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US 5,343,691 AGranted
Reducing thermal deposits in propulsion systems
AssigneeGeneral Electric Company
InventorGeorge A. Coffinberry
Life of this patent
Estimating the term…
Abstract
This invention provides a method to mix a relatively large amount of non-condensable gas with fuel prior to gasification heating thus reducing the residence time of the fuel adjacent to hot surfaces. The non-condensable gas may be air, a cryogenic such as methane, or a chemical fraction of the gasified fuel which by itself does not promote the formation of significant amounts of gums or coke deposits.
Claims3
A method for combusting fuel in a gas turbine engine comprising the following steps:
- mixing a compressed gas with liquid fuel in a first mixing means to form a liquid and gas mixture prior to heating the liquid and gas mixture,
- flowing the liquid and gas mixture through a heat exchanger and gasifying all of the liquid fuel and gas thereby forming a fuel and air gaseous mixture,
- flowing a first portion of the fuel and air gaseous mixture to the gas turbine engine combustion section and combusting the fuel and air gaseous mixture,
- flowing a second portion of the fuel and air gaseous mixture to a second mixer, and
- mixing air compressed by the compressor section of the gas turbine engine with the second portion of the fuel and air gaseous mixture in the second mixer thereby forming a relatively cool air and fuel gaseous mixture and flowing the relatively cool air and fuel gaseous mixture to the first mixing means to serve as the compressed gas for mixing with the liquid fuel.
2 more elements
Dependencies are inferred from the claim text.