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
~ - - _. -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
- Page 184 and 185: 174 BI I - CARRIER - ...... -+ SAMP
- Page 186 and 187: olten- I rr Molten-salt breeder rea
- Page 188 and 189: I COLD LEG RETURN LIN 178 CORE OUTL
- Page 190 and 191: March 17 following the fission prod
- Page 192 and 193: Table 15.3. Comparison of Values fo
- Page 194 and 195: likely cause of failure is the rapi
- Page 196 and 197: 186 Fig. 15.6. Inner Surfoce of Col
- Page 198 and 199: 188 Fig. 15.8. Inner Surface of Cor
- Page 200 and 201: on final salt samples. 'This value
- Page 202 and 203: P c9 P 082 P 8'ZF P 1.11 .c OF P S0
- Page 204 and 205: HFIR FUEL ELLEMENT ,EXPERIMEUT 194
- Page 206 and 207: Our materials program has been conc
- Page 208 and 209: 198 SPLIT STRAP SLEEVE BAND (a) S F
- Page 210 and 211: others, but all three stringers in
- Page 212 and 213: - Y) a - 70 60 50 40 (0 m 30 + m 20
- Page 214 and 215: 204 Fig. 16.7. Photomicrographs of
- Page 216: 206 Fig. 16.9. Photomicrographs of
- Page 219 and 220: AXF-5QRG 4-4 4 a9g/rm3 4f 56 % ~ AX
- Page 221 and 222: Carbon Corporation, Poco Graphite,
- Page 223 and 224: was found. In view of the low react
- Page 225 and 226: SIC TEMPERATURE STAINLESS STEEL TUB
- Page 227 and 228: 18.1. IMPRQVING THE RESISTANCE are
- Page 229 and 230: These aging studies will be expande
- Page 231 and 232: 221 Fig. 18.3. Hastellay N Containi
- Page 233: Fig. 18.5. Hasvellcy N (Titanium Mo
- Page 237 and 238: 227 Toble 18.3. Thermal Convection
- Page 239 and 240: 229 ORNL-DWG 67-io980 Impurity Anal
- Page 241 and 242: 231 Fig. 18.16. Hastelloy N Thermal
- Page 243 and 244: time what the effective diffusiviti
- Page 245 and 246: Figure 18.20 shows an area near the
- Page 247 and 248: The third design, which is also a d
- Page 249 and 250: Part 6. Molten-Salt Processing and
- Page 251 and 252: that the behavior of the rare-earth
- Page 253 and 254: 22. Distillation of MSRE Fuel Carri
- Page 255 and 256: 23. Steady-State Fission Product Co
- Page 257 and 258: sec (50 hr). These latter residence
- Page 259 and 260: analysis of filtered samples and th
- Page 261 and 262: 25. Modifications to MSRE Fuel Proc
- Page 263: nickel line through a sintered meta
- Page 267 and 268: 1. R. K. Adams 2. G. M. Adamson 3.
- Page 269 and 270: 344. E. H. Taylor 345. W. Terry 346
~ -<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 />
,