool slowly. To harden, this steel is heated to above the critical range and cooled rapidly by quenching in a suitable medium, and temper- ,ing is done in the usual manner by reheating after quenching to the desired point. It is also machinable in hardened and tempered condition for many commercial purposes up to approximately 450 Brinell hardness.
I claim as my invention:
1. A die block for hot forging made of steel alloy consisting of carbon ranging from .25 to 1.10%, chromium .25 to 1.50%, molybdenum .05 to 2.00%, copper .25 to 6.00%, and the balance essentially all iron.
2. A die block for hot forging made of steel alloy consisting of carbon ranging from .25 to .60%, chromium from .25 to 1.00%, molybdenum from .05 to 1.00%, copper from .25 to 4.00%, and the balance essentially all iron.
3. A tempered die block for hot forging made of steel alloy consisting of carbon ranging from .25 to 1.10%, chromium .25 to 1.50%, molybdenum .05 to 2.00%, copper .25 to 6.00%, and the balance essentially all iron.
4. A tempered die block for hot forging made of steel, alloy consisting of carbon ranging from .25 to .60%, chromium from .25 to 1.00%, molybdenum from .05 to 1.00%, copper from .25 to 4.00%, and the balance essentially all iron.
WILLIAM F. FINKL.
US35104A 1935-08-07 1935-08-07 Die block Expired - Lifetime US2104979A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US35104A US2104979A (en) 1935-08-07 1935-08-07 Die block

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35104A US2104979A (en) 1935-08-07 1935-08-07 Die block

Publications (1)

Publication Number Publication Date
US2104979A true US2104979A (en) 1938-01-11

Family

ID=21880664

Family Applications (1)

Application Number Title Priority Date Filing Date
US35104A Expired - Lifetime US2104979A (en) 1935-08-07 1935-08-07 Die block

Country Status (1)

Country Link
US (1) US2104979A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2950968A (en) * 1957-05-31 1960-08-30 Carpenter Steel Co Deep-hardened alloy steel having improved impact strength
US4253874A (en) * 1976-11-05 1981-03-03 British Steel Corporation Alloys steel powders

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2950968A (en) * 1957-05-31 1960-08-30 Carpenter Steel Co Deep-hardened alloy steel having improved impact strength
US4253874A (en) * 1976-11-05 1981-03-03 British Steel Corporation Alloys steel powders

Similar Documents

Publication Publication Date Title
US2034278A (en) Laminated metal stock
US2715576A (en) Age hardening alloy steel of high hardenability and toughness
US2747989A (en) Ferritic alloys
US2289449A (en) Die steel for hot working
US2104979A (en) Die block
US3165402A (en) Alloy steel and method of heat treatment therefor
US2753260A (en) High silicon-carbon tool steel
US2707680A (en) Alloy of iron, nickel, and molybdenum
US2438267A (en) Graphitic steel
US2447089A (en) Low alloy high tensile strength, high impact strength steel
US2253385A (en) Steel
US1721555A (en) Steel
US1732202A (en) Air-toughened alloy steel
US2585372A (en) Method of making low-alloy steel
US2347375A (en) Armor plate
US1950549A (en) Manufacturing hardened articles
US2266952A (en) Stainless steel treatment and product
US1211826A (en) Iron alloy.
US3951650A (en) Low carbon, Ni-Cr-Mo system cast iron roll
US702996A (en) Alloy.
US2053346A (en) Roll for fabricating hot metal
US2519627A (en) Graphitic steel of controllable hardenability and article made therefrom
US1976341A (en) Air hardening steel
US2206847A (en) Alloy steel
US2212496A (en) Alloy steel