Turbine engine thermal management
作者： Jeffrey Glover , Brandon Wayne Miller
DOI:
关键词: Turbine 、 Four-stroke engine 、 External combustion engine 、 Heat exchanger 、 Combustion chamber 、 Internal combustion engine 、 Cylinder (engine) 、 Engine coolant temperature sensor 、 Marine engineering 、 Engineering
摘要: A gas turbine engine (10) including core (16) is provided. Air may enter the through an inlet and travel air flowpath (64) extending (16), e.g., generally along axial direction of (10). The additionally includes a cooling (70) outwardly radial R extends between in flow communication with outlet defined by opening outer casing (18) (16). Moreover, heat exchanger (72) positioned at least partially within over or (72).
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