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Improvements relating to the manufacture of metal ribs and other structural members for use in the construction of wings, control members and other metal parts of aircraft

机译:有关用于制造飞机机翼,控制构件和其他金属零件的金属肋和其他结构构件的制造方面的改进

摘要

596,561. Flanging and dimpling ; making rods and bars and parts of aircraft. PRESTON, G., and HESTON AIRCRAFT CO., Ltd. July 30, 1945, No. 19531. [Classes 83 (ii) and 83 (iv)] Ribs &c. of aircraft parts are flanged and dimpled between dies in a press. A blank is positioned by pins 17 on a die comprising a wood block 9 with metal side plates 12 located by dowels 14 and is flanged in a rubber press of known construction. Wood side plates 18, 19, with dimpling projections corresponding with depressions in the plates 12 are then positioned against the flanges by pins 24 engaging slots 25 and the press again actuated to effect dimpling. Dies 29 flange lightening holes. Separate dies may be used for each operation.
机译:596,561。翻边和凹坑;制造棒,条和飞机零件。 G. PRESTON和HESTON AIRCRAFT CO。,Ltd.,1945年7月30日,编号19531。[Class 83(ii)和83(iv)] Ribs&c。在冲压机中,飞机零件的一部分被折边并凹进模具之间。毛坯通过销钉17定位在模具上,该模具包括木块9,该木块9具有通过销钉14定位的金属侧板12,并且在已知结构的橡胶压机中凸缘连接。然后,通过与槽25相接合的销24,将木质侧板18、19以及具有与板12中的凹陷相对应的凹入突起的凸出部分抵靠凸缘定位,并且再次致动压力机以进行凹入。模制29个法兰减轻孔。每个操作可以使用单独的模具。

著录项

  • 公开/公告号GB596561A

    专利类型

  • 公开/公告日1948-01-06

    原文格式PDF

  • 申请/专利号GB19450019531

  • 发明设计人

    申请日1945-07-30

  • 分类号B21D22/04;

  • 国家 GB

  • 入库时间 2022-08-24 02:40:08

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