Oil coolers for aerospace propulsion applications manage thermal loads within gas turbine and reciprocating engine lubrication circuits, employing air-cooled or fuel-cooled plate-fin, tube-and-shell, or brazed-core heat-transfer assemblies manufactured from titanium, aluminium alloy, or nickel-based materials, and integrated within the engine oil system to maintain lubricant viscosity and prevent thermal degradation under MIL-SPEC and EASA-compliant design requirements.
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