SU415326A1 - - Google Patents

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Publication number
SU415326A1
SU415326A1 SU1661028A SU1661028A SU415326A1 SU 415326 A1 SU415326 A1 SU 415326A1 SU 1661028 A SU1661028 A SU 1661028A SU 1661028 A SU1661028 A SU 1661028A SU 415326 A1 SU415326 A1 SU 415326A1
Authority
SU
USSR - Soviet Union
Prior art keywords
alloy
beryllium
kgf
zirconium
magnesium
Prior art date
Application number
SU1661028A
Other languages
Russian (ru)
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 filed Critical
Priority to SU1661028A priority Critical patent/SU415326A1/ru
Application granted granted Critical
Publication of SU415326A1 publication Critical patent/SU415326A1/ru

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Description

Изобрете1НИе относитс  к области разработки сплавов на основе берилли , нрнмен емых в качестве -коиструкциониого материала дл  летательных аппаратов, дл  которых определ ющим фактором  вл етс  сочетание высокой жесткости с высокой прочиоси.ю при рабочих температурах до . Известен сплав на основе берилли , содержащий (в вес. %): Бериллий90 Магний0,5-1,0 Алюминийостальное В предлагаемый сплав дополнительно введены цирконий ,и титаи. Это позвол ет cyHiecTBe«HO nOiBbicHTb пластичность сн.ава. Сплав содержит (в вес- % 50-90 Бериллий 0,5-2,5 Магний 0,05-2,0 Титаи 0,005-2,0 Циркоиий Примеси: медь |Ие более остальное Алюмииий 0,2 Сплав имеет следующие свойства: Предел упругости кгс/мм- 22000- Предел прочности, кгс/мм Предел тек)честн, кгс/ммОтносительное удлииение, % Ударна  в зкость, кгс/смУдельное электросопро0 ,042-0,043 тивлеиие. Ом мм Коэффиилеит линейного расширени  10, 1/град15- 19 Удельна  теплоемкость, кал/г град0,45-О Удельный вес, ,0-2 д мет и 3 о б р с т с и и   основе берилли , содержащий Сплав на юмнинй, магиин, о г л и ч а ю щ, и и с   тем, о, с целью повышени  пластич иости сплава, него дополнителыно введены цирконий и тнн при следующем соотношении компоненн (в вес. %): Берилл й50-90 Магний0,5-2,5 Титан0,05-2,0 Цирконий0,005-2,0 АлюминийостальноеThe invention relates to the development of beryllium-based alloys, which are designed as structural materials for aircraft, for which the determining factor is the combination of high rigidity with high proc. At operating temperatures up to. A beryllium-based alloy is known, containing (in wt.%): Beryllium90 Magnesium 0.5-1.0 Alumina Other zirconium and titi have been added to the proposed alloy. This allows the cyHiecTBe "HO nOiBbicHTb plasticity of the sn. Av. The alloy contains (in weight% 50-90 Beryllium 0.5-2.5 Magnesium 0.05-2.0 Titanium, 0.005-2.0 Circus Impurities: copper | Ie more than the rest of Aluminum 0.2 The alloy has the following properties: Limit elasticity kgf / mm-22000- Tensile strength, kgf / mm Limit tech) honest, kgf / mm Relative elongation,% Impact viscosity, kgf / cm Specific electroconduction, 042-0,043 tivleiye. Ohm mm Linear expansion coefficient 10, 1 / deg15-19 Specific heat, cal / g deg 0.45-O Specific weight, 0-2 d met and 3 o b s t and s and beryllium, containing alloy for light, magic, ohl and h and y, and with that, oh, in order to increase the ductility of the alloy, it was additionally introduced by zirconium and tnn in the following component ratio (% by weight): Beryl 50-90 Magnesium 0.5- 2.5 Titanium 0.05-2.0 Zirconium 0.005-2.0 Alumina

SU1661028A 1971-05-26 1971-05-26 SU415326A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1661028A SU415326A1 (en) 1971-05-26 1971-05-26

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1661028A SU415326A1 (en) 1971-05-26 1971-05-26

Publications (1)

Publication Number Publication Date
SU415326A1 true SU415326A1 (en) 1974-02-15

Family

ID=20476581

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1661028A SU415326A1 (en) 1971-05-26 1971-05-26

Country Status (1)

Country Link
SU (1) SU415326A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4359396A (en) * 1980-12-04 1982-11-16 Allied Corporation Hydride of beryllium-based intermetallic compound
AU680571B2 (en) * 1994-01-21 1997-07-31 Brush Wellman Inc. Semi-solid processed magnesium-beryllium alloys

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4359396A (en) * 1980-12-04 1982-11-16 Allied Corporation Hydride of beryllium-based intermetallic compound
AU680571B2 (en) * 1994-01-21 1997-07-31 Brush Wellman Inc. Semi-solid processed magnesium-beryllium alloys

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