Abstract

The article describes a possibility of airframe weight-saving structural technique during supporting rib development by design space tailoring. For scientific mission is given below the supporting rib, the loading pattern, the shearingforce and bending-moment diagrams. The researches are undertaken by structural calculation aimed to choosing of the supporting rib design space, web thickness, a number of supporting carrier gates. Herewith, it should be noted that requirements of structural availability without crippling and attainment of safety margin are achieved. Calculation and optimization of supporting rib design space held for supporting rib, which is made of different metallic materials. The article says, that usage of modern method of airframe assembly allows to optimize the design spaces of supporting rib and reduce the weight of it. According to researches, analysis of total resulting is done, and recommendations for use are given.

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