Inventor

LORICCO NICHOLAS M

US38 patents

⚠️ This page may combine multiple inventors who share the name “LORICCO NICHOLAS M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

LORICCO NICHOLAS M

UNITED TECHNOLOGIES CORP

Trough seal for gas turbine engine

Dual-wall impingement cavity for components of gas turbine engines

Double wall turbine gas turbine engine vane platform cooling configuration with baffle impingement

Segregated cooling air passages for turbine vane

Gas turbine engine component cooling passage turbulator

Turbine vane cooling arrangement

Cooling for gas turbine engine components

Turbine vane cooling arrangement

Doublet vane assembly for a gas turbine engine

Turbine blade cooling hole arrangement

Divided baffle for components of gas turbine engines

Fluidic machining method and system

Cooling passage with structural rib and film cooling slot

Hybrid cooling schemes for airfoils of gas turbine engines

Gas turbine engine component cooling cavity with vortex promoting features

Gas turbine engine component cooling passage and space casting core

Gas turbine engine component with film cooling hole

Determining presence of internal corrosion within a rotor blade by measuring magnetic characteristic(s)

Airfoil with rib communication

Airfoils having tapered tip flag cavity and cores for forming the same

Divided baffle for components of gas turbine engines

Die cast tip cover and method of managing radial deflection of die cast tip

Fluidic machining method and system

Film hole with protruding flow accumulator

Gas turbine engine blade with ceramic tip and cooling arrangement

Film hole with in-wall accumulator

Double wall turbine gas turbine engine vane with discrete opposing skin core cooling configuration

Double wall turbine gas turbine engine vane platform cooling configuration with main core resupply

Gas turbine engine airfoil with cooling path

Cooled turbine vane with alternately orientated film cooling hole rows

Gas turbine engine component with film cooling hole with accumulator

RAYTHEON TECH CORP

Turbine blade cooling hole arrangement

Feather seal mateface cooling pockets

Systems and methods of hybrid blade tip repair

Turbine blade trailing edge cooling feed

Turbine vane having dual source cooling

Systems and methods of blade leading edge repair using field assisted sintering technology

FLODESIGN SONICS INC

Acoustophoretic enhanced system for use in tanks