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Process for the production of composite parts through a combination of expanding, deep drawing and subsequent massive forming

机译:通过扩展,深冲和随后的大量成形相结合的方法来生产复合零件的过程

摘要

The invention relates to a method for producing a composite part (28) formed from core material (3) and shell material (2) by means of a deep-drawing process (6), wherein in a first process step the shell material (28) covering at least part of the process-based composite part (28) on the outside. 2) is produced by a deep-drawing process (6) from a sheet-metal blank (1), in which the core material (3) is used as a stamp insert for deep-drawing the shell material (2), the shell material (2) and core material (3) in tight Surface contact with each other, and then the preformed hybrid semi-finished product (14) made of deep-drawn shell material (2) and partially enclosed core material (3) is subjected to a joint forming process (13) in which the final shape of the composite part (28) is produced in a plastic-forming manner. Here, the sheet-like blank (1) for the shell material (2) is provided with at least one perforation (17) and the core material (3) in the area of the at least one perforation (17) is expanded and deep-drawn the sheet-like blank (1) so that the covering material (2) in the area of the section (16) of the core material (3) to be coated is applied to the core material (3), after which the core material (3) and the covering material (2) applied to the core material (3) by means of a further joint Massive deformation (13) is further deformed.
机译:本发明涉及一种通过深冲工艺(6)生产由芯材(3)和壳材料(2)形成的复合部件(28)的方法,其中在第一步中,壳材料(28) )至少在外部覆盖了基于过程的复合部件(28)的一部分。 2)是通过钣金毛坯(1)的深冲工艺(6)制成的,其中将芯材(3)用作压模嵌件,以对壳材料(2)进行深冲使材料(2)和芯材(3)彼此紧密地表面接触,然后对由深冲壳材料(2)和部分包封的芯材(3)制成的预成型的混合半成品(14)进行处理进入接头成形工艺(13),其中以塑性成形的方式生产复合部件(28)的最终形状。在此,用于壳体材料(2)的片状坯料(1)设置有至少一个穿孔(17),并且在至少一个穿孔(17)的区域中的芯材(3)被扩展和深化。拉伸片状坯料(1),以便将要涂覆的芯材(3)的部分(16)区域中的覆盖材料(2)涂覆到芯材(3)上,芯材料(3)和通过进一步接合施加到芯材料(3)上的覆盖材料(2)进一步发生大规模变形(13)。

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