Process for re-designing a distressed component used under thermal and structural loading
A process for redesigning a distressed component in which the distressed component is under thermal and structural loads, for improving the life of the component. The process includes obtaining the operating conditions of the machine in which the distressed component is used, finding the boundary conditions under which the distressed component operates, producing a 3-dimensional model of the distressed component with such detail that the distress levels are accurately represented on the model, subjecting the model to a series of technical analysis to predict a life for the component, reiterating the technical analysis until the levels of distress on the model accurately represent the distress that appears on the actual component, and then predicting a remaining life of the component based on the analysis, or redesigning the model and reanalyzing the model until a maximum life for the component has been found.
1. A process for operating a gas turbine engine based upon a remaining life of a distressed engine component, the process comprising the steps of:
determining a remaining life of a distressed engine component used in a first engine having a first set of boundary conditions;
obtaining a solid model of the engine component with levels of distress on the component;
performing a technical analysis on the solid model to determine a second set of boundary conditions in which the remaining life of the distressed component is substantially the longest;
re-using the distressed engine component in a second engine having the second set of boundary conditions such that the distressed component will have a longer remaining life in the second engine than in the first engine.
2. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 1 , and further comprising:
the step of performing a technical analysis on the engine component includes performing a structural and a thermal analysis of the engine component.
3. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 2 , and further comprising:
the step of performing a technical analysis on the engine component includes generating a solid model of the distressed component with such accuracy that the component distress features can be measured from a scanned solid model.
4. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 1 , and further comprising:
the first engine is a base load engine and the second engine is a low load engine, and the process further includes the steps of determining the boundary conditions for the distressed component that will allow a longer remaining life for the component; and,
operating the engine at the boundary conditions that provide the longer life for the distressed component than under the operating conditions of the base load engine.
5. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 3 , and further comprising:
the step of generating a solid model of the distressed component includes scanning the distressed component with a non-contact and material independent 3-D digitization of the component with such accuracy that the component distress features can be measured from the scanned solid model.
6. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 5 , and further comprising the step of:
the non-contact and material independent solid digitization includes a white light scanner.
7. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 1 , and further comprising:
the step of performing a technical analysis on the engine component includes performing a structural and a vibrational analysis of the engine component.
8. The process for operating a gas turbine engine based upon a remaining life of a distressed engine component of claim 1 , and further comprising the step of:
the second engine is a peak load engine or a low load engine.