DE602007005567D1 - Keilförmige Befestigung von Leitschaufeln im äusseren Schaufelkranz mit variabler Teilung - Google Patents
Keilförmige Befestigung von Leitschaufeln im äusseren Schaufelkranz mit variabler TeilungInfo
- Publication number
- DE602007005567D1 DE602007005567D1 DE602007005567T DE602007005567T DE602007005567D1 DE 602007005567 D1 DE602007005567 D1 DE 602007005567D1 DE 602007005567 T DE602007005567 T DE 602007005567T DE 602007005567 T DE602007005567 T DE 602007005567T DE 602007005567 D1 DE602007005567 D1 DE 602007005567D1
- Authority
- DE
- Germany
- Prior art keywords
- vanes
- wedge
- shaped mounting
- variable pitch
- vane ring
- 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.)
- Active
Links
Classifications
-
- 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
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
-
- 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
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
-
- 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/292—Three-dimensional machined; miscellaneous tapered
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- 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
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49236—Fluid pump or compressor making
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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/519,637 US7665963B2 (en) | 2006-09-06 | 2006-09-12 | Curved variable pitch wedge retention in vane outer base |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602007005567D1 true DE602007005567D1 (de) | 2010-05-12 |
Family
ID=38828731
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602007005567T Active DE602007005567D1 (de) | 2006-09-12 | 2007-09-11 | Keilförmige Befestigung von Leitschaufeln im äusseren Schaufelkranz mit variabler Teilung |
Country Status (5)
Country | Link |
---|---|
US (1) | US7665963B2 (de) |
EP (1) | EP1905959B1 (de) |
JP (1) | JP2008069775A (de) |
DE (1) | DE602007005567D1 (de) |
SG (1) | SG141321A1 (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8210807B2 (en) | 2008-08-28 | 2012-07-03 | United Technologies Corporation | Gas turbine airfoil assemblies and methods of repair |
US8967977B2 (en) | 2010-08-30 | 2015-03-03 | United Technologies Corporation | Locked spacer for a gas turbine engine shaft |
GB201015862D0 (en) * | 2010-09-22 | 2010-10-27 | Rolls Royce Plc | A damped assembly |
US9610644B2 (en) | 2011-02-08 | 2017-04-04 | United Technologies Corporation | Mate face brazing for turbine components |
US9541540B2 (en) | 2012-10-04 | 2017-01-10 | United Technologies Corporation | Non-destructive test inspection method for evaluating thermal degradation of bismaleimide resin |
WO2014137468A1 (en) * | 2013-03-07 | 2014-09-12 | Rolls-Royce Canada, Ltd. | Gas turbine engine comprising an outboard insertion system of vanes and corresponding assembling method |
GB201306123D0 (en) * | 2013-04-05 | 2013-05-22 | Rolls Royce Plc | Vane assembly and method of making the same |
US9840929B2 (en) * | 2013-05-28 | 2017-12-12 | Pratt & Whitney Canada Corp. | Gas turbine engine vane assembly and method of mounting same |
WO2015088821A1 (en) | 2013-12-12 | 2015-06-18 | United Technologies Corporation | Gas turbine engine component cooling passage with asymmetrical pedestals |
US9567871B2 (en) | 2014-04-23 | 2017-02-14 | Sikorsky Aircraft Corporation | Impeller retention apparatus |
US20190234222A1 (en) * | 2018-01-30 | 2019-08-01 | United Technologies Corporation | Angled vane slot |
US11268394B2 (en) | 2020-03-13 | 2022-03-08 | General Electric Company | Nozzle assembly with alternating inserted vanes for a turbine engine |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2834537A (en) * | 1954-01-18 | 1958-05-13 | Ryan Aeronautical Co | Compressor stator structure |
US2857093A (en) * | 1954-12-02 | 1958-10-21 | Cincinnati Testing & Res Lab | Stator casing and blade assembly |
US3339833A (en) * | 1963-12-04 | 1967-09-05 | Rolls Royce | Axial fluid flow machine such as a compressor or turbine |
US3778185A (en) * | 1972-08-28 | 1973-12-11 | United Aircraft Corp | Composite strut joint construction |
FR2568953B1 (fr) * | 1984-08-08 | 1989-02-10 | Ratier Figeac Soc | Aube fixe pour reacteurs |
US4907946A (en) * | 1988-08-10 | 1990-03-13 | General Electric Company | Resiliently mounted outlet guide vane |
FR2654463A1 (fr) * | 1989-11-15 | 1991-05-17 | Snecma | Element de stator de turbomachine. |
US5074752A (en) * | 1990-08-06 | 1991-12-24 | General Electric Company | Gas turbine outlet guide vane mounting assembly |
US5494404A (en) * | 1993-12-22 | 1996-02-27 | Alliedsignal Inc. | Insertable stator vane assembly |
US6619917B2 (en) * | 2000-12-19 | 2003-09-16 | United Technologies Corporation | Machined fan exit guide vane attachment pockets for use in a gas turbine |
US7637718B2 (en) * | 2005-09-12 | 2009-12-29 | Pratt & Whitney Canada Corp. | Vane assembly with outer grommets |
US7510372B2 (en) * | 2006-04-19 | 2009-03-31 | United Technologies Corporation | Wedge repair of mechanically retained vanes |
-
2006
- 2006-09-12 US US11/519,637 patent/US7665963B2/en not_active Expired - Fee Related
-
2007
- 2007-08-21 SG SG200706123-7A patent/SG141321A1/en unknown
- 2007-09-06 JP JP2007230898A patent/JP2008069775A/ja active Pending
- 2007-09-11 EP EP07253600A patent/EP1905959B1/de not_active Ceased
- 2007-09-11 DE DE602007005567T patent/DE602007005567D1/de active Active
Also Published As
Publication number | Publication date |
---|---|
EP1905959A3 (de) | 2008-06-04 |
JP2008069775A (ja) | 2008-03-27 |
US20080063521A1 (en) | 2008-03-13 |
US7665963B2 (en) | 2010-02-23 |
EP1905959A2 (de) | 2008-04-02 |
SG141321A1 (en) | 2008-04-28 |
EP1905959B1 (de) | 2010-03-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |