Component testing
AssigneeMTU Aero Engines AG
InventorsChristian EICHLER, Dieter FRENO, Andreas HIEBER, Philipp FARAH, Salome GASSMAnn
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Abstract
The present invention relates to a method for testing a component, in particular an aircraft engine, comprising the steps of: determining (S40) a value of a first toleranced parameter (A1; A2) of the component; determining (S50) a value of a second toleranced parameter (E1; ...; E4) of the component; and classifying (S70) the component in a predefined quality class if this value pair lies outside of a predefined tolerance range, the upper and/or lower limit (G) of which for the second parameter depends on the first parameter, in particular linearly, in at least one first permissible value range (Ta1,1) of the first parameter.
Claims21
1-14. (canceled)
A method for testing a component, wherein the method comprises:
- determining (S40) a value of a first tolerated parameter (A1;
- A2) of the component;
- determining (S50) a value of a second tolerated parameter (E1;...;E4) of the component;
- and
- classifying (S70) the component in a specified quality class if the value pair is outside a specified tolerance range, the upper and/or lower limit (G) of which for the second parameter in at least one first permissible value range (Ta1,1) of the first parameter depend(s) on the first parameter.
Dependencies are inferred from the claim text.