SE466559B - Gasturbinmotor med foerstaerkare och foerbiledningsinjektor med variabel yta - Google Patents
Gasturbinmotor med foerstaerkare och foerbiledningsinjektor med variabel ytaInfo
- Publication number
- SE466559B SE466559B SE8800465A SE8800465A SE466559B SE 466559 B SE466559 B SE 466559B SE 8800465 A SE8800465 A SE 8800465A SE 8800465 A SE8800465 A SE 8800465A SE 466559 B SE466559 B SE 466559B
- Authority
- SE
- Sweden
- Prior art keywords
- hollow
- elements
- gas
- bypass
- gases
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/38—Introducing air inside the jet
- F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
-
- 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)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Combustion Of Fluid Fuel (AREA)
- Separation By Low-Temperature Treatments (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1456287A | 1987-02-13 | 1987-02-13 |
Publications (3)
Publication Number | Publication Date |
---|---|
SE8800465D0 SE8800465D0 (sv) | 1988-02-11 |
SE8800465L SE8800465L (sv) | 1988-08-14 |
SE466559B true SE466559B (sv) | 1992-03-02 |
Family
ID=21766218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8800465A SE466559B (sv) | 1987-02-13 | 1988-02-11 | Gasturbinmotor med foerstaerkare och foerbiledningsinjektor med variabel yta |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS63227930A (fr) |
DE (1) | DE3803992A1 (fr) |
FR (1) | FR2610994B1 (fr) |
GB (1) | GB2202589B (fr) |
SE (1) | SE466559B (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3903713A1 (de) * | 1989-02-08 | 1990-08-09 | Mtu Muenchen Gmbh | Strahltriebwerk |
US5261229A (en) * | 1992-08-03 | 1993-11-16 | General Electric Company | Noise-suppressed exhaust nozzles for jet engines |
FR2712962B1 (fr) * | 1993-11-24 | 1995-12-29 | Snecma | Dispositif de postcombustion comprenant un dispositif accroche-flammes perfectionné. |
FR2763648B1 (fr) * | 1997-05-22 | 1999-07-02 | Snecma | Systeme de rechauffe dichotomique reduisant les pertes en sec |
US7596950B2 (en) * | 2005-09-16 | 2009-10-06 | General Electric Company | Augmentor radial fuel spray bar with counterswirling heat shield |
US7603863B2 (en) * | 2006-06-05 | 2009-10-20 | General Electric Company | Secondary fuel injection from stage one nozzle |
JP5625585B2 (ja) * | 2010-07-27 | 2014-11-19 | 株式会社Ihi | アフタバーナ及び航空機エンジン |
JP6229590B2 (ja) | 2014-04-30 | 2017-11-15 | 株式会社Ihi | アフタバーナ及び航空機エンジン |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3060680A (en) * | 1957-12-30 | 1962-10-30 | Rolls Royce | By-pass gas-turbine engine and control therefor |
GB928475A (en) * | 1961-12-27 | 1963-06-12 | Rolls Royce | Improvements in or relating to by-pass gas turbine engines |
GB1029900A (en) * | 1964-11-27 | 1966-05-18 | Rolls Royce | By-pass gas turbine jet engine |
DE1923150A1 (de) * | 1968-05-08 | 1970-01-15 | Man Turbo Gmbh | Zweistromturbinenstrahltriebwerk |
US4335573A (en) * | 1970-09-02 | 1982-06-22 | General Electric Company | Gas turbine engine mixer |
US3698186A (en) * | 1970-12-24 | 1972-10-17 | United Aircraft Corp | Afterburner combustion apparatus |
BE795529A (fr) * | 1972-02-17 | 1973-06-18 | Gen Electric | Allumeur monte sur un dispositif d'augmentation de la poussee de turboreacteurs et refroidi a l'air |
US4072008A (en) * | 1976-05-04 | 1978-02-07 | General Electric Company | Variable area bypass injector system |
JPS5641815A (en) * | 1979-09-12 | 1981-04-18 | Mitsui Toatsu Chem Inc | Purifying method for wet process phosphoric acid solution |
US4461146A (en) * | 1982-10-22 | 1984-07-24 | The United States Of America As Represented By The Secretary Of The Navy | Mixed flow swirl augmentor for turbofan engine |
-
1988
- 1988-02-04 FR FR8801282A patent/FR2610994B1/fr not_active Expired - Lifetime
- 1988-02-10 DE DE19883803992 patent/DE3803992A1/de not_active Withdrawn
- 1988-02-11 SE SE8800465A patent/SE466559B/sv not_active IP Right Cessation
- 1988-02-11 GB GB8803121A patent/GB2202589B/en not_active Expired - Fee Related
- 1988-02-12 JP JP2905188A patent/JPS63227930A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
FR2610994A1 (fr) | 1988-08-19 |
GB8803121D0 (en) | 1988-03-09 |
JPH0587652B2 (fr) | 1993-12-17 |
GB2202589B (en) | 1991-10-02 |
FR2610994B1 (fr) | 1993-06-11 |
DE3803992A1 (de) | 1988-08-25 |
SE8800465L (sv) | 1988-08-14 |
SE8800465D0 (sv) | 1988-02-11 |
JPS63227930A (ja) | 1988-09-22 |
GB2202589A (en) | 1988-09-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5220400B2 (ja) | ダクト燃焼式混成流ターボファン | |
US4876851A (en) | Infrared radiation screening device | |
US4817378A (en) | Gas turbine engine with augmentor and variable area bypass injector | |
US6668541B2 (en) | Method and apparatus for spraying fuel within a gas turbine engine | |
US4544098A (en) | Cooled exhaust nozzle flaps | |
SE453612B (sv) | Brennkammare | |
US5117628A (en) | Mixed flow augmentor pre-mixer | |
US4177637A (en) | Inlet for annular gas turbine combustor | |
US2856755A (en) | Combustion chamber with diverse combustion and diluent air paths | |
RU2358139C2 (ru) | Устройство для подачи воздуха и топлива к кольцу форсунок в форсажной камере | |
SE453221B (sv) | Brennkammarfoder for gasturbinmotor | |
GB2265704A (en) | Fuel injector for the after-burner chamber of a turbomachine | |
KR101774093B1 (ko) | 가스 터빈 엔진에서 사용되는 스테이지가 형성되고 접선방향으로 형성된 연료-공기 노즐을 가진 캔-애뉼러형 연소실 | |
EP2957835A1 (fr) | Procédé de recirculation des gaz d'échappement provenant d'une chambre de combustion d'un brûleur d'une turbine à gaz et turbine à gaz pour l'exécution de ce procédé | |
US7584615B2 (en) | Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance | |
US8272219B1 (en) | Gas turbine engine combustor having trapped dual vortex cavity | |
EP2966356A1 (fr) | Agencement de combustion sequentielle avec un melangeur | |
SE466559B (sv) | Gasturbinmotor med foerstaerkare och foerbiledningsinjektor med variabel yta | |
US3338051A (en) | High velocity ram induction burner | |
DE59807856D1 (de) | Brenner für den Betrieb eines Wärmeerzeugers | |
SE453936B (sv) | Munstycke for gasturbin-flygmotor | |
US5479774A (en) | Combustion chamber assembly in a gas turbine engine | |
US3300976A (en) | Combined guide vane and combustion equipment for bypass gas turbine engines | |
GB2269449A (en) | Combustion chamber with fuel injectors of different types | |
US5941060A (en) | Gas turbine having sequential combustion |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
Ref document number: 8800465-0 Effective date: 19940910 Format of ref document f/p: F |