VERFAHREN ZUR HERSTELLUNG VON GEBLAESESCHEIBEN AUS TITAN UNTER ANWENDUNG EINER DIFFUSIONSBINDUNG
A method of making a titanium fan disc for a gas turbine engine comprises providing a pair of identical forged titanium cylinders each having a central bore and a flat end surface at right angles to its central axis, preparing the flat end surface of each cylinder to a high degree of smoothness, abu...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | ger |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | A method of making a titanium fan disc for a gas turbine engine comprises providing a pair of identical forged titanium cylinders each having a central bore and a flat end surface at right angles to its central axis, preparing the flat end surface of each cylinder to a high degree of smoothness, abutting the prepared surfaces of the cylinders one against the other in axial alignment, removing air from between said surfaces, and diffusion bonding the cylinders end-to-end by hot isostatic pressing to form the disc. A flange may be provided on each cylinder with a recess to accept a titanium ring 24 which shields the cylinder from an electron beam used to form a weld 28 to seal the joint line for evacuation. The flange is ultimately machined away. |
---|