Zucca et al., 2015 - Google Patents
Enlarging fuel flexibility for Frame 5 DLN: combustor operability and emissions with high C2+ contentZucca et al., 2015
- Document ID
- 9966541306938332208
- Author
- Zucca A
- Forte A
- Giannini N
- Romano C
- Modi R
- Publication year
- Publication venue
- Turbo Expo: Power for Land, Sea, and Air
External Links
Snippet
Fuel flexibility is a key feature for Dry Low NOx (DLN) combustors, which shall be capable of accepting a wider range of fuel compositions to meet more and more challenging requests from the Oil and Gas market segment (upstream and downstream applications). Non …
- 239000000446 fuel 0 title abstract description 80
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/346—Feeding into different combustion zones for staged combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
- F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/36—Supply of different fuels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/14—Special features of gas burners
- F23D2900/14004—Special features of gas burners with radially extending gas distribution spokes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2209/00—Safety arrangements
- F23D2209/10—Flame flashback
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N5/00—Systems for controlling combustion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/40—Control of fuel supply specially adapted to the use of a special fuel or a plurality of fuels
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP6050821B2 (en) | Combustor and method for supplying fuel to combustor | |
Patel et al. | Effect of hydrogen enrichment on combustion characteristics of methane swirling and non-swirling inverse diffusion flame | |
Alkabie et al. | Lean low NOx primary zones using radial swirlers | |
Therkelsen et al. | Parametric study of low-swirl injector geometry on its operability | |
Liu et al. | Industrial gas turbine engine response and combustion performance to fuel changeovers in compositions and heating values | |
Lam et al. | Hydrogen enriched combustion testing of Siemens SGT-400 at high pressure conditions | |
Cerutti et al. | Hydrogen fueled dry low NOx gas turbine combustor conceptual design | |
Magnusson et al. | Operation of SGT-600 (24 MW) DLE gas turbine with over 60% H2 in natural gas | |
Zucca et al. | Enlarging fuel flexibility for Frame 5 DLN: combustor operability and emissions with high C2+ content | |
Alabaş | Effect of biogas addition on combustion instability of propane flame at different external acoustic enforcement frequencies | |
Snyder et al. | Emission and performance of a lean-premixed gas fuel injection system for aeroderivative gas turbine engines | |
Mohammad et al. | Hydrogen Enrichment Impact on Gas Turbine Combustion Characteristics | |
Nazeer et al. | Full scale testing of a low swirl fuel injector concept for ultra-low NOx gas turbine combustion systems | |
Andersson et al. | Extended fuel flexibility testing of Siemens industrial gas turbines: A novel approach | |
York et al. | Premixed pilot flames for improved emissions and flexibility in a heavy duty gas turbine combustion system | |
Hubbard et al. | Extension of Fuel Flexibility for Siemens Energy SGT-300-2S Dry Low Emission Combustion System | |
Bonaldo et al. | Engine testing using highly reactive fuels on Siemens industrial gas turbines | |
Liu et al. | Effect of change in fuel compositions and heating value on ignition and performance for Siemens SGT-400 dry low emission combustion system | |
Hubbard et al. | Reduction of burner variants for differing fuel compositions by combining intelligent control methods and experimental data of siemens SGT-400 dry low emission combustion system | |
Liu et al. | Extension of fuel flexibility in the Siemens dry low emissions SGT-300-1S to cover a Wobbe Index range of 15 to 49 Mj/m3 | |
Liu et al. | Effect of change in fuel compositions and heating value on ignition and performance for Siemens SGT-400 dry low emission combustion system | |
Rodrigues et al. | Development and Performance of a Perforated Plate Burner under Relevant Gas Turbine Engine Conditions. | |
Sigfrid et al. | Experimental investigations of lean stability limits of a prototype syngas burner for low calorific value gases | |
Liu et al. | Extension of Fuel Flexibility on Dry Low Emission Combustion System–from Medium to High Calorific Value Fuels and H2 Enriched Natural Gas | |
Popovic et al. | Fuel flexibility with low emissions in heavy duty industrial gas turbines |