Digital twin of helicopter rotor blade adjustment mechanism

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Mirosław Wendeker

m.wendeker@pollub.pl

Michał Piłat

j.pytka@pollub.pl

Abstract

The article presents a new approach to monitoring and maintenance of dynamic helicopter systems by developing a digital twin of the rotor blade adjustment mechanism. The advanced digital model not only enables accurate tracking and analysis of a helicopter's operating conditions, but also contributes significantly to its safety and performance.In the article there are disscused the details of the solution in question, its importance and the technical challenges that had to be overcome on the way to its implementation.


 


 

Keywords:

helicopter, wirnik nośny, control dial, digital twin

References

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