Investigation of the Effect of Dwell Period in Load Controlled Fatigue Tests of Inconel718 Superalloy

Numan Berat Yondu, Murat Baydogan

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

1 Atıf (Scopus)

Özet

The mechanical property of Inconel718 is examined in terms of fatigue behavior. The main concern of this work is to determine the material's fatigue properties under pure bending fatigue conditions with additional interruptions and thermal effects. Test conditions will include room temperature, 450°C, and dwell times to simulate the material's operating environment in the engine application. Additional to fatigue testing hardness measurements and nano indentation testing were performed at ambient temperature. Fractographic and microstructural examinations of the tested specimens are performed with an optical microscope and SEM (scanning electron microscope) to understand the material's reaction to different deformation factors.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığı23rd European Conference on Fracture, ECF 2022
EditörlerPedro Moreira, Luis Reis
YayınlayanElsevier B.V.
Sayfalar1567-1575
Sayfa sayısı9
ISBN (Elektronik)9781713870302
DOI'lar
Yayın durumuYayınlandı - 2022
Etkinlik23rd European Conference on Fracture, ECF 2022 - Funchal, Portugal
Süre: 27 Haz 20221 Tem 2022

Yayın serisi

AdıProcedia Structural Integrity
Hacim42
ISSN (Elektronik)2452-3216

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???event.eventtypes.event.conference???23rd European Conference on Fracture, ECF 2022
Ülke/BölgePortugal
ŞehirFunchal
Periyot27/06/221/07/22

Bibliyografik not

Publisher Copyright:
© 2022 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (https://creativecommons.org/licenses/by-nc-nd/4.0) Peer-review under responsibility of the scientific committee of the 23 European Conference on Fracture - ECF23.

Finansman

The present investigation is conducted as a part of thesis program in Istanbul Technical University Material Engineering Masters program under supervision of Prof. Murat Baydogan. The authors would like to thank TUSAS Engine Industry for supplying the material and specimen machining.

FinansörlerFinansör numarası
Türk Havacılık ve Uzay Sanayii

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