ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT AND CONTROL DEVICE OF ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT
ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT AND CONTROL DEVICE OF ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT
- New search for: SUGITA SHUN
- New search for: IWAKAWA AKIRA
- New search for: HASHIMOTO MARIKO
- New search for: TAKEMURA YUICHI
- New search for: SUGITA SHUN
- New search for: IWAKAWA AKIRA
- New search for: HASHIMOTO MARIKO
- New search for: TAKEMURA YUICHI
To properly determine a maintenance timing with respect to each of a plurality of electric driving systems.SOLUTION: Electric vertical takeoff/landing aircrafts 100, 100a-d equipped with a plurality of electric driving systems 10, 10a-d having a driving motor 12 rotation-driving a rotary blade 30 and a drive portion 11 driving the driving motor, include: a drive information detecting portion 55 that detects drive information including at least either one of motor information that is an index of a deterioration state of the driving motor or drive portion information that is an index of a deterioration of the drive portion, for each of the plurality of electric driving systems; and a maintenance necessity detecting portion 57 that detects whether maintenance is necessary or not to each of the plurality of electric driving systems, on the basis of the detected drive information.SELECTED DRAWING: Figure 3
【課題】複数の電駆動システムのそれぞれに対する保守時期を適切に判断する。【解決手段】回転翼３０を回転駆動させる駆動用モータ１２と駆動用モータを駆動させる駆動部１１とを有する複数の電駆動システム１０、１０ａ〜ｄを備える電動垂直離着陸機１００、１００ａ〜ｄは、駆動用モータの劣化状態の指標となるモータ情報と、駆動部の劣化状態の指標となる駆動部情報と、のうちの少なくとも一方を含む駆動情報を、複数の電駆動システムのそれぞれに対して検出する駆動情報検出部５５と、検出された駆動情報に基づいて、複数の電駆動システムのそれぞれに対する保守要否を検出する保守要否検出部５７と、を備える。【選択図】図３
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ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT AND CONTROL DEVICE OF ELECTRIC VERTICAL TAKEOFF/LANDING AIRCRAFT
電動垂直離着陸機および電動垂直離着陸機の制御装置
2021-03-11
Patent
Electronic Resource
Japanese
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