CN87104497A - 一种钛叶片的保护端梢和焊接端梢的方法 - Google Patents
一种钛叶片的保护端梢和焊接端梢的方法 Download PDFInfo
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- CN87104497A CN87104497A CN87104497.8A CN87104497A CN87104497A CN 87104497 A CN87104497 A CN 87104497A CN 87104497 A CN87104497 A CN 87104497A CN 87104497 A CN87104497 A CN 87104497A
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- Prior art keywords
- blade
- temperature
- millimeter
- titanium
- welding
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- 239000010936 titanium Substances 0.000 title claims abstract description 8
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims abstract description 6
- 238000000034 method Methods 0.000 title claims description 7
- 238000003466 welding Methods 0.000 title abstract description 6
- 239000010949 copper Substances 0.000 claims abstract description 9
- 239000000203 mixture Substances 0.000 claims abstract description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052802 copper Inorganic materials 0.000 claims abstract description 6
- 239000011261 inert gas Substances 0.000 claims abstract description 3
- 238000003780 insertion Methods 0.000 claims 1
- 230000037431 insertion Effects 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 abstract description 6
- 229910052759 nickel Inorganic materials 0.000 abstract description 3
- 229910052742 iron Inorganic materials 0.000 abstract description 2
- 229910052750 molybdenum Inorganic materials 0.000 abstract description 2
- 208000034189 Sclerosis Diseases 0.000 abstract 1
- 230000003628 erosive effect Effects 0.000 abstract 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 5
- 229910001069 Ti alloy Inorganic materials 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- -1 titanium carbides Chemical class 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0292—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with more than 5% preformed carbides, nitrides or borides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Ceramic Products (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Coating With Molten Metal (AREA)
- Polishing Bodies And Polishing Tools (AREA)
Abstract
一种用于钛蒸汽透平叶片(1)的保护端梢(5),它的成分为:TiC 28%~40%,Cr+Co12%~26%,Mo 1%~6%,Ni 3%~8%,CH 0.3%~1.5%,其它为铁。端梢(5)被焊接到叶片(1)上,它们之间插有其厚度为7/100毫米~15/100毫米的铜带。将叶片(1)和它的端梢(5)的温度在真空或惰性气体的烘箱中升高到900°~950°,该温度保持30~75分钟,再将烘箱温度下降到环境温度。最佳的焊接能使端梢(5)硬化,使其具有非常良好的防水滴冲蚀能力。
Description
本发明涉及一种用钛合金制造的透平叶片的保护端梢。
蒸汽透平的钛合金叶片用于有较大尺寸的最后的低压级特别有利,然而在上述最后级中,蒸汽中含有的水滴将碰击圆周速度很高的运动叶片。
为了保护这种叶片的进气边,在该进气边上焊接端梢,该端梢的成份为:
Tic:28%~40%
Cr+Co:1%~26%
Mo:1%~6%
Ni:3%~8%
Cu:0.3%~1.3%
Fe:其他部分
钛碳化物的膨胀系数和剪切模数与钛相同,粘合剂由防腐蚀性强的钴、铬和可改善部件韧性的镍组成。
钛碳化物容易与铁的基体结合。
端梢的结构是马氏体,由于存在铬和钛,它的耐磨性强,由于存在镍,它的韧性高。
本发明还涉及一种端梢的焊接方法,该方法的步骤为:
端梢放置在叶片上,并在它们之间插入一个厚度为7/100毫米~15/100毫米的铜带;
在真空或隋性气体的烘箱中,将叶片和它的端梢加热到700℃~950℃,并将该温度保持30~70分钟;
将温度降到环境温度。
用这种方法,叶片、铜带和端梢之间的焊接是同时进行且为最佳。此外,至少部分地将钛碳化物成溶液,使得端梢的硬度大于50HRC。
如果端梢的硬度要大于60HRC,则温度要提高,然后降温度,在温度为450℃~500℃时保持6小时,然后下降到环境温度。在此阶段,实际上将全部钛碳化物成溶液,并同时进行了减小应力的热处理。
本发明的一个实施例将通过下列附图作为例子予以说明。
图1为本发明固定在叶片上的钛碳化物的端梢。
图2为图1所示叶片的平面图。
图3为图1所示叶片的剖面。
图1所示蒸汽透平叶片有根部1和带有进气边3和排气边4的扭曲叶身2。端梢覆盖了叶片2宽度的三分之一以上。铜带6置于叶片和端梢之间(见图2和图3)。
叶片用钛合金制成,端梢5的成份为:
Tic:28%~40%
Cr+Co:12%~26%
Mo:1%~6%
Ni:3%~8%
Cu:0.3%~1.5%
Fe:其他部分
具有较好效果的两种特殊成份是:
Tic Cr Co Mo Ni Cu Fe
成份1:32% 20% 0% 2% 3% 1% 其他部分
成份2:33% 14% 9% 5% 6% 0.8% 其他部分
端梢是通过机加工的粉末烧结和压实得到的,端梢的长度与欲保护的叶片部分长度相等(500毫米),它的宽度是足够的。它的形状是平直的或弯曲的,有或没有角度或弯成圆形,其目的是为了与叶片的进气边相配合。
叶片2和端梢5之间余层的机加工精度不大于1/10毫米。
准备好的叶片2,通过插在叶片2和端梢5之间其厚度为7/100毫米~15/100毫米的铜带,将端梢5焊接在叶片2上。
为了进行焊接,叶片2和端梢5一起被放入烘箱,端梢5用2~3个钼压板加热。
温度升高到900℃~950℃之间,根据叶片进气边的厚度将该温度保持30~75分钟,然后烘箱被冷却到环境温度。
除了焊接外,通过将大部分的钛碳化物成熔液使端梢与结构硬化处理,该端梢5的硬度为50HRC~55HRC。
为了进一步提高端梢5的硬度,要进行下述的附加处理:
将烘箱的温度升高到450℃~500℃并使它保持4~6小时,从而使全部钛碳化物基本上成熔液,同时完成减小应力的处理。
Claims (3)
1、一种钛透平叶片(1)的保护端梢(5)。其特征是它的成份为
TiC: 28%~40%
Cr+Co: 12%~26%
Mo: 1%~6%
Ni: 3%~8%
Cu: 0.3%~1.5%
Fe: 其他部分。
2、一种将权利要求1所述的端梢(5)焊接到叶片(1)上的方法,其特征在于该方法的步骤为:将端梢(5)放置在叶片(1)上,在它们之间插入其厚度为7/100毫米~15/100毫米的铜带(6);在真空或隋性气体的烘箱中,将叶片(1)和它的端梢(5)加热到900℃~950℃,并将该温度保持30~75分钟;然后冷却到环境温度。
3、根据权利要求2所述的方法,其特征是冷却到环境温度后,再将温度升高到450℃~500℃,将该温度保持4~6小时,然后再降回到环境温度。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8607661 | 1986-05-28 | ||
FR8607661A FR2599425B1 (fr) | 1986-05-28 | 1986-05-28 | Plaquette de protection pour aube en titane et procede de brasage d'une telle plaquette. |
Publications (2)
Publication Number | Publication Date |
---|---|
CN87104497A true CN87104497A (zh) | 1987-12-16 |
CN1009472B CN1009472B (zh) | 1990-09-05 |
Family
ID=9335746
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN87104497A Expired CN1009472B (zh) | 1986-05-28 | 1987-05-28 | 一种钛合金透平叶片的保护端梢 |
Country Status (11)
Country | Link |
---|---|
US (1) | US4795313A (zh) |
EP (1) | EP0249092B1 (zh) |
JP (1) | JPS62297442A (zh) |
CN (1) | CN1009472B (zh) |
AT (1) | ATE50824T1 (zh) |
CS (3) | CS276725B6 (zh) |
DE (1) | DE3761833D1 (zh) |
ES (1) | ES2013272B3 (zh) |
FR (1) | FR2599425B1 (zh) |
GR (1) | GR3000501T3 (zh) |
ZA (1) | ZA873837B (zh) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2075874T3 (es) * | 1990-12-19 | 1995-10-16 | Asea Brown Boveri | Procedimiento para la fabricacion de un alabe de turbina a partir de una aleacion base de titanio. |
DE69321298T2 (de) * | 1992-06-05 | 1999-04-08 | Gec Alsthom Electromecanique S.A., Paris | Verfahren zur Herstellung eines Einsatzes auf einem zu beschichtenden Formkörper aus Stahl oder aus Titanlegierung |
US5165859A (en) * | 1992-06-26 | 1992-11-24 | Hudson Products Corporation | Leading edge protection for fan blade |
US5351395A (en) * | 1992-12-30 | 1994-10-04 | General Electric Company | Process for producing turbine bucket with water droplet erosion protection |
DE4310896C1 (de) * | 1993-04-02 | 1994-03-24 | Thyssen Industrie | Verfahren zum Herstellen von verschleißfesten Kanten an Turbinenschaufeln |
US5449273A (en) * | 1994-03-21 | 1995-09-12 | United Technologies Corporation | Composite airfoil leading edge protection |
CN1041642C (zh) * | 1994-06-17 | 1999-01-13 | 株式会社日立制作所 | 高韧性13Cr5Ni系不锈钢及其用途 |
GB2293631B (en) * | 1994-09-30 | 1998-09-09 | Gen Electric | Composite fan blade trailing edge reinforcement |
US5531570A (en) * | 1995-03-06 | 1996-07-02 | General Electric Company | Distortion control for laser shock peened gas turbine engine compressor blade edges |
IL117347A (en) * | 1995-03-06 | 1999-10-28 | Gen Electric | Laser shock peened gas turbine engine compressor airfoil edges |
FR2742689B1 (fr) * | 1995-12-22 | 1998-02-06 | Gec Alsthom Electromec | Procede pour fabriquer une aube en titane alpha beta comprenant un insert de titane beta metastable, et aube realisee par un tel procede |
DE10326541A1 (de) * | 2003-06-12 | 2005-01-05 | Mtu Aero Engines Gmbh | Verfahren zur Schaufelspitzenpanzerung der Laufschaufeln eines Gasturbinentriebwerkes und Vorrichtung zur Durchführung des Verfahrens |
US7222422B2 (en) * | 2004-02-16 | 2007-05-29 | General Electric Company | Method for refurbishing surfaces subjected to high compression contact |
US7841834B1 (en) * | 2006-01-27 | 2010-11-30 | Florida Turbine Technologies, Inc. | Method and leading edge replacement insert for repairing a turbine engine blade |
US20080181808A1 (en) | 2007-01-31 | 2008-07-31 | Samuel Vinod Thamboo | Methods and articles relating to high strength erosion resistant titanium alloy |
US7780419B1 (en) | 2007-03-06 | 2010-08-24 | Florida Turbine Technologies, Inc. | Replaceable leading edge insert for an IBR |
US20090068446A1 (en) * | 2007-04-30 | 2009-03-12 | United Technologies Corporation | Layered structures with integral brazing materials |
DE102008047043A1 (de) * | 2008-09-13 | 2010-03-18 | Mtu Aero Engines Gmbh | Ersatzteil für eine Gasturbinen-Schaufel einer Gasturbine, Gasturbinen-Schaufel sowie ein Verfahren zur Reparatur einer Gasturbinen-Schaufel |
DE102009047798A1 (de) * | 2009-09-30 | 2011-04-14 | Siemens Aktiengesellschaft | Turbinenschaufel, insbesondere Endstufenlaufschaufel für eine Dampfturbine |
CN102107306B (zh) * | 2009-12-23 | 2013-06-05 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种涡轮导向叶片缺陷的修补方法 |
US8376712B2 (en) * | 2010-01-26 | 2013-02-19 | United Technologies Corporation | Fan airfoil sheath |
US9151173B2 (en) | 2011-12-15 | 2015-10-06 | General Electric Company | Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components |
CN103603695B (zh) * | 2011-12-31 | 2016-06-22 | 无锡透平叶片有限公司 | 一种叶片合金槽及其加工方法 |
US9470097B2 (en) * | 2013-03-14 | 2016-10-18 | Rolls-Royce Corporation | Airfoil with leading edge reinforcement |
US10428657B2 (en) | 2013-06-21 | 2019-10-01 | Pratt & Whitney Canada Corp. | Method for repairing a blade |
US9682449B2 (en) * | 2014-05-09 | 2017-06-20 | United Technologies Corporation | Repair material preform |
EP3020925A1 (en) | 2014-10-29 | 2016-05-18 | Alstom Technology Ltd | Rotor blade with edge protection |
FR3041684B1 (fr) * | 2015-09-28 | 2021-12-10 | Snecma | Aube comprenant un bouclier de bord d'attaque et procede de fabrication de l'aube |
GB2549113A (en) * | 2016-04-05 | 2017-10-11 | Rolls Royce Plc | Composite bodies and their manufacture |
JP7245215B2 (ja) * | 2020-11-25 | 2023-03-23 | 三菱重工業株式会社 | 蒸気タービン動翼 |
FR3123380B1 (fr) * | 2021-05-28 | 2024-10-11 | Safran Aircraft Engines | Bouclier de bord d'attaque amélioré |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2661286A (en) * | 1950-01-13 | 1953-12-01 | Mallory Sharon Titanium Corp | Titanium base alloys containing silicon |
GB692867A (en) * | 1950-03-24 | 1953-06-17 | Hard Metal Tools Ltd | Improvements relating to turbine blades |
US2664355A (en) * | 1950-10-06 | 1953-12-29 | Battelle Development Corp | Ti-mn-fe alloys |
US2714245A (en) * | 1951-12-07 | 1955-08-02 | Sintercast Corp America | Sintered titanium carbide alloy turbine blade |
FR1146511A (fr) * | 1951-12-07 | 1957-11-13 | Sintercast Corp America | Aube de turbine |
BE560921A (zh) * | 1956-09-21 | |||
US2903785A (en) * | 1957-02-11 | 1959-09-15 | Gen Motors Corp | Method of hot working titanium |
GB1096294A (en) * | 1964-06-12 | 1967-12-29 | English Electric Co Ltd | Turbine blades |
US3561886A (en) * | 1969-02-07 | 1971-02-09 | Gen Electric | Turbine bucket erosion shield attachment |
US4010530A (en) * | 1975-07-24 | 1977-03-08 | United Technologies Corporation | Method for making blade protective sheaths |
JPS52103306A (en) * | 1976-02-27 | 1977-08-30 | Mitsubishi Metal Corp | Lightweight hard alloy for parts of hot rolling equipment |
GB1479855A (en) * | 1976-04-23 | 1977-07-13 | Statni Vyzkumny Ustav Material | Protective coating for titanium alloy blades for turbine and turbo-compressor rotors |
JPS5560605A (en) * | 1978-10-27 | 1980-05-07 | Toshiba Corp | Method of manufacturing turbine blade having anti- corrosive plate |
JPS5564104A (en) * | 1978-11-10 | 1980-05-14 | Hitachi Ltd | Rotor blade of turbine |
GB2076019B (en) * | 1980-05-16 | 1984-03-28 | Metallurg Ind Inc | Erosion-resistant alloys |
JPS5798651A (en) * | 1980-12-11 | 1982-06-18 | Seiko Epson Corp | Hard external parts for watch |
JPS59126752A (ja) * | 1983-01-07 | 1984-07-21 | Taiho Kogyo Co Ltd | 鉄系摺動材料およびその製法 |
JPS60228657A (ja) * | 1984-04-26 | 1985-11-13 | Sumitomo Precision Prod Co Ltd | アルミニウム合金構造物の製造方法 |
-
1986
- 1986-05-28 FR FR8607661A patent/FR2599425B1/fr not_active Expired
-
1987
- 1987-05-26 AT AT87107673T patent/ATE50824T1/de not_active IP Right Cessation
- 1987-05-26 EP EP87107673A patent/EP0249092B1/fr not_active Expired - Lifetime
- 1987-05-26 DE DE8787107673T patent/DE3761833D1/de not_active Expired - Fee Related
- 1987-05-26 ES ES87107673T patent/ES2013272B3/es not_active Expired - Lifetime
- 1987-05-26 JP JP62129588A patent/JPS62297442A/ja active Pending
- 1987-05-27 ZA ZA873837A patent/ZA873837B/xx unknown
- 1987-05-28 CN CN87104497A patent/CN1009472B/zh not_active Expired
- 1987-05-28 US US07/054,926 patent/US4795313A/en not_active Expired - Fee Related
- 1987-05-28 CS CS873892A patent/CS276725B6/cs unknown
- 1987-05-28 CS CS903827A patent/CS276857B6/cs unknown
-
1990
- 1990-05-23 GR GR90400323T patent/GR3000501T3/el unknown
- 1990-08-02 CS CS903827A patent/CS382790A3/cs unknown
Also Published As
Publication number | Publication date |
---|---|
CN1009472B (zh) | 1990-09-05 |
JPS62297442A (ja) | 1987-12-24 |
FR2599425A1 (fr) | 1987-12-04 |
CS382790A3 (en) | 1992-01-15 |
CS276857B6 (en) | 1992-08-12 |
ES2013272B3 (es) | 1990-05-01 |
CS389287A3 (en) | 1992-03-18 |
ATE50824T1 (de) | 1990-03-15 |
DE3761833D1 (de) | 1990-04-12 |
FR2599425B1 (fr) | 1988-08-05 |
ZA873837B (en) | 1987-11-24 |
CS276725B6 (en) | 1992-08-12 |
US4795313A (en) | 1989-01-03 |
EP0249092A1 (fr) | 1987-12-16 |
EP0249092B1 (fr) | 1990-03-07 |
GR3000501T3 (en) | 1991-07-31 |
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