According to the present teachings, an aircraft engine configured to controllably shed ice during icing conditions is presented. The engine has a member operating at a first angular velocity having a surface divided into a first ice accumulating surface configured to collect ice, and a first shadow surface configured to resist the collection of ice. A first flange is disposed between the first ice accumulating surface and the first shadow surface.
ICE SHEDDING AIRCRAFT ENGINE
2019-10-10
Patent
Elektronische Ressource
Englisch
METHOD AND SYSTEM TO PROMOTE ICE SHEDDING FROM ROTOR BLADES OF AN AIRCRAFT ENGINE
Europäisches Patentamt | 2023
|METHOD AND SYSTEM TO PROMOTE ICE SHEDDING FROM ROTOR BLADES OF AN AIRCRAFT ENGINE
Europäisches Patentamt | 2021
|METHOD AND SYSTEM TO PROMOTE ICE SHEDDING FROM ROTOR BLADES OF AN AIRCRAFT ENGINE
Europäisches Patentamt | 2021
|