GAS TURBINE ENGINE COMPONENT WITH INTEGRALLY FORMED STIFFENERS

A gas turbine engine component includes a tubular body section (66) including a plurality of fiber wraps encompassed within a matrix composition and one or more integrally-formed stiffeners (84) extending from an outer surface (86) of the body section and in a component circumferential direction aro...

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Bibliographische Detailangaben
1. Verfasser:	KLING, Colin J
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE 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 gas turbine engine component includes a tubular body section (66) including a plurality of fiber wraps encompassed within a matrix composition and one or more integrally-formed stiffeners (84) extending from an outer surface (86) of the body section and in a component circumferential direction around the body section. The stiffener includes one or more fiber wraps extending radially outwardly from the body section over a form and to the body section from the form.