RU2006130731A - MOUNTING ASSEMBLY AND METHOD OF MOUNTING TURBO MACHINE SHOULDER FEET, TURBO MACHINE BLOWER, TURBO COMPRESSOR AND TURBO MACHINE CONTAINING THE INSTALLATION INSTALLATION - Google Patents
MOUNTING ASSEMBLY AND METHOD OF MOUNTING TURBO MACHINE SHOULDER FEET, TURBO MACHINE BLOWER, TURBO COMPRESSOR AND TURBO MACHINE CONTAINING THE INSTALLATION INSTALLATION Download PDFInfo
- Publication number
- RU2006130731A RU2006130731A RU2006130731/06A RU2006130731A RU2006130731A RU 2006130731 A RU2006130731 A RU 2006130731A RU 2006130731/06 A RU2006130731/06 A RU 2006130731/06A RU 2006130731 A RU2006130731 A RU 2006130731A RU 2006130731 A RU2006130731 A RU 2006130731A
- Authority
- RU
- Russia
- Prior art keywords
- blade
- film
- mounting
- leg
- socket
- Prior art date
Links
Classifications
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- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
-
- 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
- F01D5/288—Protective coatings for blades
-
- 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
- F05D2230/90—Coating; Surface treatment
-
- 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
- F05D2300/40—Organic materials
- F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
- F05D2300/432—PTFE [PolyTetraFluorEthylene]
-
- 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
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/611—Coating
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Claims (17)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0508768A FR2890126B1 (en) | 2005-08-26 | 2005-08-26 | ASSEMBLY AND METHOD FOR THE FOOT ASSEMBLY OF A TURBOMACHINE, BLOWER, COMPRESSOR AND TURBOMACHINE BLADE COMPRISING SUCH AN ASSEMBLY |
FR0508768 | 2005-08-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2006130731A true RU2006130731A (en) | 2008-02-27 |
Family
ID=36698666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2006130731/06A RU2006130731A (en) | 2005-08-26 | 2006-08-25 | MOUNTING ASSEMBLY AND METHOD OF MOUNTING TURBO MACHINE SHOULDER FEET, TURBO MACHINE BLOWER, TURBO COMPRESSOR AND TURBO MACHINE CONTAINING THE INSTALLATION INSTALLATION |
Country Status (7)
Country | Link |
---|---|
US (1) | US20070048142A1 (en) |
EP (1) | EP1777371A1 (en) |
JP (1) | JP2007064220A (en) |
CN (1) | CN1920259A (en) |
CA (1) | CA2557109A1 (en) |
FR (1) | FR2890126B1 (en) |
RU (1) | RU2006130731A (en) |
Families Citing this family (44)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102007011729B4 (en) * | 2007-03-10 | 2018-08-16 | MTU Aero Engines AG | Method and device for processing components of a gas turbine |
US20080318467A1 (en) * | 2007-06-19 | 2008-12-25 | Denomme Gary M | Relay receptacle shorting plug |
FR2918703B1 (en) * | 2007-07-13 | 2009-10-16 | Snecma Sa | ROTOR ASSEMBLY OF TURBOMACHINE |
FR2918702B1 (en) * | 2007-07-13 | 2009-10-16 | Snecma Sa | CLINKING FOR TURBOMACHINE BLADE |
US20090038739A1 (en) | 2007-08-09 | 2009-02-12 | United Technologies Corporation | Replacement of a lubricant layer bonded to a part of a gas turbine engine |
GB2452515B (en) * | 2007-09-06 | 2009-08-05 | Siemens Ag | Seal coating between rotor blade and rotor disk slot in gas turbine engine |
US9488059B2 (en) * | 2009-08-05 | 2016-11-08 | Hamilton Sundstrand Corporation | Fan blade dovetail with compliant layer |
EP2371521B1 (en) * | 2010-04-02 | 2014-07-02 | Techspace Aero S.A. | Method of manufacturing a rectifier |
US8721294B2 (en) * | 2010-05-20 | 2014-05-13 | United Technologies Corporation | Airfoil with galvanically isolated metal coating |
US8672634B2 (en) * | 2010-08-30 | 2014-03-18 | United Technologies Corporation | Electroformed conforming rubstrip |
JP5725849B2 (en) * | 2010-12-27 | 2015-05-27 | 三菱日立パワーシステムズ株式会社 | fixing jig |
GB201101909D0 (en) * | 2011-02-04 | 2011-03-23 | Rolls Royce Plc | A method of tip grinding the blades of a gas turbine rotor |
GB201106276D0 (en) * | 2011-04-14 | 2011-05-25 | Rolls Royce Plc | Annulus filler system |
FR2975428B1 (en) * | 2011-05-17 | 2015-11-20 | Snecma | TURBOMACHINE AUBES WHEEL |
CH705377A1 (en) | 2011-08-09 | 2013-02-15 | Alstom Technology Ltd | A process for reconditioning a rotor of a turbomachine. |
US8763504B2 (en) * | 2012-02-13 | 2014-07-01 | Thomas A. Tardif | Bi-directional fence attachment for a power tool table |
JP6085096B2 (en) * | 2012-04-05 | 2017-02-22 | 三菱日立パワーシステムズ株式会社 | Removal method of moving blade of fuel gas compressor |
US20130302173A1 (en) * | 2012-05-11 | 2013-11-14 | E. I. Du Pont De Nemours And Company | Wear resistant turbine fan blade |
WO2013169272A1 (en) * | 2012-05-11 | 2013-11-14 | E. I. Du Pont De Nemours And Company | Wear resistant article |
US20130302170A1 (en) * | 2012-05-11 | 2013-11-14 | E. I. Du Pont De Nemours And Company | Rotor disk and rotor assembly |
EP2719865A1 (en) * | 2012-10-12 | 2014-04-16 | MTU Aero Engines GmbH | Insert for disc-blade connections of fluid flow engines |
US10273816B2 (en) * | 2013-02-12 | 2019-04-30 | United Technologies Corporation | Wear pad to prevent cracking of fan blade |
US9970311B2 (en) * | 2013-03-05 | 2018-05-15 | United Technologies Corporation | Consumable assembly tool for a gas turbine engine |
EP2964521A4 (en) * | 2013-03-07 | 2016-10-19 | United Technologies Corp | Aluminum fan blades with root wear mitigation |
US10415402B2 (en) | 2013-03-13 | 2019-09-17 | United Technologies Corporation | Blade wear pads and manufacture methods |
US9745856B2 (en) | 2013-03-13 | 2017-08-29 | Rolls-Royce Corporation | Platform for ceramic matrix composite turbine blades |
US9506356B2 (en) | 2013-03-15 | 2016-11-29 | Rolls-Royce North American Technologies, Inc. | Composite retention feature |
JP2016527426A (en) * | 2013-05-29 | 2016-09-08 | ゼネラル・エレクトリック・カンパニイ | Composite airfoil metal patch |
CN105899762B (en) * | 2014-01-16 | 2017-11-07 | 通用电气公司 | Compound blade root stress elimination pad |
EP2902588B1 (en) * | 2014-01-31 | 2020-06-24 | Ansaldo Energia IP UK Limited | Composite turbine blade for high-temperature applications |
GB201411182D0 (en) * | 2014-06-24 | 2014-08-06 | Rolls Royce Plc | Rotor blade manufacture |
US9963979B2 (en) | 2014-11-17 | 2018-05-08 | Rolls-Royce North American Technologies Inc. | Composite components for gas turbine engines |
DE102016201523A1 (en) | 2016-02-02 | 2017-08-03 | MTU Aero Engines AG | Blade of a turbomachine with blade root insulation |
JP6778147B2 (en) * | 2017-05-31 | 2020-10-28 | 三菱重工業株式会社 | Method for manufacturing composite blades and composite blades |
US10767498B2 (en) | 2018-04-03 | 2020-09-08 | Rolls-Royce High Temperature Composites Inc. | Turbine disk with pinned platforms |
US10577961B2 (en) | 2018-04-23 | 2020-03-03 | Rolls-Royce High Temperature Composites Inc. | Turbine disk with blade supported platforms |
US10890081B2 (en) | 2018-04-23 | 2021-01-12 | Rolls-Royce Corporation | Turbine disk with platforms coupled to disk |
US11346363B2 (en) | 2018-04-30 | 2022-05-31 | Raytheon Technologies Corporation | Composite airfoil for gas turbine |
GB201818203D0 (en) * | 2018-11-08 | 2018-12-26 | Rolls Royce Plc | Blade mounting |
CN109333351B (en) * | 2018-11-15 | 2020-06-05 | 中国航空制造技术研究院 | Blade position fixing method in blisk repairing process |
JP7236316B2 (en) * | 2019-04-17 | 2023-03-09 | 三菱重工業株式会社 | Composite material wing and molding method for composite material wing |
CN113833691A (en) * | 2020-06-08 | 2021-12-24 | 中国航发商用航空发动机有限责任公司 | Fan assembly and turbofan engine |
CN113356930B (en) * | 2021-05-31 | 2022-05-20 | 北京南方斯奈克玛涡轮技术有限公司 | Turbine rotor device with reinforced cooling structure |
FR3127522A1 (en) | 2021-09-24 | 2023-03-31 | Safran Aircraft Engines | METHOD FOR PREPARING A FOOT OF A TURBOMACHINE BLADE |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB709636A (en) * | 1951-05-09 | 1954-06-02 | Rolls Royce | Improvements in or relating to compressor and turbine bladed rotors |
US5356545A (en) * | 1991-01-15 | 1994-10-18 | General Electric Company | Curable dry film lubricant for titanium alloys |
US5160243A (en) | 1991-01-15 | 1992-11-03 | General Electric Company | Turbine blade wear protection system with multilayer shim |
US5312696A (en) * | 1991-09-16 | 1994-05-17 | United Technologies Corporation | Method for reducing fretting wear between contacting surfaces |
WO1996041068A1 (en) * | 1995-06-07 | 1996-12-19 | National Research Council Of Canada | Anti-fretting barrier |
US6102664A (en) * | 1995-12-14 | 2000-08-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Blading system and method for controlling structural vibrations |
US5935360A (en) * | 1997-09-24 | 1999-08-10 | General Electric Company | Method for repairing a strip bonded to an article surface |
US6290466B1 (en) * | 1999-09-17 | 2001-09-18 | General Electric Company | Composite blade root attachment |
-
2005
- 2005-08-26 FR FR0508768A patent/FR2890126B1/en active Active
-
2006
- 2006-08-23 CA CA002557109A patent/CA2557109A1/en not_active Abandoned
- 2006-08-23 EP EP06119409A patent/EP1777371A1/en not_active Withdrawn
- 2006-08-25 JP JP2006229024A patent/JP2007064220A/en not_active Withdrawn
- 2006-08-25 RU RU2006130731/06A patent/RU2006130731A/en not_active Application Discontinuation
- 2006-08-25 US US11/509,582 patent/US20070048142A1/en not_active Abandoned
- 2006-08-28 CN CNA2006101119422A patent/CN1920259A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
CA2557109A1 (en) | 2007-02-26 |
US20070048142A1 (en) | 2007-03-01 |
EP1777371A1 (en) | 2007-04-25 |
JP2007064220A (en) | 2007-03-15 |
FR2890126B1 (en) | 2010-10-29 |
CN1920259A (en) | 2007-02-28 |
FR2890126A1 (en) | 2007-03-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FA93 | Acknowledgement of application withdrawn (no request for examination) |
Effective date: 20090826 |