Advancements in the Fabrication Technology of Titanium for the C-5A. Presented at the Materials Engineering Exposition and Congress(1968) Held in Detroit, Michigan on 14-17 October 1968

Advancements in the Fabrication Technology of Titanium for the C-5A. Presented at the Materials Engineering Exposition and Congress(1968) Held in Detroit, Michigan on 14-17 October 1968

The application of titanium for aircraft structural and functional components on the C-5A consists of sheet, plate, forgings, extrusions, tubing, and ducting. Parts are made from commercially pure titanium and the following alloys: Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-8Al-1Mo-1V, Ti-5Al-2.58Sn, and Ti-3Al-2...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: White, Kyle R
Format: Report
Sprache:eng
Schlagworte:
AIRCRAFT EQUIPMENT
AMPTIAC COLLECTION
C-5A AIRCRAFT
Fabrication Metallurgy
FASTENINGS
SYMPOSIA
TITANIUM ALLOYS
TRANSPORT AIRCRAFT
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Beschreibung
Zusammenfassung:The application of titanium for aircraft structural and functional components on the C-5A consists of sheet, plate, forgings, extrusions, tubing, and ducting. Parts are made from commercially pure titanium and the following alloys: Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-8Al-1Mo-1V, Ti-5Al-2.58Sn, and Ti-3Al-2.5V. There Are approximately 1.3 million titanium fasteners used on each C-5A out of a total usage of 2 million fasteners. Titanium fasteners are made of Ti-6Al-4V, Ti-6Al-6V-2Sn, Ti-1Al-8V-5Fe alloys and consists of tapered interference fasteners as well as streight shank fasteners.