145419 ⎘
Geometry; Two-dimensional rectangular square
JOINTS BETWEEN ACOUSTIC PANELS
#2Bore compartment seals for gas turbine engines
#3LABYRINTH SEAL COMPRISING AN ABRADABLE ELEMENT WITH VARIABLE CELL DENSITY
#4Impact-cooling tubular insert for a turbomachine distributor
#5Inserts for airfoils of gas turbine engines
#6ANGLED IMPINGEMENT INSERTS WITH COOLING FEATURES
#7Reduced stress boss geometry for a gas turbine engine
#8Turbine airfoil multilayer exterior wall
#9TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES
#10BLADES AND VANES FOR GAS TURBINE ENGINES AND THE MANUFACTURE THEREOF
#11BLADE OF A TURBOMACHINE, INCLUDING A COOLING CHANNEL AND A DISPLACEMENT BODY SITUATED THEREIN, AS WELL AS A METHOD FOR MANUFACTURING
#12Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole
#13Nozzle assembly and method for forming nozzle assembly
#14Turbine assembly
#15Dual walled component for a gas turbine engine
#16Seal carrier for a turbomachine, in particular a gas turbine
#17AIRFOIL PLATFORM COOLING CORE CIRCUITS WITH ONE-WALL HEAT TRANSFER PEDESTALS FOR A GAS TURBINE ENGINE COMPONENT AND SYSTEMS FOR COOLING AN AIRFOIL PLATFORM
#18Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element
#19Reduced stress boss geometry for a gas turbine engine
#20Angled impingement inserts with cooling features
#21TURBINE COMPONENTS WITH NEGATIVE CTE FEATURES
#22Turbine rotor blade
#23Gas turbine filtration system with inlet filter orientation assembly
#24Blade or vane for a turbomachine and axial turbomachine
#25Variable area nozzle and associated propulsion system and method
#26Borescope assembly and method of installing borescope plugs
#27Brush seal
#28Closure bucket for turbo-machine
#29Fan diffuser having a circular inlet and a rotationally asymmetrical outlet
#30Assembly for directing combustion gas
#31Gas turbine blade and gas turbine having the same
#32Microcircuit cooling for blades
#33Modular transvane assembly
#34Ceramic matrix composite turbine engine components with unitary stiffening frame
#35Seal in a gas turbine engine having a shim base and a honeycomb structure with a number of cavities formed therein