Inventor

THAM KOK-MUN

US38 patents

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

THAM KOK-MUN

SIEMENS AG

Turbine abradable layer with zig zag groove pattern

Turbine abradable layer with progressive wear zone multi level ridge arrays

Turbine abradable layer with nested loop groove pattern

Compressor usable within a gas turbine engine

Turbine shroud with abradable layer having ridges with holes

Vane carrier temperature control system in a gas turbine engine

Turbine abradable layer with compound angle, asymmetric surface area ridge and groove pattern

Seal assembly including grooves in an aft facing side of a platform in a gas turbine engine

Shrouded turbine blade

Turbine shroud with abradable layer having dimpled forward zone

Segmented turbine blade squealer tip and cooling method

Compressor bleed cooling system for mid-frame torque discs downstream from a compressor assembly in a gas turbine engine

Outer rim seal assembly in a turbine engine

Turbine abradable layer with inclined angle surface ridge or groove pattern

SIEMENS ENERGY INC

Turbine abradable layer with progressive wear zone multi depth grooves

Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface

Turbine abradable layer with progressive wear zone terraced ridges

Turbine blade having contoured tip shroud

Additive manufacturing of abradable mesh structure on ring segment surface

Gas turbine engine with rotor centering cooling system in an exhaust diffuser

Shrouded turbine airfoil with leakage flow conditioner

LEE CHING-PANG

Outer rim seal assembly in a turbine engine

Turbine blade angel wing with pumping features

Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling

Finned seal assembly for gas turbine engines

Flow directing member for gas turbine engine

Seal including flexible seal strips

Aft outer rim seal arrangement

THAM KOK-MUN

Vane carrier thermal management arrangement and method for clearance control

External cooling fluid injection system in a gas turbine engine

Flow directing member for gas turbine engine

Flow discourager integrated turbine inter-stage U-ring

Air injection system in a gas turbine engine

SIEMENS ENERGY GLOBAL GMBH & CO KG

Turbine blade with squealer tip and densified oxide dispersion strengthened layer

Cover plate with flow inducer and method for cooling turbine blades

Method for starting up a gas turbine engine of a combined cycle power plant

LAURELLO VINCENT P

Gas turbine engine with improved cooling between turbine rotor disk elements

Gas turbine compressor with bleed path