FR1095392A - Gas turbine blades - Google Patents
Gas turbine bladesInfo
- Publication number
- FR1095392A FR1095392A FR1095392DA FR1095392A FR 1095392 A FR1095392 A FR 1095392A FR 1095392D A FR1095392D A FR 1095392DA FR 1095392 A FR1095392 A FR 1095392A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- turbine blades
- blades
- gas
- turbine
- 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
- 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
- F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1095392T | 1953-12-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1095392A true FR1095392A (en) | 1955-06-01 |
Family
ID=9617515
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1095392D Expired FR1095392A (en) | 1953-12-01 | 1953-12-01 | Gas turbine blades |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1095392A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3076634A (en) * | 1959-06-12 | 1963-02-05 | Ass Elect Ind | Locking means for compressor and turbine blades |
US3216699A (en) * | 1963-10-24 | 1965-11-09 | Gen Electric | Airfoil member assembly |
US3378230A (en) * | 1966-12-16 | 1968-04-16 | Gen Electric | Mounting of blades in turbomachine rotors |
US4053257A (en) * | 1976-02-20 | 1977-10-11 | Westinghouse Electric Corporation | Stator vane assembly for gas turbines |
FR2522063A1 (en) * | 1982-02-22 | 1983-08-26 | United Technologies Corp | ROTOR AUBES ASSEMBLY |
WO1995030070A1 (en) * | 1994-04-29 | 1995-11-09 | United Technologies Corporation | Ramped dovetail rails for rotor blade assembly |
EP1418310A2 (en) * | 2002-10-18 | 2004-05-12 | General Electric Company | Method and apparatus for facilitating failure prevention of gas turbine blades |
WO2007045815A1 (en) * | 2005-10-19 | 2007-04-26 | Rolls-Royce Plc | A blade mounting |
-
1953
- 1953-12-01 FR FR1095392D patent/FR1095392A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3076634A (en) * | 1959-06-12 | 1963-02-05 | Ass Elect Ind | Locking means for compressor and turbine blades |
US3216699A (en) * | 1963-10-24 | 1965-11-09 | Gen Electric | Airfoil member assembly |
US3378230A (en) * | 1966-12-16 | 1968-04-16 | Gen Electric | Mounting of blades in turbomachine rotors |
US4053257A (en) * | 1976-02-20 | 1977-10-11 | Westinghouse Electric Corporation | Stator vane assembly for gas turbines |
FR2522063A1 (en) * | 1982-02-22 | 1983-08-26 | United Technologies Corp | ROTOR AUBES ASSEMBLY |
WO1995030070A1 (en) * | 1994-04-29 | 1995-11-09 | United Technologies Corporation | Ramped dovetail rails for rotor blade assembly |
US5993162A (en) * | 1994-04-29 | 1999-11-30 | United Technologies Corporation | Ramped dovetail rails for rotor blade assembly |
EP1418310A2 (en) * | 2002-10-18 | 2004-05-12 | General Electric Company | Method and apparatus for facilitating failure prevention of gas turbine blades |
EP1418310A3 (en) * | 2002-10-18 | 2006-08-30 | General Electric Company | Method and apparatus for facilitating failure prevention of gas turbine blades |
WO2007045815A1 (en) * | 2005-10-19 | 2007-04-26 | Rolls-Royce Plc | A blade mounting |
GB2442695A (en) * | 2005-10-19 | 2008-04-09 | Rolls Royce Plc | A blade mounting |
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