FAN CASING ASSEMBLIES AND METHOD OF MOUNTING A COOLER TO A FAN CASING

A fan casing assembly for a turbine engine including a fan casing having a peripheral wall (54), a surface cooler (50) having a first surface (66) confronting the peripheral wall (54) and forward and aft projections, which are radially spaced from the first surface (66) and located between the perip...

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Bibliographische Detailangaben
Hauptverfasser:	DREISCHARF, Derek Thomas, LUSCHEK, Bernard Albert, HUNDLEY, Walter Arthur
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A fan casing assembly for a turbine engine including a fan casing having a peripheral wall (54), a surface cooler (50) having a first surface (66) confronting the peripheral wall (54) and forward and aft projections, which are radially spaced from the first surface (66) and located between the peripheral wall (54) and the first surface (66), and a mounting bracket (90) to mount the surface cooler (50) to the fan casing and a method of mounting a surface cooler (50) to a fan casing of a turbine engine.