2006
DOI: 10.1007/s11106-006-0120-z
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The phase equilibrium diagram for the Fe-Nb-Ti System

Abstract: 669.017.13.1′293′295 Microstructure analysis, differential thermal analysis, x-ray diffraction, and electron probe microanalysis have been applied to the phase equilibria in the Fe − Nb − Ti ternary system over the complete composition range. The 950°C isothermal section of the diagram has been constructed. Positions have been determined for the monovariant transformation lines in the melting diagram. No ternary intermetallides have been found.

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Cited by 6 publications
(3 citation statements)
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“…A solid solution ( β ‐Ti, Nb) can accommodate ≈10 at%. Fe at 950 °C, which is almost twice less compared to Fe–Ti–V system. Fe has quite a low solubility in ( β ‐Ti, Mo) .…”
Section: Joining With a Third Materials Compatible With Titaniummentioning
confidence: 90%
“…A solid solution ( β ‐Ti, Nb) can accommodate ≈10 at%. Fe at 950 °C, which is almost twice less compared to Fe–Ti–V system. Fe has quite a low solubility in ( β ‐Ti, Mo) .…”
Section: Joining With a Third Materials Compatible With Titaniummentioning
confidence: 90%
“…On the contrary, Nb weakened the alloy and the Vickers hardness number of Sample 11 decreased to 381. Nb has not only a large solubility in Ti, but can also help to dissolve Fe in Ti [32,33]. Therefore, the added 5 wt.% of Nb effectively kept Fe in ␤-Ti and prevented the formation of Fe-Ti intermetallics.…”
Section: Optical Microscopymentioning
confidence: 99%
“…Необходимо было создать сплав, не содержащий титан, но обладающий требуемыми свойствами. Исследования фазовых равновесий в сплавах кобальта с карбидами тугоплавких металлов [4,5] и представление о возможности получения естественного композита в условиях равновесной эвтектической кристаллизации из расплава [6], позволило разработать литейный износостойкий сплав на основе кобальта с карбидом ниобия не содержащий титан [7]. Сплав внедрён под маркой ХТН-61 и внесён в чертежи производства двигателей на предприятиях ОАО «Мотор-Сич» и ГП ЗМКБ «Прогресс» согласно «Техническим условиям» (ТУ) [8] и используется в турбинах крупногабаритных двигателей Д18Т, устанавливаемых в самолётах АН-225 «Мрія» и АН-124 «Руслан».…”
Section: Introductionunclassified