Inventor

MONGILLO JR DOMINIC J

US102 patents

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

MONGILLO JR DOMINIC J

UNITED TECHNOLOGIES CORP

Coolable airfoil structure

Turbomachinery airfoil with optimized heat transfer

Coolable airfoil structure

Cooling channels for gas turbine engine component

Impingement skin core cooling for gas turbine engine blade

Cooled rotor blade

Cooled rotor blade and method for cooling a rotor blade

Cooled rotor blade with vibration damping device

Turbine outer air seal

Fanned trailing edge teardrop array

Dilution hole assembly

Gas turbine engine components, blade outer air seal assemblies, and blade outer air seal segments thereof

Turbine airfoil tip shelf and squealer pocket cooling

Fanned trailing edge teardrop array

Cooled rotor blade

Cooled rotor blade

Hot section engine components having segment gap discharge holes

Dual-wall impingement cavity for components of gas turbine engines

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

Double wall turbine gas turbine engine blade cooling configuration

Aft flowing serpentine cavities and cores for airfoils of gas turbine engines

Additively manufactured core

Leading edge hybrid cavities and cores for airfoils of gas turbine engine

Airfoil turn caps in gas turbine engines

Seal arrangement for turbine engine component

Gas turbine engine components having internal hybrid cooling cavities

Gas turbine engine component cooling with resupply of cooling passage

Cored airfoil platform with outlet slots

Blade outer air seal having partial coating

Turbine airfoil tip shelf and squealer pocket cooling

Spanwisely variable density pedestal array

Obtuse angle chevron trip strip

Blade outer air seal for a gas turbine engine

Gas turbine engine serpentine cooling passage with chevrons

RAYTHEON TECH CORP

Cooling schemes for airfoils for gas turbine engines

Airfoil cooling holes

Components for gas turbine engines

Turbine blade cooling hole arrangement

Leading edge hybrid cavities for airfoils of gas turbine engine

MONGILLO JR DOMINIC J

Cooling hole with curved metering section

Turbine airfoil tip shelf and squealer pocket cooling

RTX CORP

Components for gas turbine engines

Dual tip flag

PROPHETER-HINCKLEY TRACY A

Gas turbine engine airfoil impingement cooling

UNITED TECHNLOGIES CORP

Local indented trailing edge heat transfer devices

LEVASSEUR GLENN

EDM method for multi-lobed cooling hole

ZESS GARY A

Trailing edge cooling

NADEAU DANIEL C

Gas turbine engine airfoil internal cooling features

JOE CHRISTOPHER R

Blade outer air seal having partial coating

GAUTSCHI STEVEN BRUCE

Trailing edge or tip flag antiflow separation