145373 ⎘
Components; Stators; Fluid guiding means, e.g. vanes Cascades, i.e. assemblies of similar profiles acting in parallel
SYMMETRIC CASCADE THRUST REVERSERS AND RELATED METHODS
#2METHOD OF OBTAINING A GRID OF BLADES OF AN AIRCRAFT THRUST REVERSING DEVICE
#3THRUST REVERSER COMPRISING MOVABLE CASCADES AND A SEALING MEMBRANE
#4Aircraft nacelle equipped with at least one thrust reversal device comprising a downstream deflector, aircraft comprising at least one propulsion unit having such a nacelle
#5Reverser with movable cascades for an aircraft propulsion assembly, comprising a system for limiting the buckling of an actuator of the reverser
#6ACTUATING SYSTEM FOR A CASCADE THRUST REVERSER
#7Thrust reverser cascade with one or more flow disrupters
#8Thrust reverser cascade with one or more flow stabilizers
#9Cascade thrust reverser assembly for a gas turbine engine
#10Gas turbine engines with improved guide vane configurations
#11Symmetric cascade thrust reversers and related methods
#12Textile cascade assembly
#13Thrust reverser cascade including acoustic treatment
#14Thrust reverser system for an aircraft propulsion system
#15Stator vane and aircraft gas turbine engine
#16Abradable member for a turbine of a turbomachine, comprising a wear face provided with guide vanes
#17Mobile-cowl thrust reverser comprising a thrust-reduction mechanism that is independent of the mobile cowl
#18Thrust reverser cascade including acoustic treatment
#19Textile cascade assembly
#20Exhaust baffle component for an air turbine assembly
#21Long-fibre-reinforced-joints-composite thrust reverser cascade
#22Aircraft nacelle having a fan ramp with articulated flaps
#23Grid-type thrust reverser for turbojet engine
#24Rear assembly of an aircraft turbojet engine nacelle comprising a thrust reverser with sliding cascades
#25Aircraft engine assembly with isolation valve outside uncontained rotor impact area
#26TANGENTIAL ON BOARD INJECTOR NOZZLE WITH A FULL SWEEPING NOZZLE
#27Diffuser-deswirler for a gas turbine engine
#28Guide vane cascade for a turbomachine
#29Thrust reverser system with cascades
#30Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct
#31Intermediate housing hub comprising discharge flow guiding channels formed by the discharge fins
#32VARIABLE AREA EXHAUST MIXER FOR A GAS TURBINE ENGINE
#33THRUST REVERSER CASCADE
#34Thrust reverser cascade
#35Axial adjustment of the translating cowl using an eccentric
#36Fan cowl mounted to thrust reverser
#37Cascade segment for thrust reverser with repeating modular units, and method of manufacturing same
#38Method of fabricating a thrust reverser cascade assembly
#39Vane assembly of a gas turbine engine
#40Inflatable cascade assembly, system, and method for a cascade thrust reverser system
#41Thrust reverser assembly
#42Debris filter apparatus for preventing clogging of turbine vane cooling holes
#43Method for manufacturing and assembly of a thrust reverser cascade
#44Method and system for leading edge auxiliary vanes
#45GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE
#46Contouring a blade/vane cascade stage
#47METHOD OF DESIGNING GUIDE VANE FORMATIONS
#48Diffuser-deswirler for a gas turbine engine
#49Cascade pivot door-type thrust reverser for turbofan engine
#50Gas turbine engine vanes
#51Contouring a blade/vane cascade stage
#52Contouring a blade/vane cascade stage
#53Stage of variable-pitch blades for a turbine engine, turbine engine and associated installation method
#54Flow path routing within a gas turbine engine
#55Method and assembly for bonding complex composite assemblies
#56Guide vane assembly for a rotary machine and methods of assembling the same
#57Dual turn thrust reverser cascade systems and methods
#58Discharge flow duct of a turbine engine comprising a VBV grating with variable setting
#59Gas turbine blade
#60Variable turbomachine vane cascade
#61Geared turbofan gas turbine engine architecture
#62Service routing configuration for a gas turbine engine diffuser system
#63Gas turbine engine with an offtake
#64Internally heated engine inlet screen for aircraft engines
#65Thrust reverser cascade systems and methods
#66Turbofan engine assembly and methods of assembling the same
#67Cooling air heat exchanger scoop
#68Cascade assembly for a thrust reverser of an aircraft nacelle
#69Method and system for modulated turbine cooling
#70Gas turbine components having non-uniformly applied coating and methods of assembling the same
#71Air mixing systems having mixing chambers for gas turbine engines
#72Guide vane ring element for a turbomachine
#73Gas turbine
#74Motive air conditioning system for gas turbines
#75Airfoils
#76Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle
#77Gas-turbine engine with oil cooler in the engine cowling
#78EXTENDED THRUST REVERSER CASCADE
#79Nacelle for an aircraft engine with variable section nozzle
#80Tangential on-board injection vanes
#81Vane assembly of a gas turbine engine
#82Blade or vane for a turbomachine and axial turbomachine
#83Stator segment
#84Thrust reverser device
#85Thrust reverser unit having both nested cascades translating linearly and only one cascade rotational
#86VARIABLE VANE DRIVE SYSTEM
#87Blade cascade for a turbomachine
#88GAS TURBINE ENGINE MULTI-VANED STATOR COOLING CONFIGURATION
#89TURBINE SECTION OF HIGH BYPASS TURBOFAN
#90Gas turbine engine component having tip vortex creation feature
#91Flow path routing within a gas turbine engine
#92Method of designing guide vane formations
#93Metallic-coated polymer thrust reverser cascades
#94Variable area exhaust mixer for a gas turbine engine
#95THRUST REVERSER FAN RAMP PARTIALLY FORMED ON AFT END OF FAN CASE
#96Gas turbine engine for aircraft engine
#97Integrated inducer heat exchanger for gas turbines
#98Gas turbine combustion chamber arrangement of axial type of construction
#99Gas turbine arrangement and method for operating a gas turbine arrangement
#100Bleed outlet structure for a bleed valve
#101Vane with enhanced heat transfer
#102Aeroengine thrust reverser
#103AXIAL TURBINE
#104Methods and apparatus for assembling gas turbine engines