Icing of Ducted Tail Rotor Based on Design of ILX-27 Unmanned Helicopter
Pawel Gula, Adam Dziubiński, Institute of Aviation; Piotr Neckarz, PZL Mielec A Sikorsky Company
May 17, 2016
Icing of Ducted Tail Rotor Based on Design of ILX-27 Unmanned Helicopter
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Icing of Ducted Tail Rotor Based on Design of ILX-27 Unmanned Helicopter
Authors / Details: Pawel Gula and Adam Dziubiński, Institute of Aviation; Piotr Neckarz, PZL Mielec A Sikorsky CompanyAbstract
The main objective of this paper is to describe the work done in the Polish unmanned helicopter ILX-27 project. The paper presents the effects of icing on the characteristics of helicopter’s tail rotor. Simulation of ice accretion process on areas particularly prone to icing and ice formations’ influence on operation safety are demonstrated. The influence of ice cover on whole ducted fan device thrust, a force and moment components on the blade are presented. The ice accretion causes mainly an increase of rotor drag.
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Icing of Ducted Tail Rotor Based on Design of ILX-27 Unmanned Helicopter
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