| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
|---|
| 03/03/2004 | EP1394471A1 Burner |
| 03/03/2004 | EP1394470A2 Multiple-domes annular combustor for a gas turbine engine |
| 03/03/2004 | EP1394389A1 Improved heat exchanger for power generation equipment |
| 03/03/2004 | EP1394386A1 Process for combusting fuels, in particular gas in an oxidizer of high temperature |
| 03/03/2004 | CN1478993A Improved heat exchanger of generating equipment |
| 03/03/2004 | CN1140722C Air jet engine with rotating combustion chamber with specific heat converting effect |
| 03/02/2004 | US6698209 Method of and appliance for suppressing flow eddies within a turbomachine |
| 03/02/2004 | US6698208 Atomizer for a combustor |
| 03/02/2004 | US6698207 Flame-holding, single-mode nozzle assembly with tip cooling |
| 03/02/2004 | US6698206 Combustion chamber |
| 02/26/2004 | US20040038086 Thermal barrier coatings with low thermal conductivity |
| 02/26/2004 | US20040038085 Heat resistant layer is made of a mixed oxide containing 15 mol % of at least one lanthanide sesquioxide, selected from LA, Pr, Nd, Sm, Eu, Tb and mixtures, and balance oxide selected from zirconia, ceria, and hafnia |
| 02/26/2004 | US20040037673 Hay bale carrier |
| 02/26/2004 | US20040037162 Vortex generator with controlled wake flow |
| 02/26/2004 | US20040036230 Sealing structure for combustor liner |
| 02/26/2004 | US20040035386 Fuel injection apparatus |
| 02/26/2004 | US20040035115 Combustor dome for gas turbine engine |
| 02/26/2004 | US20040035114 Gas turbine combustor, combustion method of the gas turbine combustor, and method of remodeling a gas turbine combustor |
| 02/25/2004 | EP1391657A2 Gas turbine combustor, combustion method of the gas turbine combustor, and method of remodeling a gas turbine combustor |
| 02/25/2004 | EP1391652A2 Fuel injection apparatus |
| 02/25/2004 | EP1391582A2 Sealing structure for combustor liner |
| 02/25/2004 | EP1390670A1 Heat shield arrangement for a hot-gas conducting component, in particular for structural pieces of gas turbines and method for production of said arrangement |
| 02/25/2004 | CN1477230A Hign temp-resistant article and its mfg. method |
| 02/24/2004 | US6695234 Liquid fuel injection nozzles |
| 02/24/2004 | US6694745 Method for running up a gas turbine plant |
| 02/19/2004 | WO2004015332A1 Premixed exit ring pilot burner |
| 02/19/2004 | WO2002059238A9 Sub-critical water-fuel composition and combustion system |
| 02/19/2004 | US20040032089 Combustion chamber sealing ring, and a combustion chamber including such a ring |
| 02/19/2004 | DE10233161A1 Burner with pilot burner for creating heat has cavity between swirler and combustion chamber |
| 02/18/2004 | EP1389714A1 Combustion chamber for gas turbine |
| 02/18/2004 | EP1389713A1 Premixed exit ring pilot burner |
| 02/18/2004 | EP1389690A1 Screw interiorly cooled |
| 02/17/2004 | US6691518 Process for the operation of an annular combustion chamber, and annular combustion chamber |
| 02/17/2004 | US6691516 Fully premixed secondary fuel nozzle with improved stability |
| 02/17/2004 | US6691515 Dry low combustion system with means for eliminating combustion noise |
| 02/12/2004 | WO2004013538A2 Porous burner for gas turbine applications |
| 02/12/2004 | WO2004013465A1 Thermally free aft frame for a transition duct |
| 02/12/2004 | US20040029058 Method and appliance for supplying fuel to a premixiing burner |
| 02/12/2004 | US20040025514 Gas turbine and method for damping oscillations of an annular combustion chamber |
| 02/12/2004 | US20040025512 Performance enhanced control of DLN gas turbines |
| 02/12/2004 | US20040025508 Multimode system for injecting an air/fuel mixture into a combustion chamber |
| 02/11/2004 | EP1387986A1 Device and method for injecting a liquid fuel in an air flow for a combustion chamber |
| 02/10/2004 | US6688534 Air assist fuel nozzle |
| 02/10/2004 | US6688111 Method for operating a combustion chamber |
| 02/10/2004 | US6688110 Air impingement cooling system |
| 02/10/2004 | US6688109 Turbine engine burner |
| 02/10/2004 | US6688107 Gas turbine combustion device |
| 02/05/2004 | US20040024516 Automatic mapping logic for a combustor in a gas turbine engine |
| 02/05/2004 | US20040021235 Fuel-air premixing system for a catalytic combustor |
| 02/05/2004 | US20040020212 Plate-like body connecting method, connected body, tail pipe for gas turbine combustor, and gas turbine combustor |
| 02/05/2004 | US20040020211 Trapped vortex combustor |
| 02/05/2004 | US20040020210 Fuel injection nozzle for gas turbine combustor, gas turbine combustor, and gas turbine |
| 02/05/2004 | US20040020209 Gas turbine combustor and combustion control method thereof |
| 02/05/2004 | US20040020208 Fluidic control of fuel flow |
| 02/05/2004 | DE10330023A1 Vortex generator used in the swirling and mixing of fuel/air mixtures in pre-mixing combustion chambers comprises an outlet opening for targeted introduction of a secondary flow into the core flow of the wake produced |
| 02/05/2004 | DE10233805A1 Ringförmige Brennkammer für eine Gasturbine Annular combustor for a gas turbine |
| 02/04/2004 | EP1387062A2 Method/system for mapping a combustor in a gas turbine engine |
| 02/04/2004 | EP1385610A1 Delivery system for liquid catalysts |
| 02/04/2004 | CN1137341C Premixing burner for heat generator |
| 02/03/2004 | US6684642 Gas turbine engine having a multi-stage multi-plane combustion system |
| 02/03/2004 | US6684641 Fluid distributor, burner device, gas turbine engine, and cogeneration system |
| 02/03/2004 | US6684640 Gas turbine engine combustion system |
| 02/03/2004 | US6684620 Combustion chamber arrangement for gas turbines |
| 01/29/2004 | WO2004010050A1 Process for combustion of a liquid hydrocarbon |
| 01/29/2004 | CA2493912A1 Process for combustion of a liquid hydrocarbon |
| 01/28/2004 | EP1384950A2 Annular combustion chamber for a gas turbine |
| 01/28/2004 | EP1384033A1 Ultra low nox emissions combustion system for gas turbine engines |
| 01/28/2004 | EP1095228B1 Igniter with porous sleeve |
| 01/27/2004 | US6681578 Combustor liner with ring turbulators and related method |
| 01/27/2004 | US6681577 Method and apparatus for relieving stress in a combustion case in a gas turbine engine |
| 01/22/2004 | US20040011059 Combustion-chamber arrangement |
| 01/22/2004 | US20040011058 Annular combustion chamber with two offset heads |
| 01/22/2004 | US20040011056 Design and control strategy for catalytic combustion system with a wide operating range |
| 01/22/2004 | US20040011055 Gas turbine combustor, pre-mixer for turbine combustors and premixing method for gas turbine combustors |
| 01/22/2004 | US20040011054 Gas turbine combustor and operating method thereof |
| 01/22/2004 | US20040011053 Gas-turbine engine control system |
| 01/22/2004 | US20040011044 Method for increasing heat transfer from combustors |
| 01/22/2004 | US20040011043 Diffuser for gas turbine engine |
| 01/22/2004 | US20040011042 Gas-turbine engine combustor |
| 01/22/2004 | US20040011041 Gas-turbine engine combustor |
| 01/22/2004 | US20040011021 Gas-turbine engine combustor |
| 01/22/2004 | US20040011020 Gas turbine control apparatus and gas turbine system using the same |
| 01/22/2004 | DE10325691A1 Wiederaufheizverbrennungssystem für eine Gasturbine Wiederaufheizverbrennungssystem for a gas turbine |
| 01/21/2004 | EP1382379A2 Vortex generator with controlled downstream flowpattern |
| 01/21/2004 | EP1381813A1 Gas turbine with combined can-type and annular combustor and method of operating a gas turbine |
| 01/21/2004 | EP1381812A1 Turbine premixing combustor |
| 01/21/2004 | EP1381811A1 Combustion chamber, in particular of a gas turbine |
| 01/21/2004 | CN1469792A Process for drilling holes in a metallic workpiece having a thermal barrier coating |
| 01/20/2004 | US6679063 Combustion chamber head for a gas turbine |
| 01/20/2004 | US6679062 Architecture for a combustion chamber made of ceramic matrix material |
| 01/20/2004 | US6679061 Premix burner arrangement for operating a combustion chamber |
| 01/20/2004 | US6678953 Method for making damped combustion cowl structure |
| 01/15/2004 | US20040006995 Low emissions combustor for a gas turbine engine |
| 01/15/2004 | US20040006993 Dual fuel fin mixer secondary fuel nozzle |
| 01/15/2004 | US20040006992 Gas only fin mixer secondary fuel nozzle |
| 01/15/2004 | US20040006991 Fully premixed secondary fuel nozzle with improved stability and dual fuel capability |
| 01/15/2004 | US20040006990 Fully premixed secondary fuel nozzle with improved stability |
| 01/15/2004 | US20040006989 Fully premixed secondary fuel nozzle with dual fuel capability |
| 01/15/2004 | US20040006988 Fully premixed secondary fuel nozzle |
| 01/15/2004 | DE10214570A1 Mischluftloch in Gasturbinenbrennkammer mit Brennkammerschindeln Mixed air hole in gas turbine combustion chamber with combustion chamber shingles |