FAN CASING AND MOUNT BRACKET FOR OIL COOLER

A turbine engine for an aircraft can includes a casing. The casing can be a fan casing surrounding a fan assembly for drawing air into the turbine engine. The fan casing can have a peripheral wall. A surface cooler can be provided in the turbine engine confronting the peripheral wall of the fan casi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Burdette, Jason Levi, Dreischarf, Derek Thomas, Luschek, Bernard Albert, Hundley, Walter Arthur
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A turbine engine for an aircraft can includes a casing. The casing can be a fan casing surrounding a fan assembly for drawing air into the turbine engine. The fan casing can have a peripheral wall. A surface cooler can be provided in the turbine engine confronting the peripheral wall of the fan casing. The surface cooler can have a mounting bracket for mounting the surface cooler to the fan casing.