A Study of Self-Glazing Titanium Carbide Base

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A Study of Self-Glazing Titanium Carbide Base A STUDY OF SELF-GLAZING TITANIUM CARBIDE BASE CERMETS Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University By Robert Franklin Stoops, B.S., M.S. The Ohio State University 1951 Approved by Adviser ACKNOWLEDGMENTS The author wishes to thank Mr. Earle T. Montgomery, Senior Research Engineer, Mr. Thomas S. Shevlin, Research Engineer, and Mr. Harold Greenhouse of the staff of the Ohio State University Research Foundation Project 441 for their guidance, aid, and advice and for the design and construction of the equipment used in this investigation. He also wishes to express his appreciation to his adviser, Dr. G. A. Bole, Director of Ceramic Research, Engineering Experiment Station, The Ohio State University, under whose general supervision this work was accomplished. The work described herein was supported, in part, by the Materials Laboratory, Research Division of Wright Air Development Center through a contract between the Air Research and Development Command and The Ohio State University Research Foundation. ii 892567 The University assumes no responsibility for the accuracy or the correctness of any of the statements or opinions advanced in this dissertation. iii TABLE OF CONTENTS Page INTRODUCTION ............................................ 1 SURVET OF LITERATURE.................................... 3 Highly-rRefractory Materials......................... 3 Auxiliary Me t a l s .................................. 7 Cermets.............................................. 17 Sintering In the Presence of a Liquid Phase............20 MODE OF INVESTIGATION.................................... 23 MATERIALS AND EQUIPMENT.................................. 25 Materials............................................ 25 Equipment...................... 30 PROCEDURE................................................ 39 Tests for Physical Properties......................... 39 Titanium Carbide + Silicon Carbide Boron Carbide Base Compositions.................. 41 Titanium Carbide + Titanium Diboride + Silicon Base Compositions....................... 45 RESULTS AND DISCUSSION .................................. 49 Titanium Carbide + Silicon Carbide + Boron Carbide Base Compositions............... 49 Titanium Carbide + Titanium Diboride + Silicon Base Compositions ......................... 67 GENERAL S U M M A R Y .......................................... 97 iv TABLE OF CONTENTS Page CONCLUSIONS............................................ 99 BIBLIOGRAPHY ............................................ 101 AUTOBIOGRAPHY .......................................... 105 v ILLUSTRATIONS Figures Page 1. Ratios of Specific Volumes of Oxides of Metals To Those of the Metals............................ .11 2. Phase Diagram of the Cobalt-Silicon System............ 16 3. Molybdenum-Resistor Furnace ........................... 32 4. Section Through Center of Molybdenum-Resistor Furnace . 33 5. High Frequency Induction Furnace..................... 34 6. Cross Section of High Frequency Induction Furnace.... 35 7. Globar Tube Furnace................................. 37 8. Hot Modulus of Rupture Furnace. .................. 38 9. 721 R + Co Sintered at 3875°F. (Photomicrograph).......53 10. 721 R Jr NiAl Sintered at 3375°F. (Photomicrograph). 54 11. 721 R Sintered at 4100°F. (Photomicrograph).......... 58 12. 721 Sintered at 4100°F. (Photomicrograph) ............. 59 13. Effect of Sintering Temperature on Porosity of TiC + SiC + B.C Base Cermets...................... 63 4 14. Effect of Sintering Temperature on Porosity of TiC + TiB2 Si Base Cermets........................ 72 15. Composition III R Co Sintered at 2800°F. (Photomicrograph) ................................ 74 16. Long Time Oxidation in Open Air at 2000°F................ 77 17. Effect of Changes in Composition on Oxidation of TiC + Ti®2 + Si + Co Cermets...................... 83 vi ILLUSTRATIONS Figures Page IS. Effect of Sintering Temperature on Transverse Strength of TiC + T±B^ 4- Si 4- Co Cermets.......... 87 19. Graphite Boats Containing Fired B a r s ............... 89 20. Ill R B + Co Sintered at 2800°F. (Photomicrograph) .... 91 21. Change of Modulus of Rupture of Composition III R B +• Co with Temperature......................94 Tables I. Data on Highly-Refractory Materials. .............26 II. Particle Sizes of Milled Carbides.................... 28 III. Data on Raw Materials........... 29 IV. Compositions Studied........... 46 V. Results of Wetting Tests .............................. 52 VI. Results of Sintering Tests on 721 Base Composition .... 56 VII. Porosities of Sintered Cermet Pellets Based on 721 .... 62 VIII. Effect of Sintering Temperature on Properties of 721 R 4- C o ....................................... 65 IX. Porosities of Sintered Cermet Pellets Based on TiC 4- TiB2 + Si................................... 69 X. Results of Oxidation Tests . ......................... 75 XI. Values for the Parameter "k" from Long Time Oxidation Tests................................... 76 vii ILLUSTRATIONS Tables Page XII. Effect of Sintering Temperature on Properties of TiC ♦ TiB£ 4- Si + Co Cermets.........................86 XIII. Change of Modulus of Rupture of Composition III R B + Co with temperature.......................93 XIV. Results of Thermal Shock Tests......................... 95 viii INTRODUCTION The efficiency of gas turbines would be greatly increased if they could be operated at temperatures above those currently being used. The metallic alloys from which the turbine blades are made have a relatively short service life at an operating temperature of 1800°F. At present, a material is being sought which will have a useful service life at a temperature between 1800°F. and 2400°F. Such a material should have a high tensile strength to density ratio in this temperature range because the stresses developed in turbine rotor blades are caused mainly by centrifugal forces. The material should also be resistant to oxidation and to thermal and mechanical shock. Much research has been directed toward combining highly-refrac- tory ceramic materials with metals in order to obtain a material that possesses both the high strength to density ratio at elevated temper­ atures of ceramics and the thermal and mechanical shock resistance of metals. Some of these combinations, called "cermets", which show promise utilize titanium carbide as the ceramic phase. However, these cermets lack the necessary oxidation resistance, since their chief constituent, titanium carbide, oxidizes readily at elevated temperatures. If these compositions are to be used successfully in turbine blades, they must be coated with an oxidation resistant material or other constituents must be added to the cermet composi­ tions which will render them oxidation resistant. In an investigation of the titanium carbide - silicon carbide - boron carbide system, Accountius^ found several compositions rich in titanium carbide which had excellent oxidation resistance. These materials were oxidation resistant as a result of the formation of a glass on their surfaces when they were exposed to oxidizing condi­ tions. The purpose of this investigation is to develop a self-glaz­ ing cermet by using one of these oxidation resistant compositions as a base material. SURVEY OF LITERATURE HIGHLY-REFRACTORY CERAMIC MATERIALS Schwarzkopf^ has stated that materials will have high strength at elevated temperatures if the individual crystals have high strength interatomic bonds and if the various crystals have high boundary strength. Highly-refractory materials possess relatively strong inter­ atomic bonds since the energy requirements for melting are related to the atom-to-atom bond strength. He suggests that the powder metal­ lurgy technique could be utilized to control boundary strength. Titanium Carbide Titanium carbide is one of the. most refractory materials known. It has a melting temperature of 5684°F. Gangler, Robards, and 17 McNutt ', who investigated the physical properties at elevated temper­ atures of hot-pressed TiC, MgO, ZrC, B^C, 85$ SiC 15$ B^C, ZrOg, and stabilized Zr02, found that titanium carbide had the best resistance to thermal shock and was generally the most promising of the composi­ tions tested. It had a short-time tensile strength of 15,850 p.s.i. at 1800°F. and 9400 p.s.i. at 2200°F. Deutsch, Repko, and Lidman^ concluded from their investigation that titanium carbide base cermets may eventually be used as gas turbine blade materials in the temper­ ature range of 1600°F. to 2400°F. 33 Nowotny and Glenk asserted that titanium carbide tends to have a lattice which is deficient in carbon. The best titanium carbide -3- that they could obtain had only 19*36# carbon, whereas the theoret­ ical value is 20.0#. Franssen"^ has stated that, as a rule, com­ mercial titanium carbides do not contain more than 18# of fixed carbon; but, in order to obtain a fixed carbon content of 18#, an excess of carbon must be used. This free carbon remains in the carbide as graphite. Skaupy^ also thinks that commercial titanium carbides contain less than theoretical carbon, but that they contain an oxide of titanium in solid solution in the titanium carbide. This oxide of titanium comes from the process in which rutile and carbon are combined to make titanium carbide. Such a carbide containing oxygen will not produce dense sintered compacts. Skaupy believes that the carbide made by Kennametal, Inc., is superior to other commercial titanium carbides because
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