Search patents:
Post processing of components that are laser peened
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014065921A3
A method of post processing a laser peened component to remove a laser remelt layer is proposed. The post processing includes a series of ...
Composite article having layer with co-continuous material regions
Filed: January 1st, 1970 [Granted]
Patent Number: EP2530185A3
A composite article includes a substrate, at least one protective layer on the substrate, and an intermediate layer between the protective layer ...
Secondary load path for gas turbine engine
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014042774A3
A waiting link to support an engine on an aircraft includes a body portion including a first body portion opening, a second body portion opening, ...
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 ...
Casting cores and manufacture methods
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014058509A3
A casting core assembly (140) includes a metallic core (144, 146, 148; 360; 380; 400) and a ceramic core (142). A protuberant portion (184) of ...
High strength-to-density nanocellular foam
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014062268A3
A nanocellular foam has pores, interconnecting ligaments, and nodes where three or more ligaments intersect. The ligament cross section ...
Mullite-containing investment casting core
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014105436A1
An investment casting core includes a mullite-containing core body. The body can be made by providing a mullite-containing powder, forming the powder into a  ...
Gas turbine engine combustor with integrated combustor vane
Filed: January 1st, 1970 [Granted]
Patent Number: WO2014099074A3
A combustor section for a gas turbine engine includes a combustor vane which extends at least partially into a combustion chamber.