A novel process chain for the automated repair of leading edges in aircraft engines

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

Autoren

  • Robert Kenneweg
  • Klaas Maximilian Heide
  • Volker Böß
  • Berend Denkena
  • Hans Henrik Westermann

Externe Organisationen

  • MTU Maintenance
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Details

OriginalspracheEnglisch
Seiten (von - bis)483-496
Seitenumfang14
FachzeitschriftProduction Engineering
Jahrgang18
Ausgabenummer3-4
Frühes Online-Datum29 Jan. 2024
PublikationsstatusVeröffentlicht - Juni 2024

Abstract

Due to impacts and constant stress, the leading edges of aircraft engine blades often lose their shape, while the other parts of the blade are still functional. This results in unnecessary performance losses. Currently, there is no method for a fast and effective repair process as the initial shape of the blade cannot be restored. This paper presents an automated re-contouring process chain for leading edges without prior material application. Thus, it is a sustainable approach to extend the lifespan until an energy-consuming welding process can be performed. It consists of an in-machine scanning process to obtain information about the worn shape, a subsequent target model generation based on the worn shape, and an automated process planning. The process chain is evaluated using a universal, leading edge workpiece. The results show that the target requirements for shape and smoothness are fulfilled.

ASJC Scopus Sachgebiete

Zitieren

A novel process chain for the automated repair of leading edges in aircraft engines. / Kenneweg, Robert; Heide, Klaas Maximilian; Böß, Volker et al.
in: Production Engineering, Jahrgang 18, Nr. 3-4, 06.2024, S. 483-496.

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

Kenneweg, R, Heide, KM, Böß, V, Denkena, B & Westermann, HH 2024, 'A novel process chain for the automated repair of leading edges in aircraft engines', Production Engineering, Jg. 18, Nr. 3-4, S. 483-496. https://doi.org/10.1007/s11740-023-01233-3
Kenneweg, R., Heide, K. M., Böß, V., Denkena, B., & Westermann, H. H. (2024). A novel process chain for the automated repair of leading edges in aircraft engines. Production Engineering, 18(3-4), 483-496. https://doi.org/10.1007/s11740-023-01233-3
Kenneweg R, Heide KM, Böß V, Denkena B, Westermann HH. A novel process chain for the automated repair of leading edges in aircraft engines. Production Engineering. 2024 Jun;18(3-4):483-496. Epub 2024 Jan 29. doi: 10.1007/s11740-023-01233-3
Kenneweg, Robert ; Heide, Klaas Maximilian ; Böß, Volker et al. / A novel process chain for the automated repair of leading edges in aircraft engines. in: Production Engineering. 2024 ; Jahrgang 18, Nr. 3-4. S. 483-496.
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abstract = "Due to impacts and constant stress, the leading edges of aircraft engine blades often lose their shape, while the other parts of the blade are still functional. This results in unnecessary performance losses. Currently, there is no method for a fast and effective repair process as the initial shape of the blade cannot be restored. This paper presents an automated re-contouring process chain for leading edges without prior material application. Thus, it is a sustainable approach to extend the lifespan until an energy-consuming welding process can be performed. It consists of an in-machine scanning process to obtain information about the worn shape, a subsequent target model generation based on the worn shape, and an automated process planning. The process chain is evaluated using a universal, leading edge workpiece. The results show that the target requirements for shape and smoothness are fulfilled.",
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