FLAMEHOLDER FOR A REHEAT ASSEMBLYThere is provided a flameholder (370) for a reheat assembly (300) of a gas turbine engine (10). The flameholder comprises a fuel atomizer (379A, 379B), an air passageway (375A, 375B) and a fuel passag…DRIVE·4d ago·1 min readFollowF02C3/14ROLLS ROYCE PLC [GB]
GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLYA combustion section (114) defines an axial direction, a radial direction, and a circumferential direction. The combustion section (114) includes a casing (400) that defines a diffusion chamber (406).…DRIVE·Mar 11·1 min readFollowF02C3/14GEN ELECTRIC [US]
METHOD FOR OPERATING A GAS TURBINE ASSEMBLY FOR A POWER PLANT AND GAS TURBINE ASSEMBLY FOR A POWER PLANTA method for operating a gas turbine assembly for a power plant comprises the steps of:- providing a gas turbine assembly (1) comprising a compressor (2), a combustor assembly (4), a turbine (5) and a…DRIVE·Mar 11·1 min readFollowF02C3/14ANSALDO ENERGIA SWITZERLAND AG [CH]
GAS TURBINE ENGINE WITH SELECTED COMBUSTOR OUTLET TEMPERATURE MEASUREMENTS AND A METHOD OF OPERATING A GAS TURBINE ENGINEA gas turbine engine includes a combustor assembly (5) having a plurality of can combustor units (8) and a control unit (20). Each combustor unit (8) has a first-stage combustor (12), a second-stage c…DRIVE·Feb 18·2 min readFollowF02C3/14ANSALDO ENERGIA SWITZERLAND AG [CH]
GAS TURBINE ENGINEA gas turbine engine includes an annular combustion chamber (7) and a plurality of combustors (6) communicating with the annular combustion chamber (7). Each combustor (6) defines a respective gas flo…DRIVE·Feb 18·1 min readFollowF02C3/14ANSALDO ENERGIA SWITZERLAND AG [CH]
GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLYA combustion section (114) defines an axial direction, a radial direction, and a circumferential direction. The combustion section (114) includes a casing (400) that defines a diffusion chamber (406).…DRIVE·Nov 26·2 min readFollowF02C3/14GEN ELECTRIC [US]
HYDROGEN POWERED GEARED TURBO FAN ENGINE WITH AN OFF-SET REDUCED COREAn aircraft propulsion system includes a fan shaft (410) connected to a fan (406) and defining a centerline axis (404) of the aircraft propulsion system (400), one or more offset cores (402) arranged …DRIVE·Oct 8·1 min readFollowF02C3/14RTX CORP [US]
SYSTEM AND METHODS FOR IGNITING AND OPERATING A GAS TURBINE ENGINE WITH ALTERNATIVE FUELSA power generation system (100) includes a combustion system (108), a liquid supply system (104), and a vapor supply system (106). The combustion system (108) is configured to generate power by combus…DRIVE·Feb 19·1 min readFollowF02C3/14GENERAL ELECTRIC TECHNOLOGY GMBH [CH]
INTEGRATED FUEL CELL AND ENGINE COMBUSTOR ASSEMBLYAn engine assembly (500) comprises a combustor (510), a fuel cell stack (520) integrated with the combustor (510) wherein the fuel cell stack (520) is configured to direct fuel and air exhaust (522) f…DRIVE·Dec 4·1 min readFollowF02C3/14GEN ELECTRIC [US]
FLUID MONITORING SYSTEMA fluid monitoring system includes a controller (130) configured to determine that a value of at least one fluid property of a fluid is greater than a threshold value, and to control actuators to iden…DRIVE·Jun 26·2 min readFollowF02C3/14GENERAL ELECTRIC TECHNOLOGY GMBH [CH]
COMBUSTOR ARRANGEMENTA combustor arrangement (100) includes a fuel injector (114), and a seal (200, 1300) arranged around the fuel injector (114) and having an upstream end (202, 1302) and a downstream end (204, 1304). Th…DRIVE·Jun 26·2 min readFollowF02C3/14ROLLS ROYCE PLC [GB]
METHOD FOR OPERATING A GAS TURBINE ASSEMBLY AND GAS TURBINE ASSEMBLYA gas turbine assembly (1) extends along a longitudinal axis (A) and comprises a compressor (2), a combustor assembly (4) and at least one gas turbine (5); the compressor (2) comprising an inlet (9) s…DRIVE·Apr 3·1 min readFollowF02C3/14ANSALDO ENERGIA SWITZERLAND AG [CH]
GAS TURBINE FOR POWER PLANT COMPRISING A DAMPING DEVICEA gas turbine for power plant; the gas turbine (1) having an axis (9) and comprising: a compressor sector (2) for compressing ambient air; a combustor sector (4) for mixing and combusting the compress…DRIVE·Aug 30·2 min readFollowF02C3/14ANSALDO ENERGIA SWITZERLAND AG [CH]
GAS TURBINE FOR POWER PLANT APPLICATIONS WITH PRE-HEATED FUEL GAS AND METHOD FOR OPERATING THIS GAS TURBINEA gas turbine assembly for power plant application fed by pre-heated fuel gas; the gas turbine comprises: a compressor configured for compressing incoming air; a sequential combustor assembly configur…DRIVE·Jun 14·2 min readFollowF02C3/14ANSALDO ENERGIA SWITZERLAND AG [CH]
INTEGRATED FRONT PANEL FOR A BURNER OF A GAS TURBINE ENGINEA gas turbine engine (10) includes a compressor (14) and a turbine (26) with a burner (22) and a combustor (24) between the compressor (14) and the turbine (26). The burner (22) is downstream of the c…DRIVE·Dec 28·1 min readFollowF02C3/14GEN ELECTRIC [US]
METHOD OF CONFIGURING A COMBUSTORThis burner comprises a burner outer cylinder, a cylindrical burner inner cylinder provided inside the burner outer cylinder, a compressed air flow channel demarcated between the burner outer cylinder…DRIVE·Nov 12·1 min readFollowF02C3/14MITSUBISHI HITACHI POWER SYS [JP]
Can-annular gas turbine unit with staged premix-combustionThe invention concerns a gas turbine system, comprising a compressor, at least one combustion chamber (10), and eventually a secondary combustion chamber, for generating working gas. An intermediate t…DRIVE·Jan 15·1 min readFollowF02C3/14ALSTOM TECHNOLOGY LTD [CH]
System and method for conditioning a working fluid in a combustorA system for conditioning a working fluid in a combustor includes a primary combustion chamber (20), a liner (18) circumferentially surrounding the primary combustion chamber (20), and a primary nozzl…DRIVE·Mar 20·2 min readFollowF02C3/14GEN ELECTRIC [US]
Turbomachine with detonation chamber and aircraft provided with such a turbomachineThe turbomachine (1) has a continuous detonation wave engine (6) provided with an annular detonation chamber (7), and a fuel injection system (8) and a priming unit (9) for continuous production of ho…DRIVE·Nov 21·1 min readFollowF02C3/14MBDA FRANCE [FR]
Damping device for damping pressure oscillations within a combustion chamber of a turbineA damping device (122; 222; 322; 422; 522) for damping pressure oscillations within a combustion chamber (106; 206; 306; 406; 506) of a turbine (102; 202; 302; 402; 402; 502) comprises a radially exte…DRIVE·Dec 21·1 min readFollowF02C3/14SIEMENS AG [DE]
InjectorA turbine containing system (10) is disclosed. The system includes an intake section (14), a compressor section (16) downstream from the intake section (14), a combustor section (20) having a primary …DRIVE·Jun 23·1 min readFollowF02C3/14GEN ELECTRIC [US]
