COOLING SYSTEM
To provide a cooling system which is simple and light-weight.SOLUTION: A cooling system 60 includes: rotors (VTOL rotors 20 and cruise rotors 22) which generate at least one of a lift force and a thrust force of an air craft 10; component groups 24 each comprising a plurality of electric components...
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| Format: | Patent |
| Sprache: | eng ; jpn |
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| Zusammenfassung: | To provide a cooling system which is simple and light-weight.SOLUTION: A cooling system 60 includes: rotors (VTOL rotors 20 and cruise rotors 22) which generate at least one of a lift force and a thrust force of an air craft 10; component groups 24 each comprising a plurality of electric components which rotate the rotor; and a cooling circuit 62 which cools the component groups 24. The cooling system 60 includes the plurality of component groups 24 corresponding to the multiple rotors. The plurality of component groups 24 are cooled by the same cooling circuit 62.SELECTED DRAWING: Figure 9
【課題】簡素で軽い冷却システムを提供する。【解決手段】航空機１０の揚力と推力の少なくとも一方を発生させるロータ（ＶＴＯＬロータ２０、クルーズロータ２２）と、ロータを回転させる複数の電気コンポーネントからなるコンポーネント群２４と、コンポーネント群２４を冷却する冷却回路６２と、を備える冷却システム６０であって、複数のロータに対応する複数の前記コンポーネント群２４を有し、複数のコンポーネント群２４は、同じ冷却回路６２で冷却される。【選択図】図９ |
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