CA2696994A1 - Bruleur pour une turbomachine, tole de guidage pour un tel bruleur, et turbomachine equipee d'un tel bruleur - Google Patents
Bruleur pour une turbomachine, tole de guidage pour un tel bruleur, et turbomachine equipee d'un tel bruleur Download PDFInfo
- Publication number
- CA2696994A1 CA2696994A1 CA2696994A CA2696994A CA2696994A1 CA 2696994 A1 CA2696994 A1 CA 2696994A1 CA 2696994 A CA2696994 A CA 2696994A CA 2696994 A CA2696994 A CA 2696994A CA 2696994 A1 CA2696994 A1 CA 2696994A1
- Authority
- CA
- Canada
- Prior art keywords
- baffle plate
- burner
- section
- mounting
- elevations
- 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.)
- Abandoned
Links
- 125000006850 spacer group Chemical group 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims description 10
- 238000001816 cooling Methods 0.000 description 9
- 230000008646 thermal stress Effects 0.000 description 8
- 239000002184 metal Substances 0.000 description 7
- 238000003466 welding Methods 0.000 description 5
- 210000001503 joint Anatomy 0.000 description 4
- 239000000446 fuel Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000035882 stress Effects 0.000 description 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
- F23R3/04—Air inlet arrangements
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03042—Film cooled combustion chamber walls or domes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007050664A DE102007050664A1 (de) | 2007-10-24 | 2007-10-24 | Brenner für eine Strömungsmaschine, Leitblech für einen derartigen Brenner sowie eine Strömungsmaschine mit einem derartigen Brenner |
DE102007050664.5 | 2007-10-24 | ||
PCT/EP2008/008936 WO2009053049A1 (fr) | 2007-10-24 | 2008-10-22 | Brûleur pour une turbomachine, tôle de guidage pour un tel brûleur, et turbomachine équipée d'un tel brûleur |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2696994A1 true CA2696994A1 (fr) | 2009-04-30 |
Family
ID=40405029
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2696994A Abandoned CA2696994A1 (fr) | 2007-10-24 | 2008-10-22 | Bruleur pour une turbomachine, tole de guidage pour un tel bruleur, et turbomachine equipee d'un tel bruleur |
Country Status (6)
Country | Link |
---|---|
US (1) | US20100205969A1 (fr) |
EP (1) | EP2201300B1 (fr) |
JP (1) | JP5324588B2 (fr) |
CA (1) | CA2696994A1 (fr) |
DE (1) | DE102007050664A1 (fr) |
WO (1) | WO2009053049A1 (fr) |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH255541A (de) * | 1947-05-12 | 1948-06-30 | Bbc Brown Boveri & Cie | Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen. |
US2625792A (en) * | 1947-09-10 | 1953-01-20 | Rolls Royce | Flame tube having telescoping walls with fluted ends to admit air |
US2544538A (en) * | 1948-12-01 | 1951-03-06 | Wright Aeronautical Corp | Liner for hot gas chambers |
DE825777C (de) * | 1949-08-19 | 1951-12-20 | Canadian Patents Dev | Flammrohr von Brennkammern, insbesondere fuer Gasturbinen |
US3064425A (en) * | 1959-10-05 | 1962-11-20 | Gen Motors Corp | Combustion liner |
US3572031A (en) * | 1969-07-11 | 1971-03-23 | United Aircraft Corp | Variable area cooling passages for gas turbine burners |
US3752225A (en) * | 1970-06-02 | 1973-08-14 | Gen Motors Corp | Duct for hot gas |
US3751910A (en) * | 1972-02-25 | 1973-08-14 | Gen Motors Corp | Combustion liner |
US3854285A (en) * | 1973-02-26 | 1974-12-17 | Gen Electric | Combustor dome assembly |
GB1550368A (en) * | 1975-07-16 | 1979-08-15 | Rolls Royce | Laminated materials |
JPS5556521A (en) * | 1978-10-23 | 1980-04-25 | Hitachi Ltd | Combustion device |
GB2204672B (en) * | 1987-05-06 | 1991-03-06 | Rolls Royce Plc | Combustor |
DE4223733C2 (de) * | 1992-07-18 | 1995-05-18 | Gutehoffnungshuette Man | Verbindung von Mischrohr und Flammrohr einer Gasturbine |
US5704208A (en) * | 1995-12-05 | 1998-01-06 | Brewer; Keith S. | Serviceable liner for gas turbine engine |
GB9623615D0 (en) * | 1996-11-13 | 1997-07-09 | Rolls Royce Plc | Jet pipe liner |
US6199371B1 (en) * | 1998-10-15 | 2001-03-13 | United Technologies Corporation | Thermally compliant liner |
ES2309029T3 (es) * | 2001-01-09 | 2008-12-16 | Mitsubishi Heavy Industries, Ltd. | Camara de combustion de turbina de gas. |
JP3924136B2 (ja) * | 2001-06-27 | 2007-06-06 | 三菱重工業株式会社 | ガスタービン燃焼器 |
US7631481B2 (en) * | 2004-12-01 | 2009-12-15 | United Technologies Corporation | Cooled duct for gas turbine engine |
-
2007
- 2007-10-24 DE DE102007050664A patent/DE102007050664A1/de not_active Withdrawn
-
2008
- 2008-10-22 WO PCT/EP2008/008936 patent/WO2009053049A1/fr active Application Filing
- 2008-10-22 CA CA2696994A patent/CA2696994A1/fr not_active Abandoned
- 2008-10-22 JP JP2010530336A patent/JP5324588B2/ja not_active Expired - Fee Related
- 2008-10-22 US US12/678,323 patent/US20100205969A1/en not_active Abandoned
- 2008-10-22 EP EP08842721.6A patent/EP2201300B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
US20100205969A1 (en) | 2010-08-19 |
WO2009053049A1 (fr) | 2009-04-30 |
EP2201300B1 (fr) | 2015-06-03 |
JP5324588B2 (ja) | 2013-10-23 |
JP2011501098A (ja) | 2011-01-06 |
DE102007050664A1 (de) | 2009-04-30 |
EP2201300A1 (fr) | 2010-06-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0318312B1 (fr) | Cartouche pour la chambre de combustion d' une turbine à gaz | |
US8166764B2 (en) | Flow sleeve impingement cooling using a plenum ring | |
US9383104B2 (en) | Continuous combustion liner for a combustor of a gas turbine | |
KR101044662B1 (ko) | 성형 냉각 홀을 구비한 유출 냉각 전이 덕트 | |
US9423135B2 (en) | Combustor having mixing tube bundle with baffle arrangement for directing fuel | |
CN107592904B (zh) | 受控的防漏燃烧器护环 | |
CN101936532A (zh) | 冷却一件式筒形燃烧器和相关方法 | |
EP3214371B1 (fr) | Ensemble de manchons et procédé de sa fabrication | |
CN107917423B (zh) | 燃烧器壁元件及其制造方法 | |
US8646279B2 (en) | Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamber | |
CN108061309B (zh) | 燃气轮机及其燃烧器 | |
US9366169B2 (en) | Seal for an exhaust aftertreatment device in an internal combustion engine | |
EP2230456A2 (fr) | Chemise de combustion avec embase d'orifice de mélange | |
US8156744B2 (en) | Annular combustion chamber for a gas turbine engine | |
EP2532836A2 (fr) | Chemise de combustion et pièce de transition | |
EP1612478A1 (fr) | Générateur de vapeur à chauffage direct | |
CA2696994A1 (fr) | Bruleur pour une turbomachine, tole de guidage pour un tel bruleur, et turbomachine equipee d'un tel bruleur | |
EP1552218B1 (fr) | Bruleur, notamment bruleur venturi avec tube de chambre de combustion | |
US11480340B2 (en) | Guiding device in a combustion chamber | |
CN108061308B (zh) | 燃气轮机的后火焰燃料喷射装置 | |
US20170023250A1 (en) | Cowling part and combustor assembly for a gas turbine | |
US20150330634A1 (en) | Combustion liner with bias effusion cooling | |
RU2805719C1 (ru) | Жаровая труба камеры сгорания газотурбинного двигателя ДН80 и ДУ80 | |
CN108224475B (zh) | 燃气轮机的燃烧器和该燃气轮机 | |
CA1289368C (fr) | Garniture sur chemisage de chambre de combustion |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Discontinued |
Effective date: 20131022 |