The invention relates to an inductive component, an inductive device and an aircraft. In one aspect, there is described an inductive component (200) comprising an inductive element (100) comprising a stack of an outer plurality of first strips of magnetic material (107a), a central plurality of second strips of superconducting material (105), and an outer plurality of third strips of magnetic material (107b), the inductive element (100) is flexible and is configured to be wound on itself to form at least one loop of the stack of the first strip (107a), the second strip (105) and the third strip (107b). Thus, an increased ratio between the weight of an aircraft comprising such an inductive component and the available electrical power onboard the aircraft system can be advantageously obtained.
本发明涉及电感部件、电感设备和飞行器。在一个方面中,描述了一种包括电感元件(100)的电感部件(200),该电感元件包括外部多个第一磁性材料条(107a)、中心多个第二超导材料条(105)和外部多个第三磁性材料条(107b)的堆叠体,电感元件(100)是柔性的并且被配置成自身卷绕地形成第一条(107a)、第二条(105)和第三条(107b)的所述堆叠体的至少一个环。因此,可以有利地获得包括这种电感部件的飞行器的重量与飞行器系统的机载可用电功率之间的增加的比率。
Inductive component, inductive device and aircraft
电感部件、电感设备和飞行器
2023-12-29
Patent
Elektronische Ressource
Chinesisch
IMPROVED INDUCTIVE COMPONENT FOR ELECTRIC OR HYBRID AIRCRAFT
Europäisches Patentamt | 2024
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