Propulsion System Instrumentation Development and Integration on Small- and Medium-Sized Electric Unmanned Aircraft

2022 ◽  
Author(s):  
Or D. Dantsker ◽  
Renato Mancuso
2014 ◽  
Vol 250 ◽  
pp. 204-211 ◽  
Author(s):  
D. Verstraete ◽  
K. Lehmkuehler ◽  
A. Gong ◽  
J.R. Harvey ◽  
G. Brian ◽  
...  

2014 ◽  
Vol 7 (1) ◽  
pp. 126-134 ◽  
Author(s):  
Kyle Merical ◽  
Troy Beechner ◽  
Paul Yelvington

1998 ◽  
Author(s):  
David J. Bents ◽  
Ted Mockler ◽  
Jaime Maldonado ◽  
James L. Harp ◽  
Joseph F. King ◽  
...  

2016 ◽  
Vol 2016 (8) ◽  
pp. 97-103
Author(s):  
Dominik Głowacki ◽  
Mirosław Rodzewicz

AbstractThis paper concerns fatigue testing of the rotor of the propulsion system for the MOSUPS – an unmanned aircraft designed in a joint wing configuration, and equipped with a ducted propeller. The work presents the analysis of the stresses and deformations of the rotor structure as well as the form of the loading cycle. The aim of the paper is to introduce the concept of a simplified method of fatigue testing of multi-blade rotors. With the sophisticated geometry of the rotor in mind – the authors applied the FEM tools and implemented the ANSYS and nCode programs. The prototype of the fatigue stand built by the authors is also presented in the paper.


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