Szczegóły publikacji

Opis bibliograficzny

Influence of rivet material and squeeze force on the riveting process and residual stresses in riveted joints used in aircraft structures / Adam KORBEL, Valeria MANITCAIA, Tomasz MACHNIEWICZ // Bulletin of the Polish Academy of Sciences. Technical Sciences ; ISSN 0239-7528. — 2025 — vol. 73 iss. 5 art. no. e154721, s. 1–15. — Bibliogr. s. 13–15, Abstr. — Publikacja dostępna online od: 2025-08-19

Autorzy (3)

Słowa kluczowe

FEAresidual stressfinite element analysisrivet materialriveting processfatigue crack initiation site

Dane bibliometryczne

ID BaDAP161727
Data dodania do BaDAP2025-08-28
Tekst źródłowyURL
DOI10.24425/bpasts.2025.154721
Rok publikacji2025
Typ publikacjiartykuł w czasopiśmie
Otwarty dostęptak
Creative Commons
Czasopismo/seriaBulletin of the Polish Academy of Sciences, Technical Sciences

Abstract

The paper presents the results of experimental research and finite element analyses (FEA) on the impact of the aircraft rivet installation process and the type of rivet material on the geometric parameters of the driven rivet head, rivet hole expansion (relative interference), residual stresses in sheets, clamping stress and clamping force between sheets in three-row riveted lap joints, as well as linking the obtained results with observations of fatigue crack initiation sites in real riveted joints. The research was conducted for universal head rivets (MS20470AD5-5 and MS20615-5M5) with a shank diameter of 3.96 mm and a length of 7.94 mm, made of two materials, namely aluminium alloy (2117-T4) and nickel-copper alloy (Monel 400), used to join two AA2024-T3 sheets with a thickness of 1.0 mm and 1.6 mm. The experimental tests focused on determining the mechanical properties of sheet and rivet materials (using the digital image correlation DIC technique), geometric parameters of driven rivet heads, and rivet hole expansion, depending on the rivet material and the riveting force level. The results obtained from the numerical models revealed that at the same degree of rivet squeezing, rivets made of Monel 400 generate significantly higher negative residual stresses and residual clamping than rivets made of AA2117-T4, which will affect the contribution of friction to load transfer by a given rivet row and the fretting phenomenon in real riveted joints. The region of compressive residual hoop stress in sheets and the clamping force influence the fatigue crack initiation site and the crack path.

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artykuł
#142949Data dodania: 7.10.2022
Effect of aircraft rivet installation process and production variables on residual stress, clamping force and fatigue behaviour of thin sheet riveted lap joints / Adam KORBEL // Thin-Walled Structures ; ISSN 0263-8231. — 2022 — vol. 181 art. no. 110041, s. 1–18. — Bibliogr. s. 17–18, Abstr. — Publikacja dostępna online od: 2022-09-20
fragment książki
#160126Data dodania: 20.6.2025
Comparison of residual strains and stresses in riveted joints made with MS20470E5-5 and MS20615-5M5 aircraft rivets / KORBEL A., MANITCAIA V., MACHNIEWICZ T. // W: SIM Szkoła Inżynierii Materiałowej [Dokument elektroniczny] : Kraków, 7–8 maja 2025 = Materials Engineering School : book of abstracts. — Wersja do Windows. — Dane tekstowe. — [Kraków : AGH], [2025]. — e-ISBN: 978-83-68219-42-5. — S. 46–47. — Wymagania systemowe: Adobe Reader. — Tryb dostępu: https://sim.agh.edu.pl/home/sim/Grafiki/_SIM2025__Book_of_Abs... [2025-05-30]. — Bibliogr. s. 47