157507 ⎘
Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers Combustion chambers comprising an annular flame tube within an annular casing
COMBUSTOR WITH BAFFLE
#2COMBUSTION CHAMBER FOR A GAS TURBINE, AND ENGINE
#3COMBUSTION SECTION WITH A PRIMARY COMBUSTION CHAMBER AND A SECONDARY COMBUSTION CHAMBER
#4COMBUSTOR OF GAS TURBINE
#5GAS TURBINE ENGINE HAVING A COMBUSTION SECTION WITH STEAM PROVIDED TO SECOND COMBSUTOR PLENUM
#6COOLING NOZZLE VANES OF A TURBINE ENGINE
#7ARTICLE AND METHOD FOR MANUFACTURING AN EXPANDED COMBUSTOR LINER
#8GAS TURBINE ENGINE
#9COMBUSTOR OF GAS TURBINE
#10TURBINE ENGINE SUPPORT STRUCTURE WITH AIRFLOW PORTS
#11COMBUSTION MODULE FOR A TURBOMACHINE
#12GAS TURBINE ENGINE CONFIGURED FOR DECREASED DIFFUSER WINDAGE AND METHOD OF ASSEMBLING THE SAME
#13Combustion section with a casing shielding
#14Combustor assembly for a turbine engine
#15Combustor with baffle
#16Combustion chamber with wall cooling
#17CTE MATCHING HANGER SUPPORT FOR CMC STRUCTURES
#18REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE
#19Combustion module for a turbomachine
#20Method and device for recursive sequential combustion
#21Combustor and gas turbine equipped with the same
#22Method of supplying fuel and air to a combustor with an ignition tube
#23Combustor dome-deflector and liner having flexible connections
#24Coupling a fuel nozzle purge flow directly to a swirler
#25Integral dome-deflector member for a dome of a combustor
#26Annular combustion chamber for an aircraft turbomachine
#27Combustor with baffle
#28Spark plug for a single-piece combustion chamber
#29ANNULAR COMBUSTOR DILUTION WITH SWIRL VANES FOR LOWER EMISSIONS
#30Multi-direction hole for rail effusion
#31Combustion tube and combustor for gas turbine, and gas turbine
#32PREMIXER ARRAY
#33Fuel injection for integral combustor and turbine vane
#34CHAMBER FOR ROTATING DETONATION ENGINE AND WALL OBSTACLES FOR SAME
#35Turbulence generator mixer for rotating detonation engine
#36Combustion chamber comprising secondary injection systems, and fuel supply method
#37Combustion chamber comprising means for cooling an annular casing zone downstream of a chimney
#38Piston ring assembly for a turbine engine
#39Fastening for a turbomachine combustion chamber
#40Lean burn combustor
#41Trapped vortex combustor for a gas turbine engine with a driver airflow channel
#42Combustion chamber for a turbomachine
#43Multi-direction hole for rail effusion
#44Two-stage combustor for gas turbine engine
#45ANNULAR GAS TURBINE COMBUSTOR FOR USE IN AIRCRAFT
#46Heat transfer arrangements and methods of making heat transfer arrangements
#47Combustor assembly for a turbine engine
#48Ultra compact combustor
#49Fluid mixing apparatus using liquid fuel and high- and low-pressure fluid streams
#50TUBULAR COMBUSTION CHAMBER WITH CERAMIC CLADDING
#51Fuel injection for integral combustor and turbine vane
#52METHOD AND SYSTEM FOR ROTATING DETONATION COMBUSTION
#53Support structure for a turbine vane of a gas turbine engine
#54Reverse flow combustor
#55Liner for a combustor with strain isolated inserts
#56Combustor of gas turbine engine and method
#57Combustor panel configuration with skewed side walls
#58VARIABLE GEOMETRY ROTATING DETONATION COMBUSTOR
#59Air tube
#60Sensor arrangement for measuring gas turbine combustor temperatures
#61COMBUSTION TUBE AND COMBUSTOR FOR GAS TURBINE, AND GAS TURBINE
#62Annular free-vortex combustor
#63Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
#64Combustor cooling panel with flow guide
#65Ring assembly for double-skin combustor liner
#66ROTATING DETONATION COMBUSTOR WITH THERMAL FEATURES
#67Cowl integration to combustor wall
#68System and method for providing compressed air to a gas turbine combustor
#69Combustor dome tiles
#70Combustor panel cooling hole arrangement
#71COMBUSTION CHAMBER ASSEMBLY FOR AN ENGINE HAVING HEAT SHIELDS AND/OR BURNER SEALS OF AT LEAST TWO DIFFERENT TYPES
#72Additive integral combustor expansion spring
#73Combustion section heat transfer system for a propulsion system
#74Dilution structure for gas turbine engine combustor
#75Tapered panel rail
#76Mixer assembly for a combustor
#77Cooled grommet for a combustor wall assembly
#78Airfoil fluid curtain to mitigate or prevent flow path leakage
#79GAS TURBINE ENGINE COMBUSTION ARRANGEMENT AND A GAS TURBINE ENGINE
#80Interrupted midrail for combustor panel
#81Combustion chamber for a turbomachine
#82Deflection mitigation structure for combustion system
#83Double wall combustors with strain isolated inserts
#84Assembly for a turbomachine combustion chamber
#85Combustor bolted segmented architecture
#86CTE matching hanger support for CMC structures
#87Combustion chamber assembly with different curvatures for a combustion chamber wall and a combustion chamber shingle fixed thereto
#88Inner cooling shroud for transition zone of annular combustor liner
#89Combustion system with deflector
#90Combustion chamber comprising two types of injectors in which the sealing members have a different opening threshold
#91Gas turbine combustor heat shield panel having multi-direction hole for rail effusion cooling
#92Combustor panel standoff pin
#93Undercut combustor panel rail
#94Pull-plane effusion combustor panel
#95Ultra compact combustor
#96Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
#97COMBUSTION CHAMBER ARRANGEMENT
#98Gas turbine annular combustor arrangement
#99COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE
#100Multi-can annular rotating detonation combustor
#101Involute trapped vortex combustor assembly
#102Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine
#103Combustor and method for improving combustor performance
#104Fuel spray nozzle comprising axially projecting air guiding element for a combustion chamber of a gas turbine engine
#105COMBUSTION CHAMBER ASSEMBLY COMPRISING THERMAL SHIELD AND BURNER GASKET AS WELL AS MANUFACTURING METHOD
#106Combustion chamber
#107Combustor mixer purge cooling structure
#108Canted combustor for gas turbine engine
#109Combustor system for high fuel/air ratio and reduced combustion dynamics
#110Gas turbine combustion liner comprising heat transfer cell heat pipes
#111Dynamics-mitigating adapter for bundled tube fuel nozzle
#112Float wall combustor panels having airflow distribution features
#113Jet in cross flow fuel nozzle for a gas turbine engine
#114Pilot nozzle with inline premixing
#115Combustor heat shield and attachment features
#116Assembly of tube and structure crossing multi chambers
#117Combustor assembly with CMC combustor dome
#118Combustion section heat transfer system for a propulsion system
#119Annular fuel manifold with a deflector
#120CTE matching hanger support for CMC structures
#121Combustor mounting assembly having a spring finger for forming a seal with a fuel injector assembly
#122Trapped vortex combustor for a gas turbine engine with a driver airflow channel
#123Combustion cylinder, gas turbine combustor, and gas turbine
#124Aerodynamic injection system for aircraft turbine engine, having improved air/fuel mixing
#125Ring-shaped combustion chamber for a turbine engine
#126Combustion chamber of a turbine engine
#127Combustor liner with gasket for gas turbine engine
#128Notched gas turbine combustor cowl
#129Gas turbine engine combustor comprising air inlet tubes arranged around the combustor
#130Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor
#131Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor
#132Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor
#133Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
#134Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
#135Non-planar combustor liner panel for a gas turbine engine combustor
#136Non-planar combustor liner panel for a gas turbine engine combustor
#137COATED COMBUSTOR PANEL SHELL FOR A GAS TURBINE ENGINE COMBUSTOR
#138Combustion systems having bayonet features
#139Tool for repairing out-of-round component
#140HOLLOW-WALL HEAT SHIELD FOR FUEL INJECTOR COMPONENT
#141Combustion chamber and a combustion chamber fuel injector seal
#142Combustion chamber in a turbine engine
#143Gas turbine engine combustor main mixer with vane supported centerbody
#144Combustion chamber and a combustion chamber fuel injector seal
#145Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
#146Annular Helmholtz damper for a gas turbine can combustor
#147Wall panel assembly for a gas turbine engine
#148Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device
#149Turbomachine combustion chamber comprising an airflow guide device of specific shape
#150Method of assembling an annular combustion chamber assembly
#151Combustion chamber assembly and a combustion chamber segment
#152Structure for cooling gas turbine engine
#153Combustor cassette liner mounting assembly
#154Combustor assembly for a turbine engine
#155Reducing noise from a combustor of a gas turbine engine
#156COMBUSTION CHAMBER
#157Combustor Effusion Plate Assembly
#158Fuel injecting device
#159Combustion chamber having a hook and groove connection
#160Turbomachine combustion chamber
#161Integrated combustor nozzle for a segmented annular combustion system
#162Mounting of integrated combustor nozzles in a segmented annular combustion system
#163Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
#164Combustion chamber system and a method of operating a combustion chamber system
#165Combustor assembly
#166Combustor assembly
#167Combustor assembly for a gas turbine engine
#168Combustor assembly
#169Combustor assembly
#170Combustion chamber having an annular outer wall with a concave bend
#171Combustion chamber coolant fluid path
#172Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine
#173Wear resistant frame liner joint assembly for a gas turbine engine
#174Staged fuel and air injection in combustion systems of gas turbines
#175Method for mounting a combustion chamber of a gas turbine engine
#176CONTINUOUS ROTATING DETONATION ENGINES AND ASSOCIATED SYSTEMS AND METHODS
#177GAS-TURBINE SYSTEM
#178Combustor for gas turbine engine
#179Annular turbomachine combustion chamber
#180System and method having annular flow path architecture
#181Combustor assembly for a turbine engine
#182Apparatus and method for air extraction at a gas turbine engine combustor
#183Combustor assembly for a turbine engine
#184Piston ring assembly for a turbine engine
#185Combustor cooling system
#186Combustor shape cooling system
#187Combustion chamber and a combustion chamber segment
#188Combustor hole arrangement for gas turbine engine
#189Combustion chamber comprising additional injection devices opening up directly into corner recirculation zones, turbomachine comprising such a chamber and fuel supply method for such a chamber
#190Sealed conical-flat dome for flight engine combustors
#191Sequential combustor and method for operating the same
#192Combustor tile
#193Combustion systems
#194GAS TURBINE COMBUSTOR
#195Cooling a quench aperture body of a combustor wall
#196Combustion systems
#197Controlled-leak combustor grommet
#198Multi-streamed dilution hole configuration for a gas turbine engine
#199Cooled grommet for a combustor wall assembly
#200TWO-STAGE COMBUSTOR FOR GAS TURBINE ENGINE
#201Thermal mechanical dimple array for a combustor wall assembly
#2023D non-axisymmetric combustor liner
#203Cooling an igniter body of a combustor wall
#204Gas turbine combustor
#205Combustor wall cooling channel formed by additive manufacturing
#206Combustor having a beveled grommet
#207Gas turbine engine wall assembly with offset rail
#208Turbine engine multi-walled structure with internal cooling element(s)
#209Turbine engine combustor heat shield with multi-angled cooling apertures
#210Inner diffuser case for a gas turbine engine
#211Turbine engine combustor heat shield with one or more cooling elements
#212Engine component
#213Engine component
#214Circumferentially and axially staged annular combustor for gas turbine engine
#215Angled radial fuel/air delivery system for combustor
#216Gas turbine engine quench pattern for gas turbine engine combustor
#217Passage geometry for gas turbine engine combustor
#218Thermal barrier coating of a combustor dilution hole
#219Sealed combustor liner panel for a gas turbine engine
#220Method to operate a combustor of a gas turbine
#221Attachment scheme for a ceramic bulkhead panel
#222Gas turbine engine combustor bulkhead assembly
#223Pre-diffuser strut for gas turbine engine
#224Combustor wall aperture body with cooling circuit
#225Combustor with axial staging for a gas turbine engine
#226Liner retaining feature for a combustor
#227Gas turbine engine wave geometry combustor liner panel
#228Gas turbine engine combustor liner panel
#229Liner element for a combustor, and a related method
#230Combustor for gas turbine engine
#231Combustor arrangement with fastening system for combustor parts
#232Combustor front panel
#233Annular combustion chamber
#234Single-walled combustor for a gas turbine engine and method of manufacture
#235Combustor panel with increased durability
#236System and method of control for a gas turbine engine
#237Hollow-wall heat shield for fuel injector component
#238Conical-flat heat shield for gas turbine engine combustor dome
#239Gas turbine engine combustor liner assembly with convergent hyperbolic profile
#240Combustor assembly with chutes
#241Annular combustion chamber of a gas turbine and gas turbine with such a combustion chamber
#242Combustor liners with U-shaped cooling channels
#243Combustor for gas turbine engine
#244Combustion chamber arrangement
#245MULTI-FUEL TURBINE COMBUSTOR, MULTI-FUEL TURBINE COMPRISING SUCH A COMBUSTOR AND CORRESPONDING METHOD
#246Ultra compact combustor having reduced air flow turns
#247Aircraft turbomachine combustion chamber module and method for designing same
#248Grommet assembly and method of design
#249Interface heat shield for a combustor of a gas turbine engine
#250Inner diffuser case struts for a combustor of a gas turbine engine
#251Combustor with grommet having projecting lip
#252Combustor assembly for a turbine engine
#253Assembly for directing combustion gas
#254Combustor dome heat shield
#255Continuous detonation combustion engine and system
#256Annular combustor with scoop ring for gas turbine engine
#257Helmholtz damper for gas turbine with cooling air flow
#258Annular combustion chamber for a turbine engine
#259HEAT-SHIELD ELEMENT FOR A COMPRESSOR-AIR BYPASS AROUND THE COMBUSTION CHAMBER
#260Annular combustion chamber in a turbine engine
#261Combustion chamber of a combustor for a gas turbine
#262Gas turbine engine and method of operating thereof
#263Combustors with complex shaped effusion holes
#264Combustor for gas turbine engine
#265Combustor for gas turbine engine
#266Slinger combustor
#267Hot gas path duct for a combustor of a gas turbine
#268Combustor for gas turbine engine
#269Combustion chamber heat shield and seal assembly and a method of manufacturing a combustion chamber heat shield and seal assembly
#270Turbine engine including a continuous wave detonation chamber and cooling bypass flow and aircraft provided with such a turbine engine
#271Laser-ignition combustor for gas turbine engine
#272Combustion system
#273Gas turbine engine combustor liner
#274Combustor bulkhead assembly
#275GAS TURBINE ASYMMETRIC FUEL NOZZLE COMBUSTOR
#276Gas turbine combustor
#277GAS TURBINE ASYMMETRIC NOZZLE GUIDE VANES
#278Turbine engine combustor and stator vane assembly
#279Turbine engine combustor wall with non-uniform distribution of effusion apertures
#280Annular combustion chamber for a turbine engine including improved dilution openings
#281Gas turbine engine combustor surge retention
#282Combustor having a beveled grommet
#283Non-combustion energy source and configuration for brayton cycle heat engines
#284Gas-turbine combustion chamber having non-symmetrical fuel nozzles
#285Annular combustor
#286Annular combustion chamber of a gas turbine
#287GAS TURBINE ENGINE, COMBUSTOR AND DOME PANEL
#288Two-stage combustor for gas turbine engine
#289Two-stage combustor for gas turbine engine
#290Gas turbine combustion chamber arrangement of axial type of construction
#291IMPINGEMENT COOLING OF COMBUSTOR LINERS
#292Combustion system and method of assembling the same
#293METHOD OF OPERATING A COMBUSTION CHAMBER
#294CONICAL REVERSE-FLOW COMBUSTION CHAMBER FOR A TURBOMACHINE
#295Turbomachine combustion chamber having a perforated chamber end wall and with no deflector
#296Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamber
#297Reheat burner injection system with fuel lances
#298WALL FOR A TURBOMACHINE COMBUSTION CHAMBER INCLUDING AN OPTIMISED ARRANGEMENT OF AIR INLET APERTURES
#299HEAD PART OF AN ANNULAR COMBUSTION CHAMBER
#300Head part of an annular combustion chamber