145334 ⎘
Manufacture essentially without removing material by rolling
Surface treatment system design for high fatigue life hollow fan blades
#2TURBINE COMPONENT WITH A THIN INTERIOR PARTITION
#3Variable stator vane and method of fabricating variable stator vane
#4Manufacturing method of turbine casing
#5Thin seal for an engine
#6Turbine component with a thin interior partition
#7Method for spin forming lipskins
#8AEROFOIL COMPONENT AND METHOD
#9Thin seal for an engine
#10Method for producing a contoured ring rolling product
#11Method of manufacturing a component from a nickel-based superalloy
#12Process of forming and a seal for an engine
#13Wear liner for fixed stator vanes
#14Thin seal for an engine
#15HT Enhancement Bumps/Features on Cold Side
#16Ductile high-temperature molybdenum-based alloys
#17Process of forming and a seal for an engine
#18Segment of an abradable ring seal for a turbomachine, and process for the manufacture of such a piece
#19Piece of abradable material for the manufacture of a segment of an abradable ring seal for a turbomachine, and process for the manufacture of such a piece
#20Fan housing having flush mounted stator blades
#21Turbomachine flow divider and related turbomachine
#22Tie shaft for gas turbine engine and flow forming method for manufacturing same
#23Rolling tool device
#24Radial compressor and method for producing a radial compressor
#25METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED USING THIS METHOD
#26Bearing housing cover for a charging device
#27METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED ACCORDING TO THIS METHOD
#28Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method
#29Gas turbine engine blade for aircraft and manufacturing method thereof
#30METHOD FOR PRODUCING AN ANNULAR WALL STRUCTURE
#31ANNULAR GAS TURBINE ENGINE CASE AND METHOD OF MANUFACTURING
#32ANNULAR GAS TURBINE ENGINE CASE AND METHOD OF MANUFACTURING
#33Annular gas turbine engine case and method of manufacturing
#34ANNULAR GAS TURBINE ENGINE CASE AND METHOD OF MANUFACTURING
#35Sheet metal blank
#36Component of variable thickness having residual compressive stresses therein, and method therefor
#37Metallic article with integral end band under compression
#38Method of manufacturing a duct for a gas turbine engine
#39Sheet metal turbine or compressor static shroud