Patent classifications
F23D11/26
Self-pumping fuel injector for a gas turbine engine and method of operation
A self-pumping fuel injector includes a pump and a motor for, in-part, delivering fuel to a combustor at higher fuel pressures during start-up and ramping-up conditions. Each pump may include a stationary flow interuptor that intermittently and variably supplies fuel to a rotating spindle that, in-turn, expels the fuel into a nozzle of the injector for improve fuel spray distributions.
Self-pumping fuel injector for a gas turbine engine and method of operation
A self-pumping fuel injector includes a pump and a motor for, in-part, delivering fuel to a combustor at higher fuel pressures during start-up and ramping-up conditions. Each pump may include a stationary flow interuptor that intermittently and variably supplies fuel to a rotating spindle that, in-turn, expels the fuel into a nozzle of the injector for improve fuel spray distributions.
Fuel nozzle, and combustor and gas turbine having the same
A fuel nozzle includes a main cylinder extending in one direction; an auxiliary cylinder surrounding the main cylinder and defining a fuel passage between the auxiliary cylinder and the main cylinder; a shroud spaced that is apart from the auxiliary cylinder and surrounds the auxiliary cylinder; a swirler vane that is disposed between the auxiliary cylinder and the shroud and defines a fuel cavity communicating with the fuel passage so that fuel flowing in the fuel passage flows into the fuel cavity; and a fuel flow guide disposed inside the fuel cavity to guide fuel that flows from the fuel passage and enters the fuel cavity and to distribute the guided fuel in the fuel cavity. A fuel aperture is formed in the swirler vane to communicate with the fuel passage and the fuel cavity so that the fuel flows into the fuel cavity via the fuel aperture.
CONTROL METHOD FOR A CATALYTIC COMBUSTION APPARATUS AND A CATALYTIC COMBUSTION SYSTEM
A method for controlling a catalytic combustion apparatus having a heater capable of heating fuel to be supplied to a catalyst includes a step of supplying oxidant gas to the catalytic combustion apparatus, and an injection step of injecting the fuel into the catalytic combustion apparatus. The injection step also includes an electric power feeding step of supplying electric power to the heater, and a setting step of setting an injection amount of the fuel to be injected into the catalytic combustion apparatus in response to output of the heater.
Electronic fuel control for gas turbine engines
A fuel injector for a gas turbine engine includes a feed arm defining a conduit extending between an inlet end and an outlet end and a plunger. The plunger is disposed within the conduit and is movable between a plunger first position and a plunger second position. A flow area defined between the plunger and the feed arm is smaller in the plunger first position than in the plunger second position to bias fuel flow through the fuel injector. Fuel systems, gas turbine engines, and methods of controlling fuel flow in gas turbine engine fuel systems are also described.
Electronic fuel control for gas turbine engines
A fuel injector for a gas turbine engine includes a feed arm defining a conduit extending between an inlet end and an outlet end and a plunger. The plunger is disposed within the conduit and is movable between a plunger first position and a plunger second position. A flow area defined between the plunger and the feed arm is smaller in the plunger first position than in the plunger second position to bias fuel flow through the fuel injector. Fuel systems, gas turbine engines, and methods of controlling fuel flow in gas turbine engine fuel systems are also described.
Jet burner
A jet burner of the present disclosure basically includes a burner unit and an air blower disposed at a rear end of a burning chamber of the burner unit, wherein the burner unit is installed with a fuel bucket for storing fuel and the burning chamber having a tubular shape. Interior of the burning chamber is installed with a least one nozzle, at least one fuel pipe coupled to the fuel bucket is installed at each the nozzle, a front end of the burning chamber is installed with at least one jet pipe, and a pipe diameter of each the jet pipe is less than an inner diameter of the burning chamber. Under the reaction of the jet pipe, the burning stay time of the fuel in the interior of the burning chamber is increased, as to achieve the objective of increasing the fuel burning efficiency.
Jet burner
A jet burner of the present disclosure basically includes a burner unit and an air blower disposed at a rear end of a burning chamber of the burner unit, wherein the burner unit is installed with a fuel bucket for storing fuel and the burning chamber having a tubular shape. Interior of the burning chamber is installed with a least one nozzle, at least one fuel pipe coupled to the fuel bucket is installed at each the nozzle, a front end of the burning chamber is installed with at least one jet pipe, and a pipe diameter of each the jet pipe is less than an inner diameter of the burning chamber. Under the reaction of the jet pipe, the burning stay time of the fuel in the interior of the burning chamber is increased, as to achieve the objective of increasing the fuel burning efficiency.
Booster burner
A booster burner of the present disclosure basically has a burning unit, an air blower disposed at a rear end of a burning chamber of the burning unit and a high-pressure gas providing unit; wherein the burning unit has a fuel bucket for storing fuel and a burning chamber having a tubular shape, interior of the burning chamber has at least one nozzle, at least one fuel tube coupled to the fuel bucket is disposed at each the nozzle; and the high-pressure gas supplying unit has a gas storage bucket for storing high-pressure gas, each the nozzle is installed with a high-pressure pipe coupled to the gas storage bucket. Through the high-pressure gas, the slight atomization and acceleration effect is applied to the fuel which enters the nozzle, such that fuel molecules are refined and more completely burned, and the objective of increasing the fuel burning efficiency is achieved.
Booster burner
A booster burner of the present disclosure basically has a burning unit, an air blower disposed at a rear end of a burning chamber of the burning unit and a high-pressure gas providing unit; wherein the burning unit has a fuel bucket for storing fuel and a burning chamber having a tubular shape, interior of the burning chamber has at least one nozzle, at least one fuel tube coupled to the fuel bucket is disposed at each the nozzle; and the high-pressure gas supplying unit has a gas storage bucket for storing high-pressure gas, each the nozzle is installed with a high-pressure pipe coupled to the gas storage bucket. Through the high-pressure gas, the slight atomization and acceleration effect is applied to the fuel which enters the nozzle, such that fuel molecules are refined and more completely burned, and the objective of increasing the fuel burning efficiency is achieved.