Comparison of Selected Rivet and Riveting Instructions
Sheet metal parts are widely used in airframes. Most sheet metal parts used in aircraft assembly are joined using rivets. A number of riveting parameters directly influence fatigue properties of a structure. These include a rivet length, driven head diameter, tolerance of a rivet hole and a rivet sh...
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| Format: | Article |
| Language: | English |
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Sciendo
2014-06-01
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| Series: | Fatigue of Aircraft Structures |
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| Online Access: | https://doi.org/10.1515/fas-2014-0004 |
| _version_ | 1797971095487250432 |
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| author | Kaniowski Jerzy |
| author_facet | Kaniowski Jerzy |
| author_sort | Kaniowski Jerzy |
| collection | DOAJ |
| description | Sheet metal parts are widely used in airframes. Most sheet metal parts used in aircraft assembly are joined using rivets. A number of riveting parameters directly influence fatigue properties of a structure. These include a rivet length, driven head diameter, tolerance of a rivet hole and a rivet shank diameter, and a protective layer among others. Unfavourable selection or change of these parameters can lead to stress concentrations and early crack nucleation. Crack growth can cause failure of a whole structure. |
| first_indexed | 2024-04-11T03:27:18Z |
| format | Article |
| id | doaj.art-b4c1d48647f048a2bfc5d114d6aeddbf |
| institution | Directory Open Access Journal |
| issn | 2300-7591 |
| language | English |
| last_indexed | 2024-04-11T03:27:18Z |
| publishDate | 2014-06-01 |
| publisher | Sciendo |
| record_format | Article |
| series | Fatigue of Aircraft Structures |
| spelling | doaj.art-b4c1d48647f048a2bfc5d114d6aeddbf2023-01-02T07:25:21ZengSciendoFatigue of Aircraft Structures2300-75912014-06-0120146396210.1515/fas-2014-0004fas-2014-0004Comparison of Selected Rivet and Riveting InstructionsKaniowski Jerzy0Institute of Aviation, Al. Krakowska 110/114, 02-256 Warsaw, PolandSheet metal parts are widely used in airframes. Most sheet metal parts used in aircraft assembly are joined using rivets. A number of riveting parameters directly influence fatigue properties of a structure. These include a rivet length, driven head diameter, tolerance of a rivet hole and a rivet shank diameter, and a protective layer among others. Unfavourable selection or change of these parameters can lead to stress concentrations and early crack nucleation. Crack growth can cause failure of a whole structure.https://doi.org/10.1515/fas-2014-0004riveted jointsrivetsriveting parametersriveting instructions and standards |
| spellingShingle | Kaniowski Jerzy Comparison of Selected Rivet and Riveting Instructions Fatigue of Aircraft Structures riveted joints rivets riveting parameters riveting instructions and standards |
| title | Comparison of Selected Rivet and Riveting Instructions |
| title_full | Comparison of Selected Rivet and Riveting Instructions |
| title_fullStr | Comparison of Selected Rivet and Riveting Instructions |
| title_full_unstemmed | Comparison of Selected Rivet and Riveting Instructions |
| title_short | Comparison of Selected Rivet and Riveting Instructions |
| title_sort | comparison of selected rivet and riveting instructions |
| topic | riveted joints rivets riveting parameters riveting instructions and standards |
| url | https://doi.org/10.1515/fas-2014-0004 |
| work_keys_str_mv | AT kaniowskijerzy comparisonofselectedrivetandrivetinginstructions |