136853 ⎘
Blades; Blade-carrying members ; Heating, heat-insulating, cooling or antivibration means on the blades or the members; Fixing blades to rotors; Blade roots ; Blade spacers between two discs or rings
Control of leakage for gas turbine engine compressor blades
#2ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE
#3Gas turbine engine including a rotating blade assembly
#4Composite reinforced rotor
#5Rotor blade pair for rotational equipment
#6Trunnion retention for a turbine engine
#7REDUCED SCALE RUNNER AND METHOD OF MANUFACTURING THEREOF
#8Turbomachine stage and method of making same
#9Turbine blade assembly with ceramic matrix composite components
#10Platform with axial attachment for blade with circumferential attachment
#11Pinned platform for blade with circumferential attachment
#12Turbine wheel assembly
#13Movable ring assembly for a turbine engine turbine
#14Multi-piece turbine disk for ceramic matrix composite components
#15Fan for a turbomachine
#16Trunnion retention for a turbine engine
#17Outer drum rotor assembly
#18Turbomachine stage and method of making same
#19Rotor blade assembly comprising a ring segment shaped or disc segment shaped blade carrier and a radially inner reinforcement structure
#20Rotor with a locking plate for securing an antirotation lock against unscrewing
#21Propeller blades
#22Fan blade pitch setting
#23Fan for a turbomachine
#24Trunnion retention for a turbine engine
#25Method for manufacturing a stage of a steam turbine
#26Bonded fan platform
#27Turbine blisk including ceramic matrix composite blades and methods of manufacture
#28Gas turbine hub
#29Tip-controlled integrally bladed rotor for gas turbine engine
#30Low speed fan for gas turbine engines
#31Expandable Boundary Layer Turbine
#32Method for Building stages of centrifugal radial turbines
#33Blisk with low stresses at blade root, preferably for an aircraft turbine engine fan
#34RETENTION ASSEMBLY WITH A CONICAL INTERFACE FOR A PROPELLER BLADE
#35Turbine or compressor stage including an interface part made of ceramic material
#36Double split blade lock ring
#37Rotor cover plate
#38Turbine rotor assembly
#39Damper for a turbine rotor assembly
#40Turbine blade for a gas turbine engine
#41Damper for a turbine rotor assembly
#42Fan rotor and associated turbojet engine
#43Radial impeller with a radially free basic rim
#44Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping
#45Turbine and method for manufacturing turbine
#46Gas turbine engine rotor construction
#47Blade retention disk
#48Rotor assembly for gas turbine engine
#49Turbine engine rotor wheel with blades made of a composite material provided with a spring ring
#50Rotor Disc
#51Multi-component bladed rotor for a turbomachine
#52Split disk assembly for a gas turbine engine
#53Turbomachine rotor wheel having composite material blades
#54Method of forming a rotating blade assembly
#55SHROUDED SINGLE CRYSTAL DUAL ALLOY TURBINE DISK
#56Turbine wheel for turbomachine and the assembly method for such a wheel
#57Airfoil attachment for gas turbine engines