FR2384950A1 - Insulated combustor for gas turbine - has floating ceramic tube between flame pipe and downstream intermediate section - Google Patents
Insulated combustor for gas turbine - has floating ceramic tube between flame pipe and downstream intermediate sectionInfo
- Publication number
- FR2384950A1 FR2384950A1 FR7808733A FR7808733A FR2384950A1 FR 2384950 A1 FR2384950 A1 FR 2384950A1 FR 7808733 A FR7808733 A FR 7808733A FR 7808733 A FR7808733 A FR 7808733A FR 2384950 A1 FR2384950 A1 FR 2384950A1
- Authority
- FR
- France
- Prior art keywords
- ceramic tube
- gas turbine
- intermediate section
- tube
- combustor
- 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.)
- Withdrawn
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
- F23R3/005—Combined with pressure or heat exchangers
-
- 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
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
The gas turbine combustor ensures optimum cooling of its metal parts and uses a floating ceramic tube for the zone of max. temp. to enhance the service life. It is applicable to units with a heat exchanger where a portion of the air from the compressor is diverted for cooling. The flame tube (2) forms a ring chamber (3) with the outside housing, for admitting preheated air from the compressor and exchanger. The head (7) of the tube is set in the plenum chamber (8) with its fuel injecting nozzle (6) receiving the cooled air via a port (9). The flame tube is linked to the intermediate section by the floating ceramic tube protected by refractory pads.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19772713414 DE2713414A1 (en) | 1977-03-26 | 1977-03-26 | COMBUSTION CHAMBER FOR GAS TURBINE ENGINES |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2384950A1 true FR2384950A1 (en) | 1978-10-20 |
Family
ID=6004756
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7808733A Withdrawn FR2384950A1 (en) | 1977-03-26 | 1978-03-24 | Insulated combustor for gas turbine - has floating ceramic tube between flame pipe and downstream intermediate section |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS53120011A (en) |
DE (1) | DE2713414A1 (en) |
FR (1) | FR2384950A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1777461A2 (en) * | 2005-10-20 | 2007-04-25 | United Technologies Corporation | Attachment of a ceramic combustor can |
EP2927593A1 (en) * | 2014-03-31 | 2015-10-07 | Siemens Aktiengesellschaft | Silo combustion chamber for a gas turbine |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS57154856U (en) * | 1981-03-19 | 1982-09-29 | ||
US4471623A (en) * | 1982-10-15 | 1984-09-18 | The United States Of America As Represented By The Secretary Of The Air Force | Combustion chamber floatwall panel attachment arrangement |
US4686823A (en) * | 1986-04-28 | 1987-08-18 | United Technologies Corporation | Sliding joint for an annular combustor |
US6397603B1 (en) * | 2000-05-05 | 2002-06-04 | The United States Of America As Represented By The Secretary Of The Air Force | Conbustor having a ceramic matrix composite liner |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2163822A1 (en) * | 1971-01-11 | 1972-07-20 | Gen Motors Corp | Gas turbine engine |
US3880575A (en) * | 1974-04-15 | 1975-04-29 | Gen Motors Corp | Ceramic combustion liner |
DE7430508U (en) * | 1976-06-10 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Gas turbine engine with heat exchanger |
-
1977
- 1977-03-26 DE DE19772713414 patent/DE2713414A1/en active Pending
-
1978
- 1978-03-24 FR FR7808733A patent/FR2384950A1/en not_active Withdrawn
- 1978-03-27 JP JP3525078A patent/JPS53120011A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE7430508U (en) * | 1976-06-10 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Gas turbine engine with heat exchanger | |
DE2163822A1 (en) * | 1971-01-11 | 1972-07-20 | Gen Motors Corp | Gas turbine engine |
US3880575A (en) * | 1974-04-15 | 1975-04-29 | Gen Motors Corp | Ceramic combustion liner |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1777461A2 (en) * | 2005-10-20 | 2007-04-25 | United Technologies Corporation | Attachment of a ceramic combustor can |
EP1777461A3 (en) * | 2005-10-20 | 2010-08-25 | United Technologies Corporation | Attachment of a ceramic combustor can |
EP2927593A1 (en) * | 2014-03-31 | 2015-10-07 | Siemens Aktiengesellschaft | Silo combustion chamber for a gas turbine |
WO2015150098A1 (en) * | 2014-03-31 | 2015-10-08 | Siemens Aktiengesellschaft | Silo combustion chamber for a gas turbine |
Also Published As
Publication number | Publication date |
---|---|
JPS53120011A (en) | 1978-10-20 |
DE2713414A1 (en) | 1978-09-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RE | Withdrawal of published application |