JPS5640027A - Combustor for gas turbine - Google Patents
Combustor for gas turbineInfo
- Publication number
- JPS5640027A JPS5640027A JP11295779A JP11295779A JPS5640027A JP S5640027 A JPS5640027 A JP S5640027A JP 11295779 A JP11295779 A JP 11295779A JP 11295779 A JP11295779 A JP 11295779A JP S5640027 A JPS5640027 A JP S5640027A
- Authority
- JP
- Japan
- Prior art keywords
- inner sleeve
- combustion
- caused
- tabulator
- 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.)
- Pending
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
PURPOSE: To minimize wear of a cap collar for an inner sleeve and a tabulator for a fuel nozzle of a gas-turbine combustor and thereby to eliminate occurrence of accidents due to increase of the gap between the cap collar and the tabulator.
CONSTITUTION: Fuel sprayed into an inner case 10 from a combustion nozzle 11 is mixed with compressed air 4 supplied from a compressor 1 and ignited anc combusted by an ignition plug 12. When combustion of fuel is started, vibration due to combustion is preduced so that pressure fluctuation is caused in inner sleeve 10. Here, since the inner sleeve 10 is fixed firmly to an outer-case cover 9 by means of a support plate 13, vibration of inner sleeve 10 is not caused if fluctuation of pressure due to combustion is caused in inner sleeve 10. Thus, in accordance with the arrangement of this invention, the top of an inner sleeve of a combustor is fixed firmly to the outer-case cover by means of a support plate. Therefore, it is enabled to minimize wear caused between the inner surface of a cap collar and a tabulator for a fuel nozzle.
COPYRIGHT: (C)1981,JPO&Japio
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11295779A JPS5640027A (en) | 1979-09-05 | 1979-09-05 | Combustor for gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11295779A JPS5640027A (en) | 1979-09-05 | 1979-09-05 | Combustor for gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5640027A true JPS5640027A (en) | 1981-04-16 |
Family
ID=14599759
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11295779A Pending JPS5640027A (en) | 1979-09-05 | 1979-09-05 | Combustor for gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5640027A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009047409A (en) * | 2007-08-14 | 2009-03-05 | General Electric Co <Ge> | Combustion liner stopper in gas turbine |
| CN103363548A (en) * | 2012-04-05 | 2013-10-23 | 通用电气公司 | System and method for supporting fuel nozzles inside a combustor |
| FR3081494A1 (en) * | 2018-05-28 | 2019-11-29 | Safran Aircraft Engines | GAS TURBOMACHINE COMBUSTION MODULE WITH BOTTOM BOTTOM |
-
1979
- 1979-09-05 JP JP11295779A patent/JPS5640027A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009047409A (en) * | 2007-08-14 | 2009-03-05 | General Electric Co <Ge> | Combustion liner stopper in gas turbine |
| CN103363548A (en) * | 2012-04-05 | 2013-10-23 | 通用电气公司 | System and method for supporting fuel nozzles inside a combustor |
| CN103363548B (en) * | 2012-04-05 | 2016-12-28 | 通用电气公司 | For supporting the system and method for burner fuel nozzle |
| FR3081494A1 (en) * | 2018-05-28 | 2019-11-29 | Safran Aircraft Engines | GAS TURBOMACHINE COMBUSTION MODULE WITH BOTTOM BOTTOM |
| EP3575689A1 (en) * | 2018-05-28 | 2019-12-04 | Safran Aircraft Engines | Gas turbine engine combustion module with chamber bottom abutment |
| US11725822B2 (en) | 2018-05-28 | 2023-08-15 | Safran Aircraft Engines | Combustion module for a gas turbo engine with chamber bottom stop |
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