US3260594A - High temperature alloys - Google Patents
High temperature alloys Download PDFInfo
- Publication number
- US3260594A US3260594A US425687A US42568765A US3260594A US 3260594 A US3260594 A US 3260594A US 425687 A US425687 A US 425687A US 42568765 A US42568765 A US 42568765A US 3260594 A US3260594 A US 3260594A
- Authority
- US
- United States
- Prior art keywords
- chromium
- alloy
- creep
- tungsten
- manganese
- 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
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Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
- C21D9/54—Furnaces for treating strips or wire
- C21D9/68—Furnace coilers; Hot coilers
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
Definitions
- a single preferred composition would be:
- the chromium content must be 20% or higher to avoid catastrophic oxidation.
- the lower limit of chromium is critical if oxidation resistance and high creep at temperatures above 1800 F. and particularly above 2000 F. are to be attained.
- FIGURE 3A there is illustrated the curve of stress rupture (solid line) and the curve of creep rate in percent deflection (chain line) at 1800 F. for an alloy of the composition C .42 Ni 256 Mn 1.46 Cr 227 S1 185 W 142
- FIGURE 3B there is illustrated the curve of stress rupture (solid line) and the curve of creep rate in percent deflection (chain line) at 2000 F. for the same alloy.
- Variations in carbon are plotted against rate of creep in FIGURE 4 and variations of manganese are plotted against rate of creep in FIGURE 5 all within the matrix of this invention.
- chromium at about 17% chromium is illustrated in FIG- URE 6.
- EXAMPLE V Another series of tests were made to compare prior art alloys with the alloys 'of this invention in oxidation tests at 2200 F. and at 2250 F. The first stage tests were run for 100 hours at 2200 F. :10 F. and the second The foregoing tests show the criticality of the chromium at about 17% in withstanding oxidation at 2200 F. and the criticality of 20% chromium at 2250 F. in avoiding catastrophic oxidation.
- Experimental heat treating trays were made of the preferred alloy composition of this invention. These trays were used for four months for carrying parts to be hardened at temperatures of 1600 to 1750 F., carburizing and carbonitriding. The trays were cyclically heated to the temperature and then put through an oil quench and draw. At the end of the four month period all trays were in excellent condition. This experience illustrates the excellent resistance to thermal shock of the alloy of the invention.
- a low creep, high strength alloy resistant to corrosion and thermal shock at elevated temperatures having stress rupture characteristics at 4000 p.s.i. and 1800 F. of at least 400 hours and at 2000 F. and 2000 p.s.i. of at least hours comprising about 0.3% to 0.9% carbon, about 20% to 30% chromium, about 15% to 35% nickel, about 0.8% to 4% manganese, about 0.9% to 3.5% silicon, about 0.3% to 5% tungsten and the balance iron with residual impurities in ordinary amounts.
- a low creep, high strength alloy resistant to corrosion and thermal shock at elevated temperatures having stress rupture characteristics at 4000 p.s.i. and 1800 F. of at least 400 hours and at 2000 F. and 2000 p.s.i.
- a low creep, high strength alloy resistant to corrosion and thermal shock at temperatures of 1800 F. to 2200 F. comprising about 0.3% to 0.9% carbon, about 17% to 30% chromium, about 15 to 35% nickel,
- a low creep, high strength alloy resistant to corrosion and thermal shock at temperatures of 1800 F. Ito 2200 F. comprising about 0.35% to 0.75% carbon, about to chromium, about 30% to nickel, about 1.2% to 2.4% manganese, about 1.2% to 2.5% silicon, about 1.75% to 5% tungsten and the balance iron with residual impurities in ordinary amounts.
- a loW creep, high strength alloy resistant to corrosion and thermal shock at temperatures of 1600 F. to 2200 F. comprising about 0.4% carbon, about 23% chromium, about 30% nickel, about 1.5% manganese, about 2% silicon, about 1.75 tungsten and the balance iron With residual impurities in ordinary amounts.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Soft Magnetic Materials (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR951283A FR1379124A (fr) | 1962-12-31 | 1963-10-21 | Alliages résistant aux températures élevées |
US425687A US3260594A (en) | 1965-01-11 | 1965-01-11 | High temperature alloys |
GB560/66A GB1116103A (en) | 1965-01-11 | 1966-01-05 | Improved alloy composition |
BE674904D BE674904A (enrdf_load_html_response) | 1965-01-11 | 1966-01-10 | |
FR45388A FR89298E (fr) | 1962-12-31 | 1966-01-10 | Alliages résistant aux températures élevées |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US425687A US3260594A (en) | 1965-01-11 | 1965-01-11 | High temperature alloys |
Publications (1)
Publication Number | Publication Date |
---|---|
US3260594A true US3260594A (en) | 1966-07-12 |
Family
ID=23687617
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US425687A Expired - Lifetime US3260594A (en) | 1962-12-31 | 1965-01-11 | High temperature alloys |
Country Status (3)
Country | Link |
---|---|
US (1) | US3260594A (enrdf_load_html_response) |
BE (1) | BE674904A (enrdf_load_html_response) |
GB (1) | GB1116103A (enrdf_load_html_response) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3856516A (en) * | 1970-02-12 | 1974-12-24 | Blair Knox Co | Low creep high strength ferrous alloy |
US3865634A (en) * | 1973-08-13 | 1975-02-11 | Exxon Research Engineering Co | Heat resistant alloy for carburization resistance |
US3919073A (en) * | 1973-08-13 | 1975-11-11 | Exxon Research Engineering Co | Heat resistant alloy for carburization resistance |
US4119456A (en) * | 1977-01-31 | 1978-10-10 | Steel Founders' Society Of America | High-strength cast heat-resistant alloy |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1528478A (en) * | 1924-12-16 | 1925-03-03 | Hadfield Robert Abbott | Alloy |
-
1965
- 1965-01-11 US US425687A patent/US3260594A/en not_active Expired - Lifetime
-
1966
- 1966-01-05 GB GB560/66A patent/GB1116103A/en not_active Expired
- 1966-01-10 BE BE674904D patent/BE674904A/xx unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1528478A (en) * | 1924-12-16 | 1925-03-03 | Hadfield Robert Abbott | Alloy |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3856516A (en) * | 1970-02-12 | 1974-12-24 | Blair Knox Co | Low creep high strength ferrous alloy |
US3865634A (en) * | 1973-08-13 | 1975-02-11 | Exxon Research Engineering Co | Heat resistant alloy for carburization resistance |
US3919073A (en) * | 1973-08-13 | 1975-11-11 | Exxon Research Engineering Co | Heat resistant alloy for carburization resistance |
US4119456A (en) * | 1977-01-31 | 1978-10-10 | Steel Founders' Society Of America | High-strength cast heat-resistant alloy |
Also Published As
Publication number | Publication date |
---|---|
GB1116103A (en) | 1968-06-06 |
BE674904A (enrdf_load_html_response) | 1966-07-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: WHITE CONSOLIDATED INDUSTRIES, INC. Free format text: MERGER;ASSIGNORS:BLAW-KNOX COMPANY;KELVINATOR, INC.;WHITE-WESTINGHOUSE CORPORATION;AND OTHERS;REEL/FRAME:003926/0372 Effective date: 19781221 Owner name: BLAW-KNOX COMPANY Free format text: MERGER;ASSIGNORS:AETNA-STANDARD ENGINEERING COMPANY;BLAW-KNOX CONSTRUCTION EQUIPMENT, INC.,;BLAW-KNOX EQUIPMENT, INC.;AND OTHERS;REEL/FRAME:003926/0382 Effective date: 19781221 |