The present invention relates to an aircraft component comprising: a composite material structure comprising a fibrous reinforcement embedded in a matrix; a heating element (9) configured to heat the component, the heating element (9) being embedded in a matrix of the composite material structure.
本发明涉及一种飞行器部件,该飞行器部件包括:复合材料结构,该复合材料结构包括嵌入基体中的纤维增强件;加热元件(9),该加热元件被构造成对部件进行加热,该加热元件(9)嵌入复合材料结构的基体中。
Blade deicing device
叶片除冰装置
2024-11-01
Patent
Electronic Resource
Chinese
Shape Memory Alloy Rotor Blade Deicing
AIAA | 2013
|Shape Memory Alloy Rotor Blade Deicing
British Library Conference Proceedings | 2013
|