Abstract Based on the topological representation and transformation of the elementary chevron structure module, we propose the dependences that relate the geometrical parameters of rollers with the chevron structure element sizes for the transverse scheme of rotary creasing and bending. The calculation scheme is realized in the form of the parametrized geometrical model using CAD SolidWorks aids.
Parameters of a creasing-bending machine as applied to the scheme of transverse rotary shaping of chevron structures
Russian Aeronautics (Iz VUZ) ; 50 , 2 ; 186-192
2007-06-01
7 pages
Article (Journal)
Electronic Resource
English
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