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CN1300445C - Turbine high temperature blade and its heat treatment process - Google Patents

Turbine high temperature blade and its heat treatment process Download PDF

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Publication number
CN1300445C
CN1300445C CNB2003101041284A CN200310104128A CN1300445C CN 1300445 C CN1300445 C CN 1300445C CN B2003101041284 A CNB2003101041284 A CN B2003101041284A CN 200310104128 A CN200310104128 A CN 200310104128A CN 1300445 C CN1300445 C CN 1300445C
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CN
China
Prior art keywords
high temperature
air cooling
heat treatment
blade
treatment process
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
CNB2003101041284A
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Chinese (zh)
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CN1554857A (en
Inventor
杨功显
范华
胡维成
张波
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.)
DEC Dongfang Turbine Co Ltd
Original Assignee
DONGFANG STEAM TURBINE PLANT
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
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Priority to CNB2003101041284A priority Critical patent/CN1300445C/en
Publication of CN1554857A publication Critical patent/CN1554857A/en
Application granted granted Critical
Publication of CN1300445C publication Critical patent/CN1300445C/en
Anticipated expiration legal-status Critical
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Abstract

The present invention provides a high temperature vane for supercritical or ultra supercritical steam turbine sets and the heat treatment process of the high temperature vane. The vane is made of 12% of novel Cr steel (12% of Cr-Mo-W-V-Nb-Co-B-N steel-based alloy materials). The parameters of the heat treatment process are 1000 DEG C to 1180 DEG C *1 to 10 hours of oil cooling or air cooling of quenching treatment, and 600 DEG C to 750DEG C * 2 to 15 hours of air cooling of tempering treatment. Through experiments, the present invention completely meets design requirements and technical requirements for the high temperature endurance and the creep property of the high temperature vane of a supercritical or an ultra supercritical steam turbine set.

Description

A kind of steam turbine high-temperature blade and heat treatment process thereof
Technical field
The present invention relates to a kind of high temperature blade and heat treatment process thereof of overcritical or supercritical turbine unit.
Background technique
The former subcritical materials such as 2Cr12NiMo1W1V refractory steel or 2Cr11Mo1VNbN refractory steel that use with supercritical pressure turbine unit high temperature blade material.Because the steam parameter of steam turbine unit improves, (steam parameter is the subcritical pressure turbine unit: 538 ℃/538 ℃, 17Mpa) the high temperature blade material of Shi Yonging can not satisfy overcritical or the supercritical turbine unit (steam parameter is: 566 ℃/566 ℃, 24Mpa or 600 ℃/600 ℃, 24Mpa) high-temperature and durable of high temperature blade and croop property requirement.
Summary of the invention
Purpose of the present invention is exactly for after the steam parameter raising that solves above-mentioned steam turbine unit, be used for the technical barrier that the high temperature blade of overcritical or supercritical turbine unit can not meet the demands, filter out a kind of new substitution material and make blade, another purpose is the heat treatment process problem that solves this blade.
The objective of the invention is to reach like this: through after the various tests, adopt new 12%Cr steel to make high temperature blade, new 12%Cr steel is a 12%Cr-Mo-W-V-Nb-Co-B-N base steel alloy.Blade process of thermal treatment parameter is: Quenching Treatment is: 1000 ℃-1180 ℃ * 1-10 hour, and oil cooling or air cooling; Temper is: 600 ℃-750 ℃ * 2-15 hour, and air cooling.
Preferred Quenching Treatment is: 1060 ℃-1150 ℃ * 1-5 hour, and oil cooling or air cooling;
Preferred temper is: 650 ℃-720 ℃ * 5-8 hour, and air cooling.
Best Quenching Treatment is: 1120 ℃-1150 ℃ * 2-4 hour, and oil cooling or air cooling;
Best temper is: 680 ℃-700 ℃ * 2-15 hour, and air cooling.
The blade processing step is: the smelting of new 12%Cr steel is: electric furnace+electroslag remelting;
Moulding is adopted: hot rolling or forge hot;
Blade blank: carry out property heat treatment;
Be machined into product again.
Effect of the present invention: owing to adopt the better new 12%Cr steel (12%Cr-Mo-W-V-Nb-Co-B-N base steel alloy) of high-temperature behavior.Through the test reached designing requirement fully, satisfied overcritical or supercritical turbine unit high temperature blade to high-temperature and durable and creep technical requirements.
Embodiment
Embodiment one
Through after the various tests, decision adopts the 12%Cr-Mo-W-V-Nb-Co-B-N base steel alloy of new 12%Cr steel to make high temperature blade, replaces materials such as 2Cr12NiMo1W1V refractory steel or 2Cr11Mo1VNbN refractory steel.It is very important heat-treating technology for the high-temperature behavior of this new blade material.
1. new 12%Cr steel chemical composition and mechanical property requirements:
C Si Mn P S Ni Cr
0.12-0.17 ≤0.30 0.30~0.60 ≤0.025 ≤0.025 ≤0.40 10.50~11.50
Mo Co B V Nb W N
0.60~0.80 2.90~3.10 0.007~0.015 0.15~0.25 0.10~0.20 1.70~2.00 0.03~0.05
Cu≤0.03; Al≤0.05; Ti≤0.05; Surplus is Fe
(1) tensile test at room temperature:
σ b σ δ ψ Akv hardness HB
≥965N/mm 2 ≥690N/mm 2 ≥15% ≥45% ≥11J 291-331
(2) stress-rupture tester:
Test conditions: 650 ℃ of temperature; Stress 186N/mm 2
Smooth sample: T>55 hour;
Notched specimen: T breach/T is smooth 〉=and 1
2. process the process step of blade with new 12%Cr steel:
(1) smelting of steel is: electric furnace+electroslag remelting;
(2) moulding is adopted: hot rolling or forge hot.
3. the heat treatment process of blade: Quenching Treatment and temper
(1) Quenching Treatment: 1000 ℃ * 1 hour, oil cooling or air cooling
(2) temper: 600 ℃ * 2 hours, air cooling.
4. blade blank carries out property heat treatment, is machined into product again.
Embodiment two
The Quenching Treatment of blade: 1060 ℃ * 5 hours, oil cooling or air cooling; Temper: 650 ℃ * 5 hours, air cooling.All the other are with embodiment one.
Embodiment three
The Quenching Treatment of blade: 1120 ℃ * 3 hours, oil cooling or air cooling; Temper: 680 ℃ * 10 hours, air cooling.All the other are with embodiment one.
Embodiment four
The Quenching Treatment of blade: 1150 ℃ * 8 hours, oil cooling or air cooling; Temper: 700 ℃ * 12 hours, air cooling.All the other are with embodiment one.
Embodiment five
The Quenching Treatment of blade: 1180 ℃ * 10 hours, oil cooling or air cooling; Temper: 750 ℃ * 15 hours, air cooling.All the other are with embodiment one.

Claims (4)

1. steam turbine high-temperature blade is characterized in that: adopt the 12%Cr steel to make high temperature blade, the 12%Cr steel is a 12%Cr-Mo-W-V-Nb-Co-B-N base steel alloy, its chemical composition, by weight percentage, Mo 0.60-0.80, N 0.03-0.05, C 0.12-0.17, Si≤0.30, Mn 0.30-0.60, P≤0.025, S≤0.025, Ni≤0.40, Cr 10.50-11.50, Co 2.90-3.10, B0.007-0.015, V 0.15-0.25, Nb 0.10-0.20, W 1.70-2.00, Cu≤0.03, Al≤0.05, Ti≤0.05, surplus is Fe.
2. the heat treatment process of a steam turbine high-temperature blade as claimed in claim 1, step is:
(1) Quenching Treatment is: 1000 ℃-1180 ℃ * 1-10 hour, and oil cooling or air cooling,
(2) temper is: 600 ℃-750 ℃ * 2-15 hour, and air cooling.
3. heat treatment process as claimed in claim 2, its Quenching Treatment is: 1060 ℃-1150 ℃ * 1-5 hour, oil cooling or air cooling; Temper is: 650 ℃-720 ℃ * 5-8 hour, and air cooling.
4. heat treatment process as claimed in claim 2, its Quenching Treatment is: 1120 ℃-1150 ℃ * 2-4 hour, oil cooling or air cooling; Temper is: 680 ℃-700 ℃ * 2-15 hour, and air cooling.
CNB2003101041284A 2003-12-26 2003-12-26 Turbine high temperature blade and its heat treatment process Expired - Lifetime CN1300445C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2003101041284A CN1300445C (en) 2003-12-26 2003-12-26 Turbine high temperature blade and its heat treatment process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2003101041284A CN1300445C (en) 2003-12-26 2003-12-26 Turbine high temperature blade and its heat treatment process

Publications (2)

Publication Number Publication Date
CN1554857A CN1554857A (en) 2004-12-15
CN1300445C true CN1300445C (en) 2007-02-14

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Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101629232B (en) * 2008-07-16 2012-05-09 上海重型机器厂有限公司 Heat treatment method for supercritical turbine cylinder steel castings
CN102417969B (en) * 2011-11-23 2013-07-17 沈阳科金特种材料有限公司 Heat treatment process for high-hardenability Martensitic stainless steel for moving blades
CN102836946B (en) * 2012-09-11 2014-11-05 四川豪特石油设备有限公司 Roll forging forming process for last stage of moving blade of 600MW unit steam turbine
CN103937947B (en) * 2014-04-11 2016-01-13 上海电气电站设备有限公司 The heat treating method of Long Turbine Blades material therefor
CN104033189B (en) * 2014-06-27 2016-01-27 南京赛达机械制造有限公司 A kind of processing technology of turbine blade
CN105239021B (en) * 2014-07-08 2017-07-25 南京赛达机械制造有限公司 A kind of high pressure resistant turbine blade and its production technology
CN104120370B (en) * 2014-07-29 2016-01-20 包头市泽傲科贸有限公司 A kind of separator blade
CN105695678B (en) * 2016-04-18 2017-11-03 东北大学 The heat treatment method of BN phase morphologies in a kind of control ultra supercritical heat resisting steel
CN108031779A (en) * 2017-11-29 2018-05-15 无锡透平叶片有限公司 A kind of turbine blade and preparation method thereof
CN109943783B (en) * 2017-12-20 2021-11-19 上海电气电站设备有限公司 High-temperature casting material for steam turbine

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5247506A (en) * 1975-10-13 1977-04-15 Kobe Steel Ltd Nitrogen-containing powder-sintered high speed steel
US4242151A (en) * 1978-10-25 1980-12-30 Creusot-Loire Chromizing of steels by gaseous method
JPS61295319A (en) * 1985-06-21 1986-12-26 Sumitomo Metal Ind Ltd Method for manufacturing suction rod for wet carbon dioxide oil well
JPH04198455A (en) * 1990-11-29 1992-07-17 Hitachi Ltd Corrosion resisting alloy, hot roll and its production, and hot rolling mill
US5972287A (en) * 1997-06-25 1999-10-26 Mitsubishi Heavy Industries, Ltd. Heat-resisting steel
CN1246579A (en) * 1998-06-09 2000-03-08 三菱重工业株式会社 Deformed material welding rotor of steam turbine
CN1294636A (en) * 1998-03-23 2001-05-09 尤迪霍尔姆工具公司 Steel material and method for its mfg.

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5247506A (en) * 1975-10-13 1977-04-15 Kobe Steel Ltd Nitrogen-containing powder-sintered high speed steel
US4242151A (en) * 1978-10-25 1980-12-30 Creusot-Loire Chromizing of steels by gaseous method
JPS61295319A (en) * 1985-06-21 1986-12-26 Sumitomo Metal Ind Ltd Method for manufacturing suction rod for wet carbon dioxide oil well
JPH04198455A (en) * 1990-11-29 1992-07-17 Hitachi Ltd Corrosion resisting alloy, hot roll and its production, and hot rolling mill
US5972287A (en) * 1997-06-25 1999-10-26 Mitsubishi Heavy Industries, Ltd. Heat-resisting steel
CN1294636A (en) * 1998-03-23 2001-05-09 尤迪霍尔姆工具公司 Steel material and method for its mfg.
CN1246579A (en) * 1998-06-09 2000-03-08 三菱重工业株式会社 Deformed material welding rotor of steam turbine

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Owner name: DONGFANG ELECTRIC GROUP DONGFANG STEAM TURBINE CO.

Free format text: FORMER NAME OR ADDRESS: DONGFAN STEAM TURBINE FACTORY

CP01 Change in the name or title of a patent holder

Address after: 618201 Deyang City, Sichuan Province town of Hanwang

Patentee after: DONGFANG TURBINE Co.,Ltd. DTC

Address before: 618201 Deyang City, Sichuan Province town of Hanwang

Patentee before: Dongfang Steam Turbine Plant

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Granted publication date: 20070214

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