发明名称 Controlled strain rate forming of thick titanium plate
摘要 Thick plate is difficult to form because it cracks when localized strain exceeds the limits of the material. Forming thick titanium would significantly reduce manufacturing costs for finished parts by reducing machining time and by allowing standard stock blanks to be used where twelve inch thick or thicker blanks are needed today. Using finite element analysis, we model the plate forming to determine processing constraints that allow forming the thick, coarse grained alpha-beta titanium plate according to SPF principles with controlled strain rates. We form the part at an elevated temperature with a press ram. We complete the part by machining the formed plate, thereby greatly reducing machining time and material cost. Typically we bend a 20 cm thick plate to about 130 DEG with a 5-6 inch inner radius bend, or we form 2 inch thick plate with a complex curvature exceeding twelve inch depth over an area of 30x60 inches.
申请公布号 US6071360(A) 申请公布日期 2000.06.06
申请号 US19980093465 申请日期 1998.06.08
申请人 THE BOEING COMPANY 发明人 GILLESPIE, FRANNA S. P.
分类号 C22C14/00;C22F1/18;(IPC1-7):C22C14/00 主分类号 C22C14/00
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