AN EXHAUST GAS TURBINE OF AN EXHAUST GAS TURBOCHARGER
Application 972/MAS/1997 published 2006-10-13, filed 1997-05-07
The object of the invention is to design the exhaust gas turbine of an exhaust gas turbocharger such that simple and reliable fastening of the nozzle ring is ensured. This is achieved according to the invention in that the nozzle ring (14) bears against the covering ring (8) by means of its outer ring (11) and against the gas inlet casing (1) by means of its inner ring (12).An axial expansion gap (15) is formed between the outer ring (11) and the gas inlet casing (1) and a radial expansion gap (16) is formed between the outer ring' (11) and the gas outlet casing (2).
Applicant
ABB SCHWEIZ AG
BROWN BOVERI STRASSE 6, CH-5400 BADEN,, SWITZERLAND
Inventor
International Info
Classification: F 01 D 9/04
Publication Number:
Priority Information
196 18 314.6 GERMANY 1996-05-08