Inventor

GLEINER MATTHEW S

US32 patents

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

GLEINER MATTHEW S

UNITED TECHNOLOGIES CORP

Turbine airfoil platform cooling core

Multi-lobed cooling hole

Outer diameter platform cooling hole system and assembly

Core arrangement for turbine engine component

Component core with shaped edges

Turbine airfoil and method of cooling

Ceramic core tapered trip strips

Core arrangement for turbine engine component

Component core with shaped edges

Gas turbine component with platform cooling

BOAS thermal protection

Gas turbine engine component having platform cooling channel

BOAS thermal protection

Cooling hole with curved metering section

Gas turbine engine component having platform cooling channel

Gas turbine engine component with a cooling circuit having a flared base

GLEINER MATTHEW S

Gas turbine engine component with multi-lobed cooling hole

Cooling hole with asymmetric diffuser

Dead ended bulbed rib geometry for a gas turbine engine

Ceramic core tapered trip strips

XU JINQUAN

Multi-lobed cooling hole and method of manufacture

Multi-lobed cooling hole and method of manufacture

JENNE DOUGLAS C

Turbine airfoil with body microcircuits terminating in platform

Microcircuit skin core cut back to reduce microcircuit trailing edge stresses

RAYTHEON TECH CORP

Gas turbine component with platform cooling

Turbine blade trailing edge cooling feed

MONGILLO JR DOMINIC J

Cooling hole with curved metering section

FARRIS JOHN R

Casting core assembly methods

DEVORE MATTHEW A

Serpentine cored airfoil with body microcircuits

MURPHY RICHARD M

Anti-rotation slot for turbine vane

KOHLI ATUL

Cooling hole with thermo-mechanical fatigue resistance

WILLEY LAWRENCE J

Gas turbine engine component having platform cooling channel