RU93005214A - METHOD OF CONNECTING PREPARATIONS OR DETAILS FROM STEEL WITH DETAILS OF ALUMINUM OR TITANIUM ALLOYS AND TURBO-RADIANCE, OBTAINED BY THIS METHOD - Google Patents

METHOD OF CONNECTING PREPARATIONS OR DETAILS FROM STEEL WITH DETAILS OF ALUMINUM OR TITANIUM ALLOYS AND TURBO-RADIANCE, OBTAINED BY THIS METHOD

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Publication number
RU93005214A
RU93005214A RU93005214/08A RU93005214A RU93005214A RU 93005214 A RU93005214 A RU 93005214A RU 93005214/08 A RU93005214/08 A RU 93005214/08A RU 93005214 A RU93005214 A RU 93005214A RU 93005214 A RU93005214 A RU 93005214A
Authority
RU
Russia
Prior art keywords
steel
details
layer
friction welding
aluminum
Prior art date
Application number
RU93005214/08A
Other languages
Russian (ru)
Other versions
RU2100163C1 (en
Inventor
А. Амброзиак
Р. Лизон
Р. Рицанек
Original Assignee
Асеа Браун Бовери АГ
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
Priority claimed from DE4116088A external-priority patent/DE4116088A1/en
Application filed by Асеа Браун Бовери АГ filed Critical Асеа Браун Бовери АГ
Publication of RU93005214A publication Critical patent/RU93005214A/en
Application granted granted Critical
Publication of RU2100163C1 publication Critical patent/RU2100163C1/en

Links

Claims (1)

Способ соединения заготовок или деталей из стали с деталями из алюминиевого или титанового сплава и турбонагнетатель, полученный данным способом. Заготовки или конструкционные детали из стали соединяют с деталями из алюминиевого или титанового сплава сваркой трением с применением по меньшей мере одного промежуточного переходного слоя из вязкого металла соответствующей подгруппы, причем первым в случае на сталь наносят сваркой трением слой чистого никеля, обработанную поверхность которого соединяют сваркой трением с алюминиевым сплавом. Во втором случае сваркой трением наносят на сталь слой меди, а на титановый сплав - слой ванадия. Затем обработанные поверхности меди и ванадия соединяют одну с другой сваркой трением. На сталь, имеющую склонность к образованию мартенситных зон, перед нанесением слоя меди наносят сваркой трением слой из аустенитной стали. Способ пригоден в особенности для соединения турбинного колеса и вала или крепежной детали для вала турбонагнетателя.The method of joining billets or steel parts with aluminum or titanium alloy parts and a turbocharger produced by this method. Workpieces or structural parts made of steel are connected to parts made of aluminum or titanium alloy by friction welding using at least one intermediate transition layer of a viscous metal of the corresponding subgroup, and the first in the case of steel is applied by friction welding a layer of pure nickel, the treated surface of which is joined by friction welding with aluminum alloy. In the second case, a layer of copper is applied to the steel by friction welding, and a layer of vanadium is applied to the titanium alloy. Then the treated surfaces of copper and vanadium are connected to each other by friction welding. On steel, which has a tendency to form martensitic zones, before applying a layer of copper, a layer of austenitic steel is applied by friction welding. The method is particularly suitable for connecting a turbine wheel and a shaft or fastener for a turbocharger shaft.
RU9393005214A 1991-05-16 1992-05-14 Method of connection of steel blanks of parts with aluminium or titanium alloy parts of turboblower RU2100163C1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DEP4116088.6 1991-05-16
DE4116088A DE4116088A1 (en) 1991-05-16 1991-05-16 METHOD FOR JOINING STEEL WITH ALUMINUM OR TITANIUM ALLOY PARTS AND TURBOCHARGERS RECEIVED AFTER
PCT/CH1992/000094 WO1992020487A1 (en) 1991-05-16 1992-05-14 Process for bonding steel to aluminium or titanium alloy components and turbo-charger thus obtained

Publications (2)

Publication Number Publication Date
RU93005214A true RU93005214A (en) 1995-03-27
RU2100163C1 RU2100163C1 (en) 1997-12-27

Family

ID=6431820

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9393005214A RU2100163C1 (en) 1991-05-16 1992-05-14 Method of connection of steel blanks of parts with aluminium or titanium alloy parts of turboblower

Country Status (8)

Country Link
US (1) US5314106A (en)
EP (1) EP0513646B1 (en)
JP (1) JPH05509261A (en)
CZ (1) CZ373092A3 (en)
DE (2) DE4116088A1 (en)
PL (1) PL169339B1 (en)
RU (1) RU2100163C1 (en)
WO (1) WO1992020487A1 (en)

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