SU554703A1 - Iron-base dispersion-hardening alloy - Google Patents
Iron-base dispersion-hardening alloyInfo
- Publication number
- SU554703A1 SU554703A1 SU7602306724A SU2306724A SU554703A1 SU 554703 A1 SU554703 A1 SU 554703A1 SU 7602306724 A SU7602306724 A SU 7602306724A SU 2306724 A SU2306724 A SU 2306724A SU 554703 A1 SU554703 A1 SU 554703A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- iron
- hardening alloy
- alloy
- base dispersion
- cobalt
- Prior art date
Links
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- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
Изобретение относитс к. области ме таллургии, в частности к. дисперсионногвердеющим сплавам с малым температурным коэффициентом модул нормально упругости, используемым дл изготовлени конструкционных деталей специально назначени . Известен дисперсионно-твердеющий сплав на основе железа, содержащий следующие компоненты, вес.%: Никель42-43 Кобальт0,35 Хром5,0 Титан2,75 Алюминий0,3 Марганец0,е Кремний0,5 ЖелезоОстальное 1 Недостатком известного сплава вл ю с его низкие физико-механические свойс . Ba(d 14О кгс/ми ё.- 126 кгс/мм 87%). , ОД Наиболее близким к. предложенному сплаву по технической сущности и дости гаемому эффекту вл етс дисперсионновердеющи сплав на основе железа сле ующего состава, вес.%: Никель34-38 Кобальт121-16 Вольфрам6-8 Титан2,3 Алюминий0,0,8 Марганец0,2-О,8 БорО,001-О,03 Церий0,О01-О,О5 ЖелезоОстальное 2 Недостатком его вл ютс низкие физио-механические свойства ( 6 14555 кгс/мм, eflkl 13О-14О кгс/мм Г 3%, Е 17200 Krc/MJH). Дл повьщ1ени физико-механических войств сплава предлагаетс ввести в го состав кремний и лантан при следук ем соотнесении .компонентов, вес%: Никель34-38 Кобальт16,2-18,5 Волы} ам6-8 Титан 2,3-3 Алюминий6,3-0,8 Марганец0,2-0,8 0,001-0,05 0,001-0,05 Кремний 0,4-1,4 Лантан 0,01-0,2 Железо Остальное Механические свойства предложенно сплава после термической обработки с дующие: . Предел прочности1ФИ раст жении Дкгс/мм 165-170 Предел текучести в . / Zч Я. 145-150 кгс/мм Относительное удлинение ( 81 , %2-4 Модуль упругости (Е), кгс/мм 1700О172ОО Коэффшшент термического расширени , 1/град(8,3-8,5).Ю Пример. Сплавы выплавл ют в вакуумной печи и подвергают следующей термической об .работке: . закалка в воде с , наклеп 40% старение при в течение 8ч. Состав и свойства сплавов приведены в табл. 1 и 2.The invention relates to the field of metallurgy, in particular, to dispersion hardening alloys with a low temperature coefficient, a modulus of normal elasticity, used for the manufacture of structural parts for special purposes. Known dispersion-hardening alloy based on iron, containing the following components, wt.%: Nickel42-43 Cobalt0.35 Chromium5.0 Titanium2.75 Aluminum0.3 Manganese0, e Silicon0.5 IronOther 1 The disadvantage of the known alloy is with its low physical mechanical fasteners Ba (d 14O kgf / m y. - 126 kgf / mm 87%). , OD The closest to the proposed alloy to the technical essence and achievable effect is the dispersion-hardening iron-based alloy of the following composition, wt.%: Nickel34-38 Cobalt121-16 Tungsten6-8 Titanium2.3 Aluminum0.0.8 Manganese 0.2 -O, 8 BorO, 001-O, 03 Cerium0, O01-O, O5 IronOstal 2, Its disadvantage is its low physio-mechanical properties (6 14555 kgf / mm, eflkl 13O-14O kgf / mm G 3%, E 17200 Krc / Mjh). In order to increase the physicomechanical properties of the alloy, it is proposed to introduce silicon and lanthanum into the go composition by following the correlation of components, weight%: Nickel34-38 Cobalt 16.2-18.5 Oxen 6-6-8 Titanium 2.3-3 Aluminum6.3- 0.8 Manganese 0.2-0.8 0.001-0.05 0.001-0.05 Silicon 0.4-1.4 Lanthanum 0.01-0.2 Iron Else The mechanical properties of the proposed alloy after heat treatment with the following:. Tensile strength 1 PHY tensile Dgs / mm 165-170 Yield point in. / Zch I. 145-150 kgf / mm Relative elongation (81,% 2-4 Elastic modulus (E), kgf / mm 1700О172ОО Thermal expansion coefficient, 1 / deg (8.3-8.5). Example. Alloys melted in a vacuum furnace and subjected to the following thermal treatment: quenching in water, cold working 40% aging for 8 hours The composition and properties of the alloys are given in Tables 1 and 2.
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Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU7602306724A SU554703A1 (en) | 1976-01-04 | 1976-01-04 | Iron-base dispersion-hardening alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU7602306724A SU554703A1 (en) | 1976-01-04 | 1976-01-04 | Iron-base dispersion-hardening alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
SU554703A1 true SU554703A1 (en) | 1978-08-05 |
Family
ID=20643064
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU7602306724A SU554703A1 (en) | 1976-01-04 | 1976-01-04 | Iron-base dispersion-hardening alloy |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU554703A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4711826A (en) * | 1986-01-27 | 1987-12-08 | Olin Corporation | Iron-nickel alloys having improved glass sealing properties |
-
1976
- 1976-01-04 SU SU7602306724A patent/SU554703A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4711826A (en) * | 1986-01-27 | 1987-12-08 | Olin Corporation | Iron-nickel alloys having improved glass sealing properties |
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