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Opportunities for using the thermal imaging method of nondestructive inspection for skin delamination diagnosis in honeycomb structures used in modern aircraft. / Klochkov, N. I.; Zverkov, I. D.; Gavrilov, D. A.

в: Thermophysics and Aeromechanics, Том 30, № 4, 07.2023, стр. 661-671.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

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Klochkov NI, Zverkov ID, Gavrilov DA. Opportunities for using the thermal imaging method of nondestructive inspection for skin delamination diagnosis in honeycomb structures used in modern aircraft. Thermophysics and Aeromechanics. 2023 июль;30(4):661-671. doi: 10.1134/S0869864323040066

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BibTeX

@article{890c5b63be6c462babed18b65a73eaa8,
title = "Opportunities for using the thermal imaging method of nondestructive inspection for skin delamination diagnosis in honeycomb structures used in modern aircraft",
abstract = "The modern aviation industry has many applications for honeycomb composite panels (HCP). The HCP-manufactured product line becomes more extended. This dictates a need for most effective and inexpensive methods for nondestructive inspection for HCP integrity that can ensure a high level of flight safety. One of promising methods for nondestructive inspection is the thermal technique. This paper presents and analyses the method feasibility of revealing the delamination of outer skin from an HCP filling. This task is performed by numerical simulation and the paper presents a pictorial test with a sample of HCP typical of aircraft engineering. Our results demonstrate how the thermal imaging tools can be used for the fact of skin delamination with regard for technical restrictions found in real experiments with a physical sample of HCP.",
keywords = "composite honeycomb constructions, delamination of skin, equipment for nondestructive inspection, thermal imaging method for nondestructive inspection",
author = "Klochkov, {N. I.} and Zverkov, {I. D.} and Gavrilov, {D. A.}",
note = "Research was performed according to a government assignment (State registration No. 121030500149-8). Публикация для корректировки.",
year = "2023",
month = jul,
doi = "10.1134/S0869864323040066",
language = "English",
volume = "30",
pages = "661--671",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "PLEIADES PUBLISHING INC",
number = "4",

}

RIS

TY - JOUR

T1 - Opportunities for using the thermal imaging method of nondestructive inspection for skin delamination diagnosis in honeycomb structures used in modern aircraft

AU - Klochkov, N. I.

AU - Zverkov, I. D.

AU - Gavrilov, D. A.

N1 - Research was performed according to a government assignment (State registration No. 121030500149-8). Публикация для корректировки.

PY - 2023/7

Y1 - 2023/7

N2 - The modern aviation industry has many applications for honeycomb composite panels (HCP). The HCP-manufactured product line becomes more extended. This dictates a need for most effective and inexpensive methods for nondestructive inspection for HCP integrity that can ensure a high level of flight safety. One of promising methods for nondestructive inspection is the thermal technique. This paper presents and analyses the method feasibility of revealing the delamination of outer skin from an HCP filling. This task is performed by numerical simulation and the paper presents a pictorial test with a sample of HCP typical of aircraft engineering. Our results demonstrate how the thermal imaging tools can be used for the fact of skin delamination with regard for technical restrictions found in real experiments with a physical sample of HCP.

AB - The modern aviation industry has many applications for honeycomb composite panels (HCP). The HCP-manufactured product line becomes more extended. This dictates a need for most effective and inexpensive methods for nondestructive inspection for HCP integrity that can ensure a high level of flight safety. One of promising methods for nondestructive inspection is the thermal technique. This paper presents and analyses the method feasibility of revealing the delamination of outer skin from an HCP filling. This task is performed by numerical simulation and the paper presents a pictorial test with a sample of HCP typical of aircraft engineering. Our results demonstrate how the thermal imaging tools can be used for the fact of skin delamination with regard for technical restrictions found in real experiments with a physical sample of HCP.

KW - composite honeycomb constructions

KW - delamination of skin

KW - equipment for nondestructive inspection

KW - thermal imaging method for nondestructive inspection

UR - https://www.scopus.com/record/display.uri?eid=2-s2.0-85181254359&origin=inward&txGid=fea9b37ed967cc8dc0c9f754a3584b06

UR - https://www.mendeley.com/catalogue/6bbf2f34-bd4a-3166-b66a-8e36b9b99fc0/

U2 - 10.1134/S0869864323040066

DO - 10.1134/S0869864323040066

M3 - Article

VL - 30

SP - 661

EP - 671

JO - Thermophysics and Aeromechanics

JF - Thermophysics and Aeromechanics

SN - 0869-8643

IS - 4

ER -

ID: 59564155