BE689015A - - Google Patents
Info
- Publication number
- BE689015A BE689015A BE689015DA BE689015A BE 689015 A BE689015 A BE 689015A BE 689015D A BE689015D A BE 689015DA BE 689015 A BE689015 A BE 689015A
- Authority
- BE
- Belgium
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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US459207A US3343806A (en) | 1965-05-27 | 1965-05-27 | Rotor assembly for gas turbine engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE689015A true BE689015A (en:Method) | 1967-03-31 |
Family
ID=23823835
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE689015D BE689015A (en:Method) | 1965-05-27 | 1966-10-28 |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US3343806A (en:Method) |
| BE (1) | BE689015A (en:Method) |
Families Citing this family (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3451653A (en) * | 1967-03-22 | 1969-06-24 | Gen Electric | Turbomachinery rotors |
| US3490852A (en) * | 1967-12-21 | 1970-01-20 | Gen Electric | Gas turbine rotor bucket cooling and sealing arrangement |
| CH495496A (de) * | 1969-02-26 | 1970-08-31 | Bbc Sulzer Turbomaschinen | Turbomaschine mit gekühltem Rotor |
| US3945758A (en) * | 1974-02-28 | 1976-03-23 | Westinghouse Electric Corporation | Cooling system for a gas turbine |
| US3904307A (en) * | 1974-04-10 | 1975-09-09 | United Technologies Corp | Gas generator turbine cooling scheme |
| US4184797A (en) * | 1977-10-17 | 1980-01-22 | General Electric Company | Liquid-cooled turbine rotor |
| US4309145A (en) * | 1978-10-30 | 1982-01-05 | General Electric Company | Cooling air seal |
| US4309147A (en) * | 1979-05-21 | 1982-01-05 | General Electric Company | Foreign particle separator |
| US4526508A (en) * | 1982-09-29 | 1985-07-02 | United Technologies Corporation | Rotor assembly for a gas turbine engine |
| CA1209482A (en) * | 1983-12-22 | 1986-08-12 | Douglas L. Kisling | Two stage rotor assembly with improved coolant flow |
| DE3509193A1 (de) * | 1985-03-14 | 1986-09-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Stroemungsmaschine mit innengehaeuse |
| US4767267A (en) * | 1986-12-03 | 1988-08-30 | General Electric Company | Seal assembly |
| US5211541A (en) * | 1991-12-23 | 1993-05-18 | General Electric Company | Turbine support assembly including turbine heat shield and bolt retainer assembly |
| US5593274A (en) * | 1995-03-31 | 1997-01-14 | General Electric Co. | Closed or open circuit cooling of turbine rotor components |
| US6409472B1 (en) | 1999-08-09 | 2002-06-25 | United Technologies Corporation | Stator assembly for a rotary machine and clip member for a stator assembly |
| CN1281901C (zh) * | 2001-02-13 | 2006-10-25 | 埃德蒙兹有限公司 | 转子通风机 |
| US7837437B2 (en) * | 2007-03-07 | 2010-11-23 | General Electric Company | Turbine nozzle segment and repair method |
| FR2931873B1 (fr) * | 2008-05-29 | 2010-08-20 | Snecma | Ensemble d'un disque de turbine d'un moteur a turbine a gaz et d'un tourillon support de palier,circuit de refroidissement d'un disque de turbine d'un tel ensemble. |
| US20100260954A1 (en) * | 2008-11-26 | 2010-10-14 | Valspar Sourcing, Inc. | Polymer having polycyclic groups and coating compositions thereof |
| US8367171B2 (en) | 2008-11-26 | 2013-02-05 | Valspar Sourcing, Inc. | Polymer having polycyclic groups and coating compositions thereof |
| CN102387924B (zh) | 2009-04-09 | 2014-10-15 | 威士伯采购公司 | 具有不饱和脂环官能团的聚合物以及由其形成的涂料组合物 |
| CA2758203C (en) | 2009-04-09 | 2017-05-09 | Gregory Bryant Hayes | Polyester coating composition |
| FR2963806B1 (fr) * | 2010-08-10 | 2013-05-03 | Snecma | Dispositif de blocage d'un pied d'une aube de rotor |
| FR3003599B1 (fr) * | 2013-03-25 | 2017-11-17 | Snecma | Aubage fixe de distribution de flux ameliore |
| ES2691073T3 (es) | 2014-03-25 | 2018-11-23 | Industria De Turbo Propulsores S.A. | Rotor de turbina de gas |
| FR3019597B1 (fr) * | 2014-04-08 | 2016-03-25 | Turbomeca | Compresseur de turbomachine a aubes a calage variable |
| KR101663306B1 (ko) * | 2015-10-02 | 2016-10-06 | 두산중공업 주식회사 | 가스터빈 디스크 |
| JP7092938B2 (ja) * | 2018-08-02 | 2022-06-28 | シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | ２つのロータディスクの間にロータ組立要素を配置したロータ |
| FR3120092A1 (fr) * | 2021-02-24 | 2022-08-26 | Safran Aircraft Engines | Anneau d’étanchéité de turbine |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2557747A (en) * | 1946-10-02 | 1951-06-19 | Rolls Royce | Supplying cooling air to turbine disks of gas-turbine engines |
| US2860851A (en) * | 1953-12-11 | 1958-11-18 | Havilland Engine Co Ltd | Multi-stage turbine rotor assemblies |
| US3034298A (en) * | 1958-06-12 | 1962-05-15 | Gen Motors Corp | Turbine cooling system |
-
1965
- 1965-05-27 US US459207A patent/US3343806A/en not_active Expired - Lifetime
-
1966
- 1966-10-28 BE BE689015D patent/BE689015A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US3343806A (en) | 1967-09-26 |