Turbine shroud contour exducer relief
AssigneeGarrett Transportation I Inc.
InventorBrian D. Alexander
Life of this patent
Estimating the term…
Abstract
A turbocharger turbine having a blade-gap zone between the blades and the shroud wall. The blade-gap zone is larger at and near the exducer than at an upstream location where the shroud wall is at its minimum radius. Also disclosed is a method of customizing and manufacturing a turbine by establishing an optimized blade-gap zone at the exducer, and machining it into a turbine housing.
Claims6
A method of designing and manufacturing a turbine to meet design requirements including one or more design metrics from a group of design metrics consisting of flow, efficiency, and outlet temperature, comprising:
- providing a base turbine design;
- establishing values for the one or more design metrics for the base turbine design;
- providing a database of modification effects for a plurality of sets of turbine housing machining parameters, each set of turbine housing machining parameters including one or more turbine housing machining parameters from the group of turbine housing machining parameters consisting of an extension distance, a radial increase, and a corner geometric configuration;
- selecting an initial set of turbine housing machining parameters for the base turbine design to create a modified turbine design;
- establishing values for the one or more design metrics for the modified turbine design;
- iteratively reselecting the set of turbine housing machining parameters and reestablishing values for the one or more design metrics for the modified turbine design until the values for the one or more design metrics are optimized with regard to the design requirements to establish an optimum set of turbine housing machining parameters for the design requirements;
- and
- manufacturing a turbine of the base turbine design and manufacturing the turbine housing to meet the optimum set of turbine housing machining parameters.
A method of designing and manufacturing a turbine to meet design requirements including one or more design metrics from a group of design metrics consisting of flow, efficiency, and outlet temperature, comprising:
- providing a base turbine design;
- establishing values for the one or more design metrics for the base turbine design;
- providing a database of modification effects for a plurality of sets of turbine housing machining parameters, each set of turbine housing machining parameters including one or more turbine housing machining parameters from the group of turbine housing machining parameters consisting of an extension distance, a radial increase, a corner geometric configuration, and an outlet conical geometric configuration;
- selecting an initial set of turbine housing machining parameters for the base turbine design to create a modified turbine design;
- establishing values for the one or more design metrics for the modified turbine design;
- iteratively reselecting the set of turbine housing machining parameters and reestablishing values for the one or more design metrics for the modified turbine design until the values for the one or more design metrics are optimized with regard to the design requirements to establish an optimum set of turbine housing machining parameters for the design requirements;
- and
- manufacturing a turbine of the base turbine design and manufacturing the turbine housing to meet the optimum set of turbine housing machining parameters.
Dependencies are inferred from the claim text.