Improvement of the Design of Rocket Propelled Granite (RPG.7) Main Tubes Forging Dies

Malik Eltahir Elhadi, A. Abdelsalam, Abdelnasir Mohammed Zain
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Abstract

This paper presents a proposed new design of a forging die used for producing the forged tube of a rocket launcher. In the practiced technology for producing as the forged tube many problems raised as a result of the selection of the parting line (P.L.) at the upper tangent of the circular cross-section of the product, which resulted in a semi-parabolic cross- section that causes some technical mishaps which can be summarized in the following points: the large amount of raw material lost as turning chips during the turning process of the machined tube; The high consumption rate of tools during the turning process of the machined tube; damage caused by rough turning lathe machine as a result of the high vibrations due to turning of a non-cylindrical profiles and the short life-time of the forging die due to its embracing of the majority of the volume of the forge tube. In the proposed design the parting line (P.L.) will be located in the mid-section of the circular cross-section of the product (the forged tube) in order to solve these problems .This led to a design of a new set of hammering dies and subsequently a set of trimming dies by applying the standard design considerations and with the help of the CAD/CAM package software: ”VISI-15”. The proposed design differs significantly from the upsetting forging which have a parting line perpendicular to the longitudinal rolling direction of the forged product. When using the new designed dies, the saving in an input raw material (weapon steel) is estimated to reach up to 5 kilograms per forged tube. This became a considerable saving in the annual production cost. Minimizing the handling weight of the forged tube (from 16 Kg/Piece to 5 Kg/Piece) during the production processes results in a relatively less man power effort compared with the practiced technology. Besides the minimization of the consumption rate of the cutting tools and the rate of the replacement of the rough turning machines
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火箭推进花岗岩(RPG.7)主管锻模设计改进
本文提出了一种用于生产火箭炮锻管的锻模的新设计方案。在生产锻件管的实际工艺中,由于产品圆截面上切线的分型线选择不当,造成了产品的半抛物线形截面,造成了一些技术事故,主要表现在:加工管在车削过程中大量的车削原料损失;加工管件车削过程中刀具消耗率高;粗糙的车床由于加工非圆柱形型材时产生的高振动和锻模由于包围了锻管的大部分体积而造成的寿命短而造成的损伤。在建议的设计中,分型线(P.L.)将位于产品圆形截面(锻造管)的中间部分,以解决这些问题。这导致了一套新的锤击模具和随后的一套修边模具的设计,通过应用标准的设计考虑,并借助于CAD/CAM软件包软件:“VISI-15”。所提出的设计明显不同于镦粗锻件,镦粗锻件具有垂直于锻件纵向轧制方向的分型线。当使用新设计的模具时,估计每锻造管的输入原材料(武器钢)节省高达5公斤。这大大节省了每年的生产成本。在生产过程中,最大限度地减少锻造管的搬运重量(从16kg /片减少到5kg /片),与实践技术相比,相对较少的人力。此外,刀具的消耗率和粗车削机的更换率的最小化
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