Search patents:
Integrally bladed rotor with slotted outer rim
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014074185A3
An integrally bladed rotor has an outer rim with a plurality of blades extending radially outwardly of the outer rim. A plurality of channels are ...
Hybrid core assembly
Filed: January 1st, 1970 [Granted]
Patent Number: EP2554294A3
A hybrid core assembly (46) for a casting process includes a ceramic core portion (48) and a refractory metal core portion (50) that interfaces ...
Airfoil assembly with paired endwall contouring
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014105270A3
An airfoil assembly is disclosed. The airfoil assembly may comprise a series of airfoils such as vanes radially extending between an ID endwall ...
Twin tip turbine propulsors powered by a single gas turbine generator
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014109811A3
A gas turbine engine has a core engine incorporating a turbine, and a manifold positioned downstream of the turbine. The manifold delivers ...
Fan drive gear system flexible support features
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014099084A3
A disclosed gear assembly support for a gas turbine engine includes a first portion configured for attachment to a case of the gas turbine engine ...
Remote feature measurement
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014116334A3
A system includes a machining subsystem to machine features and an laser-line imaging subsystem to measure said features.
Auxiliary component mounts
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014081500A3
A mount for mounting a component to a gas turbine engine is disclosed. The mount may include a central portion that attaches to the ...
Bifurcated inlet scoop for gas turbine engine
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014055152A3
A bifurcated inlet scoop frame for a gas turbine engine and method of using such frame for a gas turbine engine are disclosed. The bifurcated ...