WO2014031195A3 - Gas turbine engine fan blade tip treatment - Google Patents
Gas turbine engine fan blade tip treatment Download PDFInfo
- Publication number
- WO2014031195A3 WO2014031195A3 PCT/US2013/042197 US2013042197W WO2014031195A3 WO 2014031195 A3 WO2014031195 A3 WO 2014031195A3 US 2013042197 W US2013042197 W US 2013042197W WO 2014031195 A3 WO2014031195 A3 WO 2014031195A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fan blade
- gas turbine
- turbine engine
- blade tip
- engine fan
- Prior art date
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D11/00—Electrolytic coating by surface reaction, i.e. forming conversion layers
- C25D11/02—Anodisation
- C25D11/022—Anodisation on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D11/00—Electrolytic coating by surface reaction, i.e. forming conversion layers
- C25D11/02—Anodisation
- C25D11/026—Anodisation with spark discharge
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D11/00—Electrolytic coating by surface reaction, i.e. forming conversion layers
- C25D11/02—Anodisation
- C25D11/04—Anodisation of aluminium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D9/00—Electrolytic coating other than with metals
- C25D9/04—Electrolytic coating other than with metals with inorganic materials
-
- 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
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- 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
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/312—Layer deposition by plasma spraying
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/173—Aluminium alloys, e.g. AlCuMgPb
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/174—Titanium alloys, e.g. TiAl
-
- 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
Abstract
A method of manufacturing a fan blade includes providing a metallic fan blade body, and applying at least a 200 volt potential to the fan blade body in a solution to produce a crystalline oxidation layer. A fan blade for a gas turbine engine includes a metallic fan blade body having a tip with a crystalline oxidation layer. A fan blade for a gas turbine engine includes a metallic fan blade body having a tip with a titanium dioxide layer.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13831135.2A EP2867477A4 (en) | 2012-06-28 | 2013-05-22 | Gas turbine engine fan blade tip treatment |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/536,156 US20140010663A1 (en) | 2012-06-28 | 2012-06-28 | Gas turbine engine fan blade tip treatment |
US13/536,156 | 2012-06-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2014031195A2 WO2014031195A2 (en) | 2014-02-27 |
WO2014031195A3 true WO2014031195A3 (en) | 2014-05-30 |
Family
ID=49878668
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2013/042197 WO2014031195A2 (en) | 2012-06-28 | 2013-05-22 | Gas turbine engine fan blade tip treatment |
Country Status (3)
Country | Link |
---|---|
US (1) | US20140010663A1 (en) |
EP (1) | EP2867477A4 (en) |
WO (1) | WO2014031195A2 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
HU230177B1 (en) * | 2012-12-11 | 2015-09-28 | Polinvent Kft. | Heat hardenable resin system for reinforcing of blast |
US10408224B2 (en) | 2014-01-23 | 2019-09-10 | United Technologies Corporation | Fan blades with abrasive tips |
US10221698B2 (en) * | 2014-02-14 | 2019-03-05 | United Technologies Corporation | Polymer-coated blade with abrasive tip |
FR3017884B1 (en) * | 2014-02-25 | 2017-09-22 | Snecma | DUST PROTECTION EDGE AND METHOD OF MANUFACTURE |
US9982358B2 (en) | 2014-06-04 | 2018-05-29 | United Technologies Corporation | Abrasive tip blade manufacture methods |
US20160177732A1 (en) * | 2014-07-22 | 2016-06-23 | United Technologies Corporation | Hollow fan blade for a gas turbine engine |
US10094227B2 (en) * | 2014-08-04 | 2018-10-09 | United Technologies Corporation | Gas turbine engine blade tip treatment |
US9850767B2 (en) * | 2014-08-08 | 2017-12-26 | United Technologies Corporation | Aluminum fan blade tip with thermal barrier |
US20160090849A1 (en) * | 2014-09-30 | 2016-03-31 | United Technologies Corporation | Fan blade with static dissipative coating |
US10815797B2 (en) | 2016-08-12 | 2020-10-27 | Hamilton Sundstrand Corporation | Airfoil systems and methods of assembly |
US10458035B2 (en) * | 2017-07-21 | 2019-10-29 | United Technologies Corporation | Anodization of bonded assembly |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5264011A (en) * | 1992-09-08 | 1993-11-23 | General Motors Corporation | Abrasive blade tips for cast single crystal gas turbine blades |
US5573862A (en) * | 1992-04-13 | 1996-11-12 | Alliedsignal Inc. | Single crystal oxide turbine blades |
US20110103968A1 (en) * | 2009-11-02 | 2011-05-05 | Alstom Technology Ltd | Wear-resistant and oxidation-resistant turbine blade |
US20110211967A1 (en) * | 2010-02-26 | 2011-09-01 | United Technologies Corporation | Hybrid metal fan blade |
US20110297319A1 (en) * | 2010-06-04 | 2011-12-08 | Mks Instruments, Inc. | Reduction of Copper or Trace Metal Contaminants in Plasma Electrolytic Oxidation Coatings |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3758233A (en) * | 1972-01-17 | 1973-09-11 | Gen Motors Corp | Vibration damping coatings |
JPS6355305A (en) * | 1986-08-22 | 1988-03-09 | Ebara Corp | Gas turbine |
US4884820A (en) * | 1987-05-19 | 1989-12-05 | Union Carbide Corporation | Wear resistant, abrasive laser-engraved ceramic or metallic carbide surfaces for rotary labyrinth seal members |
US6341747B1 (en) * | 1999-10-28 | 2002-01-29 | United Technologies Corporation | Nanocomposite layered airfoil |
DE10126896A1 (en) * | 2000-12-23 | 2002-07-11 | Alstom Switzerland Ltd | Protective coating used for turbines comprises a mono- or multi-layer sealing layer made from an amorphous material |
FR2884550B1 (en) * | 2005-04-15 | 2010-09-17 | Snecma Moteurs | PIECE FOR PROTECTING THE EDGE OF A BLADE |
WO2006136334A2 (en) * | 2005-06-22 | 2006-12-28 | Henkel Kommanditgesellschaft Auf Aktien | Electrodeposition material, process for providing a corrosion-protective layer of tio2 on an electrically conductive substrate and metal substrate coated with a layer of tio2 |
US7334997B2 (en) * | 2005-09-16 | 2008-02-26 | General Electric Company | Hybrid blisk |
JP4886271B2 (en) * | 2005-10-31 | 2012-02-29 | 株式会社東芝 | Steam turbine and hydrophilic coating material thereof |
US20090120101A1 (en) * | 2007-10-31 | 2009-05-14 | United Technologies Corp. | Organic Matrix Composite Components, Systems Using Such Components, and Methods for Manufacturing Such Components |
EP2390467A1 (en) * | 2010-05-31 | 2011-11-30 | Siemens Aktiengesellschaft | Protective coating for reducing drop impact erosion |
-
2012
- 2012-06-28 US US13/536,156 patent/US20140010663A1/en not_active Abandoned
-
2013
- 2013-05-22 WO PCT/US2013/042197 patent/WO2014031195A2/en active Application Filing
- 2013-05-22 EP EP13831135.2A patent/EP2867477A4/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5573862A (en) * | 1992-04-13 | 1996-11-12 | Alliedsignal Inc. | Single crystal oxide turbine blades |
US5264011A (en) * | 1992-09-08 | 1993-11-23 | General Motors Corporation | Abrasive blade tips for cast single crystal gas turbine blades |
US20110103968A1 (en) * | 2009-11-02 | 2011-05-05 | Alstom Technology Ltd | Wear-resistant and oxidation-resistant turbine blade |
US20110211967A1 (en) * | 2010-02-26 | 2011-09-01 | United Technologies Corporation | Hybrid metal fan blade |
US20110297319A1 (en) * | 2010-06-04 | 2011-12-08 | Mks Instruments, Inc. | Reduction of Copper or Trace Metal Contaminants in Plasma Electrolytic Oxidation Coatings |
Also Published As
Publication number | Publication date |
---|---|
EP2867477A2 (en) | 2015-05-06 |
WO2014031195A2 (en) | 2014-02-27 |
EP2867477A4 (en) | 2016-06-15 |
US20140010663A1 (en) | 2014-01-09 |
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