SECONDARY STRUCTURES FOR AIRCRAFT ENGINES AND PROCESSES THEREFOR

Processes for fabricating secondary structures of gas turbine engines from polymer-based materials, and secondary structures formed thereby. The processes entail performing an additive manufacturing technique to produce a secondary structure of a gas turbine engine. The additive manufacturing techni...

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Bibliographische Detailangaben
Hauptverfasser:	DIETSCH, BENJAMIN, ALLEN, WOLFE, JARED, MATTHEW, KOSTKA, JAMES, MICHAEL, DALE, DAVID, EDWARD
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F,C08G AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING CHEMISTRY COMPOSITIONS BASED THEREON GENERAL PROCESSES OF COMPOUNDING METALLURGY ORGANIC MACROMOLECULAR COMPOUNDS PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS THEIR PREPARATION OR CHEMICAL WORKING-UP TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL WORKING-UP
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Beschreibung
Zusammenfassung:	Processes for fabricating secondary structures of gas turbine engines from polymer-based materials, and secondary structures formed thereby. The processes entail performing an additive manufacturing technique to produce a secondary structure of a gas turbine engine. The additive manufacturing technique directly produces the secondary structure from a polymer-based material to have a complex three-dimensional shape characterized by portions that lie in different planes.