COMPOSITE MANUFACTURING METHOD

A method of manufacturing a composite panel, the method comprising: fitting a control member (70) through the panel; fitting a plug (75) through a compaction tool (45); engaging the control member with the plug; engaging the plug with a datum surface of the compaction tool; compacting the panel with...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	KALLINEN, RISTO
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES 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 TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A method of manufacturing a composite panel, the method comprising: fitting a control member (70) through the panel; fitting a plug (75) through a compaction tool (45); engaging the control member with the plug; engaging the plug with a datum surface of the compaction tool; compacting the panel with the compaction tool; and disengaging the plug from the control member after the panel has been compacted.