A turbine engine nozzle can include a primary outer wall extending from an engine core area to an annular wall terminus that surrounds an engine tail cone, to form a core nozzle. The turbine engine nozzle also includes a single engine core cowl extending from the engine core area to an annular cowl terminus to form a core compartment vent nozzle. The core compartment vent nozzle exhausts air from a core compartment in a trailing edge between the single engine core cowl and the primary outer wall.
TRAILING EDGE CORE COMPARTMENT VENT FOR AN AIRCRAFT ENGINE
30.03.2017
Patent
Elektronische Ressource
Englisch
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