IT1049017B - Apparato guidafiamma per potenziatore di spinta - Google Patents
Apparato guidafiamma per potenziatore di spintaInfo
- Publication number
- IT1049017B IT1049017B IT29349/75A IT2934975A IT1049017B IT 1049017 B IT1049017 B IT 1049017B IT 29349/75 A IT29349/75 A IT 29349/75A IT 2934975 A IT2934975 A IT 2934975A IT 1049017 B IT1049017 B IT 1049017B
- Authority
- IT
- Italy
- Prior art keywords
- potentiator
- pushing
- guide apparatus
- flame guide
- flame
- Prior art date
Links
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
- 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)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Combustion Of Fluid Fuel (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/539,315 US3931707A (en) | 1975-01-08 | 1975-01-08 | Augmentor flameholding apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1049017B true IT1049017B (it) | 1981-01-20 |
Family
ID=24150705
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT29349/75A IT1049017B (it) | 1975-01-08 | 1975-11-17 | Apparato guidafiamma per potenziatore di spinta |
Country Status (8)
Country | Link |
---|---|
US (1) | US3931707A (it) |
JP (1) | JPS5916170B2 (it) |
BE (1) | BE837339A (it) |
CA (1) | CA1050286A (it) |
DE (1) | DE2551005A1 (it) |
FR (1) | FR2297327A1 (it) |
GB (1) | GB1522826A (it) |
IT (1) | IT1049017B (it) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4064691A (en) * | 1975-11-04 | 1977-12-27 | General Electric Company | Cooling of fastener means for a removable flameholder |
FR2351258A1 (fr) * | 1976-05-13 | 1977-12-09 | Snecma | Dispositif d'allumage de carburant injecte dans un milieu gazeux en ecoulement rapide |
US4194358A (en) * | 1977-12-15 | 1980-03-25 | General Electric Company | Double annular combustor configuration |
US4203285A (en) * | 1978-02-06 | 1980-05-20 | The United States Of America As Represented By The Secretary Of The Air Force | Partial swirl augmentor for a turbofan engine |
US4185458A (en) * | 1978-05-11 | 1980-01-29 | The United States Of America As Represented By The Secretary Of The Air Force | Turbofan augmentor flameholder |
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 |
FR2551500B1 (fr) * | 1983-09-07 | 1985-11-08 | Snecma | Anneau-bruleur pour postcombustion de moteur a reaction |
JPS61218198A (ja) * | 1985-03-25 | 1986-09-27 | 株式会社日立製作所 | 表示装置付制御基板 |
FR2594939B1 (fr) * | 1986-02-27 | 1989-11-03 | Snecma | Structure d'accroche-flamme pour systeme de rechauffe de turboreacteur |
US5076062A (en) * | 1987-11-05 | 1991-12-31 | General Electric Company | Gas-cooled flameholder assembly |
US4893468A (en) * | 1987-11-30 | 1990-01-16 | General Electric Company | Emissions control for gas turbine engine |
US4901527A (en) * | 1988-02-18 | 1990-02-20 | General Electric Company | Low turbulence flame holder mount |
IL93630A0 (en) * | 1989-03-27 | 1990-12-23 | Gen Electric | Flameholder for gas turbine engine afterburner |
US5142858A (en) * | 1990-11-21 | 1992-09-01 | General Electric Company | Compact flameholder type combustor which is staged to reduce emissions |
US5491974A (en) * | 1993-04-15 | 1996-02-20 | General Electric Company | Removable afterburner flameholder |
US5685142A (en) * | 1996-04-10 | 1997-11-11 | United Technologies Corporation | Gas turbine engine afterburner |
FR2873168B1 (fr) * | 2004-07-16 | 2008-10-31 | Snecma Moteurs Sa | Turboreacteur comprenant une chambre de post-combustion a allumage securise |
US7647775B2 (en) * | 2005-06-30 | 2010-01-19 | United Technologies Corporation | Augmentor spray bars |
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 |
US7568346B2 (en) * | 2006-10-31 | 2009-08-04 | General Electric Company | Method and apparatus for assembling a flameholder for an augmenter |
US8209987B2 (en) * | 2008-11-26 | 2012-07-03 | United Technologies Corporation | Augmentor pilot |
US9879862B2 (en) | 2013-03-08 | 2018-01-30 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine afterburner |
US9366184B2 (en) * | 2013-06-18 | 2016-06-14 | General Electric Company | Gas turbine engine and method of operating thereof |
GB2524782B (en) * | 2014-04-02 | 2016-04-20 | Verderg Ltd | Turbine assembly |
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 |
JP6245057B2 (ja) * | 2014-04-30 | 2017-12-13 | 株式会社Ihi | アフタバーナ及び航空機エンジン |
FR3039220B1 (fr) * | 2015-07-24 | 2017-08-11 | Snecma | Dipositif de postcombustion pour turboreacteur |
RU2666835C1 (ru) * | 2017-06-20 | 2018-09-12 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Способ работы форсажного комплекса турбореактивного двигателя (ТРД) и форсажный комплекс, работающий этим способом (варианты), способ работы ТРД и ТРД, работающий этим способом |
RU2656525C1 (ru) * | 2017-06-20 | 2018-06-05 | Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Способ работы форсажного комплекса турбореактивного двигателя (ТРД) и форсажный комплекс, работающий этим способом, способ работы насоса форсажного и насос форсажный, работающий этим способом, способ работы ТРД и ТРД, работающий этим способом |
RU2682220C1 (ru) * | 2018-03-01 | 2019-03-15 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Форсажная камера сгорания турбореактивного двухконтурного двигателя |
WO2020121946A1 (ja) * | 2018-12-11 | 2020-06-18 | 株式会社エイチアンドエフ | レーザーブランキング装置 |
CN115183274B (zh) * | 2022-07-21 | 2023-08-04 | 中国航发沈阳发动机研究所 | 一种内涵点火加力燃烧室 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2546432A (en) * | 1944-03-20 | 1951-03-27 | Power Jets Res & Dev Ltd | Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream |
GB674641A (en) * | 1949-11-30 | 1952-06-25 | Armstrong Siddeley Motors Ltd | Fuel-burning means for a gaseous-fluid propulsion jet |
GB723830A (en) * | 1952-09-13 | 1955-02-09 | Armstrong Siddeley Motors Ltd | Flame stabilising device |
US2918794A (en) * | 1955-09-21 | 1959-12-29 | United Aircraft Corp | Flameholder |
FR1165618A (fr) * | 1956-12-12 | 1958-10-28 | Continental Aviat & Eng Corp | Perfectionnements aux stato-réacteurs |
US2964907A (en) * | 1957-11-15 | 1960-12-20 | Rolls Royce | Combustion stabilising device for combustion equipment |
FR1207017A (fr) * | 1958-05-29 | 1960-02-12 | Gen Electric | Dispositif d'allumage pour système de postcombustion de turboréacteur |
FR1210398A (fr) * | 1958-09-24 | 1960-03-08 | Snecma | Perfectionnements aux dispositifs de combustion |
FR1217698A (fr) * | 1958-11-05 | 1960-05-05 | United Aircraft Corp | Guide-flamme |
FR1408812A (fr) * | 1964-07-06 | 1965-08-20 | Nord Aviat | Perfectionnement apporté aux chambres de combustion de propulseurs |
FR1525092A (fr) * | 1967-01-23 | 1968-05-17 | Snecma | Turbo-réacteur à flux de gaz chaud et à flux d'air froid |
US3788065A (en) * | 1970-10-26 | 1974-01-29 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
FR2124141B1 (it) * | 1971-02-09 | 1975-02-21 | Snecma | |
US3800527A (en) * | 1971-03-18 | 1974-04-02 | United Aircraft Corp | Piloted flameholder construction |
FR2188060B1 (it) * | 1972-06-01 | 1976-06-11 | Snecma | |
US3765178A (en) * | 1972-09-08 | 1973-10-16 | Gen Electric | Afterburner flameholder |
-
1975
- 1975-01-08 US US05/539,315 patent/US3931707A/en not_active Expired - Lifetime
- 1975-11-10 GB GB46388/75A patent/GB1522826A/en not_active Expired
- 1975-11-13 DE DE19752551005 patent/DE2551005A1/de not_active Withdrawn
- 1975-11-17 IT IT29349/75A patent/IT1049017B/it active
- 1975-11-20 JP JP50138791A patent/JPS5916170B2/ja not_active Expired
-
1976
- 1976-01-06 BE BE163337A patent/BE837339A/xx unknown
- 1976-01-08 FR FR7600296A patent/FR2297327A1/fr not_active Withdrawn
- 1976-01-08 CA CA243,174A patent/CA1050286A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2297327A1 (fr) | 1976-08-06 |
US3931707A (en) | 1976-01-13 |
DE2551005A1 (de) | 1976-07-15 |
JPS5181216A (it) | 1976-07-16 |
BE837339A (fr) | 1976-05-03 |
JPS5916170B2 (ja) | 1984-04-13 |
GB1522826A (en) | 1978-08-31 |
CA1050286A (en) | 1979-03-13 |
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