US2140905A - Turbine blade - Google Patents
Turbine blade Download PDFInfo
- Publication number
- US2140905A US2140905A US77549A US7754936A US2140905A US 2140905 A US2140905 A US 2140905A US 77549 A US77549 A US 77549A US 7754936 A US7754936 A US 7754936A US 2140905 A US2140905 A US 2140905A
- Authority
- US
- United States
- Prior art keywords
- chromium
- steels
- steel
- turbine blade
- nitrogen
- 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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Classifications
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- 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
Definitions
- This invention relates to improved high-chromium alloy steel turbine blades for use at elevated temperatures.
- blades employed in tur- 5 bines possess high strength and appreciable ductility and toughness when exposed to superheated steam at high pressures.
- the steel must retain satisfactory strength and ductility for a reasonable length of time at the operating temperature, and must offer considerable resistance rosion, without decreasing undesirably the ductility of the material.
- turbine blades comprise steels having a chromium content between about 12% and 16%, carbon in amounts up to about 0.20%, about 0.05% to 0.20% nitrogen, and the remainder iron, except for the customary small amounts of impurities and alloyed additions made to ordinary steels of'similar chromium content.
- a chromium content between about 12% and 16%
- carbon in amounts up to about 0.20%, about 0.05% to 0.20% nitrogen, and the remainder iron, except for the customary small amounts of impurities and alloyed additions made to ordinary steels of'similar chromium content.
- the nitrogen content nor the carbon content exceeds about 0.12% of the steel.
- Turbine blade having high strength, high resistance to oxidation -and high ductility and toughness when exposed to superheated steam at high pressures, said turbine bladebeing composed of a steel containing about 12% to about 16% chromium, carbon in amounts up to about 0.2%, and about 0.05 to less than 0.2% nitrogen, the remainder' being substantially all iron, the nitrogen being distributed substantially uniformly throughout the steel.
- Turbine blade for use athigh temperatures and having high strength, high resistance to oxidation, and high ductility and toughness when the steel.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Patented Dec. 20, 1938 Union Carbide and Carbon Research Laboratories, Inc., a corporation of New York Serial No. 77,549
No Drawing. Application May 2, 1936,
2 Claims.
This invention relates to improved high-chromium alloy steel turbine blades for use at elevated temperatures.
It isimportant that the blades employed in tur- 5 bines possess high strength and appreciable ductility and toughness when exposed to superheated steam at high pressures. In addition to these special engineering characteristics the steel must retain satisfactory strength and ductility for a reasonable length of time at the operating temperature, and must offer considerable resistance rosion, without decreasing undesirably the ductility of the material.
The effect of nitrogen in increasing the hardenability of the high chromium steels without seriously decreasing their ductility or toughness is clearly illustrated by the following table of data representing the physical properties of several steels containing about 13% chromium, about 0.07% carbon, small fractional amounts of silicon and manganese; and the amounts of nitrogen indicated in the first column:
Condi- Percent Maximum Percent Izod Percent tion of Yield pt Stresq elonga- Red of 1m Brinell pact 15 N metal lb./sq 1n Ill/Sq m tiozn m area it. L hardness 0.025 1 139,000 151,000 l l 5 293 0 025 2 66, 000 95, 500 23 60 58 187 0 025 3 44, 000 78, 500 30 71 101 137 0. 08 1 178, 000 194, 000 6 11 4 402 0.08 2 106, 500 123, 500 21 65 60 22s 0. 08 3 6B, 500 90, 500 26 60 100 I 179 l-Oil quenched from 950 0.
2-0il quenched from 950 0., then held 2 hours at 600 C. and air cooled. v 3 ==He1d 3 hours at 750 C. and air cooled. 4 25 to the oxidation that normally occurs at elevated temperatures;
In the early attempts to employ high chromium steels for this purpose, it was found that the chromium content must be closely controlled if the desired physical characteristics were to be attained. If the chromium content is too low. the strength of the steel is too low and the steel does not offer sufficient resistance to oxidation. 5 On the other hand, if the chromium is too high, thesteel cannot be given satisfactorily high strength, without at the same time rendering it excessively brittle. Thus, it was found necessary-to employ a steel containing between about 40 11% andabout 14% chromium. Even in steels of this type difliculty has been met in securing the desired strength without producing an undesirable brittleness. Some improvement has been secured by introducing small amounts of certain 4 hardening elements, such as nickel, copper, tung-= sten, and molybdenum.
I have found that certain chromium steels containing nitrogen perform unusually well as turbine blades. Although the usefulness of this 50 discovery is not limited to or by any theory, it is believed that the presence of chromium nitrides, which have a high solubility in the chromium iron solid solutions, greatly increases the hardening capacity of the steels, and it imparts im- 55 proved hardenability without rendering the metal excessively brittle or of inferior ductility. Furthermore, when nitrogen is present in the steels, it is possible to increase the chromium content and thereby secure a-greater resistance to cor- According to the present invention turbine blades comprise steels having a chromium content between about 12% and 16%, carbon in amounts up to about 0.20%, about 0.05% to 0.20% nitrogen, and the remainder iron, except for the customary small amounts of impurities and alloyed additions made to ordinary steels of'similar chromium content. Preferably, .neither the nitrogen content nor the carbon content exceeds about 0.12% of the steel.
I claim:
1. Turbine blade having high strength, high resistance to oxidation -and high ductility and toughness when exposed to superheated steam at high pressures, said turbine bladebeing composed of a steel containing about 12% to about 16% chromium, carbon in amounts up to about 0.2%, and about 0.05 to less than 0.2% nitrogen, the remainder' being substantially all iron, the nitrogen being distributed substantially uniformly throughout the steel.
2. Turbine blade for use athigh temperatures and having high strength, high resistance to oxidation, and high ductility and toughness when the steel.
. RUSSELL FRANKS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US77549A US2140905A (en) | 1936-05-02 | 1936-05-02 | Turbine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US77549A US2140905A (en) | 1936-05-02 | 1936-05-02 | Turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
US2140905A true US2140905A (en) | 1938-12-20 |
Family
ID=22138715
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US77549A Expired - Lifetime US2140905A (en) | 1936-05-02 | 1936-05-02 | Turbine blade |
Country Status (1)
Country | Link |
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US (1) | US2140905A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2693413A (en) * | 1951-01-31 | 1954-11-02 | Firth Vickers Stainless Steels Ltd | Alloy steels |
DE950855C (en) * | 1940-02-27 | 1956-10-18 | Boehler & Co Ag Geb | Materials for stresses on fatigue strength |
-
1936
- 1936-05-02 US US77549A patent/US2140905A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE950855C (en) * | 1940-02-27 | 1956-10-18 | Boehler & Co Ag Geb | Materials for stresses on fatigue strength |
US2693413A (en) * | 1951-01-31 | 1954-11-02 | Firth Vickers Stainless Steels Ltd | Alloy steels |
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