发明名称 Aluminum alloy aeronautical structural element fabrication involves machining of thick sheets
摘要 Machined metal component production comprises: fabrication of a metal sheet by casting, rolling and finishing operations; pre-machining the sheet on both faces; solution treatment of the pre-machined blank; tempering; and optional controlled traction, coating and/or cutting. Fabrication of a machined metal component comprises: (a) fabrication of a metal sheet by casting a rolling plate, optionally followed by homogenizing, one or more hot or cold rolling operations, optionally separated by one or more reheating operations, to obtain a sheet, and optionally one or more sheet cutting or finishing operations; (b) pre-machining of the sheet on one or both faces to obtain a pre-machined blank; (c) solution treatment of the pre-machined blank; (d) tempering treatment; (e) optionally, one or more stages of controlled traction, coating and cutting. Independent claims are included for: (a) use of the machined metal component as a structural element in aeronautical construction; and (b) an aluminum alloy structural element for aeronautical construction.
申请公布号 FR2848480(A1) 申请公布日期 2004.06.18
申请号 FR20020015997 申请日期 2002.12.17
申请人 PECHINEY RHENALU 发明人 HEYMES FABRICE;GODARD DAVID;WARNER TIMOTHY
分类号 B21C37/02;B64C1/00;C22F1/00;C22F1/04;C22F1/05;C22F1/053;C22F1/057;(IPC1-7):B21B3/00;B23P15/00;B21D1/05 主分类号 B21C37/02
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