| 摘要 |
The subject matter of the invention is to connect a nozzle ring (5) of an exhaust gas turbine to an inner gas inlet housing (10) of the exhaust gas turbine in a supporting manner. Owing to the supporting connection to the nozzle ring (5), the inner gas inlet housing (10) has no additional bracing on an outer gas inlet housing (9) of the exhaust gas turbine since such a bracing would influence an exhaust gas flow in a flow channel of the exhaust gas turbine. |
