|
US2014212270A1
|
|
Gas turbine engine component having suction side cutback opening
|
|
US2015192021A1
|
|
Airfoil cooling arrangement
|
|
US2014000283A1
|
|
Cover plate for a component of a gas turbine engine
|
|
US2014010632A1
|
|
Airfoil cooling arrangement
|
|
US2014000287A1
|
|
Gas turbine engine turbine vane airfoil profile
|
|
US2013343873A1
|
|
Turbine engine variable area vane
|
|
US2013177448A1
|
|
Core for a casting process
|
|
US2013052008A1
|
|
Gas turbine engine airfoil baffle
|
|
US2012328450A1
|
|
Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals
|
|
US2012171045A1
|
|
Turbine component fixture and coating system
|
|
US2012076660A1
|
|
Conduction pedestals for a gas turbine engine airfoil
|
|
US2010329835A1
|
|
Airfoil with hybrid drilled and cutback trailing edge
|
|
US2010040460A1
|
|
Platforms with curved side edges and gas turbine engine systems involving such platforms
|
|
US2010040479A1
|
|
Gas turbine engine systems involving baffle assemblies
|
|
US2009269184A1
|
|
Gas turbine engine systems involving turbine blade platforms with cooling holes
|
|
US2009263251A1
|
|
Reduced weight blade for a gas turbine engine
|
|
US2009116953A1
|
|
Turbine airfoil with platform cooling
|
