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 in | Key engineering materials Vol. 746; pp. 36 - 47 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Zurich
Trans Tech Publications Ltd
01.07.2017
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Subjects | |
Online Access | Get full text |
ISSN | 1013-9826 1662-9795 1662-9795 |
DOI | 10.4028/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. |
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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 |
Author_xml | – givenname: Valeriy Ivanovich surname: Platonov fullname: Platonov, Valeriy Ivanovich email: mpf-tula@rambler.ru organization: Tula State University – givenname: Sergey Nikolaevich surname: Larin fullname: Larin, Sergey Nikolaevich email: larin_1@rambler.ru organization: Tula State University – givenname: Evgeniya Vitalievna surname: Leonova fullname: Leonova, Evgeniya Vitalievna email: mpf-tula@rambler.ru organization: Tula State University |
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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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