William R. Ryan

System for modulating fuel supply to individual fuel nozzles in a can-annular gas turbine

Pilot fuel flow tuning for gas turbine combustors

Method and System for Controlling Fuel to a Dual Stage Nozzle

Attachment system for ceramic combustor liner

Low leakage spring clip/ring combinations for gas turbine engine

Cantilevered framework support for turbine vane

Combustor assembly comprising a combustor device, a transition duct and a flow conditioner

Self-Contained Oil Feed Heat Shield for a Gas Turbine Engine

TURBINE ENGINE WITH ENHANCED FLUID FLOW STRAINER SYSTEM

Alternately Swirling Mains in Lean Premixed Gas Turbine Combustors