157525 ⎘
Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
Fuel nozzle for a turbine combustor, and methods of forming same
#302Combustion chamber head of a gas turbine
#303Fuel nozzle assembly for a gas turbine engine
#304Burner and Method for Reducing Self-Induced Flame Oscillations
#305Attenuation of combustion dynamics using a Herschel-Quincke filter
#306Resonator assembly for mitigating dynamics in gas turbines
#307Resonating Swirler
#308COMBUSTOR OF GAS TURBINE
#309Damping device and gas turbine combustor
#310Gas Turbine Combustion System
#311Non-rotational stabilization of the flame of a premixing burner
#312SYSTEM AND METHOD FOR SUPPRESSING COMBUSTION INSTABILITY IN A TURBOMACHINE
#313Gas turbine having a combustion oscillation suppressing device
#314Attachment structure of combustion oscillation detecting device
#315FUEL DELIVERY SYSTEM FOR A TURBINE ENGINE
#316Passive noise attenuation system
#317Segmented combustor cap
#318COMBUSTOR SYSTEM AND METHOD OF REDUCING COMBUSTION INSTABILITY AND/OR EMISSIONS OF A COMBUSTOR SYSTEM
#319Forward-section resonator for high frequency dynamic damping
#320COMBUSTOR STRUCTURE
#321Method for reducing emissions from a combustor
#322Combustor with reduced carbon monoxide emissions
#323Combustor dynamic attenuation and cooling arrangement
#324MULTI-TUBE, CAN-ANNULAR PULSE DETONATION COMBUSTOR BASED ENGINE WITH TANGENTIALLY AND LONGITUDINALLY ANGLED PULSE DETONATION COMBUSTORS
#325Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities
#326Flame holder for minimizing combustor screech
#327Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber
#328Combustor assembly including one or more resonator assemblies and process for forming same
#329Multi-response time burner system for controlling combustion driven pulsation
#330Assembly for reducing noise in turbofan engines
#331Turbine engine fuel injector with helmholtz resonators
#332System for reducing combustor dynamics
#333Damping of vibration of a combustion chamber by resonators
#334System for damping thermo-acoustic instability in a combustor device for a gas turbine
#335Thermoacoustic Oscillation Damping In Gas Turbine Combustors With Annular Plenum
#336Combustion chamber for a gas turbine engine
#337Methods and apparatus to facilitate decreasing combustor acoustics
#338Method for control of thermoacoustic instabilities in a combustor
#339Gas turbine fuel injector with a removable pilot assembly
#340Injection assembly for a combustor
#341Fuel injector for a gas turbine engine
#342Resonator device at junction of combustor and combustion chamber
#343Flow modulation method and apparatus
#344Gas-turbine combustion chamber wall for a lean-burning gas-turbine combustion chamber
#345Turbine engine tailcone resonator
#346Gas turbine combustion chamber wall with dampening effect on combustion chamber vibrations
#347Acoustic resonator with impingement cooling tubes
#348Lean premix burner with circumferential atomizer lip
#349Method of suppressing combustion instabilities using a resonator adopting counter-bored holes
#350Resonator performance by local reduction of component thickness
#351Two-branch mixing passage and method to control combustor pulsations
#352Combustion chamber of a gas turbine engine with an upstream fairing for separating the gas stream, annular wall forming a cap of the upstream fairing of the chamber, and gas turbine engine with the chamber
#353Thermal power plant with sequential combustion and reduced-COemission, and a method for operating a plant of this type
#354Acoustic damper
#355Premix burner
#356Burner with stepped fuel injection
#357Augmentor liner
#358Method and apparatus for assembling gas turbine engine combustors
#359Aerodynamic trip for a combustion system
#360Method and apparatus for decreasing combustor acoustics
#361Combustion chamber for a gas turbine engine
#362Premix burner
#363Combustion chamber for a gas turbine with at least two resonator devices
#364Burner
#365Acoustically stiffened gas-turbine fuel nozzle
#366Gas turbine control apparatus and gas turbine system using the same
#367Reheat combustion system for a gas turbine
#368Gas turbine combustor and a gas turbine equipped therewith
#369Burner for a gas turbine engine
#370Resonator adopting counter-bored holes and method of suppressing combustion instabilities
#371Gas turbine
#372Burner, method for operating a burner and gas turbine
#373Combustion chamber for a gas turbine
#374Burner
#375Gas turbine combustor
#376Fuel injection arrangement
#377Method and apparatus to decrease combustor acoustics
#378Combustion liner cap assembly for combustion dynamics reduction
#379High frequency dynamics resonator assembly
#380Burner unit and method for operation thereof
#381Method and device for affecting thermoacoustic oscillations in combustion systems
#382Method and device for affecting thermoacoustic oscillations in combustion systems
#383Gas turbine can annular combustor
#384Turbine engine having a multicavity damper
#385Acoustic damper for combustor