Inventor

ZELESKY MARK F

US103 patents

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

ZELESKY MARK F

UNITED TECHNOLOGIES CORP

Coolable airfoil structure

Turbomachinery airfoil with optimized heat transfer

Coolable vane or blade for a turbomachine

Stator vane for a rotary machine

Coolable airfoil structure

Cooled rotor assembly for a turbine engine

Cooled turbine blade

Seal ring for gas turbine engines

Gas turbine engine component having vascular engineered lattice structure

Coolable air foil for a gas turbine engine

Cooled turbine blade

Gas turbine engine airfoil cooling circuit

Apparatus and method for quadrail ergonomic assembly

Gas turbine engine component having vascular engineered lattice structure

Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustor

Self-opening cooling passages for a gas turbine engine

Intercooled cooling air with improved air flow

Self-cooled orifice structure

Dual walled seal assembly

Split compressor turbine engine

Airfoil having environmental barrier topcoats that vary in composition by location

Gas turbine engine assembly with mid-vane outer platform gap

Turbine engine cooling system with an open loop circuit

Gas turbine engine including seal plate providing increased cooling adjacent contact area

Tip clearance control for gas turbine engine

Combustor panel cooling arrangements

Airfoil cooling

Cooling hole with curved metering section

Multiple piece engine component

Gas turbine engine component having vascular engineered lattice structure

Combustor panels and configurations for a gas turbine engine

Additively manufactured casting articles for manufacturing gas turbine engine parts

Additive manufacturing system utilizing an epitaxy process and method of operation

ZELESKY MARK F

Tip leakage flow directionality control

Tip leakage flow directionality control

Tip leakage flow directionality control

Tri-lobed cooling hole and method of manufacture

XU JINQUAN

Multi-lobed cooling hole and method of manufacture

Multi-lobed cooling hole and method of manufacture

MIRONETS SERGEY

Hybrid blade outer air seal for gas turbine engine

Hybrid airfoil for a gas turbine engine

GLEINER MATTHEW S

Gas turbine engine component with multi-lobed cooling hole

Cooling hole with asymmetric diffuser

MARTIN THOMAS J

Vortex generators for improved film effectiveness

Turbomachinery component cooling scheme

PROPHETER-HINCKLEY TRACY A

Gas turbine engine airfoil impingement cooling

LEVASSEUR GLENN

EDM method for multi-lobed cooling hole

KOHLI ATUL

Cooling hole with thermo-mechanical fatigue resistance

SLAVENS THOMAS N

Modulated turbine vane cooling

RAYTHEON TECH CORP

Vane arc segment with thermal insulation element