GB0802967D0 - A blade mounting - Google Patents
A blade mountingInfo
- Publication number
- GB0802967D0 GB0802967D0 GBGB0802967.0A GB0802967A GB0802967D0 GB 0802967 D0 GB0802967 D0 GB 0802967D0 GB 0802967 A GB0802967 A GB 0802967A GB 0802967 D0 GB0802967 D0 GB 0802967D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade mounting
- blade
- mounting
- 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.)
- Withdrawn
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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- 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
- F04D29/34—Blade mountings
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/313—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being perpendicular to each other
-
- 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
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0521242.8A GB0521242D0 (en) | 2005-10-19 | 2005-10-19 | A blade mounting |
PCT/GB2006/003544 WO2007045815A1 (en) | 2005-10-19 | 2006-09-22 | A blade mounting |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0802967D0 true GB0802967D0 (en) | 2008-03-26 |
GB2442695A GB2442695A (en) | 2008-04-09 |
Family
ID=35452013
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB0521242.8A Ceased GB0521242D0 (en) | 2005-10-19 | 2005-10-19 | A blade mounting |
GB0802967A Withdrawn GB2442695A (en) | 2005-10-19 | 2006-09-22 | A blade mounting |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB0521242.8A Ceased GB0521242D0 (en) | 2005-10-19 | 2005-10-19 | A blade mounting |
Country Status (3)
Country | Link |
---|---|
US (1) | US20090136356A1 (en) |
GB (2) | GB0521242D0 (en) |
WO (1) | WO2007045815A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007051838A1 (en) * | 2007-10-30 | 2009-05-07 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine blade root comprises two surfaces, which is auxiliary to bearing of gas turbine blade root, which is conjoined in right angle, and transient area of surfaces is formed with tapered and even edge |
US9239062B2 (en) * | 2012-09-10 | 2016-01-19 | General Electric Company | Low radius ratio fan for a gas turbine engine |
US9677421B2 (en) * | 2012-10-24 | 2017-06-13 | United Technologies Corporation | Gas turbine engine rotor drain feature |
KR101882109B1 (en) * | 2016-12-23 | 2018-07-25 | 두산중공업 주식회사 | Gas turbine |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1719415A (en) * | 1927-09-14 | 1929-07-02 | Westinghouse Electric & Mfg Co | Turbine-blade attachment |
FR1095392A (en) * | 1953-12-01 | 1955-06-01 | Csf | Gas turbine blades |
US3471127A (en) * | 1966-12-08 | 1969-10-07 | Gen Motors Corp | Turbomachine rotor |
BE755608A (en) * | 1969-09-04 | 1971-02-15 | Gen Electric | COMPRESSOR BLADES |
US4050134A (en) * | 1974-10-29 | 1977-09-27 | Westinghouse Electric Corporation | Method for removing rotatable blades without removing the casting of a turbine |
US3986793A (en) * | 1974-10-29 | 1976-10-19 | Westinghouse Electric Corporation | Turbine rotating blade |
US4523890A (en) * | 1983-10-19 | 1985-06-18 | General Motors Corporation | End seal for turbine blade base |
US5067876A (en) * | 1990-03-29 | 1991-11-26 | General Electric Company | Gas turbine bladed disk |
US5088894A (en) * | 1990-05-02 | 1992-02-18 | Westinghouse Electric Corp. | Turbomachine blade fastening |
US5067877A (en) * | 1990-09-11 | 1991-11-26 | United Technologies Corporation | Fan blade axial retention device |
US5431542A (en) * | 1994-04-29 | 1995-07-11 | United Technologies Corporation | Ramped dovetail rails for rotor blade assembly |
US5599190A (en) * | 1995-01-27 | 1997-02-04 | The Whitaker Corporation | Communication wiring system including a reconfigurable outlet assembly |
DE19705323A1 (en) * | 1997-02-12 | 1998-08-27 | Siemens Ag | Turbo-machine blade |
US5836744A (en) * | 1997-04-24 | 1998-11-17 | United Technologies Corporation | Frangible fan blade |
US6439851B1 (en) * | 2000-12-21 | 2002-08-27 | United Technologies Corporation | Reduced stress rotor blade and disk assembly |
JP4316168B2 (en) * | 2001-08-30 | 2009-08-19 | 株式会社東芝 | Method for selecting blade material and shape of steam turbine blade and steam turbine |
US6619924B2 (en) * | 2001-09-13 | 2003-09-16 | General Electric Company | Method and system for replacing a compressor blade |
US6739837B2 (en) * | 2002-04-16 | 2004-05-25 | United Technologies Corporation | Bladed rotor with a tiered blade to hub interface |
US6846159B2 (en) * | 2002-04-16 | 2005-01-25 | United Technologies Corporation | Chamfered attachment for a bladed rotor |
GB0302116D0 (en) * | 2003-01-30 | 2003-03-05 | Rolls Royce Plc | A rotor |
GB0316158D0 (en) * | 2003-07-10 | 2003-08-13 | Rolls Royce Plc | Method of making aerofoil blisks |
-
2005
- 2005-10-19 GB GBGB0521242.8A patent/GB0521242D0/en not_active Ceased
-
2006
- 2006-09-22 WO PCT/GB2006/003544 patent/WO2007045815A1/en active Application Filing
- 2006-09-22 US US11/992,303 patent/US20090136356A1/en not_active Abandoned
- 2006-09-22 GB GB0802967A patent/GB2442695A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2442695A (en) | 2008-04-09 |
WO2007045815A1 (en) | 2007-04-26 |
US20090136356A1 (en) | 2009-05-28 |
GB0521242D0 (en) | 2005-11-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |