Szczegóły publikacji

Opis bibliograficzny

Using HSM technology in machining of thin-walled aircraft structures / Paweł BAŁON, Edward Rejman, Bartłomiej KIEŁBASA, Robert Smusz // Acta Mechanica et Automatica ; ISSN 1898-4088. — 2022 — vol. 16 no. 1, s. 27-33. — Bibliogr. s. 33, Abstr. — P. Bałon - dod. afiliacja: SZEL-TECH, Mielec, Poland


Autorzy (4)


Słowa kluczowe

high speed machiningmillingaviationintegral structuresthin walled parts

Dane bibliometryczne

ID BaDAP138955
Data dodania do BaDAP2022-02-02
Tekst źródłowyURL
DOI10.2478/ama-2022-0004
Rok publikacji2022
Typ publikacjiartykuł w czasopiśmie
Otwarty dostęptak
Creative Commons
Czasopismo/seriaActa Mechanica et Automatica

Abstract

Subtracting manufacturing technologies have entered that realm of production possibilities which, even a few years ago, could not be directly adapted to direct production conditions. The current machines, i.e. heavy, rigid cutting machines using high spindle speed and high feed speed, allow for manufacturing very thin and relatively long parts for use in the automotive or aerospace industry. In addition, the introduction and implementation of new 70XX aluminium alloys with high strength parameters, as well as monolithic diamond cutting tools for special machining, have had a significant impact on the introduction of high-speed machining (HSM) technologies. The main ad-vantage of the applied manufacturing method is obtaining a very good smoothness and surface roughness, reaching even Sz = 6–10 μm and Sa <3 μm, and about four times faster and more efficient machining compared to conventional machining (for the beam part). Moreover, fixed and repeatable milling process of the HSM method, reduction of operational control, easy assembly of components and increase in the finishing efficiency compared to other methods of plastic processing (forming) are other benefits. The authors present a method using HSM for the manufacturing of aircraft parts, such as the chassis beam at the front of a commuter aircraft. The chassis beam assembly is made of two parts, front and rear, which – through a bolted connection – form a complete element replacing the previous part made using traditional technology, i.e., cavity machining, bending and plastic forming. The implementation of HSM technology eliminates many operations related to the construction of components, assembling the components (riveting) and additional controls during construc-tion and assembly.

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High speed machining of the thin-walled aircraft constructions — Obróbka z wysokimi prędkościami skrawania cienkościennych konstrukcji lotniczych / Paweł Bałon, Edward Rejman, Robert Smusz, Bartłomiej Kiełbasa // Mechanika ; ISSN 1392-1207. — 2017 — vol. 90 no. 8-9, s. 726–729. — Bibliogr. s. 729, Abstr. — P. Bałon - afiliacja: SZEL-TECH company
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Implementation of high speed machining in thin-walled aircraft integral elements / Paweł Bałon, Edward Rejman, Robert Smusz, Janusz SZOSTAK, Bartłomiej Kiełbasa // Open Engineering [Dokument elektroniczny]. — Czasopismo elektroniczne ; ISSN 2391-5439. — 2018 — vol 8 iss. 1, s. 162–169. — Wymagania systemowe: Adobe Reader. — Bibliogr. s. 169, Abstr. — Publikacja dostępna online od: 2018-06-18. — P. Bałon - afiliacja: SZEl-TECH Szeliga Grzegorz, Mielec, Poland