Mechanisms of adhesion and diffusion bonding of powdered alloy sheet.

1988 ◽  
Vol 35 (2) ◽  
pp. 53-57
Author(s):  
Tsuyoshi Morishita ◽  
Shigemi Ohsaki ◽  
Kiyohiro Kamei
Author(s):  
Ho Sung Lee ◽  
Jong Hoon Yoon ◽  
Yeong Moo Yi ◽  
Dong Hyuk Shin

1989 ◽  
Vol 20 (4) ◽  
pp. 627-636 ◽  
Author(s):  
O. Buck ◽  
R. B. Thompson ◽  
D. K. Rehbein ◽  
D. D. Palmer ◽  
L. J. H. Brasche

1994 ◽  
Vol 170-172 ◽  
pp. 737-742 ◽  
Author(s):  
Oscar A. Kaibyshev ◽  
Ramil Ya. Lutfullin ◽  
Rinat V. Safiullin ◽  
S.N. Fatkullin

2007 ◽  
Vol 20 (4) ◽  
pp. 307-312 ◽  
Author(s):  
W HAN ◽  
K ZHANG ◽  
B WANG ◽  
D WU

1984 ◽  
Vol 21 (1) ◽  
pp. 61-64 ◽  
Author(s):  
W. T. Chandler ◽  
A. K. Ghosh ◽  
W. M. Mahoney

Author(s):  
I E Bottomley

The diffusion bonding (DB)/superplastic forming (SPF) manufacturing process, for titanium 6A1/4V material, has been developed within British Aerospace for the manufacture of military aircraft components. Diffusion bonding of titanium alloys offers the potential for parent metal joint strengths, and when combined with SPF, complex aircraft components offering significant cost and weight savings can be manufactured. This paper briefly describes the DB/SPF development programme and the manufacture of the Tornado heat exchanger ducts and European Fighter Aircraft (EFA) foreplane components.


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