145415 ⎘
Geometry
Sub-classes:Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
#2GEAR REDUCTION FOR LOWER THRUST GEARED TURBOFAN
#3LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE
#4Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
#5Turbine blades having damper pin slot features and methods of fabricating the same
#6Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
#7TURBINE ABRADABLE LAYER WITH AIRFLOW DIRECTING PIXELATED SURFACE FEATURE PATTERNS
#8Turbine engine flow path
#9Turbine component thermal barrier coating with depth-varying material properties
#10Turbine component thermal barrier coating with crack isolating engineered groove features
#11Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
#12Edge treatment for gas turbine engine component
#13Acoustic liner with varied properties
#14Turbine engine impeller
#15Interior cooling channels
#16Diaphragm and blades for turbomachinery
#17Parabolic radial flow impeller with tilted or offset blades
#18Turbomachine with variable stator
#19Airfoil shape for a turbine bucket