IT8820431A0 - Camera di combustione. - Google Patents
Camera di combustione.Info
- Publication number
- IT8820431A0 IT8820431A0 IT8820431A IT2043188A IT8820431A0 IT 8820431 A0 IT8820431 A0 IT 8820431A0 IT 8820431 A IT8820431 A IT 8820431A IT 2043188 A IT2043188 A IT 2043188A IT 8820431 A0 IT8820431 A0 IT 8820431A0
- Authority
- IT
- Italy
- Prior art keywords
- combustion chamber
- combustion
- chamber
- Prior art date
Links
- 238000002485 combustion reaction Methods 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
- F23R3/002—Wall structures
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)
- Regulation And Control Of Combustion (AREA)
- Spinning Or Twisting Of Yarns (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8710647A GB2204672B (en) | 1987-05-06 | 1987-05-06 | Combustor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IT8820431A0 true IT8820431A0 (it) | 1988-05-03 |
| IT1217476B IT1217476B (it) | 1990-03-22 |
Family
ID=10616867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT20431/88A IT1217476B (it) | 1987-05-06 | 1988-05-03 | Camera di combustione |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4864827A (it) |
| JP (1) | JPS63311024A (it) |
| DE (1) | DE3815382C2 (it) |
| FR (1) | FR2614973B1 (it) |
| GB (1) | GB2204672B (it) |
| IT (1) | IT1217476B (it) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2219653B (en) * | 1987-12-18 | 1991-12-11 | Rolls Royce Plc | Improvements in or relating to combustors for gas turbine engines |
| US4934145A (en) * | 1988-10-12 | 1990-06-19 | United Technologies Corporation | Combustor bulkhead heat shield assembly |
| GB9018014D0 (en) * | 1990-08-16 | 1990-10-03 | Rolls Royce Plc | Gas turbine engine combustor |
| GB9106085D0 (en) * | 1991-03-22 | 1991-05-08 | Rolls Royce Plc | Gas turbine engine combustor |
| US5435139A (en) * | 1991-03-22 | 1995-07-25 | Rolls-Royce Plc | Removable combustor liner for gas turbine engine combustor |
| US5353865A (en) * | 1992-03-30 | 1994-10-11 | General Electric Company | Enhanced impingement cooled components |
| DE4444961A1 (de) * | 1994-12-16 | 1996-06-20 | Mtu Muenchen Gmbh | Einrichtung zur Kühlung insbesondere der Rückwand des Flammrohrs einer Brennkammer für Gasturbinentriebwerke |
| CA2288557C (en) * | 1998-11-12 | 2007-02-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor cooling structure |
| US6536201B2 (en) | 2000-12-11 | 2003-03-25 | Pratt & Whitney Canada Corp. | Combustor turbine successive dual cooling |
| DE10064264B4 (de) * | 2000-12-22 | 2017-03-23 | General Electric Technology Gmbh | Anordnung zur Kühlung eines Bauteils |
| US6530225B1 (en) | 2001-09-21 | 2003-03-11 | Honeywell International, Inc. | Waffle cooling |
| DE10214573A1 (de) * | 2002-04-02 | 2003-10-16 | Rolls Royce Deutschland | Brennkammer einer Gasturbine mit Starterfilmkühlung |
| RU2263251C2 (ru) * | 2003-10-27 | 2005-10-27 | Федеральное Государственное Унитарное предприятие "Научно-производственное предприятие "Мотор" (ФГУП "НПП "Мотор") | Элемент стенки жаровой трубы камеры сгорания |
| US7010921B2 (en) * | 2004-06-01 | 2006-03-14 | General Electric Company | Method and apparatus for cooling combustor liner and transition piece of a gas turbine |
| FR2893389B1 (fr) * | 2005-11-15 | 2008-02-08 | Snecma Sa | Paroi transversale de chambre de combustion munie de trous de multiperforation |
| DE102007050664A1 (de) * | 2007-10-24 | 2009-04-30 | Man Turbo Ag | Brenner für eine Strömungsmaschine, Leitblech für einen derartigen Brenner sowie eine Strömungsmaschine mit einem derartigen Brenner |
| US8245514B2 (en) * | 2008-07-10 | 2012-08-21 | United Technologies Corporation | Combustion liner for a gas turbine engine including heat transfer columns to increase cooling of a hula seal at the transition duct region |
| DE102009046066A1 (de) * | 2009-10-28 | 2011-05-12 | Man Diesel & Turbo Se | Brenner für eine Turbine und damit ausgerüstete Gasturbine |
| US9416970B2 (en) * | 2009-11-30 | 2016-08-16 | United Technologies Corporation | Combustor heat panel arrangement having holes offset from seams of a radially opposing heat panel |
| RU2461780C1 (ru) * | 2011-05-13 | 2012-09-20 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Камера сгорания непрерывного действия |
| US9057523B2 (en) * | 2011-07-29 | 2015-06-16 | United Technologies Corporation | Microcircuit cooling for gas turbine engine combustor |
| US8910378B2 (en) | 2012-05-01 | 2014-12-16 | United Technologies Corporation | Method for working of combustor float wall panels |
| US9528702B2 (en) * | 2014-02-21 | 2016-12-27 | General Electric Company | System having a combustor cap |
| US9528704B2 (en) | 2014-02-21 | 2016-12-27 | General Electric Company | Combustor cap having non-round outlets for mixing tubes |
| FR3064050B1 (fr) * | 2017-03-14 | 2021-02-19 | Safran Aircraft Engines | Chambre de combustion d'une turbomachine |
| FR3111414B1 (fr) * | 2020-06-15 | 2022-09-02 | Safran Helicopter Engines | Production par fabrication additive de pièces complexes |
| GB202211589D0 (en) * | 2022-08-09 | 2022-09-21 | Rolls Royce Plc | A combustor assembly |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH268524A (de) * | 1947-10-02 | 1950-05-31 | Ernst Nyrop Johan | Zerstäubungsanlage. |
| IL42390A0 (en) * | 1972-08-02 | 1973-07-30 | Gen Electric | Impingement cooled combustor dome |
| FR2312654A1 (fr) * | 1975-05-28 | 1976-12-24 | Snecma | Perfectionnements aux chambres de combustion pour moteurs a turbine a gaz |
| GB1550368A (en) * | 1975-07-16 | 1979-08-15 | Rolls Royce | Laminated materials |
| US4184326A (en) * | 1975-12-05 | 1980-01-22 | United Technologies Corporation | Louver construction for liner of gas turbine engine combustor |
| DE2723546A1 (de) * | 1977-05-25 | 1978-11-30 | Motoren Turbinen Union | Brennkammer, insbesondere ringumkehrbrennkammer fuer gasturbinentriebwerke |
| US4180974A (en) * | 1977-10-31 | 1980-01-01 | General Electric Company | Combustor dome sleeve |
| GB2020370B (en) * | 1978-03-04 | 1982-06-09 | Lucas Industries Ltd | Combustion assembly |
| GB2087065B (en) * | 1980-11-08 | 1984-11-07 | Rolls Royce | Wall structure for a combustion chamber |
| DE3143994A1 (de) * | 1981-11-05 | 1983-05-11 | Bayer Ag, 5090 Leverkusen | Verfahren zur herstellung von duennwandigen gegenstaenden aus thermoplastischen polyurethanen oder polyurethanharnstoffen durch extrusion |
| JPH0660740B2 (ja) * | 1985-04-05 | 1994-08-10 | 工業技術院長 | ガスタービンの燃焼器 |
-
1987
- 1987-05-06 GB GB8710647A patent/GB2204672B/en not_active Expired - Fee Related
-
1988
- 1988-04-19 US US07/183,098 patent/US4864827A/en not_active Expired - Fee Related
- 1988-04-29 FR FR8805826A patent/FR2614973B1/fr not_active Expired - Fee Related
- 1988-05-03 IT IT20431/88A patent/IT1217476B/it active
- 1988-05-05 DE DE3815382A patent/DE3815382C2/de not_active Expired - Fee Related
- 1988-05-06 JP JP63110259A patent/JPS63311024A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| GB2204672A (en) | 1988-11-16 |
| IT1217476B (it) | 1990-03-22 |
| FR2614973B1 (fr) | 1994-03-25 |
| GB2204672B (en) | 1991-03-06 |
| FR2614973A1 (fr) | 1988-11-10 |
| GB8710647D0 (en) | 1988-06-08 |
| JPS63311024A (ja) | 1988-12-19 |
| US4864827A (en) | 1989-09-12 |
| DE3815382A1 (de) | 1988-11-24 |
| DE3815382C2 (de) | 2000-02-10 |
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