ORNL-2106 - the Molten Salt Energy Technologies Web Site
ORNL-2106 - the Molten Salt Energy Technologies Web Site ORNL-2106 - the Molten Salt Energy Technologies Web Site
ANP PROJECT PROGRESS REPORT Fig. 3.4.39. Crack and Deposit Evident in Fig. 3.4.38 at a Higher Magnification. Etchant: electrolytic oxalic acid. SOOX. 200
EFFECTOF ENVIRONMENTONCREEP- RUPTURE PROPERTIES OF HASTELLOY 6 C. R. Kennedy' Revised design data obtained from creep tests of solution-annealed Hastelloy B sheet stock in various environments at 1300, 1500, and 1650°F ore summarized in Figs, 3.5.1, 3.5.2, and 3.5.3. The times to 0.5, 1, 2, 5, and 10% total strain at each temperature in the various environments are the same, and for stresses for which the rupture life is more than 300 hr the effect of environment is shown to be negligible. The creep curves obtained at 1500OF in air and in argon, shown in Fig, 3.5.4, appear to indicate that the better performance in air than in the other environments at stresses for which the rupture life is less than 'On assignment from Pratt 8, Whitney Aircraft. 3.5. MECHANICAL PROPERTIES STUDIES D. A. Douglas (0 20 50 400 200 TIME (hr) PERIOD ENDING JUNE 16, 1956 300 hr is caused by the ability of air to strengthen Hastelloy B during third-stage creep. For rupture lives longer than 300 hr there is considerably less third-stage creep because of the aging characteristics of the alloy, and, as seen in Figs. 3.5.1, 35.2, and 3.5.3, the effect of environ- ment diminishes. Design curves produced from limited data for solution-annealed Hastelloy B sheet tested at 1800OF in argon and in the fuel mixture (No. 30) NaF-ZrF,-UF, (50-46-4 mole %) are shown in Fig. 3.5.5. At 180OOF Hastelloy B does not age perceptibly and the amount of third- stage creep is great in tests at all stress levels. Thus the fuel dxture strengthens the alloy at all stress levels, Of the environments tested, only those which are "surface active" (produce a thin, tightly adherent film on the surface of the metal) affect the creep properties of the metal. It can be seen from Figs. 3.5.1, 3.5.2, 3.5.3, and 3.5.5 that, of the environments tested, only 500 tow 2 5FeRu ORNL-LR-DWG 14729 D 5000 10,Ooo Fig. 3.5.1. Design Curves for Hastelloy B Sheet Solution Annealed at 210OOF for 2 hr and Tested in Argon and in the Fuel Mixture (No. 30) NaF-ZrF,-UF, (50-46-4 mole 56) at 1300OF. 2 01
- Page 135 and 136: Fig. 3.2.10. Apparatus for Studying
- Page 137 and 138: STATIC TESTS OF INCONEL CASTINGS R.
- Page 139 and 140: t (JnOOSll 3n918-3NOt IOH (JoOOSI)
- Page 141 and 142: after the l00hr test. The extent of
- Page 143 and 144: tests of the Lindsay Mix specimens,
- Page 145 and 146: LJ DEVELOPMENT OF NICKEL-MOLYBDENUM
- Page 147 and 148: LJ PERIOD ENDING JUNE 10, 1956 Fig.
- Page 149 and 150: 2. Canning of the billets with '/,-
- Page 151 and 152: 165 . c, e . c3 a PERIOD ENDING JUN
- Page 153 and 154: u allow the billet to start through
- Page 155 and 156: NEUTRON SHIELD MATERIAL FOR HIGH-TE
- Page 157 and 158: PERIOD ENDfNG JUNE 10, 7956 Fig. 3.
- Page 159 and 160: wrought plate used as base material
- Page 161 and 162: J point. A mixture of 50-50 vol % L
- Page 163 and 164: WELDING PROCEDURE: VERTICAL FIXED,
- Page 165 and 166: 4 2 t 4 2 in. t 2 WCLASSFKO ORNL-LR
- Page 167 and 168: FABRICATION OF JOINTS BETWEEN PUMP
- Page 169 and 170: * h WELDING PROCEDURE PERlOD ENDING
- Page 171 and 172: 1 1 6 in. PUMP BARREL t SECTION AA
- Page 173 and 174: '4 x 6 x 20-in. INCONEL PLATES (/*-
- Page 175 and 176: UNCLASSIFIED PHOTO 17248 Fig. 3.4.1
- Page 177 and 178: through the radiator by passing col
- Page 179 and 180: L, . 1 Q t V ERIOD ENDING JUNE 10,
- Page 181 and 182: to permit the examination of indivi
- Page 183 and 184: LJ . t L t * I LJ Fig. 3.4.33. Tube
- Page 185: Fig. 3.4.37. Inner Surface of Tube
- Page 189 and 190: PERIOD ENDING JUNE 10, 1956 UNCLASS
- Page 191 and 192: Fig. 35.7. Surface Effect on the St
- Page 193 and 194: 44,000 42,000 40,000 - ._ (D 8000 v
- Page 195 and 196: \:r 1 U UNCL 1158 W ioo,ooo 80,000
- Page 197 and 198: fuel mixture (No. 30) NaF-ZrF -UF,
- Page 199 and 200: i u * ‘*$ , .\. The Lindsay Chemi
- Page 201 and 202: 6, * c L . c e 4 gi depths greater
- Page 203 and 204: i 4 Part 4 HEAT TRANSFER AND PHYSIC
- Page 205 and 206: 4.1. HEAT TRANSFER AND PHYSICAL PRO
- Page 207 and 208: This relationship gives the ratio o
- Page 209 and 210: The parameters of the’experiment
- Page 211 and 212: t Fig. 4.1.7. Fuel Annulus of the V
- Page 213 and 214: uncooled wall temperature that woul
- Page 215 and 216: SHIELD MOCKUP REACTOR STUDY L. C. P
- Page 217 and 218: Liquid (688 to 8986C) I . HT - H3Q
- Page 219 and 220: THERMAL CONDUCTIVITY W. D. Powers T
- Page 221 and 222: cd Fig.4.2.4. Slingers from MTR In-
- Page 223 and 224: a plug when they came in contact wi
- Page 225 and 226: couples were used on this loop to e
- Page 227 and 228: 0 20 40 60 80 lo0 I20 440 (60 180 2
- Page 229 and 230: "fast" neutron in a graphite reacto
- Page 231 and 232: eached thermal equilibrium in an in
- Page 233 and 234: 0.5 0.4 - a3 l- W z 0.2 0.1 UNCLASS
- Page 235 and 236: TABLE 4.2.3. RESULTS OF EXAMINATION
ANP PROJECT PROGRESS REPORT<br />
Fig. 3.4.39. Crack and Deposit Evident in Fig. 3.4.38 at a Higher Magnification. Etchant: electrolytic<br />
oxalic acid. SOOX.<br />
200
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