JP2015129490A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2015129490A5 JP2015129490A5 JP2014001977A JP2014001977A JP2015129490A5 JP 2015129490 A5 JP2015129490 A5 JP 2015129490A5 JP 2014001977 A JP2014001977 A JP 2014001977A JP 2014001977 A JP2014001977 A JP 2014001977A JP 2015129490 A5 JP2015129490 A5 JP 2015129490A5
- Authority
- JP
- Japan
- Prior art keywords
- water
- supply
- combustor
- combustor according
- nozzle
- 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.)
- Granted
Links
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 11
- 239000000446 fuel Substances 0.000 claims 2
- 239000008400 supply water Substances 0.000 claims 1
Claims (7)
複数の前記ノズルの全部または一部に接続されて各々の燃料配管に水を供給する水供給手段を備え、
前記水供給手段は、供給する水の量を供給される前記ノズル毎に可変とすることを特徴とする燃焼器。 In a combustor with multiple nozzles that supply fuel,
Water supply means connected to all or part of the plurality of nozzles to supply water to each fuel pipe;
The said water supply means makes variable the quantity of the water to supply for every said nozzle supplied.
水の供給量を可変する供給量可変部と、
燃焼器運転状況に応じた水の供給量が設定された水供給情報を予め記憶され、前記燃焼器運転状況と前記水供給情報とに基づき前記供給量可変部を制御する制御部と、
を備えることを特徴とする請求項1〜5のいずれか一つに記載の燃焼器。 The water supply means
A supply amount variable section for changing the supply amount of water;
Water supply information in which the amount of water supplied according to the combustor operation status is set in advance, and a control unit that controls the supply amount variable unit based on the combustor operation status and the water supply information;
The combustor according to any one of claims 1 to 5, further comprising:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014001977A JP6193131B2 (en) | 2014-01-08 | 2014-01-08 | Combustor and gas turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014001977A JP6193131B2 (en) | 2014-01-08 | 2014-01-08 | Combustor and gas turbine |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2015129490A JP2015129490A (en) | 2015-07-16 |
JP2015129490A5 true JP2015129490A5 (en) | 2016-07-21 |
JP6193131B2 JP6193131B2 (en) | 2017-09-06 |
Family
ID=53760377
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2014001977A Active JP6193131B2 (en) | 2014-01-08 | 2014-01-08 | Combustor and gas turbine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP6193131B2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP7171496B2 (en) * | 2019-04-05 | 2022-11-15 | 三菱重工業株式会社 | Combustor and gas turbine |
JP7446077B2 (en) | 2019-10-04 | 2024-03-08 | 三菱重工業株式会社 | Gas turbine combustor, gas turbine and oil fuel combustion method |
JP7307701B2 (en) * | 2020-05-01 | 2023-07-12 | 三菱重工業株式会社 | gas turbine combustor |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0915406B1 (en) * | 1997-11-10 | 2003-05-07 | ALSTOM (Switzerland) Ltd | Method for monitoring the supply system of a gas turbine with a plurality of burners and device for carrying out this method |
JPH11350978A (en) * | 1998-06-08 | 1999-12-21 | Mitsubishi Heavy Ind Ltd | Fuel nozzle purging device |
JP2005195284A (en) * | 2004-01-08 | 2005-07-21 | Mitsubishi Heavy Ind Ltd | Fuel nozzle for gas turbine, combuster for gas turbine and combustion method of combuster for gas turbine |
JP2008031847A (en) * | 2006-07-26 | 2008-02-14 | Hitachi Ltd | Gas turbine combustor, its operating method, and modification method of gas turbine combustor |
US8631656B2 (en) * | 2008-03-31 | 2014-01-21 | General Electric Company | Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities |
US8973366B2 (en) * | 2011-10-24 | 2015-03-10 | General Electric Company | Integrated fuel and water mixing assembly for use in conjunction with a combustor |
-
2014
- 2014-01-08 JP JP2014001977A patent/JP6193131B2/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP2014040999A5 (en) | ||
JP2011220669A5 (en) | ||
WO2015116287A3 (en) | Multi-swirler fuel/air mixer with centralized fuel injection | |
JP2013231580A5 (en) | ||
JP2019508651A5 (en) | ||
JP2013181746A5 (en) | ||
JP2014040998A5 (en) | ||
CL2018003189A1 (en) | Biorenewable kerosene, fuel for aviation turbines, fuel mixture for aviation turbines, and manufacturing method. | |
JP2014173841A5 (en) | ||
JP2014163664A5 (en) | ||
GB2557599B (en) | Gas turbine engine fuel supply system having de-priming and re-priming sub-systems | |
EP2634487A3 (en) | System and method for reducing combustion dynamics in a combustor | |
EP2662624A3 (en) | System for supplying a working fluid to a combustor | |
JP2014153052A5 (en) | ||
GB2557602B (en) | Gas turbine engine fuel supply system having de-priming and re-priming ecology valve | |
JP2013148345A5 (en) | ||
WO2014099075A3 (en) | Gas turbine engine asymmetric fuel nozzle combustor | |
JP2015129490A5 (en) | ||
NO20200866A1 (en) | Self-Regulating Turbine Flow | |
CL2015000330A1 (en) | Oxygen lance characterized in that it has at least three tubes arranged coaxially with each other and that delimit at least one annular groove, the outermost tube for the passage of superheated steam being made and presenting a steam supply point, the central tube being made as an annular groove, the innermost tube being made for the passage of hot oxygen with a maximum temperature of 180 ° C and presenting an oxygen supply point. | |
GB201811512D0 (en) | Fuel nozzle for a gas turbine engine | |
JP2015090229A5 (en) | ||
WO2013126125A3 (en) | Radial inflow gas turbine engine with advanced transition duct | |
CH707575A8 (en) | Combustion chamber with aerodynamic struts. | |
HUE056819T2 (en) | A radial flow gas turbine generator |