CFRP FUSELAGE FRAME FIXED TO VERTICAL TAIL FIN

To meet the need to reduce aircraft production costs related to corrosion protection measures being taken with use of different materials such as aluminum for frames and CFRP for the outer skin of an aircraft, and to reduce thermal fatigue resulting from thermal expansion effects on interconnected s...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PAUL DIEP, PHIYEN T PHAM
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS 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!