+ - - VR : . LA + 7 ' 11 ! 4 ادرار ! - . . IT - . ! LI UNCLASSIFIED ORNL IN I 1 ' . W : 1.24 E- SIN : . : Y Wi cher -2 166 i I M ' . . MAP 77 - . . :.. " . 1 . - 1 .. 1 Y . .. . "" 11'. ' . ' * .. . , ". , , -,- $:, . . * . : . F U . . . hi --- - 1 " . : " 2.1 il 1 ii' 17 ry w 1. ! AY Milli ORNA-P-166 . ..$ mary of paper to be presented at American Nuclear Society Symposium on "Vapor It üsition Techniques for Fabrication of Fuels and Refractory Metal Tubing" in San Francisco, California, November 30 to December 3, 1964. . CONF-654-9 A . TECHNIQUES FOR DEPOSITION AND SYSTEMATIC STUDY OF PROPERTIES OF PYROLYTIC CARBUIN ON CERAMIC FUEL PARTICIES* MASTER SW hu : AUG 1 3 1964 EXT- R. L. Beatty, J. L. Cook, and F. L. Carlsen, Jr.** Metals and Ceramics Division Oak Ridge National Laboratory Oak Ridge, Tennessee . 4. RT1 Techniques have been developed for fluidized-bed coating of carbide : i . . and oxide fuel particles with pyrolytic carbon at temperatures to 2000 C under precisely controlled conditions. Systematic studies of the effects of deposition conditions on coating properties were accomplished using either Sic or graphite resistance-heated furnaces. The particles were coated in graphite tubes 3/4 in. or l in. I.D., with 30° included-angle nozzles and the heating elements and gas-entrance ports of the nozzles were positioned so as to minimize the variation of temperature in the " ! beds. Temperature control was based upon calibrations of tube temperature (monitored during operation) with measurements of the true bed temperature. Detailed evaluation of the coated particles included coatins density TË 2 measurements, electron microscopy and diffraction, and determination of * such crystallographic parameters as interlayer spacing, Co, apparent crystallite size, Ic, and preferred orientation by x-ray diffraction. 115 *Research sponsored by the U. S. Atomic Energy Commission under contract with the Union Carbide Corporation. **Sponsored by W. 0. Harms, member ANS. -LEGAL NOTICE Q MOT FOR PUBLIC RELEASE - OFFICIAL DISTRIBUTION MAY BE MADE. OFFICIAL REQUESTS MAY BE FILLED. REPORT CONTAINS NOTHING OF PATENT INTEREST PROCEDURES ON FILE IN RECEMMS. SECTION 24 -- - 3 O " " . 11 MLN MULLA T 'I TIM " 2 Terjerature of applicacion is a dominant coating variable in that it aifects -... measurable properties of the coatings. For example, the apparent crystallite size increases and the strength decreases with increasing coatină temperature. Coating density passes through a minimum in the intermediate temperature range. Another major variable, though not an independent one, is deposition rate. This rate is contro led by the temperature of the fluid bed, the temperature of the fluidizing gas, tine hydrocarbon gas flow rate, and the setioce area of the charge being coated. The importance of methane partiai pressure and average deposi- tion rate on the properties of coatings applied at 1400 C is shown in Fig. 1. In these experiments, the fuel particles consisted of dense uranium dicarbide, 150-2504 in diameter, and the average coating thickness was 50u. The total flow rate of methane plus helium (760 cm3/min), initial charge size (10 6), and volume of car- bon deposited were held constant. The inside diameter of the re- action vessel was 3/4 in. Density was measured by a helium pycnometer - technique and values of C. and L, were determined by refined x-ray. diffractometer methods. Preferred orientation was evaluated by the technique described by Bacon on coatings stripped from small graphite disks included in the fluid-bed coating runs after the method used by Bokros." In this technique a pole figure is derived Ko in the form of the integrated intensity, I(6), of the (002) reflection as a function of the inclination angle, ø, relative to the normal of the deposition plane. This functional relationship is approximated by cosy, where the anisotropy parameter, M, is N.NL SA : 11 . UNS SSII :) ORNL-6.10 64-531iR 2.5 5 10 170 - ► DEPOZITION RATE (u/hr) 50 100 ' COATING DENSITY I A CRYSTALLITE SIZE, Lc. A ANISOTROPY PARAME 0 INTER LAYER SPACING, Co 3.52 4. ... 46 T 3. 50 . 3.48 COATING DENSITY (g/cm3) --- - 3.46 O INTER LAYER SPACING, CA (A) CRYSTALLITE SIZE, LE (A) statit- M1 (0oz / Cox = M+1) lo... 3.44 . cm -- - 3.42 J 22 - 10 20 500 1000 50 100 200 METHANE PARTIAL PRESSURE (mm) 4 TIR . . . Effect of Methane Partial Pressure on Properties of 50.4-thick Pyrolytic Carboil Coatings Deposited on Spheridal Uranium Carbide Particles in a Fluidized Bed at 1400°C. * ,,! ti . ' . 2 tu.' . Wii SW. mor . . . " SM r AU . V 2 . .1 me , . W , . PLE .'" '. W h", 2. OK . 1, H2 . t ! . - 5 - M " * . t. . . 4 - -. - . . Y PEX LPINES in NO Higure 1. Effect of Methane Partial Pressure or Properties of 50-4- thick Pyrolytic Cazdon Coatings Deposited on Spheroidal Uranium Carbide Particles in a Fluiäized Bed at 1400°C. lii' A2 W . TW . phone WWW.BS S 1 I ZEMLDT 2 NIN P W WW ' ' VINA WW ih "Wi of . " related to the Bacon anisotropy factor, Coz/ooxs by 0oz/Cox = M + 1. It is of interest to note that coniitions which gave a minimum in density and in Lc yielded a coating with maximum anisotropy, and that essentially random orientation was obtained at average deposi- tion rates greater than about 30u/hr. Electron diffraction and transmission microscopy studies showed that the as-deposited coatings consisted 01 turbostratically stacked monolayers having the hexagonal graphite structure with a basal-plane crystallite size, La, of approximately 100 A. LOW density dieposits contained microvcids approximately 100 A in diameter and the density of the microvoids increased as the coating density decreased. There was no significant change in I, with density. i 1. Carlsen, F. L., Jr., et al., "Development of Fueled Graphite Con- taining Pyrolytic-Carbon Coated Carbide Particles for Nonpurged, Gas-Cooled Reactor Systems." (To be published in Nuclear Science and Engineering.) 2. Cools, J. L., et al., ÜCR Program semiann. Frogr. kept. Mar. 31, 1963, ORNL-3523, pp. 103-06. 3. Bacon, G. E., J. Appl. Chem. 6, 77-81 (1956). 4. Bokros, J. C., Private Communic tion. 5. Stiegler, J. O., et al., An Electrin Optical Study of Structural Features of pyrolytic Carbons, ORNL-IM-863 (in press). Features of jyro ytic Carbons, ORNL-T **** 1. . - . . . . www 1. " I) ! DATE FILMED 1/ 1865 . 11 -LEGAL NOTICE The report was prepared M M sacows of Government sponsored work. Metters the United Satos, nor the Commission, nor any person acting on ball of the Coundon: A. Makes any warranty or representation, expressed or implied, with respect to the accu- racy, completeness, or wefulness of the tutormation contained to me report, ur that the we of my tabormation, apparatus, method, or process dlaclavad to the report may not Infringe privately owned rights; or B. Ammos y Mantuities of the rompect to the we of, or for d ecorating from the undang tuloration, appuntu, method, or process dlachend to the report. As wood la the abovo, "pernou actug au bohall of the conteston" Includes my a- ploym or contractor of the Commington, or aployee of mucha contractor, to the ocent that much employee of contractor of the Companiesdon, or anployw dl woch contractor preparea, diewentualns, or provide recome to my hotormation part to his employment of contract with the Commiston, or wo employment with me contractor. - END . PI d '