US2406363A - High-temperature alloy - Google Patents
High-temperature alloy Download PDFInfo
- Publication number
- US2406363A US2406363A US459715A US45971542A US2406363A US 2406363 A US2406363 A US 2406363A US 459715 A US459715 A US 459715A US 45971542 A US45971542 A US 45971542A US 2406363 A US2406363 A US 2406363A
- Authority
- US
- United States
- Prior art keywords
- alloy
- pounds per
- elongation
- square inch
- per square
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 title description 21
- 239000000956 alloy Substances 0.000 title description 21
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- 229910000519 Ferrosilicon Inorganic materials 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/07—Alloys based on nickel or cobalt based on cobalt
Definitions
- the present invention is an alloy particularly adapted for use under high temperature conditions and stresses such as encountered in the operation of supercharger turbines and thelike. Since the buckets in supercharger turbines rotate at a speed of about 20,000 revolutions per minute while subjected to temperatures in the neighborhood of 1500' F., the bucket material should have high physical properties at the operating temperature of the turbine.
- ferro silicon is desirable, its presence is not absolutely essential and it may be omitted. Although iron usually will be present in the alloy, it is considered an impurity. It is not harmful, however, in quantities up to about 3%.
- the quantity of carbon present in the alloy is in the range of 1 An alloy containing about 69% cobalt, about 0.1% to about 1.0% and preferably should be about 0.64% of the content of the alloy.
- the alloy as cast has a tensile strength of 72,100 to 77,400 pounds per square inch and an elongation in two inches of 25 to 22%.
- the alloy has been aged for 100 hours at 1500 F. it has a room temperature tensile st". ength of about 127,300 pounds to 132,500 pounds per square inch and an elongation of 3 to 4%.
- the aged alloy has a tensile strength of 78,400) 79,000 pounds per square inch and an elongation of 10%.
- composition is changed by substituting columbium for titanium imilar improvement in the properties of the aged alloy.
- columbium for titanium imilar improvement in the properties of the aged alloy.
- an alloy consisting of about 69% cobalt,about 24% chromium, about 5% tungsten carbide, about 1.2% columbium and about 1% term silicon has at room temperature and in the as-cast condition a tensllestrength of 113,200-to 117,300 pounds per square inch andan elongation of 7% in two inches.
- the alloy in the as-cast condition has a tensile strength of about 65,200 to about 70,000 pounds per square inch and an elongation of about 25to 26%. After the alloy was aged 100 hours at 1500 F.
- the aged alloy had a tensile strength of about 131,500 to 134,500 pounds per square inch and an elongation of 3%.
- the aged alloy had a tensile strength of 67,800 to 71,900 pounds per square inch and an elongation of 11 to 12%.
- Under a stress of 39,000 pounds per square inch the aged alloy failed in 10 hours at a temperature of 1500 F.
- the elongation at time of failure was 20%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Description
Patented Aug. 27, 1946 I Sidney 0. Fisher, Schenectady, N. Y., assignor to General Electric Company, a corporation of New York No Drawing. Application September 25, 1942, Serial No. 459.715
1 Claim. 1
The present invention is an alloy particularly adapted for use under high temperature conditions and stresses such as encountered in the operation of supercharger turbines and thelike. Since the buckets in supercharger turbines rotate at a speed of about 20,000 revolutions per minute while subjected to temperatures in the neighborhood of 1500' F., the bucket material should have high physical properties at the operating temperature of the turbine.
In carrying out the present invention I employ an alloy which contains about 69% cobalt.
about 24% chromium, about 5% tungsten carbide, about 1% ferro silicon with the remainder about .8 to 5% of metal from the group consisting of titanium and columbium. While ferro silicon is desirable, its presence is not absolutely essential and it may be omitted. Although iron usually will be present in the alloy, it is considered an impurity. It is not harmful, however, in quantities up to about 3%. The quantity of carbon present in the alloy is in the range of 1 An alloy containing about 69% cobalt, about 0.1% to about 1.0% and preferably should be about 0.64% of the content of the alloy.
24% chromium, about 5% tungsten carbide, about .8% titanium and about 1% ferro silicon at room temperature and in the as-cast condition has a tensile strength of about 109,000 to 111,000 pounds per square inch and an elongation in two inches of about 8 to 6%. At 1500 F. the alloy as cast has a tensile strength of 72,100 to 77,400 pounds per square inch and an elongation in two inches of 25 to 22%. After the alloy has been aged for 100 hours at 1500 F. it has a room temperature tensile st". ength of about 127,300 pounds to 132,500 pounds per square inch and an elongation of 3 to 4%. At 1500 F. the aged alloy has a tensile strength of 78,400) 79,000 pounds per square inch and an elongation of 10%.
When a stress of 39,200 pounds per square inch was applied to the alloy at a temperature of about 1500 F. it failed in 10-hours, theelongation at the time of failure was 20%. When a stress of 32,000 pounds per square inch was applied to the alloy at a temperature of 1500 F. the time of failure was hours and the elongation at failure was 13%. When a. stress of 26,700 pounds per squar inch was applied to the alloy at a temperature of 1500 F. the time for failure was 1000 hours.
If the composition is changed by substituting columbium for titanium imilar improvement in the properties of the aged alloy may be obtained. For example an alloy consisting of about 69% cobalt,about 24% chromium, about 5% tungsten carbide, about 1.2% columbium and about 1% term silicon has at room temperature and in the as-cast condition a tensllestrength of 113,200-to 117,300 pounds per square inch andan elongation of 7% in two inches. At 1500 F. the alloy in the as-cast condition has a tensile strength of about 65,200 to about 70,000 pounds per square inch and an elongation of about 25to 26%. After the alloy was aged 100 hours at 1500 F. it had a tensile strength of about 131,500 to 134,500 pounds per square inch and an elongation of 3%. At 1500 F. the aged alloy had a tensile strength of 67,800 to 71,900 pounds per square inch and an elongation of 11 to 12%. Under a stress of 39,000 pounds per square inch the aged alloy failed in 10 hours at a temperature of 1500 F. The elongation at time of failure was 20%. Under stress of 29,800 pounds per squarelnch the aged alloy failed in 100 hours the elongation at failure being 3%.
What I claim as new and desire to secure by Letters Patent of the United States is:
An alloy containing about 69% cobalt, about 24% chromium, approximately 5% tungsten car.- bide, about 1.2% columbium and about .80% silicon.
SIDNEY O. FISHER.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US459715A US2406363A (en) | 1942-09-25 | 1942-09-25 | High-temperature alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US459715A US2406363A (en) | 1942-09-25 | 1942-09-25 | High-temperature alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2406363A true US2406363A (en) | 1946-08-27 |
Family
ID=23825877
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US459715A Expired - Lifetime US2406363A (en) | 1942-09-25 | 1942-09-25 | High-temperature alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2406363A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2515774A (en) * | 1945-05-23 | 1950-07-18 | Gen Electric | High-temperature alloy |
-
1942
- 1942-09-25 US US459715A patent/US2406363A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2515774A (en) * | 1945-05-23 | 1950-07-18 | Gen Electric | High-temperature alloy |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3061426A (en) | Creep resistant alloy | |
| US2712498A (en) | Nickel chromium alloys having high creep strength at high temperatures | |
| JPS5816047A (en) | Nickel base alloy | |
| JPS58110661A (en) | Heat resistant steel | |
| US2432618A (en) | Ferrous alloys for high-temperature use | |
| US2562854A (en) | Method of improving the high-temperature strength of austenitic steels | |
| US2684299A (en) | Cobalt base alloys and cast articles | |
| US3146136A (en) | Method of heat treating nickel base alloys | |
| US2432619A (en) | Ferrous alloys and articles | |
| US3151981A (en) | Nickel-chromium-cobalt alloy | |
| US3166412A (en) | Cast nickel-base alloy for gas turbine rotors | |
| US2829048A (en) | High damping alloy and members prepared therefrom | |
| US20210285075A1 (en) | Sx-nickel alloy having improved tmf properties, raw material, and component | |
| US2486576A (en) | Heat-treatment of cobalt base alloys and products | |
| US2406363A (en) | High-temperature alloy | |
| US2688536A (en) | High-temperature creep resistant alloy | |
| US3720509A (en) | Nickel base alloy | |
| US2975051A (en) | Nickel base alloy | |
| US2575915A (en) | Nickel base high-temperature alloy | |
| US2744010A (en) | High temperature co-cr alloys | |
| US4325756A (en) | Fatigue resistant nickel superalloy | |
| US3876423A (en) | Nickel-chromium alloys | |
| US3107999A (en) | Creep-resistant nickel-chromiumcobalt alloy | |
| US2805154A (en) | Nickel-base alloy | |
| US2515774A (en) | High-temperature alloy |