| Specialty Metals That Make Our WorldTM |
|
| |
 |
| C-103
ALLOY (Nb-10 Hf-1 Ti), CONT., P. 3 |
|
WELDING
A pickling operation should be conducted before and
after welding as well as before and after heat treating.
If pickling is performed, welding of niobium alloys
can be readily accomplished by both the TIG and electron
beam processes. It is recommended that all copper tooling
should have a hard chrome plating approximately 0.002"
thick without a nickel strike. This prevents copper
contamination which causes brittle welds. For TIG, properly
designed trailer shields and backup grooves with adequate
gas flow can give weldments a quality equal to welds
made with electron beam equipment. Where possible, the
argon and helium should be passed through hot zirconium
chips, maintained at 800° F to gather minute impurities
in the gas. Stake welds of any length can be made without
mismatch or burn-out. Girth welds by the TIG process
have been made up to 54", matching .010" to .020" material.
Welding of C-103 sheet is often accomplished without
weld wire. Material over 0.100" thick should be welded
by electron beam process.
Generally, weld wire is not used because of the high
cleanliness requirements for welding. The weld wire
often has slight serrations and laps that are difficult
to clean. Sheet is welded within two hours after pickling,
and it is not possible to pickle a roll of welding wire
each time it is used.
In
addition, the high melting point of niobium causes the
wire to deflect and give an uneven weld bead and incomplete
penetration. To eliminate these problems and still get
a weld with an adequate crown and root, the mating edges
to be welded are rolled up to form a "burned-down flange".
The material is then welded with back-up gas and a trailer
shield at a very high welding speed. The gases are a
combination of helium and argon. TIG welding of second
generation niobium alloy, C-129Y to C-103 has been very
successful.
|
|
TABLE
6 - MECHANICAL PROPERTIES OF BARE METAL TIG WELDMENTS
(C-103 TO C-103)
|
|
Thickness |
|
UTS |
YTS |
% Elongation |
| Specimen |
in inches |
Condition |
psi |
psi |
in 1 inch |
| 1 |
.030 to .030 |
Annealed |
59,500 |
40,400 |
27.0 |
| 2 |
.020 to .020 |
As Welded |
61,700 |
44,900 |
14.0 |
| 3 |
.020 to .020 |
Annealed |
60,200 |
42,100 |
16.0 |
| 4 |
.020 to .020 |
As Welded |
62,400 |
46,500 |
13.0 |
| 5 |
.020 to .020 |
Annealed |
59,600 |
41,400 |
18.0 |
| 6 |
.020 to .030 |
As Welded |
61,100 |
46,200 |
13.0 |
| 7 |
.020 to .030 |
As Welded |
61,600 |
45,200 |
14.0 |
| 8 |
.020 to .030 |
Annealed |
60,200 |
42,200 |
14.0 |
| 9 |
.020 to .030 |
Annealed |
60,400 |
42,700 |
13.0 |
| 10 |
.030 to .030 |
As Welded |
61,900 |
45,500 |
20.0 |
| 11 |
.020 to .030 |
Annealed |
60,000 |
40,700 |
25.0 |
| 12 |
.030 to .030 |
As Welded |
61,000 |
46,900 |
20.0 |
Note: All above anneals one hour at 2200°F
Page
21 of 34 Next
INDEX
CORROSION RESISTANCE
PROPERTIES FABRICATION
NIOBIUM
PRODUCTS SPECIFICATIONS
of NIOBIUM
NIOBIUM ELECTRONICS APPLICATIONS
|
|
|
|