US2553609A - Weldable and high-temperature resisting hard alloys of cobalt and iron base - Google Patents

Weldable and high-temperature resisting hard alloys of cobalt and iron base Download PDF

Info

Publication number
US2553609A
US2553609A US11364A US1136448A US2553609A US 2553609 A US2553609 A US 2553609A US 11364 A US11364 A US 11364A US 1136448 A US1136448 A US 1136448A US 2553609 A US2553609 A US 2553609A
Authority
US
United States
Prior art keywords
cobalt
iron
alloys
weldable
hard alloys
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
US11364A
Inventor
Schmidt Max
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of US2553609A publication Critical patent/US2553609A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/07Alloys based on nickel or cobalt based on cobalt

Definitions

  • Such heat resisting weldable alloys of great hardness are however important for war, for they are, for example, necessary for armoring the valve cones of aircraft motors. Therefore it is desirable to make hard alloys which keep their properties when heated if their cobalt content is reduced to a large extent.
  • the welding properties of the hard alloys ac- 0.8% to 3% carbon 0.3% to 3.5% silicon 23% to 32% chromium 2% to 30% tungsten 3% to 15% molybdenum the balance up to 100% substantiallyal13beingcobalt and iron of which the ironcontent amounts to at least 35% and does not exceed.80%

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Products (AREA)

Description

May 22, 1951 M. SCHMIDT WELDABLE AND HIGH-TEMPERATURE RESISTING HARD ALLOYS OF COBALT AND IRON BASE Filed Feb. 27, 1948 m 6% il m i m g |||i| N x R w m M w m m V J W N X ooh Q96 00 8V gm 8N 0R 3 e l fll a 2 3 0% J w m S A 2 o Patented May 22, 1951 WELDABLE AND HIGH-TEMPERATURE RE- SISTING HARD ALLOYS OF COBALT AND IRON BASE Max Schmidt, Kapfenberg, Austria Application February 2'7, 1948, Serial No. 11,364 In Germany February 29, 1940 2 Claims. (Cl. 75126) Weldable hard metals as they are known under the trade names Celsit, Percit and Stellit, generally contain 0.8-3% carbon, 0.3 to 3.5% silicon, 23 to 32% chromium, 2 to 30% tungsten, up to about 2% of iron and the remainder of approximately 74 to 26% cobalt. The high cobalt content of these alloys in combination with the carbide forming elements chromium and tungsten endow them with an extraordinary hardness even at high temperatures and this is the reason why they are known as alloys with good high temperature (red hot) hardness. However, in view of their high cobalt content usually between 65 to 40%, they require considerable quantities of cobalt, and since cobalt may be difficult to obtain in times of war, it has been attempted to lower the cobalt content by introduction of a substitute metal. For this purpose, iron has been considered. In spite of the fact that the welding properties and hardness at room temperature are not influenced by a decrease of the cobalt content, alloys with greater quantities of iron exhibit a considerable decrease in hardness when heated. In iron-containing alloys in which the cobalt content is above 30%, the hardness at 600 C. is by 45-50% less than at room temperature, while in alloys practically free from iron the hardness at the same temperature is only about 28% lower than at room temperature. A further decrease of the cobalt content leads to a still sharper decrease of the hardness when heated.
Such heat resisting weldable alloys of great hardness are however important for war, for they are, for example, necessary for armoring the valve cones of aircraft motors. Therefore it is desirable to make hard alloys which keep their properties when heated if their cobalt content is reduced to a large extent.
As a result of planned experiments it was first ascertained that by decreasing the cobalt content and increasing the iron content, even if substantial quantities of nickel which is closely related to cobalt is added, an improvement of the heat resisting properties cannot be achieved.
On the contrary, the addition of nickel which causes a stabilization of structure lessens the hardness while heated and an increase of the tungsten content does not solve the problem. It was found, however, that by the addition of certain quantities of molybdenum, alloys including iron could be obtained which, even with a substantial decrease of the cobalt content, exhibit the same properties in a heated state as alloys practically free from iron.
With these alloys, the limits of the various alloying elements lie within the following ranges:
0.8 to 3% carbon 0.3 to 3.5% silicon 23 to 32% chromium 2 to 30% tungsten 3 to 15% molybdenum The balance up to 100% substantially all being iron and cobalt, of which the iron content amounts to at least 35% and does not exceed of the total sum of the combined iron and cobalt contents.
The following is an example of a very economical alloy of proven high temperature hardness:
0.8 to 1.8% carbon 0.3 to 3.5% silicon 23 to 32% chromium 2.0 to 10% tungsten 3.0 to 8% molybdenum The remainder to 100% is iron and cobalt of which the iron content is at least 50% and does not exceed 80% of the cobalt content.
The accompanying illustration shows the results of tests in a heated state of five alloys of the following composition:
1. Alloy 2. Alloy 3. Alloy 4. Alloy 6. Alloy Per cent Per cent Per cent Per cent Per cent 1.42 l. 43 1.46 1. 38 1. 6O 1. 43 2. 80 2. l8 1. 81 2. 55 0. 47 0.93 0.83 0. 35 0. 44 27. 45 24. 7O 25. 28. 08 25. 30 5. 16 5. 31 4. 80 6. 17 4.80 4. 68 4.68
l. 07 27. 16 41. 80 28. 91 47. 33 rest rest rest rest rest From the illustration it appears that the addition of molybdenum maintains the hardness in a heated state of the alloys rich in iron and. poor in cobalt at a value which corresponds with that of alloys free from iron and rich in cobalt.
It is also possible to substitute for the tungsten content the customary equivalent quantities of molybdenum, especially in the known ratio of 2:1.
With the knowledge thus gained that by the addition of molybdenum to hard alloys of iron but poor in cobalt, these alloys in a heated state may be endowed with the same properties which the hard alloys that are practically free of iron and of a high cobalt content exhibit, it becomes possible to get along with relatively small additions of cobalt and to satisfy the needs of wartime economy for such alloys.
The welding properties of the hard alloys ac- 0.8% to 3% carbon 0.3% to 3.5% silicon 23% to 32% chromium 2% to 30% tungsten 3% to 15% molybdenum the balance up to 100% substantiallyal13beingcobalt and iron of which the ironcontent amounts to at least 35% and does not exceed.80%
of the total sum of the combined iron and cobalt contents.
2. Weldable cobalt bearing hardalloys of high. strength at elevated temperatures containing 0.8% to 1.8% carbon 0.3% to 3.5% silicon 23% to 32% chromium 2% to 10% tungsten 3% to 8% molybdenum the balance up to 100% substantially being all cobalt and iron of which the iron content amounts to at least 50% and does not exceed 80% of the total sum of the combined iron and cobalt contents.
MAX SCHMIDT.
REFERENCES. CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number? Name Date 1,277,431 Kuehnrich Sept. 3, 1918 1,376,056? Wandersee et a1. Apr. 26, 1921 2,309,372 Wissler Jan. 26, 1943 OTHER REFERENCES Stahlund Eisen, vol. 44, 1924, pages 1717 to 1720.
Chemical Abstracts, vol. No. 32,, 1942,, column 5756..
Engineering Alloys, second edition, page 1 '70,, alloy No. 1050-1. Edited by Woldman etiall Ber. 5 vised 1111945. Published by the American Society 2 for. Metals, Cleveland, Ohio.

Claims (1)

1. WELDABLE COBALT BEARING HARD ALLOYS OF HIGH STRENGTH AT ELEVATED TEMPERATURES CONTAINING 0.8% TO 3% CARBON 0.3% TO 3.5% SILICON 23% TO 32% CHROMIUM 2% TO 30% TUNGSTEN 3% TO 15% MOLYBDENUM THE BALANCE UP TO 100% SUBSTANTIALLY ALL BEING COBALT AND IRON OF WHICH THE IRON CONTENT AMOUNTS TO AT LEAST 35% AND DOES NOT EXCEED 80% OF THE TOTAL SUM OF THE COMBINED IRON AND COBALT CONTENTS.
US11364A 1940-02-29 1948-02-27 Weldable and high-temperature resisting hard alloys of cobalt and iron base Expired - Lifetime US2553609A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2553609X 1940-02-29

Publications (1)

Publication Number Publication Date
US2553609A true US2553609A (en) 1951-05-22

Family

ID=7996008

Family Applications (1)

Application Number Title Priority Date Filing Date
US11364A Expired - Lifetime US2553609A (en) 1940-02-29 1948-02-27 Weldable and high-temperature resisting hard alloys of cobalt and iron base

Country Status (1)

Country Link
US (1) US2553609A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2801165A (en) * 1955-09-30 1957-07-30 Coast Metals Inc Cobalt-base alloys
US2871552A (en) * 1946-05-10 1959-02-03 Elek Ska Svetsningsaktiebolage Weld metal deposits and arc welding electrodes for producing the same
US2888738A (en) * 1954-06-07 1959-06-02 Carborundum Co Sintered metal bodies containing boron nitride
US3307939A (en) * 1963-06-04 1967-03-07 Boehler & Co Ag Geb Corrosion-resisting cobalt-chromium-tungsten alloys
US3706448A (en) * 1970-03-23 1972-12-19 British Iron Steel Research Skids or beams for furnaces
US3778254A (en) * 1971-11-18 1973-12-11 Atomic Energy Commission Brazing filler metal for molybdenum

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1277431A (en) * 1916-10-17 1918-09-03 Paul Richard Kuehnrich Steel.
US1376056A (en) * 1919-09-10 1921-04-26 Ford Motor Co Metal alloy
US2309372A (en) * 1940-06-11 1943-01-26 Haynes Stellite Co Cutting tool

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1277431A (en) * 1916-10-17 1918-09-03 Paul Richard Kuehnrich Steel.
US1376056A (en) * 1919-09-10 1921-04-26 Ford Motor Co Metal alloy
US2309372A (en) * 1940-06-11 1943-01-26 Haynes Stellite Co Cutting tool

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2871552A (en) * 1946-05-10 1959-02-03 Elek Ska Svetsningsaktiebolage Weld metal deposits and arc welding electrodes for producing the same
US2888738A (en) * 1954-06-07 1959-06-02 Carborundum Co Sintered metal bodies containing boron nitride
US2801165A (en) * 1955-09-30 1957-07-30 Coast Metals Inc Cobalt-base alloys
US3307939A (en) * 1963-06-04 1967-03-07 Boehler & Co Ag Geb Corrosion-resisting cobalt-chromium-tungsten alloys
US3706448A (en) * 1970-03-23 1972-12-19 British Iron Steel Research Skids or beams for furnaces
US3778254A (en) * 1971-11-18 1973-12-11 Atomic Energy Commission Brazing filler metal for molybdenum

Similar Documents

Publication Publication Date Title
US3164465A (en) Nickel-base alloys
US3046108A (en) Age-hardenable nickel alloy
US3030206A (en) High temperature chromiummolybdenum alloy
US2562854A (en) Method of improving the high-temperature strength of austenitic steels
US2373490A (en) Heat-resisting alloys
US2553609A (en) Weldable and high-temperature resisting hard alloys of cobalt and iron base
US2955934A (en) High temperature alloy
US2469718A (en) Alloys
US2975051A (en) Nickel base alloy
US3118763A (en) Cobalt base alloys
US3591371A (en) Cobalt base oxidation resistant alloy
US2780545A (en) High-temperature alloy
US2524660A (en) Watch mainspring
US2575915A (en) Nickel base high-temperature alloy
US2911298A (en) Copper base brazing alloy
US2513469A (en) Alloy articles for use at high temperatures
US2162596A (en) Furnace heating element
US2978319A (en) High strength, low alloy steels
US1987714A (en) High temperature thermostatic metal
US3068096A (en) Wear-resistant alloy
US3597193A (en) Vanadium base alloy
US3707409A (en) Nickel base alloy
US2801165A (en) Cobalt-base alloys
US3155499A (en) Brazing alloy
US2744821A (en) Iron base high temperature alloy