Metal spinning processes represents an interesting alternative to traditional sheet metal forming processes in several industrial contexts, such as automotive and aerospace. In this work, the production of a combustion chamber liner top prototype using AISI 304L stainless steel is proposed, in order to evaluate the process feasibility for the required part geometry. The prototypes production was carried out using a two-stage semiautomatic spinning process. The effects in terms of wall thickness reduction were investigated. Using optical microscopy and Scanning Electron Microscopy (SEM) techniques, the microstructural behavior of the metal subjected to the forming process was investigated, while for an evaluation of the influence on the mechanical properties Vickers micro-indentation tests were performed. The main result of the process, as observed from all the investigation techniques adopted, is the formation of strain induced martensite due to the severe plastic deformation and cold reduction of the material, ranging in this case from 30% to 50%. In some areas of the part section, some rips indicating an excessive tensile stress were also detected.

On the manufacturing of a gas turbine engine part through metal spinning process / Hassanin, A. E.; Astarita, A.; Scherillo, F.; Velotti, C.; Squillace, A.; Liguori, A.. - 1960:(2018), p. 160005. (Intervento presentato al convegno 21st International ESAFORM Conference on Material Forming, ESAFORM 2018 tenutosi a ita nel 2018) [10.1063/1.5035031].

On the manufacturing of a gas turbine engine part through metal spinning process

Hassanin A. E.;Astarita A.;Scherillo F.;Velotti C.;Squillace A.;
2018

Abstract

Metal spinning processes represents an interesting alternative to traditional sheet metal forming processes in several industrial contexts, such as automotive and aerospace. In this work, the production of a combustion chamber liner top prototype using AISI 304L stainless steel is proposed, in order to evaluate the process feasibility for the required part geometry. The prototypes production was carried out using a two-stage semiautomatic spinning process. The effects in terms of wall thickness reduction were investigated. Using optical microscopy and Scanning Electron Microscopy (SEM) techniques, the microstructural behavior of the metal subjected to the forming process was investigated, while for an evaluation of the influence on the mechanical properties Vickers micro-indentation tests were performed. The main result of the process, as observed from all the investigation techniques adopted, is the formation of strain induced martensite due to the severe plastic deformation and cold reduction of the material, ranging in this case from 30% to 50%. In some areas of the part section, some rips indicating an excessive tensile stress were also detected.
2018
On the manufacturing of a gas turbine engine part through metal spinning process / Hassanin, A. E.; Astarita, A.; Scherillo, F.; Velotti, C.; Squillace, A.; Liguori, A.. - 1960:(2018), p. 160005. (Intervento presentato al convegno 21st International ESAFORM Conference on Material Forming, ESAFORM 2018 tenutosi a ita nel 2018) [10.1063/1.5035031].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/755712
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