发明名称 MANUFACTURING METHOD OF CONSTRUCTIONAL ELEMENT FOR AIRCRAFT INDUSTRY, WHICH INCLUDES DIFFERENTIAL COLD HAMMERING
摘要 FIELD: metallurgy. ^ SUBSTANCE: manufacturing method of solid constructional element welded by forging method from aluminium alloy involves hot pressure shaping stage, at least one cold pressure shaping stage by means of plastic deformation, at which at least two zones of the above constructional element are subject to average consolidated plastic deformations differing at least by 2% and preferably differing at least by 3%. If necessary, after cold pressure shaping there performed is cutting, machining and/or shaping of constructional element welded by means of forging method. ^ EFFECT: manufacture of constructional elements, including those not subject to tempering, having variable operating properties in the space and rather economic geometrical characteristics identical to characteristics of known elements. ^ 26 cl, 5 dwg, 12 tbl, 4 ex
申请公布号 RU2440438(C2) 申请公布日期 2012.01.20
申请号 RU20080145888 申请日期 2007.04.16
申请人 ALKAN RENALJU 发明人 LEKE FILIPP;EHJME FABRIS;DANIELU ARMEL'
分类号 C22C21/00;C22F1/04 主分类号 C22C21/00
代理机构 代理人
主权项
地址