Abstract: A fuel nozzle valve includes a fuel nozzle valve liner having a channel with an opening for allowing fuel to flow therethrough and a seat. A plunger has a stud and a base substantially perpendicular to the stud, the plunger being configured to move relative to the fuel nozzle valve liner to seal or to open the opening of the fuel nozzle valve. The fuel nozzle valve further includes a metal resilient member configured to contact the base of the plunger and the seat of the fuel nozzle valve liner to seal the opening of the fuel nozzle valve when the plunger is moved to seal the fuel nozzle valve.
Type:
Grant
Filed:
March 30, 2022
Date of Patent:
October 29, 2024
Assignee:
GENERAL ELECTRIC COMPANY
Inventors:
Christopher E. Wolfe, Alfred A. Mancini, Randy Joseph Tobe
Abstract: A combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel delivery system aft of the axial fuel delivery system. The radial fuel delivery system may be configured to direct fuel at least partially towards the axial fuel delivery system. A radial fuel delivery system is also provided. The system may comprise a combustor including a combustor liner, a mixer coupled to the combustor liner, and a nozzle disposed within the mixer, wherein the mixer and the nozzle are configured to direct fuel in a direction at least partially forward.
Type:
Grant
Filed:
February 20, 2015
Date of Patent:
August 28, 2018
Assignee:
UNITED TECHNOLOGIES CORPORATION
Inventors:
Wookyung Kim, Zhongtao Dai, Kristin Kopp-Vaughan
Abstract: A fuel valve for a turbine engine, the valve has a fuel inlet connected to a supply of fuel and a purge inlet connected to a supply of purge air. Opening and closing apparatus within the valve selectively supplies air or fuel to a valve outlet. The opening and closing apparatus are movable in sequence from a first position where both the purge air and fuel to the outlet is disabled to a second position where the purge air is enabled and the fuel is disabled to a third position where the purge air is disabled and the fuel is enabled.
Abstract: A method for active suppression of hydrodynamic instabilities in a combustion system in which liquid or gaseous fuel is premixed with combustion air and the fuel/air mixture is then burnt. The mass flow of the supplied fuel is modulated on the basis of a selected time function. Simplification and increased functional reliability are achieved by the modulation which is carried out using fluidics.
Type:
Grant
Filed:
July 24, 2000
Date of Patent:
February 5, 2002
Assignee:
Alstom (Switzerland) Ltd
Inventors:
Adnan Eroglu, Christian Oliver Paschereit, Wolfgang Polifke