METHOD AND DEVICE FOR TESTING A COMPONENT PART OF AN AIRCRAFT

摘要

A method for testing a component part of an aircraft comprises the steps of determining at least one first test value of the component part of the aircraft and/or at least one first test value of a comparable component part of a further aircraft for at least one test parameter, inputting the first test parameter and the first test value into a pattern recognition system, which produces an inner correlation between the first test parameter and the first test value. The method further comprises the steps of defining at least one second test parameter, inputting the second test parameter into the pattern recognition system in order to determine a second test value by means of the inner correlation, checking whether the second test value falls within the predefined value range, and determining a third test value of the component part of the aircraft for the second test parameter if the second test value falls within the predefined value range. The invention further relates to a device for testing a component part of an aircraft.

主权项

1. A method for testing a component part of a first aircraft, said method comprising the steps of:
a) determining one of at least one first test value of the component part of the first aircraft and at least one first test value of a comparable component part of a further aircraft for at least one first test parameter, said first test parameter comprising a specification for changing or manipulating one of the component parts and said determined test value comprising the result of a measurement with the presence of a change or manipulation of said component part determined by the respective test parameter; b) inputting said at least one first test parameter and said at least one first test value into a pattern recognition system, which produces an inner correlation between said at least one first test parameter and said at least one first test value, said inner correlation representing a linking of said at least one first test parameter to said at least one first test value; c) defining at least one second test parameter; d) inputting said second test parameter into said pattern recognition system in order to determine a second test value using said inner correlation; e) checking whether the second test value falls within a predefined value range; and f) determining a third test value of said component part of the first aircraft for the second test parameter when the second test value falls within the predefined value range.