Cad/Cae Modelling of Mechanical Behavior of Composite Outlet Guide Vane for Aircraft Jet Engine

А, Гринев М; Anoshkin, A. N.; Pisarev, P. V.; Zuiko, V Yu; Ю, Зуйко В; Shipunov, G. S.

doi:10.15593/perm.mech/2015.3.04

Cited by 6 publications

(7 citation statements)

References 2 publications

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“…Математическая постановка задачи расчета НДС рассматриваемого образца, вклю-чающая соотношения теории упругости неоднородного анизотропного тела, приводилась авторами при расчетах подобных конструкций в работах [24,25]. В вариационной фор-мулировке эта постановка для области V c границей S заключается в отыскании миниму-ма функционала Лагранжа [26], вариация которого имеет вид…”

Section: таблицаunclassified

Numerical and Experimental Study of Composite Bulkhead Partition Strength With in-Situ X-Ray Monitoring

2017

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Section: таблицаunclassified

Numerical and Experimental Study of Composite Bulkhead Partition Strength With in-Situ X-Ray Monitoring

2017

PNRPU MB

View full text Add to dashboard Cite

“…Ʉɨɧɫɬɪɭɤɬɢɜɧɨ ɜ ɅɋȺ ɦɨɠɧɨ ɜɵɞɟɥɢɬɶ ɩɟ-ɪɨ ɢ ɩɨɥɤɢ, ɩɨɫɪɟɞɫɬɜɨɦ ɤɨɬɨɪɵɯ ɩɪɨɢɫɯɨɞɢɬ ɡɚɤɪɟɩɥɟɧɢɟ ɥɨɩɚɬɤɢ. Ⱦɥɹ ɤɪɟɩɥɟɧɢɹ ɜɟɪɯɧɟɣ ɩɨɥɤɢ ɤ ɨɛɟɱɚɣɤɟ ɤɨɪɩɭɫɚ ɢɫɩɨɥɶɡɭɟɬɫɹ ɛɨɥɬɨɜɨɟ ɫɨɟɞɢɧɟɧɢɟ, ɧɢɠɧɹɹ ɩɨɥɤɚ ɭɫɬɚɧɚɜɥɢɜɚɟɬɫɹ ɜ ɩɚɡɭ ɤɨɪɩɭɫɚ ɧɢɠɧɟɝɨ ɫɟɤɬɨɪɚ ɢ ɜ ɨɬɥɢɱɢɟ ɨɬ ɤɨɧɫɬɪɭɤɰɢɢ ɅɋȺ (ɩɪɨ-ɬɨɬɢɩɚ ɦɚɤɟɬɚ), ɪɚɫɫɦɨɬɪɟɧɧɨɣ ɜ ɪɚɛɨɬɟ [20], ɨɫɧɚɳɟɧɚ ɭɩɥɨɬɧɢɬɟɥɶɧɨɣ ɩɪɨɤɥɚɞɤɨɣ ɞɥɹ ɦɢɧɢɦɢɡɚɰɢɢ ɦɨɧɬɚɠɧɨɝɨ ɡɚɡɨɪɚ. ɇɚ ɜɯɨɞɧɨɣ ɤɪɨɦɤɟ ɅɋȺ ɭɫɬɚɧɚɜɥɢɜɚɟɬɫɹ ɬɢɬɚɧɨɜɚɹ ɧɚɤɥɚɞɤɚ.…”

Section: ɉɨɫɬɚɧɨɜɤɚ ɡɚɞɚɱɢ ɪɚɫɱɟɬɚ ɇⱦɋ ʌɋⱥmentioning

confidence: 99%

“…Ⱦɚɧɧɚɹ ɫɯɟɦɚ ɞɥɹ ɅɋȺ ɛɵɥɚ ɜɵɛɪɚɧɚ ɜ ɪɚɦɤɚɯ ɩɪɟɞɵɞɭɳɢɯ ɢɫɫɥɟɞɨɜɚɧɢɣ [3,20]. ɉɪɢ ɜɵɤɥɚɞɤɟ ɩɪɟɩɪɟɝɚ ɜɵɩɨɥɧɹɥɫɹ ɩɟɪɟɯɨɞ ɚɪɦɢɪɭɸɳɢɯ ɫɥɨɟɜ ɫ ɡɚɞɚɧɧɵɦ ɪɚɞɢɭɫɨɦ ɫ ɩɟɪɚ ɧɚ ɩɨɥɤɢ ɥɨɩɚɬɤɢ ɜ ɫɨɨɬɜɟɬɫɬɜɢɢ ɫ ɜɵɲɟ-ɭɤɚɡɚɧɧɨɣ ɫɯɟɦɨɣ ɚɪɦɢɪɨɜɚɧɢɹ.…”

Section: ɉɨɫɬɚɧɨɜɤɚ ɡɚɞɚɱɢ ɪɚɫɱɟɬɚ ɇⱦɋ ʌɋⱥmentioning

confidence: 99%

“…ȼ ɨɛɥɚɫɬɢ ɩɟɪɟɝɢɛɚ ɫɥɨɟɜ ɧɢɠɧɟɣ ɩɨɥɤɢ ɡɧɚɱɟɧɢɹ ɦɚɤɫɢɦɚɥɶɧɵɯ ɷɤɜɢɜɚɥɟɧɬɧɵɯ ɧɚɩɪɹɠɟɧɢɣ ɜ ɞɜɚ ɪɚɡɚ ɧɢɠɟ ɢ ɫɨɫɬɚɜɥɹɸɬ 73 Ɇɉɚ. ɋɥɟɞɭɟɬ ɨɬɦɟɬɢɬɶ, ɱɬɨ ɩɪɢ ɢɫɩɨɥɶɡɨɜɚɧɢɢ ɭɩɥɨɬɧɢɬɟɥɶɧɨɣ ɩɪɨɤɥɚɞɤɢ ɜ ɡɚɤɪɟɩɥɟɧɢɢ ɧɢɠɧɟɣ ɩɨɥɤɢ ɩɨ ɫɪɚɜɧɟ-ɧɢɸ ɫ ɜɚɪɢɚɧɬɨɦ ɡɚɤɪɟɩɥɟɧɢɹ, ɪɚɫɫɦɨɬɪɟɧɧɵɦ ɜ ɪɚɛɨɬɟ [20], ɩɪɨɢɫɯɨɞɢɬ ɫɦɟɳɟɧɢɟ ɨɛ-ɥɚɫɬɢ ɜɵɫɨɤɢɯ ɧɚɩɪɹɠɟɧɢɣ ɫ ɩɟɪɟɝɢɛɚ ɫɥɨɟɜ ɧɢɠɧɟɣ ɩɨɥɤɢ ɜ ɩɟɪɟɝɢɛ ɫɥɨɟɜ ɜɟɪɯɧɟɣ ɩɨɥ-ɤɢ. ɉɪɢ ɷɬɨɦ ɧɚɛɥɸɞɚɟɬɫɹ ɭɦɟɧɶɲɟɧɢɟ ɦɚɤɫɢɦɚɥɶɧɵɯ ɧɚɩɪɹɠɟɧɢɣ ɜ ɤɨɧɫɬɪɭɤɰɢɢ ɩɨɱɬɢ ɜ ɞɜɚ ɪɚɡɚ.…”

Section: ⱥɧɚɥɢɡ ɇⱦɋ ɢ ɨɰɟɧɤɚ ɩɪɨɱɧɨɫɬɢ ʌɋⱥ ɢɡ ɉʉɇunclassified

“…ȼ ɪɚɛɨɬɟ [20] ɩɪɟɞɫɬɚɜɥɟɧɵ ɪɟɡɭɥɶɬɚɬɵ ɤɨɦɩɶɸɬɟɪɧɨɝɨ ɦɨɞɟɥɢɪɨɜɚɧɢɹ ɦɟɯɚɧɢɱɟɫɤɨ-ɝɨ ɩɨɜɟɞɟɧɢɹ ɅɋȺ ɩɨɞ ɞɟɣɫɬɜɢɟɦ ɚɷɪɨɞɢɧɚɦɢɱɟɫɤɢɯ ɧɚɝɪɭɡɨɤ ɞɥɹ ɨɛɨɫɧɨɜɚɧɢɹ ɜɵɛɨɪɚ ɦɚɬɟɪɢɚɥɚ ɢ ɫɯɟɦɵ ɚɪɦɢɪɨɜɚɧɢɹ ɨɫɧɨɜɧɨɣ ɪɚɛɨɱɟɣ ɱɚɫɬɢ -ɩɟɪɚ ɥɨɩɚɬɤɢ. ɉɪɢ ɷɬɨɦ ɝɪɚ-ɧɢɱɧɵɟ ɭɫɥɨɜɢɹ ɜ ɨɛɥɚɫɬɹɯ ɡɚɤɪɟɩɥɟɧɢɣ ɞɟɬɚɥɢ ɡɚɞɚɜɚɥɢɫɶ ɩɪɢɛɥɢɠɟɧɧɨ ɞɥɹ ɫɨɤɪɚɳɟɧɢɹ ɨɛɴɟɦɚ ɜɵɱɢɫɥɟɧɢɣ, ɫɱɢɬɚɹ ɷɬɨ ɜɥɢɹɧɢɟ ɧɚ ɇȾɋ ɜ ɪɚɛɨɱɟɣ ɨɛɥɚɫɬɢ ɧɟɡɧɚɱɢɬɟɥɶɧɵɦ ɜ ɫɨ-ɨɬɜɟɬɫɬɜɢɢ ɫ ɩɪɢɧɰɢɩɨɦ ɋɟɧ-ȼɟɧɚɧɚ.…”

Section: Introductionmentioning

confidence: 99%

See 2 more Smart Citations

Stress-Strain Analysis and Strength Prediction of Composite Outlet Guide Vane for Aircraft Jet Engine

Михаил¹,

Александр²,

Валерий³

et al. 2015

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Ƚɪɢɧɟɜ Ɇ.Ⱥ., Ⱥɧɨɲɤɢɧ Ⱥ.ɇ., ɉɢɫɚɪɟɜ ɉ.ȼ., Ɂɭɣɤɨ ȼ.ɘ., ɒɢɩɭɧɨɜ Ƚ.ɋ. ɂɫɫɥɟɞɨɜɚɧɢɟ ɇȾɋ ɢ ɨɰɟɧɤɚ ɩɪɨɱɧɨɫɬɢ ɤɨɦɩɨɡɢɬɧɨɣ ɥɨɩɚɬɤɢ ɫɩɪɹɦɥɹɸɳɟɝɨ ɚɩɩɚɪɚɬɚ ɚɜɢɚɰɢɨɧɧɨɝɨ ɞɜɢɝɚɬɟɥɹ // ȼɟɫɬɧɢɤ ɉɟɪɦɫɤɨɝɨ ɧɚɰɢɨɧɚɥɶɧɨɝɨ ɢɫɫɥɟɞɨɜɚɬɟɥɶɫɤɨɝɨ ɩɨɥɢɬɟɯɧɢɱɟɫɤɨɝɨ ɭɧɢɜɟɪɫɢɬɟɬɚ. Ɇɟɯɚɧɢɤɚ. -2015Ɇɟɯɚɧɢɤɚ. - . -ʋ 4. -ɋ. 293-307. DOI: 10.15593/perm.mech/2015 Grinev M.A., Anoshkin A.N., Pisarev P.V., Zuiko V.Yu., Shipunov G.S. Stress-strain analysis and strength prediction of composite outlet guide vane for aircraft jet engine. PNRPU Mechanics Bulletin. 2015. No. 4. Ɋɪ. 293-307 ȼ ɩɨɫɥɟɞɧɟɟ ɜɪɟɦɹ ɤɨɦɩɨɡɢɰɢɨɧɧɵɟ ɦɚɬɟɪɢɚɥɵ ɚɤɬɢɜɧɨ ɢɫɩɨɥɶɡɭɸɬɫɹ ɩɪɢ ɫɨɡɞɚɧɢɢ ɜɵɫɨɤɨɧɚɝɪɭɠɟɧɧɵɯ ɞɟɬɚɥɟɣ ɢ ɭɡɥɨɜ ɚɜɢɚɰɢɨɧɧɵɯ ɞɜɢɝɚɬɟɥɟɣ. Ⱦɥɹ ɷɮ-ɮɟɤɬɢɜɧɨɝɨ ɩɪɢɦɟɧɟɧɢɹ ɤɨɦɩɨɡɢɬɨɜ ɜ ɬɚɤɢɯ ɞɟɬɚɥɹɯ ɧɟɨɛɯɨɞɢɦɨ ɜɵɛɪɚɬɶ ɨɩɬɢ-ɦɚɥɶɧɭɸ ɫɯɟɦɭ ɚɪɦɢɪɨɜɚɧɢɹ ɨɫɧɨɜɧɨɣ ɪɚɛɨɱɟɣ ɱɚɫɬɢ ɤɨɧɫɬɪɭɤɰɢɢ, ɚ ɬɚɤɠɟ ɩɪɨɜɟɫ-ɬɢ ɚɧɚɥɢɡ ɧɚɩɪɹɠɟɧɧɨɝɨ ɫɨɫɬɨɹɧɢɹ ɜ ɧɚɢɛɨɥɟɟ ɧɚɝɪɭɠɟɧɧɵɯ ɡɨɧɚɯ ɫɨ ɫɥɨɠɧɨɣ ɝɟɨ-ɦɟɬɪɢɟɣ: ɜ ɭɡɥɚɯ ɤɪɟɩɥɟɧɢɹ, ɭɱɚɫɬɤɚɯ ɬɟɯɧɨɥɨɝɢɱɟɫɤɢɯ ɩɟɪɟɯɨɞɨɜ ɢ ɫɨɟɞɢɧɟɧɢɣ ɪɚɡɥɢɱɧɵɯ ɩɨɜɟɪɯɧɨɫɬɟɣ. ɇɚɫɬɨɹɳɚɹ ɪɚɛɨɬɚ ɩɨɫɜɹɳɟɧɚ ɞɟɬɚɥɶɧɨɦɭ ɢɫɫɥɟɞɨɜɚɧɢɸ ɇȾɋ ɥɨɩɚɬɤɢ ɫɩɪɹɦ-ɥɹɸɳɟɝɨ ɚɩɩɚɪɚɬɚ (ɅɋȺ) ɚɜɢɚɰɢɨɧɧɨɝɨ ɞɜɢɝɚɬɟɥɹ ɢɡ ɩɨɥɢɦɟɪɧɵɯ ɤɨɦɩɨɡɢɰɢɨɧɧɵɯ ɦɚɬɟɪɢɚɥɨɜ. ɉɪɢɜɟɞɟɧɚ ɩɨɫɬɚɧɨɜɤɚ ɨɛɴɟɦɧɨɣ ɡɚɞɚɱɢ ɦɟɯɚɧɢɤɢ ɞɟɮɨɪɦɢɪɭɟɦɨɝɨ ɬɜɟɪɞɨɝɨ ɬɟɥɚ (ɆȾɌɌ) ɞɥɹ ɪɚɫɱɟɬɚ ɧɚɩɪɹɠɟɧɧɨ-ɞɟɮɨɪɦɢɪɨɜɚɧɧɨɝɨ ɫɨɫɬɨɹɧɢɹ ɫɥɨɢɫɬɨɣ ɤɨɧɫɬɪɭɤɰɢɢ ɢ ɨɰɟɧɤɢ ɟɟ ɩɪɨɱɧɨɫɬɢ ɩɨ ɧɚɩɪɹɠɟɧɢɹɦ ɜ ɫɥɨɹɯ. ȼ ɪɚɫɱɟɬɧɨɣ ɫɯɟɦɟ ɤɨɧɫɬɪɭɤɰɢɢ ɅɋȺ ɭɱɢɬɵɜɚɟɬɫɹ ɬɟɯɧɨɥɨɝɢɱɟɫɤɢɣ ɩɨɪɹɞɨɤ ɭɤɥɚɞɤɢ, ɚɧɢɡɨɬɪɨ-ɩɢɹ ɫɜɨɣɫɬɜ ɚɪɦɢɪɭɸɳɢɯ ɫɥɨɟɜ ɢ ɫɩɨɫɨɛ ɡɚɤɪɟɩɥɟɧɢɹ ɞɟɬɚɥɢ ɜ ɡɚɦɤɨɜɨɦ ɫɨɟɞɢɧɟ-ɧɢɢ. ɋɯɟɦɚ ɚɪɦɢɪɨɜɚɧɢɹ ɥɨɩɚɬɤɢ ɨɩɪɟɞɟɥɟɧɚ ɜ ɩɪɟɞɵɞɭɳɢɯ ɪɚɛɨɬɚɯ. Ⱦɥɹ ɨɰɟɧɤɢ ɡɚɩɚɫɚ ɫɬɚɬɢɱɟɫɤɨɣ ɩɪɨɱɧɨɫɬɢ ɢɫɩɨɥɶɡɨɜɚɥɫɹ ɤɪɢɬɟɪɢɣ ɦɚɤɫɢɦɚɥɶɧɵɯ ɧɚɩɪɹɠɟɧɢɣ.ɑɢɫɥɟɧɧɨɟ ɪɟɲɟɧɢɟ ɞɚɧɧɨɣ ɡɚɞɚɱɢ ɨɫɭɳɟɫɬɜɥɹɥɨɫɶ ɦɟɬɨɞɨɦ ɤɨɧɟɱɧɵɯ ɷɥɟ-ɦɟɧɬɨɜ (ɆɄɗ) ɜ ɩɚɤɟɬɟ ANSYS Workbench ɫ ɢɫɩɨɥɶɡɨɜɚɧɢɟɦ ɜɵɫɨɤɨɩɪɨɢɡɜɨɞɢ-ɬɟɥɶɧɨɝɨ ɜɵɱɢɫɥɢɬɟɥɶɧɨɝɨ ɤɨɦɩɥɟɤɫɚ. ɉɪɨɜɟɞɟɧ ɞɟɬɚɥɶɧɵɣ ɩɨɫɥɨɣɧɵɣ ɚɧɚɥɢɡ ɧɚɩɪɹɠɟɧɧɨ-ɞɟɮɨɪɦɢɪɨɜɚɧɧɨɝɨ ɫɨɫɬɨɹɧɢɹ ɤɨɧɫɬɪɭɤɰɢɢ, ɨɫɨɛɨɟ ɜɧɢɦɚɧɢɟ ɭɞɟɥɟɧɨ ɭɱɚɫɬɤɚɦ ɩɟɪɟɝɢɛɚ ɫɥɨɟɜ ɜ ɨɤɪɟɫɬɧɨɫɬɢ ɩɨɥɨɤ ɥɨɩɚɬɤɢ, ɝɞɟ ɧɚɢɛɨɥɟɟ ɜɟɪɨɹɬɧɨ ɜɨɡ-ɧɢɤɧɨɜɟɧɢɟ ɜɵɫɨɤɢɯ ɦɟɠɫɥɨɟɜɵɯ ɧɚɩɪɹɠɟɧɢɣ. ɉɨɥɭɱɟɧɚ ɨɰɟɧɤɚ ɜɥɢɹɧɢɹ ɭɫɥɨɜɢɹ ɡɚɤɪɟɩɥɟɧɢɹ ɥɨɩɚɬɤɢ ɧɚ ɯɚɪɚɤɬɟɪ ɧɚɩɪɹɠɟɧɧɨɝɨ ɫɨɫɬɨɹɧɢɹ. ɉɨɤɚɡɚɧɨ, ɱɬɨ ɧɚɢɛɨ-ɥɟɟ ɨɩɚɫɧɵɦɢ, ɨɩɪɟɞɟɥɹɸɳɢɦɢ ɡɚɩɚɫ ɩɪɨɱɧɨɫɬɢ ɤɨɧɫɬɪɭɤɰɢɢ, ɹɜɥɹɸɬɫɹ ɧɚɩɪɹɠɟ- Ʉɥɸɱɟɜɵɟ ɫɥɨɜɚ:ɥɨɩɚɬɤɚ ɫɩɪɹɦɥɹɸɳɟɝɨ ɚɩɩɚɪɚɬɚ, ɩɨɥɢɦɟɪɧɵɟ ɤɨɦɩɨɡɢɰɢɨɧɧɵɟ ɦɚɬɟɪɢɚɥɵ, ɭɝɥɟɩɥɚɫɬɢɤ, ɦɟɯɚɧɢɤɚ ɤɨɦɩɨɡɢɰɢɨɧɧɵɯ ɦɚɬɟɪɢɚɥɨɜ, ɧɚɩɪɹɠɟɧɧɨ-ɞɟɮɨɪɦɢɪɨɜɚɧɧɨɟ ɫɨɫɬɨɹɧɢɟ, ɦɟɬɨɞ ɤɨɧɟɱɧɵɯ ɷɥɟɦɟɧɬɨɜ (ɆɄɗ), ɫɯɟɦɚ ɚɪɦɢɪɨɜɚɧɢɹ, ɠɟɫɬɤɨɫɬɶ, ɩɪɨɱɧɨɫɬɶ, ANSYS

show abstract

Experimental-theoretical study of the mechanical behavior of polymer composite construction when developing a method of reliable detection of defects by microfocus radiography

Anoshkin¹,

Кавалеров²,

Osokin³

et al. 2018

AIP Conference Proceedings

View full text Add to dashboard Cite

Cad/Cae Modelling of Mechanical Behavior of Composite Outlet Guide Vane for Aircraft Jet Engine

Cited by 6 publications

References 2 publications

Numerical and Experimental Study of Composite Bulkhead Partition Strength With in-Situ X-Ray Monitoring

Numerical and Experimental Study of Composite Bulkhead Partition Strength With in-Situ X-Ray Monitoring

Stress-Strain Analysis and Strength Prediction of Composite Outlet Guide Vane for Aircraft Jet Engine

Experimental-theoretical study of the mechanical behavior of polymer composite construction when developing a method of reliable detection of defects by microfocus radiography

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