SU451766A1 - Titanium based alloy - Google Patents

Titanium based alloy

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Publication number
SU451766A1
SU451766A1 SU1904608A SU1904608A SU451766A1 SU 451766 A1 SU451766 A1 SU 451766A1 SU 1904608 A SU1904608 A SU 1904608A SU 1904608 A SU1904608 A SU 1904608A SU 451766 A1 SU451766 A1 SU 451766A1
Authority
SU
USSR - Soviet Union
Prior art keywords
based alloy
titanium based
titanium
alloy
manganese
Prior art date
Application number
SU1904608A
Other languages
Russian (ru)
Inventor
Николай Федорович Аношкин
Анатолий Георгиевич Павлов
Лев Васильевич Теслицкий
Александр Ефимович Калашников
Светлана Ильинична Козлова
Original Assignee
Предприятие П/Я Г-4361
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Предприятие П/Я Г-4361 filed Critical Предприятие П/Я Г-4361
Priority to SU1904608A priority Critical patent/SU451766A1/en
Application granted granted Critical
Publication of SU451766A1 publication Critical patent/SU451766A1/en

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Description

Изобретение относитс  к конструки ным материалам на основе титана. Известен сплав на основе титана, рый содержит, %: 3,5-5,0 Алюьи1ний 0,8-2,0 Марганец Титан основа Дл  повышени  механических свойс предложенный сплав ввод т ниобий, следующем соотношении компонентов, Алюминий 2,О-5,О 0,2-1.5 Марганец 4,0-1О,0 Ниобий Титан основа. При изготовлении сплава примен ю кондиционные шихтовые материалы в отходов производства трехслойных лис ( ОТЧ-ВН2АЭ-ОТЧ). Предложениый сплав обеспечивает щие механические свойства: Предел 1ФОЧНОСТИ, кг/мм 80,О-10О,О Предел текучести, кг/мм 75-80 Относительное удлинение 10-14 на базе 5, % 40-60 Поперечное сужение, % редмет изобретени  Сплав на основе титана, включающий миний и марганец, отличаюший- тей, что, с целью пстышени  механиких свойств, в сплав введен ниобий; следук цем соотношении, %: | 2,0-5,0 Алюминий 0,2-1,5 Марганец 4,О-1О,О Ниобий Титан основа.The invention relates to titanium based construction materials. Known alloy based on titanium, ry contains,%: 3.5-5.0 Aluminum 0.8-2.0 Manganese Titanium base To increase the mechanical properties of the proposed alloy, niobium is introduced, the following ratio of components, Aluminum 2, O-5, About 0.2-1.5 Manganese 4.0-1O, 0 Niobium Titanium base. In the manufacture of the alloy, the use of standardized charge materials in the production of three-layer foxes (OTCH-VN2AE-OTCH) is used. The proposed alloy provides mechanical properties: Limit of FOCALNESS, kg / mm 80, О-10О, О Yield strength, kg / mm 75-80 Elongation 10-14 on base 5,% 40-60 titanium based, including minium and manganese, which is distinguished by the fact that niobium was introduced into the alloy in order to reduce the mechanical properties; following ratio,%: | 2.0-5.0 Aluminum 0.2-1.5 Manganese 4, O-1O, O Niobium Titanium base.

SU1904608A 1973-04-06 1973-04-06 Titanium based alloy SU451766A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1904608A SU451766A1 (en) 1973-04-06 1973-04-06 Titanium based alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1904608A SU451766A1 (en) 1973-04-06 1973-04-06 Titanium based alloy

Publications (1)

Publication Number Publication Date
SU451766A1 true SU451766A1 (en) 1974-11-30

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ID=20548643

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1904608A SU451766A1 (en) 1973-04-06 1973-04-06 Titanium based alloy

Country Status (1)

Country Link
SU (1) SU451766A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4229216A (en) * 1979-02-22 1980-10-21 Rockwell International Corporation Titanium base alloy
CN103614590A (en) * 2013-12-12 2014-03-05 西北有色金属研究院 Low-temperature, high-strength and fatigue-resistant titanium niobium aluminum alloy

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4229216A (en) * 1979-02-22 1980-10-21 Rockwell International Corporation Titanium base alloy
CN103614590A (en) * 2013-12-12 2014-03-05 西北有色金属研究院 Low-temperature, high-strength and fatigue-resistant titanium niobium aluminum alloy
CN103614590B (en) * 2013-12-12 2015-10-07 西北有色金属研究院 A kind of low-temperature high-strength antifatigue titanium aluminium niobium alloy

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