Inventor

MONGILLO DOMINIC J

US69 patents

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

MONGILLO DOMINIC J

UNITED TECHNOLOGIES CORP

Gas turbine engine component having vascular engineered lattice structure

Coolable air foil for a gas turbine engine

Turbine vane platform leading edge cooling holes

Turbine blade including revised platform

Turbine blade including revised trailing edge cooling

Chevron trip strip

Baffle assembly for gas turbine engine components

Gas turbine engine component having vascular engineered lattice structure

Gas turbine engine component having vascular engineered lattice structure

Gas turbine engine component having trip strips

Self-cooled orifice structure

Cooled turbine airfoil

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

Cooling arrangement with purge partition

Turbine blade with tip vortex control and tip shelf

Gas turbine engine component having engineered vascular structure

Turbine component with tip film cooling and method of cooling

Platform cooling circuit for a gas turbine engine component

Airfoil turn caps in gas turbine engines

Cooling hole with curved metering section

Gas turbine engine component having shaped pedestals

Multi-chamber platform cooling structures

Low loss airflow port

Airfoil turn caps in gas turbine engines

Chevron trip strip

Gas turbine engine component having vascular engineered lattice structure

Combustor panels and configurations for a gas turbine engine

Gas turbine engine component having engineered vascular structure

Low turn loss baffle flow diverter

Seal assembly with baffle for gas turbine engine

Variable thickness core for gas turbine engine component

Dual-fed airfoil tip

Turbine vane cooling arrangement

Airfoil having serpentine core resupply flow control

Gas turbine engine airfoil cooling circuit arrangement

Fan cooling hole array

RAYTHEON TECH CORP

Forming lined cooling aperture(s) in a turbine engine component

Forming lined cooling aperture(s) in a turbine engine component

Forming lined cooling aperture(s) in a turbine engine component

Forming cooling aperture(s) in a turbine engine component

Methods for forming cooling apertures in a turbine engine component

Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine component

Energy beam positioning during formation of a cooling aperture

Cooling passage configuration

Trailing edge insert for airfoil vane

RTX CORP

Forming and/or inspecting cooling aperture(s) in a turbine engine component

Cooling arrangement for gas turbine engine component

CHON YOUNG H

Angled tripped airfoil peanut cavity

PAPPLE MICHAEL LESLIE CLYDE

Platform cooling circuit for a gas turbine engine component

GREGG SHAWN J

Gas turbine engine airfoil cooling circuit arrangement