FAN CASE WITH INTERLEAVED LAYERS

A fan case for a gas turbine engine includes an annular liner (72) and an annular case body (74). The liner (72) has a plurality of liner fiber layers (76). The case body (74) surrounds the liner (72). The case body (74) includes a plurality of first and second fiber layers (78, 80). The first fiber...

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Bibliographische Detailangaben
Hauptverfasser:	KLING, Colin J, LUSSIER, Darin S
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS STEAM ENGINES TRANSPORTING WEAPONS WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	A fan case for a gas turbine engine includes an annular liner (72) and an annular case body (74). The liner (72) has a plurality of liner fiber layers (76). The case body (74) surrounds the liner (72). The case body (74) includes a plurality of first and second fiber layers (78, 80). The first fiber layers (78) extend axially beyond the second fiber layers (80) in axially forward and aft directions and the second fiber layers (80) are interleaved with the first fiber layers (78). The first fiber layers (78) each have a first fiber architecture and the second fiber layers (80) each have a second, different fiber architecture.