Stan R. Seagle RMI Company — U.S.A. TITANIUM TECHNOLOGY FORECAST l - INTRQD ]; TIQN Titanium usage continues to grow being spurred by an expanding commercia al aerospace indu ustry an ncr ased requiremen nts non- space applications Currently, on—ae space usage is approximately 0% f SA c nsumption The ap1d gr th rate of t segment suggests tha t onfae sp ce u age f titanium will be a larger portion of total market in the 1990s. High specific strength (strength/density) to 1000 E‘ is the ke property utilized in applying itanium allo 5 in aerospace ' I n ' o applica ons n on—aerospace s ium's ex ellent corr051on re51stance is often the cr1t1cal, and m t important characteris s two proper 1es, sp ic st e h d corrosion resistance, differentiate titanium fro om other materials and account for nearly all the titanium applications. Titanium, a relatively new commercial metal, has demonstrated excellent performance in aerospace to moderately eleva ted temperatures and outstanding corrosion resis ance in neutral ' id A i and mi ci y ac1d1c chlor e environments s we move nto th 90s, new titanium al are expect d to be used at higher temperatures, at h her strength levels an 1n ore aggressive env1ronm a n, the tu bi ind str 1 re e cont nually 1 proved q t enha ce bo y to th performance and safety. Specific background on these expected advances in alloy and process technology are discussed below. 2 , HIGH TEMPERATURE ALLOYS Fi ure l contains elevated temperature stress—rupture data on the os ad (i co a al oy an use ed extensivesly in the U.S.A for the hi 1gh temperature compressor portion of turbines The maximum design temperature for this alloy is about 1000 F. More recen ly, the temperature capability of tita anium has be I I Engl and T1—1 00 by 1 in 1834 s being in o est quantit in new Rol Roy n in s while the Ti 1100 is being evaluate U S A eng1n p oducers pote 1al use e a lications temperature ex e ds about 1050 to , rcfa oxid tion of tita iu alloy 0 su ecomes to develop suitable coeatings that could be used with