TURBO COMPRESSOR HOUSING, METHOD FOR PRODUCING SAME

The invention relates to a turbocompressor housing (TCC) which extends along a longitudinal axis (X). The turbocompressor housing (TCC) has an inflow (INL1) in an axial inflow section (INA1) leading into an interior (CAC) and an outflow (EXT) in an axial outflow section (EXA1) leading out of the int...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: MEYER, Marcus, NASS, Dieter
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The invention relates to a turbocompressor housing (TCC) which extends along a longitudinal axis (X). The turbocompressor housing (TCC) has an inflow (INL1) in an axial inflow section (INA1) leading into an interior (CAC) and an outflow (EXT) in an axial outflow section (EXA1) leading out of the interior (CAC). The invention is characterized in that the turbocompressor housing (TCC) is welded on a radial separating plane (SPL) between the axial inflow section (INA1) and the axial outflow section (EXA1) by means of a welding seam (WSE) which extends in the circumferential direction and through the wall thickness. The interior (CAC) of the inflow section (INA1) is at least partly provided with a coating (CLD) in a coated region (CLA).