MIL-S-7809A
PMl!ud of form |
Produet.tze |
LocatfOll of lo11dt11&a1ula of: test a~ |
Bars, fiat |
(ladaes) l;: wide and over |
Coincides with the axis located midway between the edge |
and center of the section
Plates, shapes, sheets, 0.250 Coincides with the central longitudinal axis, or with the or strips axis located midway between the flat surfaces, as appli·
cable
Plates and sllapea 0.250 to 1.0 Coincides with the longitudinal axis from a random posi· tion from a aide edge or from a random position between a side edge midway between the center and edge of the plate with the axis of the specimen midway between the two flat surfaces, as applicable
Full section or prepare test specimens 1* inches wide
(or smaller, if_ necessary)
TABLE VII. Relationship of bend test inside diamiets,.
to tll.ialmesa of specimm
4.6.3 Preparing specimens for e:r:am:i:~
tion. After completion o.f test fillet welds, the
Thldmeu of material (Saches)
0.500 and less
0.501 ·to 1.600 inclusive
1.501 to 4.000 inclusive
Ratio ot bead dlomoter to thick-
1iesa of 111edmen
1
2
s
specimens shall be allowed to remain in still air at room temperature for 24 hours before
examination. Before sectioning for test cuts, the test specimen shall be visually examined at not more than 10 diameters magnification for cracks in the base metal. Following this examination, at least three test cut sections
4.6.2 We"lding procedure. The size of the
fillet welds on test specimens shall not exD ceed 1/2 of the thickness of test plates % inch and over (T/2 in .figure 1)• For test plate
thickness less than '3J8 inch, the size of the
fillet welds shall not exceed the plate thickD
ness. Welds shall be made in one pass, except
that fillet welds larger than=% inch may be made in two passes. The initial temperature during welding for test specimens 1 inch or less in diameter shall not exceed 100° F. Test specimens over 1 inch thick may be preD heated, at the option of the contractor. SpeciD mens shall be permitted to cool to not less than .100° F nor more than 125'° F between passes or between welds D, E, F, and G (see figure 1). A class MIL-6013 welding elecD trode conforming to Specification ·MIL-E-
15599 shall be' used to determine weld-crack susceptibility of the steel.
shall be taken not less than 2 inches apart and at least 2 inches from either end of the specimen, as shown in figure 1. Specimens may be annealed after welding and prior to sectioning in order to facilitate machining.
4.6.4 E~a.mina.tionfor cracks. The test cut sections selected shall be surface-ground and examined with the aid of magnetic-particle inspection methods for cracks in the test plate adjacent to the test welds. The presence of cracks in the base metal shall be cause for rejection of the particular heat of steel th.at is represented by the test plate. The occurD
rence of cracks in the weld metal only shall
not be cause for rejection. Specimens sh811
be examined for cracks adjacent to all welds in accordance with Specification MII-1-6868. Examination shall be by means of the con·
tinuous method, using half-wave direct cur·
9
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