COEFFICIENT OF THERMAL EXPANSION CONTROL STRUCTURE

The present invention is directed to the incorporation of a substructure into tooling for constructing composite structures in order to control thermal expansion of the tooling during aerospace manufacturing processes. Substructure, such as headers and/or gussets is added to the tooling to constrain...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LITAKER, CASEY, GRANT, NEWKIRK, TODD, LELAND, CLEARY, WILLIAM, RUSSELL, JR, DOYON, JOSHUA, JOSEPH
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:The present invention is directed to the incorporation of a substructure into tooling for constructing composite structures in order to control thermal expansion of the tooling during aerospace manufacturing processes. Substructure, such as headers and/or gussets is added to the tooling to constrain the growth of the laminate expansion and/or control the diametric growth of the tool during the curing cycle. The thickness of the face-sheet of the tooling also may be reduced in order to further reduce the effective coefficient of thermal expansion (CTE) of the tooling.