Inventor

LACY BENJAMIN PAUL

US102 patents

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

LACY BENJAMIN PAUL

GEN ELECTRIC

Method of forming a microchannel cooled component

Premixed direct injection nozzle

Methods and systems to facilitate reducing NOx emissions in combustion systems

Turbine shroud including plurality of cooling passages

Interwoven near surface cooled channels for cooled structures

Turbine nozzle with cooling channel coolant distribution plenum

Article and method of forming an article

System and method for turbine nozzle cooling

Article, component, and method of forming an article

Hot gas path component trailing edge having near wall cooling features

Hot gas path component having cast-in features for near wall cooling

Hot gas path component cooling system having a particle collection chamber

Article and method of forming an article

Hot gas path component having near wall cooling features

Article and process for producing an article

Hot gas path component

Thermal management article and method of forming the same, and method of thermal management of a substrate

Sealing device for providing a seal in a turbomachine

Method and system for providing cooling for turbine components

Turbine component and methods of assembling the same

Method for manufacturing turbine nozzle having non-linear cooling conduit

Fuel nozzle assembly

Turbine nozzle with inner band and outer band cooling

Adaptive cover for cooling pathway by additive manufacture

Adaptive cover for cooling pathway by additive manufacture

Article, component, and method of forming an article

Additively manufactured blade extension with internal features

LACY BENJAMIN PAUL

Hot gas path component cooling system

Cooling structures for turbine rotor blade tips

Pre-mixing apparatus for a turbine engine

Curved cooling passages for a turbine component

Combustor liner cooling system

Cooling structures in the tips of turbine rotor blades

Turbine shroud cooling assembly for a gas turbine system

Airfoil

Airfoil

Apparatus for cooling a platform of a turbine component

Shim for sealing transition pieces

Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event

Bucket assembly for turbine system

BUNKER RONALD SCOTT

Articles which include chevron film cooling holes, and related processes

ZIMINSKY WILLY STEVE

Premixed direct injection nozzle for highly reactive fuels

KRAEMER GILBERT OTTO

Gas turbine premixing systems

ZHANG XIUZHANG JAMES

Cooling structures in the tips of turbine rotor blades

EVULET ANDREI TRISTAN

Coanda injection system for axially staged low emission combustors

ZUO BAIFANG

Methods and systems to enhance flame holding in a gas turbine engine

SIMPSON STANLEY FRANK

Airfoil

YORK WILLIAM DAVID

Gas turbine premixer with internal cooling

WEI BIN

Process and system for forming shaped air holes

HELMICK DAVID ANDREW

Methods and systems to thermally protect fuel nozzles in combustion systems