发明名称 Method of manufacturing pressure vessel liners
摘要 A method of manufacturing a liner for use in a pressure vessel includes a cold drawing process that shapes a transition zone (20b) part of an aluminum alloy liner shell (10). The transition zone (20b) links a thinner walled drum part (18) and a thicker walled end region (20a), which is at an open top of the shell. The transition zone (20b) may be shaped by the cold drawing process such that it reduces susceptibility of the shell to fracture during removal from a cold drawing press and also redistributes shell material in preparation for a subsequent process in which a threaded neck is formed from the end region (20a). This process is particularly suited to processing harder aluminum alloy materials such as AA7060 or AA7032.
申请公布号 US9433995(B2) 申请公布日期 2016.09.06
申请号 US201414775187 申请日期 2014.03.14
申请人 Luxfer Gas Cylinders Limited 发明人 Chalandon Bernard Alain Jacques;Daval Romary Georges Marcel;Hepples Warren
分类号 B21D22/21;B21D51/24;B21D22/28;B21D35/00;F17C1/14 主分类号 B21D22/21
代理机构 Polster Lieder 代理人 Polster Lieder
主权项 1. A method of manufacturing a liner for use in a pressure vessel, the method comprising the steps of: (a) providing a cup-shaped shell (10) of aluminium alloy, with closed crown end (16) and open top, the shell having a drum region (18) with thinner walls, an end region (20a) at the open top with thicker walls and an intermediate transition zone (20b) of tapering thickness; (b) cold drawing the shell using a punch (24) with generally cylindrical walls and a shaped upper region (24a) that, during the drawing operation, meets with the transition zone (20b) of the shell; (c) forming the end region (20a) and transition zone (20b) to close the open top and to form a neck (32) extending therefrom; and (d) cutting a thread into the neck.
地址 GB