COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE AND A METHOD FOR OPERATING THE SAME
A cooled fuel injector system of a combustor section of a gas turbine engine is provided. At least a part of the fuel injector system is exposed to core gas flow traveling through the engine. The cooled fuel injector system includes a source of a first cooling fluid and a fuel injector system compon...
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Main Author | |
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Format | Patent |
Language | English |
Published |
16.01.2020
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Subjects | |
Online Access | Get full text |
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Summary: | A cooled fuel injector system of a combustor section of a gas turbine engine is provided. At least a part of the fuel injector system is exposed to core gas flow traveling through the engine. The cooled fuel injector system includes a source of a first cooling fluid and a fuel injector system component. The first cooling fluid is at a temperature lower than a temperature of the core gas flow proximate the fuel injector system. The fuel injector system component includes a vascular engineered structure lattice (VESL) structure, which VESL structure is in fluid communication with the source of the cooling fluid. |
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Bibliography: | Application Number: US201916519471 |