FR2330867A1 - Stabilisateur de flamme amovible - Google Patents
Stabilisateur de flamme amovibleInfo
- Publication number
- FR2330867A1 FR2330867A1 FR7632874A FR7632874A FR2330867A1 FR 2330867 A1 FR2330867 A1 FR 2330867A1 FR 7632874 A FR7632874 A FR 7632874A FR 7632874 A FR7632874 A FR 7632874A FR 2330867 A1 FR2330867 A1 FR 2330867A1
- Authority
- FR
- France
- Prior art keywords
- flame stabilizer
- removable flame
- removable
- stabilizer
- flame
- 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.)
- Granted
Links
- 239000003381 stabilizer Substances 0.000 title 1
Classifications
-
- 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
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)
- Gas Burners (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/628,749 US4064691A (en) | 1975-11-04 | 1975-11-04 | Cooling of fastener means for a removable flameholder |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2330867A1 true FR2330867A1 (fr) | 1977-06-03 |
| FR2330867B1 FR2330867B1 (enExample) | 1980-08-01 |
Family
ID=24520135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7632874A Granted FR2330867A1 (fr) | 1975-11-04 | 1976-10-29 | Stabilisateur de flamme amovible |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4064691A (enExample) |
| DE (1) | DE2650373A1 (enExample) |
| FR (1) | FR2330867A1 (enExample) |
| GB (1) | GB1561265A (enExample) |
| SE (1) | SE7610993L (enExample) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2429326A1 (fr) * | 1978-06-22 | 1980-01-18 | Snecma | Perfectionnements aux dispositifs accroche-flammes pour chambres de combustion, notamment pour canaux de post-combustion de turboreacteurs |
| EP0315485A3 (en) * | 1987-11-05 | 1990-05-23 | General Electric Company | Gas-cooled flameholder assembly |
| EP0550126A1 (en) * | 1992-01-02 | 1993-07-07 | General Electric Company | Thrust augmentor heat shield |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4594851A (en) * | 1983-12-16 | 1986-06-17 | The United States Of America As Represented By The Secretary Of The Air Force | Flameholder with removable flameholder attachments |
| FR2594939B1 (fr) * | 1986-02-27 | 1989-11-03 | Snecma | Structure d'accroche-flamme pour systeme de rechauffe de turboreacteur |
| US4901527A (en) * | 1988-02-18 | 1990-02-20 | General Electric Company | Low turbulence flame holder mount |
| US5103638A (en) * | 1990-01-29 | 1992-04-14 | Rolls-Royce Inc. | Mounting arrangement |
| US5072785A (en) * | 1990-06-12 | 1991-12-17 | United Technologies Corporation | Convectively cooled bolt assembly |
| US5211541A (en) * | 1991-12-23 | 1993-05-18 | General Electric Company | Turbine support assembly including turbine heat shield and bolt retainer assembly |
| US5226788A (en) * | 1991-12-23 | 1993-07-13 | General Electric Company | Turbine heat shield and bolt retainer assembly |
| US5491974A (en) * | 1993-04-15 | 1996-02-20 | General Electric Company | Removable afterburner flameholder |
| US5396761A (en) * | 1994-04-25 | 1995-03-14 | General Electric Company | Gas turbine engine ignition flameholder with internal impingement cooling |
| US5396763A (en) * | 1994-04-25 | 1995-03-14 | General Electric Company | Cooled spraybar and flameholder assembly including a perforated hollow inner air baffle for impingement cooling an outer heat shield |
| RU2270354C2 (ru) * | 1995-02-15 | 2006-02-20 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Смеситель форсажной камеры сгорания турбореактивного двухконтурного двигателя |
| US5813221A (en) * | 1997-01-14 | 1998-09-29 | General Electric Company | Augmenter with integrated fueling and cooling |
| US6334303B1 (en) * | 1997-12-08 | 2002-01-01 | Volvo Aero Corporation | Flameholder device for afterburners in gas turbine engines |
| US6351941B1 (en) * | 2000-02-29 | 2002-03-05 | General Electric Company | Methods and apparatus for reducing thermal stresses in an augmentor |
| US7251941B2 (en) * | 2004-03-10 | 2007-08-07 | General Electric Company | Ablative afterburner |
| US7565804B1 (en) | 2006-06-29 | 2009-07-28 | General Electric Company | Flameholder fuel shield |
| US7581398B2 (en) | 2006-06-29 | 2009-09-01 | General Electric Company | Purged flameholder fuel shield |
| GB2449477B (en) * | 2007-05-24 | 2009-05-13 | Rolls Royce Plc | A duct installation |
| US20140026590A1 (en) * | 2012-07-25 | 2014-01-30 | Hannes A. Alholm | Flexible combustor bracket |
| US10563868B2 (en) * | 2017-05-08 | 2020-02-18 | General Electric Company | Coupling method and structure for a propulsion system hot section |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB706698A (en) * | 1951-01-10 | 1954-04-07 | Rolls Royce | Improvements relating to combustion equipment of gas turbine engines |
| US2714287A (en) * | 1950-01-03 | 1955-08-02 | Westinghouse Electric Corp | Flameholder device for turbojet afterburner |
| US2862359A (en) * | 1952-10-28 | 1958-12-02 | Gen Motors Corp | Fuel manifold and flameholder in combustion apparatus for jet engines |
| FR1242865A (fr) * | 1959-04-29 | 1960-10-07 | Nord Aviat | Assemblage monobloc des éléments du dispositif de combustion dans un statoréacteur |
| US3056261A (en) * | 1959-09-01 | 1962-10-02 | Gen Electric | Flameholder configuration |
| GB919303A (en) * | 1960-10-14 | 1963-02-20 | Rolls Royce | Improvements relating to reheat systems for gas turbine engines |
| FR1406603A (fr) * | 1964-06-09 | 1965-07-23 | Snecma | Dispositif de brûleur et son montage dans une chambre de combustion |
| FR1478757A (fr) * | 1966-04-29 | 1967-04-28 | United Aircraft Corp | Porte-flamme de post-combustion de turbo-réacteur |
| FR2122308A1 (enExample) * | 1971-01-19 | 1972-09-01 | Snecma | |
| US3698186A (en) * | 1970-12-24 | 1972-10-17 | United Aircraft Corp | Afterburner combustion apparatus |
| US3765178A (en) * | 1972-09-08 | 1973-10-16 | Gen Electric | Afterburner flameholder |
| US3931707A (en) * | 1975-01-08 | 1976-01-13 | General Electric Company | Augmentor flameholding apparatus |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3102392A (en) * | 1959-04-21 | 1963-09-03 | Snecma | Combustion equipment for jet propulsion units |
| GB938553A (en) * | 1961-05-09 | 1963-10-02 | Rolls Royce | Reheat combustion apparatus for a gas turbine engine |
| US3236048A (en) * | 1963-09-25 | 1966-02-22 | Gen Motors Corp | Vaporizing manifold and flameholder for afterburners |
| US3315468A (en) * | 1965-10-01 | 1967-04-25 | Gen Electric | Cooled flameholder assembly |
| GB1211583A (en) * | 1968-05-16 | 1970-11-11 | Mini Of Technology | Improvements in or relating to combustion devices |
| US3932988A (en) * | 1972-10-25 | 1976-01-20 | Beaufrere Albert H | Fuel slinger combustor |
-
1975
- 1975-11-04 US US05/628,749 patent/US4064691A/en not_active Expired - Lifetime
-
1976
- 1976-10-04 SE SE7610993A patent/SE7610993L/xx unknown
- 1976-10-07 GB GB41739/76A patent/GB1561265A/en not_active Expired
- 1976-10-29 FR FR7632874A patent/FR2330867A1/fr active Granted
- 1976-11-03 DE DE19762650373 patent/DE2650373A1/de not_active Withdrawn
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2714287A (en) * | 1950-01-03 | 1955-08-02 | Westinghouse Electric Corp | Flameholder device for turbojet afterburner |
| GB706698A (en) * | 1951-01-10 | 1954-04-07 | Rolls Royce | Improvements relating to combustion equipment of gas turbine engines |
| US2862359A (en) * | 1952-10-28 | 1958-12-02 | Gen Motors Corp | Fuel manifold and flameholder in combustion apparatus for jet engines |
| FR1242865A (fr) * | 1959-04-29 | 1960-10-07 | Nord Aviat | Assemblage monobloc des éléments du dispositif de combustion dans un statoréacteur |
| US3056261A (en) * | 1959-09-01 | 1962-10-02 | Gen Electric | Flameholder configuration |
| GB919303A (en) * | 1960-10-14 | 1963-02-20 | Rolls Royce | Improvements relating to reheat systems for gas turbine engines |
| FR1406603A (fr) * | 1964-06-09 | 1965-07-23 | Snecma | Dispositif de brûleur et son montage dans une chambre de combustion |
| FR1478757A (fr) * | 1966-04-29 | 1967-04-28 | United Aircraft Corp | Porte-flamme de post-combustion de turbo-réacteur |
| US3698186A (en) * | 1970-12-24 | 1972-10-17 | United Aircraft Corp | Afterburner combustion apparatus |
| FR2122308A1 (enExample) * | 1971-01-19 | 1972-09-01 | Snecma | |
| US3765178A (en) * | 1972-09-08 | 1973-10-16 | Gen Electric | Afterburner flameholder |
| US3931707A (en) * | 1975-01-08 | 1976-01-13 | General Electric Company | Augmentor flameholding apparatus |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2429326A1 (fr) * | 1978-06-22 | 1980-01-18 | Snecma | Perfectionnements aux dispositifs accroche-flammes pour chambres de combustion, notamment pour canaux de post-combustion de turboreacteurs |
| EP0315485A3 (en) * | 1987-11-05 | 1990-05-23 | General Electric Company | Gas-cooled flameholder assembly |
| EP0550126A1 (en) * | 1992-01-02 | 1993-07-07 | General Electric Company | Thrust augmentor heat shield |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2650373A1 (de) | 1977-05-05 |
| FR2330867B1 (enExample) | 1980-08-01 |
| US4064691A (en) | 1977-12-27 |
| GB1561265A (en) | 1980-02-20 |
| SE7610993L (sv) | 1977-05-04 |
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| Publication | Publication Date | Title |
|---|---|---|
| BE837339A (fr) | Stabilisateur de flamme pour turbo-reacteurs | |
| FR2330867A1 (fr) | Stabilisateur de flamme amovible | |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |