JPS57207115A - Annealing method for material of turbine rotor to relieve stress - Google Patents
Annealing method for material of turbine rotor to relieve stressInfo
- Publication number
- JPS57207115A JPS57207115A JP9281981A JP9281981A JPS57207115A JP S57207115 A JPS57207115 A JP S57207115A JP 9281981 A JP9281981 A JP 9281981A JP 9281981 A JP9281981 A JP 9281981A JP S57207115 A JPS57207115 A JP S57207115A
- Authority
- JP
- Japan
- Prior art keywords
- temp
- base
- steel
- deposited
- turbine rotor
- 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.)
- Granted
Links
Classifications
-
- 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
- C21D9/38—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for roll bodies
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
PURPOSE:To relieve stress remaining in steel deposited to coat the surface of the base of a rotor by annealing the deposited coating layer while maintaining it at a temp. below the average temp. of the base. CONSTITUTION:A prescried part of a turbine rotor made of 12% Cr steel as base metal is coated with deposited steel having a higher coefft. of thermal expansion than the base metal. This coating layer 2 is then annealed while spraying air for cooling. During the end of the ennealing and the beginning of a cooling stage for returning to ordinary temp., the layer 2 is maintained at a temp. below the temp. of the base 1 of the rotor. Thus, stress remaining in the steel deposited to coat the surface of the base is relieved.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9281981A JPS57207115A (en) | 1981-06-16 | 1981-06-16 | Annealing method for material of turbine rotor to relieve stress |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9281981A JPS57207115A (en) | 1981-06-16 | 1981-06-16 | Annealing method for material of turbine rotor to relieve stress |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS57207115A true JPS57207115A (en) | 1982-12-18 |
JPH0114287B2 JPH0114287B2 (en) | 1989-03-10 |
Family
ID=14065030
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9281981A Granted JPS57207115A (en) | 1981-06-16 | 1981-06-16 | Annealing method for material of turbine rotor to relieve stress |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS57207115A (en) |
-
1981
- 1981-06-16 JP JP9281981A patent/JPS57207115A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPH0114287B2 (en) | 1989-03-10 |
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