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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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
Subjects
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ISSN1013-9826
1662-9795
1662-9795
DOI10.4028/www.scientific.net/KEM.746.36

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Abstract 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.
AbstractList 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.
Author Leonova, Evgeniya Vitalievna
Platonov, Valeriy Ivanovich
Larin, Sergey Nikolaevich
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  email: mpf-tula@rambler.ru
  organization: Tula State University
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Keywords Fracture
Stringer Radiator Panel Pnevmoforming
Research
Pressure
Stress
Strain
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Notes 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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Snippet Stringer radiator panels made of aluminum and titanium alloys used in the hull structure of the aircraft, which is necessary to maintain the required...
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SubjectTerms Aircraft components
Aluminum
Creep (materials)
Damage accumulation
Damage assessment
Deformation
Domes
Energy theory
Gas pressure
Machining
Panels
Process parameters
Radiators
Sheets
Thickness
Titanium alloys
Titanium base alloys
Workpieces
Title Study of Isothermal Pneumatic Forming of High-Strength Materials Subject to Energy Theory of Short-Term Creep and Damage
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