CA1125660A - Aubes refroidies de turbomoteur a combustion - Google Patents
Aubes refroidies de turbomoteur a combustionInfo
- Publication number
- CA1125660A CA1125660A CA353,911A CA353911A CA1125660A CA 1125660 A CA1125660 A CA 1125660A CA 353911 A CA353911 A CA 353911A CA 1125660 A CA1125660 A CA 1125660A
- Authority
- CA
- Canada
- Prior art keywords
- airfoil
- vane
- cooling air
- cavity
- sidewalls
- 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
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US5362979A | 1979-06-29 | 1979-06-29 | |
| US053,629 | 1979-06-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1125660A true CA1125660A (fr) | 1982-06-15 |
Family
ID=21985545
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA353,911A Expired CA1125660A (fr) | 1979-06-29 | 1980-06-12 | Aubes refroidies de turbomoteur a combustion |
Country Status (2)
| Country | Link |
|---|---|
| JP (2) | JPS569623A (fr) |
| CA (1) | CA1125660A (fr) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4511306A (en) * | 1982-02-02 | 1985-04-16 | Westinghouse Electric Corp. | Combustion turbine single airfoil stator vane structure |
| JP2602123B2 (ja) * | 1990-10-18 | 1997-04-23 | 株式会社堀場製作所 | シャシダイナモメータ上の自動車運転用ロボット |
| JP2537226Y2 (ja) * | 1991-09-10 | 1997-05-28 | 株式会社堀場製作所 | シャシダイナモメータ上の自動車運転用ロボット |
| JP2566448Y2 (ja) * | 1991-09-10 | 1998-03-25 | 株式会社堀場製作所 | シャシダイナモメータ上の自動車運転用ロボット |
| FR2899271B1 (fr) * | 2006-03-29 | 2008-05-30 | Snecma Sa | Ensemble d'une aube et d'une chemise de refroidissement, distributeur de turbomachine comportant l'ensemble, turbomachine, procede de montage et de reparation de l'ensemble |
| WO2024053326A1 (fr) * | 2022-09-05 | 2024-03-14 | 三菱重工業株式会社 | Guide de fluide de refroidissement pour turbine à gaz, et turbine à gaz |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3275294A (en) * | 1963-11-14 | 1966-09-27 | Westinghouse Electric Corp | Elastic fluid apparatus |
| GB1564608A (en) * | 1975-12-20 | 1980-04-10 | Rolls Royce | Means for cooling a surface by the impingement of a cooling fluid |
-
1980
- 1980-06-12 CA CA353,911A patent/CA1125660A/fr not_active Expired
- 1980-06-27 JP JP8673480A patent/JPS569623A/ja active Pending
-
1985
- 1985-07-02 JP JP10016185U patent/JPS6117401U/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6117401U (ja) | 1986-01-31 |
| JPS569623A (en) | 1981-01-31 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP1079072B1 (fr) | Refroidissement des extrémités des aubes de turbine | |
| US6561758B2 (en) | Methods and systems for cooling gas turbine engine airfoils | |
| CN101148994B (zh) | 灰孔圆顶叶片 | |
| US6431832B1 (en) | Gas turbine engine airfoils with improved cooling | |
| US7131817B2 (en) | Method and apparatus for cooling gas turbine engine rotor blades | |
| US4761116A (en) | Turbine blade with tip vent | |
| CN1982654B (zh) | 钝形顶部涡轮叶片 | |
| EP1273758B1 (fr) | Procédé et dispositif de refroidissement par pellicule d'une aube | |
| US6174135B1 (en) | Turbine blade trailing edge cooling openings and slots | |
| EP1621727B1 (fr) | Aube de rotor de turbine et rotor de moteur à turbine à gaz comportant de telles aubes | |
| US6746209B2 (en) | Methods and apparatus for cooling gas turbine engine nozzle assemblies | |
| KR100789030B1 (ko) | 터빈 날개부, 노즐의 필렛 영역의 냉각 방법 및 유동 제어 구조체 | |
| US8366383B2 (en) | Air sealing element | |
| JP4731237B2 (ja) | ガスタービンエンジンロータブレードを冷却するための装置 | |
| JP2001107702A (ja) | 断熱コーティングされたスクィーラ先端空洞 | |
| JP2001050004A (ja) | 先端を断熱した翼形部 | |
| US9669458B2 (en) | Micro channel and methods of manufacturing a micro channel | |
| EP3002412A1 (fr) | Refroidissement interne de composants d'une turbine à gaz | |
| US6485262B1 (en) | Methods and apparatus for extending gas turbine engine airfoils useful life | |
| US6932570B2 (en) | Methods and apparatus for extending gas turbine engine airfoils useful life | |
| US7165940B2 (en) | Method and apparatus for cooling gas turbine rotor blades | |
| EP1106280A1 (fr) | Noyau pour controler l'épaisseur d'une aube d'une turbine et méthode | |
| GB2093923A (en) | Air cooled gas turbine vane structure | |
| GB2279705A (en) | Cooling of turbine blades of a gas turbine engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MKEX | Expiry |