Adjustment ring of a variable turbine geometry

An adjustment ring of a variable turbine geometry of an exhaust gas turbocharger is disclosed. The adjustment ring may include at least a first ring segment and a second ring segment.

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Bibliographic Details
Main Authors Mueller, Jochen, Lummer, Dirk, Jost, Robert, Jennes, Joerg
Format Patent
LanguageEnglish
Published 28.04.2020
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INTERNAL-COMBUSTION PISTON ENGINES
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:An adjustment ring of a variable turbine geometry of an exhaust gas turbocharger is disclosed. The adjustment ring may include at least a first ring segment and a second ring segment.
Bibliography:Application Number: US201715648436