ES2099596T3 - Metodo para producir un borde abrasivo en un alabe de turbina. - Google Patents
Metodo para producir un borde abrasivo en un alabe de turbina.Info
- Publication number
- ES2099596T3 ES2099596T3 ES94907629T ES94907629T ES2099596T3 ES 2099596 T3 ES2099596 T3 ES 2099596T3 ES 94907629 T ES94907629 T ES 94907629T ES 94907629 T ES94907629 T ES 94907629T ES 2099596 T3 ES2099596 T3 ES 2099596T3
- Authority
- ES
- Spain
- Prior art keywords
- producing
- deposition
- pallets
- assembly
- turbine wing
- 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
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title abstract 2
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 230000008021 deposition Effects 0.000 abstract 2
- 238000005137 deposition process Methods 0.000 abstract 1
- 230000005611 electricity Effects 0.000 abstract 1
Classifications
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Electroplating Methods And Accessories (AREA)
- Chemically Coating (AREA)
- Grinding And Polishing Of Tertiary Curved Surfaces And Surfaces With Complex Shapes (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
Abstract
UN METODO PARA PRODUCIR PUNTAS ABRASIVAS EN PALETAS DE ROTOR DE COMPRESORES O TURBINAS MEDIANTE DEPOSICION ELECTROLITICA O SIN ELECTRICIDAD EN EL CUAL AL MENOS PARTE DEL PROCESO DE DEPOSICION SE LLEVA A CABO EN LAS PALETAS ENSAMBLADAS EN UN DISCO ROTOR DE COMPRESOR O TURBINA. LAS PUNTAS SE FORMAN POR TANTO EN LAS PALETAS DESPUES DE PONERLAS EN SUS POSICIONES DE FUNCIONAMIENTO FINALES EN EL DISCO PARA QUE EL DESENSAMBLAJE SUBSECUENTE QUE HA SIDO NECESARIO HASTA ESTOS MOMENTOS SE EVITE. EL ENSAMBLAJE ESTA MONTADO PREFERIBLEMENTE CON SU EJE DE ROTACION HORIZONTAL Y LA DEPOSICION PUEDE ESTAR ACOMPAÑADA POR LA VIBRACION DEL ENSAMBLAJE EN DIRECCION VERTICAL.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB939303853A GB9303853D0 (en) | 1993-02-25 | 1993-02-25 | Rotor blades |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2099596T3 true ES2099596T3 (es) | 1997-05-16 |
Family
ID=10731055
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES94907629T Expired - Lifetime ES2099596T3 (es) | 1993-02-25 | 1994-02-25 | Metodo para producir un borde abrasivo en un alabe de turbina. |
Country Status (10)
| Country | Link |
|---|---|
| EP (1) | EP0686229B1 (es) |
| JP (1) | JPH08506872A (es) |
| AU (1) | AU684263B2 (es) |
| CA (1) | CA2153899A1 (es) |
| DE (1) | DE69402305T2 (es) |
| ES (1) | ES2099596T3 (es) |
| GB (1) | GB9303853D0 (es) |
| RU (1) | RU2118717C1 (es) |
| SG (1) | SG47413A1 (es) |
| WO (1) | WO1994019583A1 (es) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB9326082D0 (en) * | 1993-12-21 | 1994-02-23 | Baj Coatings Ltd | Rotor blades |
| US5935407A (en) | 1997-11-06 | 1999-08-10 | Chromalloy Gas Turbine Corporation | Method for producing abrasive tips for gas turbine blades |
| JP3801452B2 (ja) | 2001-02-28 | 2006-07-26 | 三菱重工業株式会社 | 耐摩耗性コーティング及びその施工方法 |
| JP2002256808A (ja) * | 2001-02-28 | 2002-09-11 | Mitsubishi Heavy Ind Ltd | 燃焼エンジン、ガスタービン及び研磨層 |
| EP1391537B1 (en) | 2001-05-31 | 2012-02-22 | Mitsubishi Heavy Industries, Ltd. | Coating forming method and coating forming material, and abrasive coating forming sheet |
| JP2002371803A (ja) * | 2001-06-13 | 2002-12-26 | Mitsubishi Heavy Ind Ltd | 動翼用耐摩耗層の形成方法、耐摩耗層及びその再生方法 |
| JP2003148103A (ja) * | 2001-11-09 | 2003-05-21 | Mitsubishi Heavy Ind Ltd | タービンおよびその製造方法 |
| DE10251902B4 (de) | 2002-11-07 | 2009-05-07 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verfahren zum Beschichten eines Substrats und beschichteter Gegenstand |
| FR2915495B1 (fr) * | 2007-04-30 | 2010-09-03 | Snecma | Procede de reparation d'une aube mobile de turbomachine |
| DE102009007666A1 (de) * | 2009-02-05 | 2010-08-12 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung einer verschleißfesten Beschichtung auf einem Bauteil |
| US9957629B2 (en) | 2014-08-27 | 2018-05-01 | Praxair S.T. Technology, Inc. | Electroplated coatings |
| DE102015213555A1 (de) | 2015-07-20 | 2017-03-09 | MTU Aero Engines AG | Dichtrippenpanzerung und Verfahren zur Herstellung derselben |
| CN116121831A (zh) * | 2022-12-13 | 2023-05-16 | 中国科学院金属研究所 | 一种cBN陶瓷颗粒/铝化物复合涂层及其制备方法 |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4279706A (en) * | 1980-03-27 | 1981-07-21 | Alsthom-Atlantique | Method and assembly for depositing a metal on a cylindrical bore which passes through a central portion of a large part |
| FR2563540B1 (fr) * | 1984-04-26 | 1989-05-05 | Alsthom Atlantique | Dispositif pour effectuer un depot metallique sur les parties frottantes d'un rotor de turbine |
| US4608128A (en) * | 1984-07-23 | 1986-08-26 | General Electric Company | Method for applying abrasive particles to a surface |
| GB2167446B (en) * | 1984-10-05 | 1988-05-05 | Baj Ltd | Electrode deposited composite coating |
| GB2182055B (en) * | 1985-10-28 | 1989-10-18 | Baj Ltd | Improvements relating to electrodeposited coatings |
| GB8818069D0 (en) * | 1988-07-29 | 1988-09-28 | Baj Ltd | Improvements relating to electrodeposited coatings |
| GB8914156D0 (en) * | 1989-06-20 | 1989-08-09 | Refurbished Turbine Components | Apparatus for use in the repair of machines |
| US5074970A (en) * | 1989-07-03 | 1991-12-24 | Kostas Routsis | Method for applying an abrasive layer to titanium alloy compressor airfoils |
| GB2241506A (en) * | 1990-02-23 | 1991-09-04 | Baj Ltd | Method of producing a gas turbine blade having an abrasive tip by electrodepo- sition. |
-
1993
- 1993-02-25 GB GB939303853A patent/GB9303853D0/en active Pending
-
1994
- 1994-02-25 DE DE69402305T patent/DE69402305T2/de not_active Expired - Lifetime
- 1994-02-25 RU RU95119998A patent/RU2118717C1/ru not_active IP Right Cessation
- 1994-02-25 WO PCT/GB1994/000374 patent/WO1994019583A1/en not_active Ceased
- 1994-02-25 ES ES94907629T patent/ES2099596T3/es not_active Expired - Lifetime
- 1994-02-25 SG SG1996000908A patent/SG47413A1/en unknown
- 1994-02-25 AU AU61126/94A patent/AU684263B2/en not_active Ceased
- 1994-02-25 EP EP94907629A patent/EP0686229B1/en not_active Expired - Lifetime
- 1994-02-25 JP JP6518774A patent/JPH08506872A/ja active Pending
- 1994-02-25 CA CA 2153899 patent/CA2153899A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| EP0686229A1 (en) | 1995-12-13 |
| AU6112694A (en) | 1994-09-14 |
| RU2118717C1 (ru) | 1998-09-10 |
| JPH08506872A (ja) | 1996-07-23 |
| AU684263B2 (en) | 1997-12-11 |
| WO1994019583A1 (en) | 1994-09-01 |
| DE69402305T2 (de) | 1997-10-16 |
| DE69402305D1 (de) | 1997-04-30 |
| SG47413A1 (en) | 1998-04-17 |
| GB9303853D0 (en) | 1993-04-21 |
| CA2153899A1 (en) | 1994-09-01 |
| EP0686229B1 (en) | 1997-03-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ES2099596T3 (es) | Metodo para producir un borde abrasivo en un alabe de turbina. | |
| MX171965B (es) | Tecnica de fabricacion o reparacion para un ensamble de rotor con paletas integradas | |
| ES2043488A2 (es) | Perfeccionamientos en la sujecion de alabes de turbomaquinas. | |
| ES2089354T3 (es) | Fabricacion de paletas para compresores de turbinas. | |
| SE8904237D0 (sv) | Boltless balance weight for turbine rotors | |
| ES2051559T3 (es) | Rodete de compresor con alabes partidores desplazados. | |
| BR0211254A (pt) | Processo para a montagem in situ de uma instalação de energia eólica, uso de um peso, peso de compensação, e, instalação de energia eólica | |
| ES2033922T3 (es) | Procedimiento para preparar nuevos derivados de xantina. | |
| AU2048888A (en) | Method of repairing turbine blades | |
| ES2027738T3 (es) | Rotor de ventilador fabricado a partir de un disco metalico delgado y su metodo de fabricacion. | |
| RU2342540C2 (ru) | Направляющее устройство для лопатки с изменяемым углом установки | |
| ES2189304T3 (es) | Instalacion de energia eolica con seguimiento del viento. | |
| GB677142A (en) | Improved mounting for turbine and like blades | |
| GB2224959B (en) | Turbine blade repair | |
| RU2002114001A (ru) | Опора двухроторного газотурбинного двигателя | |
| DE3681545D1 (de) | Rotierender kopf fuer die automatische stuckarbeit der oberflaechen von steinen, marmor oder dergleichen. | |
| KR101566525B1 (ko) | 와류 발생 조립체 | |
| ES2175235T3 (es) | Procedimiento para la fabricacion de una rueda de ferrocarril de aceroendurecida en su superficie de rodadura. | |
| GB778667A (en) | Improvements in or relating to compressor blade root fixings | |
| CN209552189U (zh) | 一种用于金刚线切割机床的多线槽导线轮机构 | |
| CN204346641U (zh) | 一种纯机械式高速主轴在线动平衡头 | |
| CN107984217A (zh) | 一种可供发动机部件旋转装配的装置 | |
| CN210908513U (zh) | 一种振镜高度调整的装置 | |
| IT1245175B (it) | Struttura copripale per un compressore centrifugo | |
| CN112677084A (zh) | 一种可实现航空发动机高压组合转子快速精准装配的夹具 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
Ref document number: 686229 Country of ref document: ES |