Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units
The design, material selection, manufacture and assembly of aircraft structural elements are critical issues in the aviation industry. This study aims to optimize the selection of joining methods of aircraft honeycomb panels by considering strength, cost, and weight parameters. Accordingly, panel...
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| Format: | Article |
| Language: | English |
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Turkish Air Force Academy
2021-01-01
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| Series: | Havacılık ve Uzay Teknolojileri Dergisi |
| Subjects: | |
| Online Access: | http://jast.hho.edu.tr/index.php/JAST/article/view/438 |
| _version_ | 1797915307476516864 |
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| author | Sena Kabave Kılınçarslan Aslan Kahraman Erhal Şeyma Korkmaz M. Hüseyin Çetin |
| author_facet | Sena Kabave Kılınçarslan Aslan Kahraman Erhal Şeyma Korkmaz M. Hüseyin Çetin |
| author_sort | Sena Kabave Kılınçarslan |
| collection | DOAJ |
| description | The design, material selection, manufacture and assembly of aircraft
structural elements are critical issues in the aviation industry. This study aims
to optimize the selection of joining methods of aircraft honeycomb panels by
considering strength, cost, and weight parameters. Accordingly, panel type,
panel thickness and joining methods were determined as input parameters,
and fracture force, displacement, cost, and weight as output parameters.
Tenon-mortise, double-sided bracket, single-sided bracket, and extrusion
methods were investigated for L and T-type panels. Panel thicknesses were
determined as 10 mm and 22 mm according to standards. Tensile test and
finite element analysis were applied to the samples to examine their
mechanical behavior. The weight and cost of the panels were determined by
the process analysis. The obtained findings were optimized according to
multi-criteria decision making and response surface analysis methods. In the
optimization model, maximization of tensile strength and minimization of
displacement, cost and weight was determined as the target function. At the
end of the study, the optimum thickness value for both types of panels was
determined as 22 mm, and the optimum joining method was tenon-mortise. |
| first_indexed | 2024-04-10T12:39:46Z |
| format | Article |
| id | doaj.art-8ef4116d8aed4fd280b901b160a9510f |
| institution | Directory Open Access Journal |
| issn | 1304-0448 |
| language | English |
| last_indexed | 2024-04-10T12:39:46Z |
| publishDate | 2021-01-01 |
| publisher | Turkish Air Force Academy |
| record_format | Article |
| series | Havacılık ve Uzay Teknolojileri Dergisi |
| spelling | doaj.art-8ef4116d8aed4fd280b901b160a9510f2023-02-15T16:14:23ZengTurkish Air Force AcademyHavacılık ve Uzay Teknolojileri Dergisi1304-04482021-01-0114199117Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin UnitsSena Kabave Kılınçarslan0https://orcid.org/0000-0001-7302-4554Aslan Kahraman Erhal1https://orcid.org/0000-0003-0915-8579Şeyma Korkmaz2https://orcid.org/0000-0002-6871-980XM. Hüseyin Çetin3https://orcid.org/0000-0003-0429-5507Karabuk UniversityKarabuk UniversityKarabuk UniversityKarabuk UniversityThe design, material selection, manufacture and assembly of aircraft structural elements are critical issues in the aviation industry. This study aims to optimize the selection of joining methods of aircraft honeycomb panels by considering strength, cost, and weight parameters. Accordingly, panel type, panel thickness and joining methods were determined as input parameters, and fracture force, displacement, cost, and weight as output parameters. Tenon-mortise, double-sided bracket, single-sided bracket, and extrusion methods were investigated for L and T-type panels. Panel thicknesses were determined as 10 mm and 22 mm according to standards. Tensile test and finite element analysis were applied to the samples to examine their mechanical behavior. The weight and cost of the panels were determined by the process analysis. The obtained findings were optimized according to multi-criteria decision making and response surface analysis methods. In the optimization model, maximization of tensile strength and minimization of displacement, cost and weight was determined as the target function. At the end of the study, the optimum thickness value for both types of panels was determined as 22 mm, and the optimum joining method was tenon-mortise.http://jast.hho.edu.tr/index.php/JAST/article/view/438honeycomb compositejoining methodstenon-mortisebracketextrusionoptimization |
| spellingShingle | Sena Kabave Kılınçarslan Aslan Kahraman Erhal Şeyma Korkmaz M. Hüseyin Çetin Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units Havacılık ve Uzay Teknolojileri Dergisi honeycomb composite joining methods tenon-mortise bracket extrusion optimization |
| title | Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units |
| title_full | Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units |
| title_fullStr | Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units |
| title_full_unstemmed | Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units |
| title_short | Investigation of Joining Methods of Honeycomb Composite Panels Used in Structural Elements of Aircraft Cabin Units |
| title_sort | investigation of joining methods of honeycomb composite panels used in structural elements of aircraft cabin units |
| topic | honeycomb composite joining methods tenon-mortise bracket extrusion optimization |
| url | http://jast.hho.edu.tr/index.php/JAST/article/view/438 |
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