2019
DOI: 10.1134/s0036029519130317
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Technological Heredity during the Production and Operation of Structural Materials

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Cited by 55 publications
(13 citation statements)
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“…For this purpose, we introduce restrictions on the vector space of objective functions and represent them in the form of expressions (8): (max) . (8) As additional restrictions when solving a multicriteria optimization problem, the following can be taken: the mass of a PCM structure with a given location scheme for viscoelastic components in the matrix m(x* 1 , x* 2 , ..., x* n , f* 1 , ..., f* )≤m per , where m per is the permissible mass of a composite structure; the cost of manufacturing the structure С(x* 1 , x* 2 , ..., x* n , f* 1 , ..., f* m )≤С per , where С per is the permissible cost price of manufacturing a structure from a composite with a given location scheme for viscoelastic components in the matrix; LI(x* 1 , x* 2 , ..., x* n , f* 1 , ..., f* m )≤ LI per labor intensity of manufacturing a structure from PCM with various types of hybrid matrices, where LI per is the permissible labor intensity of manufacturing a structure from PCM with a given scheme for the location of viscoelastic components in the matrix.…”
Section: Discussion Of Research Resultsmentioning
confidence: 99%
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“…For this purpose, we introduce restrictions on the vector space of objective functions and represent them in the form of expressions (8): (max) . (8) As additional restrictions when solving a multicriteria optimization problem, the following can be taken: the mass of a PCM structure with a given location scheme for viscoelastic components in the matrix m(x* 1 , x* 2 , ..., x* n , f* 1 , ..., f* )≤m per , where m per is the permissible mass of a composite structure; the cost of manufacturing the structure С(x* 1 , x* 2 , ..., x* n , f* 1 , ..., f* m )≤С per , where С per is the permissible cost price of manufacturing a structure from a composite with a given location scheme for viscoelastic components in the matrix; LI(x* 1 , x* 2 , ..., x* n , f* 1 , ..., f* m )≤ LI per labor intensity of manufacturing a structure from PCM with various types of hybrid matrices, where LI per is the permissible labor intensity of manufacturing a structure from PCM with a given scheme for the location of viscoelastic components in the matrix.…”
Section: Discussion Of Research Resultsmentioning
confidence: 99%
“…Among the modern methods of repairing machine parts, polymer technologies have recently been widely used [8]. This is due to the low labor intensity and cost of repair work, as well as the lack of the need to attract qualified specialists.…”
Section: Introductionmentioning
confidence: 99%
“…The primary quality markers for metal parts are machining accuracy and surface roughness. The analogy for polymer composite material (PCM) details is porosity [1,2]. The reason is in an impossibility of machining composites due to low interlayer shear strength therefore the delamination when processing can occur [3,4].…”
Section: Introductionmentioning
confidence: 99%
“…Composite Materials are becoming more popular gradually replacing traditional materials with extra strength, lighter weight, and thermal properties [1][2][3][4][5][6][7][8][9][10][11][12][13][14]. Many composites' industries are exploring the use of fiber-reinforced composites in all applications which includes aerospace, automotive and water transport, construction industry, toys, instrumentation, medicine, etc.…”
Section: Introductionmentioning
confidence: 99%