一种基于激励振动和加热组合除冰组件

本发明属于飞机防除冰系统领域，特别涉及一种基于激励振动和加热组合除冰组件。所述组件包括：激励振动器和加热器；所述激励振动器布置在蒙皮内表面，位于结冰防护区域边缘；所述加热器布置在蒙皮内表且位于蒙皮边缘处或结构件支撑部位。...

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Bibliographic Details
Format Patent
LanguageChinese
Published 08.04.2025
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:本发明属于飞机防除冰系统领域，特别涉及一种基于激励振动和加热组合除冰组件。所述组件包括：激励振动器和加热器；所述激励振动器布置在蒙皮内表面，位于结冰防护区域边缘；所述加热器布置在蒙皮内表且位于蒙皮边缘处或结构件支撑部位。
Bibliography:Application Number: CN202411779979