Abstract: A cutting tool includes a main body having a working end and an attachment end. A seat is disposed in the working end to receive a cutting insert. A main body passageway for the communication of fluid is disposed in the main body and has a passageway end disposed in the working end. A cutting insert is disposed in the seat. A nozzle is disposed in the passageway end. The nozzle has a nozzle body including front and rear surfaces. The front surface faces generally toward the seat, and the rear surface faces generally away from the seat. The nozzle body defines a plurality of nozzle passageways that extend therethrough between the front and rear surfaces. Each nozzle passageway has a fluid outlet at the front surface.

Abstract: A gas turbine engine that comprises an engine core having a compressor, a turbine, a combustor, and a rotation axis. The engine further comprising a fan case wall having a radially-inner surface, a by-pass duct between the fan case wall and around the engine core, a plurality of struts circumferentially distributed and extending across the by-pass duct, a surface cooler adjacent to the radially-inner surface of the fan case and configured to be exposed to a by-pass air flow through the by-pass duct during operation of the gas turbine engine, the surface cooler fluidly communicating with a fluid circuit of the engine requiring cooling for of a fluid, and a recirculation conduit extending between an inlet in the radially-inner surface of the fan case disposed downstream of the surface cooler and an outlet in the radially-inner surface of the fan case wall disposed upstream of the surface cooler.