SE463855B - Saett foer rekonstruktion av skovlar och ledskenor i aangturbiner vid erosionsskador - Google Patents
Saett foer rekonstruktion av skovlar och ledskenor i aangturbiner vid erosionsskadorInfo
- Publication number
- SE463855B SE463855B SE8901986A SE8901986A SE463855B SE 463855 B SE463855 B SE 463855B SE 8901986 A SE8901986 A SE 8901986A SE 8901986 A SE8901986 A SE 8901986A SE 463855 B SE463855 B SE 463855B
- Authority
- SE
- Sweden
- Prior art keywords
- vane
- erosion damage
- guide rail
- paddle
- reconstruction
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
- B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/1208—Containers or coating used therefor
- B22F3/1258—Container manufacturing
- B22F3/1275—Container manufacturing by coating a model and eliminating the model before consolidation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
-
- 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
- F01D5/005—Repairing methods or devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
- B22F2007/068—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts repairing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
10
15
20
25
30
35
Jäs,
C?
04
CO
LH
gm
der inte behöver tagas med pä köpet, och i detta syf-
te föresläs ett sätt av det inledningsvis angivna
slaget, vilket enligt uppfinningen erhàllit de känne-
tecken som framgàr av patentkravet 1.
För närmare förklaring av uppfinningen hänvisas
_till bifogade ritning, som i FIG l-7 i tvärsektionsvy
visar en ängturbinskovel i olika faser av sättet en-
ligt uppfinningen.
Angturbinskoveln 10, FIG l, antages vara utförd
av sàdan metall eller metallegering, som brukar an-
vändas till sädana skovlar. Det antages vidare att
vid en kant 11 pä skoveln uppkommit erosionsskador,
som kräver reparation.
Vid tillämpning av förfarandet enligt uppfin-
ningen fräser man bort det skadade partiet, exempel-
vis längs den prickstreckade linjen 12, FIG l, sä att
skoveln blir som i FIG 2, varefter man äter bygger
upp skoveln med ett parti 13 till dess ursprungliga
profil med användning av vax, plast eller legering
med làg smältpunkt, FIG 3.
Omkring den sálunda "rekonstruerade" skoveln an-
ordnas nu en form 14 av grafitpulver och cement med
ett ingöt 15 i omrädet av den päbyggda delen av vax,
plast eller legering, FIG 4, varefter denna del äter
avlägsnas frän skoveln genom att vaxet eller lege-
ringen smältes eller genom att plasten löses upp i
nàgot lösningsmedel, varvid en hálighet 16 kvarstär i
formen med samma dimensioner och profil som den av-
lägsnade päbyggnadsdelen, FIG 5. I formhàligheten
packas ett pulver 17 av metall eller metallegering,
som kan vara densamma som den skoveln är gjord av el-
ler kan vara härdare än metallen eller metallege-
ringen i skoveln, FIG 6, varefter formen med däri in-
nesluten skovel och metallpulver placeras i en kapsel
för hetisostatpressning, i vilken formen lämpligen
10
15
20
25
30
35
465 855
packas in i pulver av aluminiumoxid eller zirkonium-
silikat. Efter förslutning och evakuering av kapseln
pà konventionellt sätt företages hetisostatpressning.
Den därigenom erhàllna formkroppen, som utgöres av en
rekonstruerad skovel med den ursprungliga skovelns
profil, frilägges frán grafitformen genom att denna
blästras bort fràn formkroppen, FIG 7.
Den pà sä sätt framställda rekonstruerade sko-
veln är en monolitisk kropp, vid vilken man inte be-
höver räkna med uppkomsten av sprickor eller losslit-
ning av den genom hetisostatpressningen pàlagda delen
vid drift av det turbinhjul, i vilket skoveln använ-
des.
Claims (2)
1. Sätt för rekonstruktion av skovlar och led- skenor i àngturbiner vid förekommande erosionsskador, k ä n n e t e c k n a t av att efter borttagning av det erosionsskador uppvisande partiet av skoveln el- ler ledskenan uppbygges pä denna av ett lättsmält el- ler upplösbart material ett ersättningsparti, som äterställer skovelns eller ledskenans ursprungliga profil, att omkring den sàlunda rekonstruerade sko- veln eller ledskenan anordnas en grafitform med in- göt, varefter det pàbyggda partiet avlägsnas genom att materialet däri smältes eller upplöses, och att i den kvarstående hàligheten i grafitformen hetisostat- pressas ett metallpulver, varefter grafitformen av- lägsnas fràn den till en monolitisk kropp rekonstrue- rade skoveln eller ledskenan.
2. Sätt enligt krav 1, k ä n n e t e c k n a t av att genom hetisostatpressningen ästadkommes ett parti av skoveln, vilket är hàrdare än materialet i skoveln i övrigt.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8901986A SE463855B (sv) | 1989-06-01 | 1989-06-01 | Saett foer rekonstruktion av skovlar och ledskenor i aangturbiner vid erosionsskador |
EP19900850214 EP0401187A3 (en) | 1989-06-01 | 1990-05-25 | Method for reconstruction of blades and vanes in steam turbines at existing erosion damages |
JP2141763A JPH03115701A (ja) | 1989-06-01 | 1990-06-01 | 蒸気タービンの侵食損傷を受けたブレード及びベーンの復元方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8901986A SE463855B (sv) | 1989-06-01 | 1989-06-01 | Saett foer rekonstruktion av skovlar och ledskenor i aangturbiner vid erosionsskador |
Publications (3)
Publication Number | Publication Date |
---|---|
SE8901986D0 SE8901986D0 (sv) | 1989-06-01 |
SE8901986L SE8901986L (sv) | 1990-12-02 |
SE463855B true SE463855B (sv) | 1991-02-04 |
Family
ID=20376148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8901986A SE463855B (sv) | 1989-06-01 | 1989-06-01 | Saett foer rekonstruktion av skovlar och ledskenor i aangturbiner vid erosionsskador |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0401187A3 (sv) |
JP (1) | JPH03115701A (sv) |
SE (1) | SE463855B (sv) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4039807C1 (sv) * | 1990-12-13 | 1991-10-02 | Mtu Muenchen Gmbh | |
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 |
US5291937A (en) * | 1992-07-30 | 1994-03-08 | General Electric Company | Method for providing an extension on an end of an article having internal passageways |
US5304039A (en) * | 1992-07-30 | 1994-04-19 | General Electric Company | Method for providing an extension on an end of an article and extended article |
DE4225443C2 (de) * | 1992-07-31 | 1995-11-16 | Mtu Muenchen Gmbh | Verfahren zur Herstellung einer Schweißverbindung von Bauteilen für Turbomaschinen, insbesondere zur Bauteilreperatur und Verwendung des Verfahrens |
DE19803589A1 (de) * | 1998-01-30 | 1999-08-12 | Voith Hydro Gmbh & Co Kg | Verfahren zum Herstellen eines Bauteiles einer Strömungsmaschine |
US6274215B1 (en) * | 1998-12-21 | 2001-08-14 | General Electric Company | Aerodynamic article with partial outer portion and method for making |
US6568077B1 (en) * | 2000-05-11 | 2003-05-27 | General Electric Company | Blisk weld repair |
DE102005002609A1 (de) * | 2005-01-20 | 2006-08-03 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur von Turbinenlaufschaufeln |
US7282681B2 (en) * | 2005-05-05 | 2007-10-16 | General Electric Company | Microwave fabrication of airfoil tips |
US8127442B2 (en) * | 2005-12-15 | 2012-03-06 | United Technologies Corporation | Compressor blade flow form technique for repair |
FR2953747B1 (fr) * | 2009-12-14 | 2012-03-23 | Snecma | Procede de reparation d'une aube en titane par rechargement laser et compression hip moderee |
GB2477154B (en) | 2010-01-26 | 2012-03-21 | Rolls Royce Plc | A method of restoring a metallic component |
FR2972379B1 (fr) * | 2011-03-07 | 2014-01-17 | Snecma | Procede de rechargement local de piece thermomecanique endommagee et piece ainsi realisee, en particulier piece de turbine |
US20160175996A1 (en) * | 2014-04-04 | 2016-06-23 | United Technologies Corporation | Repair material preform |
CN108213832B (zh) * | 2017-12-29 | 2020-08-18 | 西安交通大学 | 一种实现单晶或定向晶合金叶片内流道复形的修复方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1088560A (en) * | 1964-10-16 | 1967-10-25 | Howe Sound Co | A method of producing shaped products of sintered powders |
US3574924A (en) * | 1968-10-28 | 1971-04-13 | North American Rockwell | Solid state repair method and means |
US4851188A (en) * | 1987-12-21 | 1989-07-25 | United Technologies Corporation | Method for making a turbine blade having a wear resistant layer sintered to the blade tip surface |
-
1989
- 1989-06-01 SE SE8901986A patent/SE463855B/sv not_active IP Right Cessation
-
1990
- 1990-05-25 EP EP19900850214 patent/EP0401187A3/en not_active Withdrawn
- 1990-06-01 JP JP2141763A patent/JPH03115701A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
SE8901986D0 (sv) | 1989-06-01 |
EP0401187A2 (en) | 1990-12-05 |
EP0401187A3 (en) | 1992-10-07 |
JPH03115701A (ja) | 1991-05-16 |
SE8901986L (sv) | 1990-12-02 |
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Legal Events
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