ORNL-4191 - the Molten Salt Energy Technologies Web Site

ORNL-4191 - the Molten Salt Energy Technologies Web Site ORNL-4191 - the Molten Salt Energy Technologies Web Site

moltensalt.org
from moltensalt.org More from this publisher
05.08.2013 Views

~ - - _. -1 EXP HEAT 168-0% Zr t- L z 100 i , e 0 3 n 80 Id u EXP HEAT 171 - 0 5% Zr 224 EXP HEAT 169 - 0 4 % Zr , - I 1 1 EXP HEAT 474-1% Zr -0.1% Re I EXP HEAT 170 -0.3 % Zr i ORNL--DWG 61 (1837 EXP HEAT 115 ---1% Lr - 4 % Re 4400 1800 2200 2600 4400 1800 2200 2600 1400 1800 2200 2600 TESTING TEMPERATURE (OF) Fig. 18.6. Results of the Hot-Ductility Study Showing the Effect of Zirconium on the Modified Hastelloy N. Symbols: O.H., tested on heating; O.C., tested on ccoling. URNL-DWG 67 11838 ALLOY NOKlhiAL COMPOSITION (wt %I NI Mo Cr Fe Zr 168 BAL i2 7 474 BAL 12 7 05 ”O MSRE GRADE HASTELLOY N BAL 46 7 r T E S T E b I N G 4 80 60 - 40 a-” I 5 20 lx a r- O z 100 0 0 3 80 a 1.1 TESTED ON COOLING IT MSRF GRADE HN 60 40 20 0 1409 1600 1800 2000 2200 2400 TEST TEMPERATURE F) Fig. 18.7. The Hot-Ductility Results of Selected Alloys. circular weld beads was 6 in. (see Fig. 18.8). The welds were made with stationary inert-gas tungsten arc torches while the disk rotated around its center in a vertical plane. This technique was selected in order to minimize the bending effect associated with the transverse shrinkage. For the radius and thickness ratio of our specimen, it is correct to assume that the stress distribution associated with the weld shrinkage is planar. The perpendicular shrinkage is negligible; that is, there are no stresses perpendicular to the plane of the disk. With these assumptions, the stress distribution may be determined by measuring only the tangential strain on the rim of the disk while machining a series of concentric sections beginning at the disk center. We followed essentially the “boring Sachs” nrethod which was set up for pipes. Since plane ,

ORWL-DWG 67-tIP39 !-in -THICK PLATE Fig. 18.8. Sketch Showing the Location of the Weld Bead in Relation to the Overall Specimen Geometry. 225 ORFIL-UIWG 67-11440 strain and stress problems can be studied with the same equations, the relationships for the pipe will be valid for the disk with the elimination of the terms due to the longitudinal stresses: Fig. 18.9. Pictorial Explanation ob the Symbols Used where

~ -<br />

- _.<br />

-1<br />

EXP HEAT 168-0% Zr<br />

t-<br />

L<br />

z 100 i ,<br />

e<br />

0 3<br />

n 80<br />

Id<br />

u<br />

EXP HEAT 171 - 0 5% Zr<br />

224<br />

EXP HEAT 169 - 0 4 % Zr<br />

,<br />

- I 1 1<br />

EXP HEAT 474-1% Zr -0.1% Re I<br />

EXP HEAT 170 -0.3 % Zr i<br />

<strong>ORNL</strong>--DWG 61 (1837<br />

EXP HEAT 115 ---1% Lr - 4 % Re<br />

4400 1800 2200 2600 4400 1800 2200 2600 1400 1800 2200 2600<br />

TESTING TEMPERATURE (OF)<br />

Fig. 18.6. Results of <strong>the</strong> Hot-Ductility Study Showing <strong>the</strong> Effect of Zirconium on <strong>the</strong> Modified Hastelloy N.<br />

Symbols: O.H., tested on heating; O.C., tested on ccoling.<br />

URNL-DWG 67 11838<br />

ALLOY NOKlhiAL COMPOSITION (wt %I<br />

NI Mo Cr Fe Zr<br />

168 BAL i2 7<br />

474 BAL 12 7 05<br />

”O<br />

MSRE GRADE<br />

HASTELLOY N BAL 46 7<br />

r T E S T E b I N G<br />

4<br />

80<br />

60<br />

- 40<br />

a-”<br />

I<br />

5 20<br />

lx<br />

a<br />

r- O<br />

z 100<br />

0<br />

0<br />

3 80<br />

a<br />

1.1<br />

TESTED ON COOLING<br />

IT MSRF GRADE HN<br />

60<br />

40<br />

20<br />

0<br />

1409 1600 1800 2000 2200 2400<br />

TEST TEMPERATURE F)<br />

Fig. 18.7. The Hot-Ductility Results of Selected<br />

Alloys.<br />

circular weld beads was 6 in. (see Fig. 18.8). The<br />

welds were made with stationary inert-gas tungsten<br />

arc torches while <strong>the</strong> disk rotated around its center<br />

in a vertical plane. This technique was selected<br />

in order to minimize <strong>the</strong> bending effect associated<br />

with <strong>the</strong> transverse shrinkage. For <strong>the</strong> radius and<br />

thickness ratio of our specimen, it is correct to<br />

assume that <strong>the</strong> stress distribution associated<br />

with <strong>the</strong> weld shrinkage is planar. The perpendicular<br />

shrinkage is negligible; that is, <strong>the</strong>re are<br />

no stresses perpendicular to <strong>the</strong> plane of <strong>the</strong> disk.<br />

With <strong>the</strong>se assumptions, <strong>the</strong> stress distribution<br />

may be determined by measuring only <strong>the</strong> tangential<br />

strain on <strong>the</strong> rim of <strong>the</strong> disk while machining<br />

a series of concentric sections beginning at <strong>the</strong><br />

disk center.<br />

We followed essentially <strong>the</strong> “boring Sachs”<br />

nrethod which was set up for pipes. Since plane<br />

,

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!