GB2108534B - Forming braze-bonded abrasive turbine blade tip - Google Patents
Forming braze-bonded abrasive turbine blade tipInfo
- Publication number
- GB2108534B GB2108534B GB08230705A GB8230705A GB2108534B GB 2108534 B GB2108534 B GB 2108534B GB 08230705 A GB08230705 A GB 08230705A GB 8230705 A GB8230705 A GB 8230705A GB 2108534 B GB2108534 B GB 2108534B
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine blade
- blade tip
- bonded abrasive
- braze
- forming braze
- 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
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
- B23K35/0244—Powders, particles or spheres; Preforms made therefrom
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/32—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
- B23K35/327—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C comprising refractory compounds, e.g. carbides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
- C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
- C23C24/103—Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US31848981A | 1981-11-05 | 1981-11-05 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2108534A GB2108534A (en) | 1983-05-18 |
| GB2108534B true GB2108534B (en) | 1985-07-24 |
Family
ID=23238391
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08230705A Expired GB2108534B (en) | 1981-11-05 | 1982-10-27 | Forming braze-bonded abrasive turbine blade tip |
Country Status (2)
| Country | Link |
|---|---|
| CA (1) | CA1202768A (en) |
| GB (1) | GB2108534B (en) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4726101A (en) * | 1986-09-25 | 1988-02-23 | United Technologies Corporation | Turbine vane nozzle reclassification |
| US4854196A (en) * | 1988-05-25 | 1989-08-08 | General Electric Company | Method of forming turbine blades with abradable tips |
| US5359770A (en) * | 1992-09-08 | 1994-11-01 | General Motors Corporation | Method for bonding abrasive blade tips to the tip of a gas turbine blade |
| US5264011A (en) * | 1992-09-08 | 1993-11-23 | General Motors Corporation | Abrasive blade tips for cast single crystal gas turbine blades |
| JP3315919B2 (en) | 1998-02-18 | 2002-08-19 | 日本碍子株式会社 | Method for manufacturing a composite member composed of two or more different types of members |
| EP1082180A4 (en) * | 1998-04-25 | 2002-10-29 | Penn State Res Found | Method of applying hard-facing material to a substrate |
| DE10000988A1 (en) * | 1999-02-17 | 2001-07-19 | Euromat Gmbh | Method for producing a protective layer on the surface of a component or the like workpiece, solder material for this and their use |
| US20040124231A1 (en) * | 1999-06-29 | 2004-07-01 | Hasz Wayne Charles | Method for coating a substrate |
| JP4367675B2 (en) | 1999-10-21 | 2009-11-18 | 日本碍子株式会社 | Adhesive composition for joining ceramic member and metal member, manufacturing method of composite member using the same composition, and composite member obtained by the manufacturing method |
| DE10000989A1 (en) * | 2000-01-13 | 2001-07-19 | Euromat Gmbh | A method for producing a protective layer on the surface of a component o. The like. Workpiece, solder material therefor and their use |
| US7331755B2 (en) * | 2004-05-25 | 2008-02-19 | General Electric Company | Method for coating gas turbine engine components |
| DE102005030848A1 (en) * | 2005-07-01 | 2007-01-11 | Mtu Aero Engines Gmbh | Method for producing a blade tip armor |
| US7653994B2 (en) * | 2006-03-22 | 2010-02-02 | General Electric Company | Repair of HPT shrouds with sintered preforms |
| US20070295785A1 (en) * | 2006-05-31 | 2007-12-27 | General Electric Company | Microwave brazing using mim preforms |
| CA2679517C (en) | 2007-05-04 | 2014-02-11 | Mtu Aero Engines Gmbh | Method for manufacturing an abrasive coating on a gas turbine component |
| US20100288977A1 (en) * | 2009-05-15 | 2010-11-18 | Metso Minerals, Inc. | Corrosion protection under influence of corrosive species |
| US20150118060A1 (en) * | 2013-10-25 | 2015-04-30 | General Electric Company | Turbine engine blades, related articles, and methods |
| DE102013223585A1 (en) * | 2013-11-19 | 2015-06-03 | MTU Aero Engines AG | Inlet lining based on metal fibers |
| US10786875B2 (en) | 2014-07-02 | 2020-09-29 | Raytheon Technologies Corporation | Abrasive preforms and manufacture and use methods |
| US10018056B2 (en) * | 2014-07-02 | 2018-07-10 | United Technologies Corporation | Abrasive coating and manufacture and use methods |
| US10030527B2 (en) | 2014-07-02 | 2018-07-24 | United Technologies Corporation | Abrasive preforms and manufacture and use methods |
| US10012095B2 (en) * | 2014-07-02 | 2018-07-03 | United Technologies Corporation | Abrasive coating and manufacture and use methods |
| IT202100000626A1 (en) * | 2021-01-14 | 2022-07-14 | Nuovo Pignone Tecnologie Srl | PRE-SINTERED PREFORMS WITH ABILITY TO RESIST TO HIGH TEMPERATURES, PARTICULARLY AS ABRASIVE COATING FOR GAS TURBINE BLADES. |
-
1982
- 1982-10-07 CA CA000413020A patent/CA1202768A/en not_active Expired
- 1982-10-27 GB GB08230705A patent/GB2108534B/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| CA1202768A (en) | 1986-04-08 |
| GB2108534A (en) | 1983-05-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19991027 |