Digital twin of helicopter rotor blade adjustment mechanism
Article Sidebar
Issue No. 3-4 (2024)
-
From the editors
Jarosław Pytka, Elżbieta Nazaruk
-
Digital twin of helicopter rotor blade adjustment mechanism
Mirosław Wendeker, Michał Piłat
-
About the glider „Junior” a bit differently
Michał Ombach
-
SZD-51-1 Junior glider design and technology
Tomasz Murawski
-
ICON A5 – on land, water, in the air
Damian Kowalczyk
Main Article Content
Authors
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:
References
[1] Cooke, A.K., Fitzpatrick, E. (2002). Helicopter Test and Evaluation. New Jersey: John Wiley & Sons.
[2] Padfield, G. (1998). Dynamika lotu śmigłowców. Sulejówek: Wydawnictwa Komunikacji i Łączności.
[3] Seddon, J., Newman, S. (2011). Basic Helicopter Aerodynamics (3rd ed.). New Jersey: John Wiley & Sons.
[4] Szabelski, K., Jancelewicz, B., Łucjanek, W. (1995). Wstęp do konstrukcji śmigłowców. Sulejówek: Wydawnictwa Komunikacji i Łączności.
[5] Witkowski, R. (2023). Wprowadzenie do wiedzy o śmigłowcach. Warszawa: Wydawnictwo Naukowe Instytutu Lotnictwa.
Article Details
Abstract views: 201
Downloads: 237

