Recent developments in chromium pertinent to its potential use in advanced jet engines are reviewed. Although chromium has a strength-to-density advantage over nickel, its inherent brittleness and further embrittlement by nitrogen during high-temperature exposure are serious limitations to its use. Twelve chromium alloys are currently under development, the strongest showing a potential 150' F (83 K) service temperature advantage over nickel-base superalloys. However, a better balance between solution strengthening and precipitate strengthening must be achieved in order to improve the low temperature ductility of these alloys. Improved coatings for protection against nitrogen embrittlement must be developed.
Lewis Research Center S U M~R YChromium-base alIoys, which have been under study now for slightly more than two decades, are attractive as potential competitors for nickel alloys for high temperature applications in advanced jet engines. Although chromium has a strength-to-density advantage over nickel, it is normally brittle at room temperature and is further embrittled by nitrogen during high temperature air exposure.The high temperature strength of chromium can be increased threefold to fourfold by solution strengthening with elements such as tantalum, columbium, tungsten, molybdenum, and rhenium. Solution strengthening, however, involves a significant increase in the ductile-brittle transition temperature. Similar or larger improvements in the strength of chromium can be achieved by precipitate strengthening with borides, carbides, and nitrides of the Groups IVa and Va elements. These precipitates do not embrittle chromium to the same extent as do solution strengthening additions and may even be ductilizing. Coarsening rate estimates suggest that carbides at least should retain sufficiently fine sizes as to be strengthening for times of 1000 hours o r longer at 2000' to 2200' F (1366 to 1478 K).Nitrogen is particularly deleterious to the ductility of chromium because of its high solubility at elevated temperatures and the nature of the CrZN precipitate. Nitrogen embrittlement of chromium during high temperature exposure can be reduced by rare earth alloying, but the effectiveness of these additions is reduced on further alloying for high temperature strength. rently under development. These include five from the United States, three from Australia, and four from the Soviet Union. The strongest of these alloys offer up to a 1 5 0 ' F (83 K) temperature advantage over nickel alloys but the impact ductile-brittle transition temperatures are high.surface alloying techniques to reduce nitrogen embrittlement and emphasis on dispersion strengthening to achieve a better balance between high temperature strength and low temperature ductility.