JPH0222217B2 - - Google Patents
Info
- Publication number
- JPH0222217B2 JPH0222217B2 JP7569284A JP7569284A JPH0222217B2 JP H0222217 B2 JPH0222217 B2 JP H0222217B2 JP 7569284 A JP7569284 A JP 7569284A JP 7569284 A JP7569284 A JP 7569284A JP H0222217 B2 JPH0222217 B2 JP H0222217B2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- blowing
- height direction
- reheating
- gas
- 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
- 238000003303 reheating Methods 0.000 claims description 21
- 238000007664 blowing Methods 0.000 claims description 20
- 239000000446 fuel Substances 0.000 claims description 14
- 239000007789 gas Substances 0.000 description 39
- 238000002485 combustion reaction Methods 0.000 description 8
- 238000009826 distribution Methods 0.000 description 8
- 239000012530 fluid Substances 0.000 description 6
- 239000002737 fuel gas Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000005495 investment casting Methods 0.000 description 1
- 238000009828 non-uniform distribution Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/003—Gas-turbine plants with heaters between turbine stages
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/185—Liquid cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP7569284A JPS60219401A (ja) | 1984-04-17 | 1984-04-17 | ガスタ−ビンの再熱用燃料吹出し翼 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP7569284A JPS60219401A (ja) | 1984-04-17 | 1984-04-17 | ガスタ−ビンの再熱用燃料吹出し翼 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS60219401A JPS60219401A (ja) | 1985-11-02 |
JPH0222217B2 true JPH0222217B2 (fr) | 1990-05-17 |
Family
ID=13583504
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP7569284A Granted JPS60219401A (ja) | 1984-04-17 | 1984-04-17 | ガスタ−ビンの再熱用燃料吹出し翼 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60219401A (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1847682A1 (fr) * | 2006-04-21 | 2007-10-24 | Siemens Aktiengesellschaft | Méthode d'alimentation d'un fluide dans le flux principal de gaz d'une turbine et aube de turbine associée. |
US7603863B2 (en) * | 2006-06-05 | 2009-10-20 | General Electric Company | Secondary fuel injection from stage one nozzle |
EP2116768B1 (fr) * | 2008-05-09 | 2016-07-27 | Alstom Technology Ltd | Brûleur |
-
1984
- 1984-04-17 JP JP7569284A patent/JPS60219401A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS60219401A (ja) | 1985-11-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA1245869A (fr) | Methode de refroidissement pour l'interface entre les ailettes et le dispositif combustor | |
JP2510573B2 (ja) | ガスタ−ビン動力装置のための熱ガスオ−バヒ−ト防護装置 | |
JP3340743B2 (ja) | 一体式プラットホームおよびフィレット冷却通路を有するロータブレード | |
US8858159B2 (en) | Gas turbine engine component having wavy cooling channels with pedestals | |
JP6283462B2 (ja) | タービンエーロフォイル | |
US5022817A (en) | Thermostatic control of turbine cooling air | |
US3628880A (en) | Vane assembly and temperature control arrangement | |
US11448076B2 (en) | Engine component with cooling hole | |
JP2009085222A (ja) | タービュレータ付き後端ライナアセンブリ及びその冷却方法 | |
US5279111A (en) | Gas turbine cooling | |
US20140373504A1 (en) | Gas turbine having an exhaust gas diffuser and supporting fins | |
EP2847435B1 (fr) | Configuration de trous de refroidissement pour évacuation thermique par convection | |
JP2017141832A (ja) | 表面輪郭 | |
EP3537047A1 (fr) | Agencements de fente pour le refroidissement d'un film de paroi flottante d'impact d'un moteur à turbine | |
US4944152A (en) | Augmented turbine combustor cooling | |
US6584766B1 (en) | Methods and apparatus for minimizing thermal stresses in a centerbody | |
US11098602B2 (en) | Turbine vane equipped with insert support | |
JPH0222217B2 (fr) | ||
US6544001B2 (en) | Gas turbine engine system | |
KR102373729B1 (ko) | 가스 터빈 로터 블레이드용 냉각 통로 | |
US10968778B2 (en) | Gas turbine | |
JPH10339440A (ja) | ガスタービン燃焼装置 | |
US20160312654A1 (en) | Turbine airfoil cooling | |
US11608754B2 (en) | Turbine nozzle assembly and gas turbine including the same | |
GB2299378A (en) | Cooling compressor guide vanes |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
EXPY | Cancellation because of completion of term |