To make flight performance and submersion performance compatible in a pilotless aircraft submersible in water.SOLUTION: This is solved by a submersible pilotless aircraft (10) individually provided with a rotor (50) having a horizontal rotary blade (51) for flight and provided with a thrust source (60) used for movement in water. Such a pilotless aircraft preferably has a plurality of the rotors and a plurality of the thrust sources. Furthermore, it is preferable that the thrust source be able to generate thrust in one direction and an opposite direction to it and that the horizontal rotary blade be able to pivot in a direction along a rotation center axis of the rotor.SELECTED DRAWING: Figure 1
【課題】水中に潜水可能な無人航空機について、その飛行性能と潜水性能とを両立させる。【解決手段】飛行用の水平回転翼(51)を有するロータ(50)と、水中での移動に用いる推力源(60)と、を個別に備える潜水可能な無人航空機(10)によりこれを解決する。かかる無人航空機は、複数の前記ロータと複数の前記推力源とを有することが好ましく、さらには、前記推力源が一の方向とその反対方向とに推力を発生させることができること、前記水平回転翼が、前記ロータの回転中心線に沿う方向に旋回可能であることが好ましい。【選択図】図1
PILOTLESS AIRCRAFT
無人航空機
2022-02-10
Patent
Electronic Resource
Japanese
PILOTLESS AIRCRAFT MEASUREMENT UNIT AND PILOTLESS AIRCRAFT
European Patent Office | 2019
|Engineering Index Backfile | 1951
|Engineering Index Backfile | 1944