Study of Isothermal Pneumatic Forming of High-Strength Materials Subject to Energy Theory of Short-Term Creep and Damage

Stringer radiator panels made of aluminum and titanium alloys used in the hull structure of the aircraft, which is necessary to maintain the required temperatures. section of the channel profile has a predetermined geometry - a circular or rectangular cross-section of the channel, and the channel it...

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Bibliographic Details
Published inKey engineering materials Vol. 746; pp. 36 - 47
Main Authors Platonov, Valeriy Ivanovich, Larin, Sergey Nikolaevich, Leonova, Evgeniya Vitalievna
Format Journal Article
LanguageEnglish
Published Zurich Trans Tech Publications Ltd 01.07.2017
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ISSN1013-9826
1662-9795
1662-9795
DOI10.4028/www.scientific.net/KEM.746.36

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Summary:Stringer radiator panels made of aluminum and titanium alloys used in the hull structure of the aircraft, which is necessary to maintain the required temperatures. section of the channel profile has a predetermined geometry - a circular or rectangular cross-section of the channel, and the channel itself can be unilateral or bilateral. The technological process of production of radiator panels is to carry out one process machining position, consisting of a series of operations performed by the gas pressure diffusion bonding two sheets and hot-forming gas channels supplied between the sheets. We consider forming a shell of material, following the energy theory of creep and defectiveness. The expressions for the evaluation process and force parameters of damage, in particular - the destruction. The effect sizes of workpiece thickness in the dome, the relative magnitudes of changes in the geometric parameters and the magnitude of damage accumulated from the time of deformation under different laws for the loading of aluminum and titanium alloys. Comparison of theoretical and experimental data on the relative thickness of the dome blanks and reference points, as well as the relative height of the workpiece indicates satisfactory their agreement.
Bibliography:Selected, peer reviewed papers from the International Science and Technical Congress on Aerospace Materials Plastic Deformation Processes. Science, Technology, Industry (METALDEFORM-2017), July 4-7, 2017, Samara, Russia
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ISSN:1013-9826
1662-9795
1662-9795
DOI:10.4028/www.scientific.net/KEM.746.36