CN1009472B - 一种钛合金透平叶片的保护端梢 - Google Patents
一种钛合金透平叶片的保护端梢Info
- Publication number
- CN1009472B CN1009472B CN87104497A CN87104497A CN1009472B CN 1009472 B CN1009472 B CN 1009472B CN 87104497 A CN87104497 A CN 87104497A CN 87104497 A CN87104497 A CN 87104497A CN 1009472 B CN1009472 B CN 1009472B
- Authority
- CN
- China
- Prior art keywords
- blade
- tip
- turbine blade
- temperature
- titanium alloy
- 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
Links
- 229910001069 Ti alloy Inorganic materials 0.000 title claims description 7
- 230000001681 protective effect Effects 0.000 title abstract description 3
- 239000000203 mixture Substances 0.000 claims description 6
- 239000010949 copper Substances 0.000 abstract description 9
- 229910052802 copper Inorganic materials 0.000 abstract description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 5
- 239000010936 titanium Substances 0.000 abstract description 5
- 229910052719 titanium Inorganic materials 0.000 abstract description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 abstract description 3
- 229910052759 nickel Inorganic materials 0.000 abstract description 3
- 229910052750 molybdenum Inorganic materials 0.000 abstract description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 2
- 238000005299 abrasion Methods 0.000 abstract 1
- 238000005219 brazing Methods 0.000 abstract 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- 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
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 3
- 229910017052 cobalt Inorganic materials 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 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
- 238000000034 method Methods 0.000 description 2
- -1 titanium carbides Chemical class 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal 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
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)
- General Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Metallurgy (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)，它的成份为：Tie20%～40%，Cr+Co12%～26%，Mo1%～6%，Ni3%～8%，CH0.3%～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)的温度在真空或情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。
日本专利JP59-60003公开了一种保护透平叶片前缘的方法，在叶片前缘先沉积上一种由50-90%（重量）Cu和10-50%（重量）Ni组成的金属，然后加上一抗腐蚀的保护端梢。这种保护端梢由钴基合金制成。但是钴的价格较贵，且资源较缺乏。
本发明的目的是使用一种含钴量更低的合金来制造透平叶片的保护端梢，但仍然具有好的抗腐蚀性及其它机械性能，能很好地保护透平叶片。
为了实现本发明的上述目的，本发明提供了一种钛合金透平叶片的保护端梢，该端梢的成分为：
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。
本发明的保护端梢可用下面方法焊到叶片上：
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;
在真空或惰性气体的烘箱中，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变成熔融状态，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变成熔融状态，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，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变成熔融状态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融状态，同时完成减小应力的处理。
Claims (1)
1、一种钛合金透平叶片(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。
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 CN87104497A (zh) | 1987-12-16 |
| CN1009472B true 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 |
|---|---|---|---|---|
| EP0491075B1 (de) * | 1990-12-19 | 1995-07-05 | Asea Brown Boveri Ag | Verfahren zur Herstellung einer Turbinenschaufel aus einer Titan-Basislegierung |
| 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 |
| FR1146511A (fr) * | 1951-12-07 | 1957-11-13 | Sintercast Corp America | Aube de turbine |
| US2714245A (en) * | 1951-12-07 | 1955-08-02 | Sintercast Corp America | Sintered titanium carbide alloy turbine blade |
| 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 DE DE8787107673T patent/DE3761833D1/de not_active Expired - Fee Related
- 1987-05-26 JP JP62129588A patent/JPS62297442A/ja active Pending
- 1987-05-26 EP EP87107673A patent/EP0249092B1/fr not_active Expired - Lifetime
- 1987-05-26 AT AT87107673T patent/ATE50824T1/de not_active IP Right Cessation
- 1987-05-26 ES ES87107673T patent/ES2013272B3/es not_active Expired - Lifetime
- 1987-05-27 ZA ZA873837A patent/ZA873837B/xx unknown
- 1987-05-28 CS CS873892A patent/CS276725B6/cs 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 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 |
|---|---|
| FR2599425A1 (fr) | 1987-12-04 |
| CS276725B6 (en) | 1992-08-12 |
| EP0249092B1 (fr) | 1990-03-07 |
| ATE50824T1 (de) | 1990-03-15 |
| CS382790A3 (en) | 1992-01-15 |
| CN87104497A (zh) | 1987-12-16 |
| EP0249092A1 (fr) | 1987-12-16 |
| JPS62297442A (ja) | 1987-12-24 |
| CS389287A3 (en) | 1992-03-18 |
| FR2599425B1 (fr) | 1988-08-05 |
| DE3761833D1 (de) | 1990-04-12 |
| GR3000501T3 (en) | 1991-07-31 |
| ZA873837B (en) | 1987-11-24 |
| US4795313A (en) | 1989-01-03 |
| ES2013272B3 (es) | 1990-05-01 |
| CS276857B6 (en) | 1992-08-12 |
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