Fuel supply system
AssigneeGeneral Electric Company
InventorsCarlos Gabriel Roman, Alberto Jose Negroni
Life of this patent
Estimating the term…
Abstract
A fuel supply system includes a fuel manifold and a main fuel line path configured to receive a fuel from the fuel manifold. The main fuel line path routes the fuel to a combustion inlet region. The fuel supply system also includes a secondary fuel line path having an inlet configured to receive a portion of the fuel and an outlet configured to route the portion of the fuel to the main fuel line path through an outlet at a location of the main fuel line path that is downstream of the inlet of the secondary fuel line path. A storage volume is fluidly coupled to the secondary fuel line path and is configured to cyclically store and release the portion of the fuel.
Claims17
A fuel supply system comprising:
- a fuel manifold;
- a main fuel line path configured to receive a fuel from the fuel manifold and route the fuel to a combustion inlet region;
- a secondary fuel line path having an inlet configured to receive a portion of the fuel and an outlet configured to route the portion of the fuel to the main fuel line path through an outlet at a location of the main fuel line path that is downstream of the inlet of the secondary fuel line path;
- and
- a storage volume fluidly coupled to the secondary fuel line path and configured to cyclically store and release the portion of the fuel.
A fuel supply system for a gas turbine engine comprising:
- a fuel manifold;
- a main fuel line path configured to receive a fuel from the fuel manifold and route the fuel to a combustion inlet region;
- a secondary fuel line path having an inlet configured to receive a portion of the fuel and an outlet configured to route the portion of the fuel to the main fuel line path through an outlet;
- a storage volume fluidly coupled to the secondary fuel line path and configured to cyclically store and release the portion of the fuel;
- a control valve located along the secondary fuel line path between the storage volume and the outlet of the secondary fuel line path, wherein the control valve is configured to oscillate between an open condition and a closed condition in response to a pressure detected within the storage volume;
- a first orifice disposed in the main fuel line path to regulate a main fuel line path flow rate;
- and
- a second orifice disposed in the secondary fuel line path to regulate a secondary fuel line path flow rate, wherein the inlet of the secondary fuel line path is located upstream of the first orifice and the outlet of the secondary fuel line path is located downstream of the first orifice.
A gas turbine system comprising:
- a compressor;
- a combustion assembly having at least one combustion chamber;
- a turbine section;
- and
- a fuel supply system configured to route fuel to the combustion assembly, the fuel supply system comprising:
- a fuel manifold;
- a main fuel line path configured to receive a fuel from the fuel manifold and route the fuel to a combustion inlet region of the combustion assembly;
- a secondary fuel line path having an inlet configured to redirect a portion of the fuel away from the main fuel line path;
- and
- a storage volume fluidly coupled to the secondary fuel line path and configured to cyclically store and release the portion of the fuel in response to a pressure differential between the main fuel line path and the secondary fuel line path.
Dependencies are inferred from the claim text.