The present invention provides a flight vehicle operating method comprising the steps of: (a) flying a flight vehicle in the direction toward a mooring portion located under the flight vehicle; (b) mooring the flight vehicle at the mooring portion by connecting the flight vehicle to the mooring portion with a cable; (c) reducing the weight of the flight vehicle, increasing the buoyancy of the flight vehicle, or increasing the buoyancy of the flight vehicle while reducing the weight of the flight vehicle, by using a first floating control portion; (d) floating the flight vehicle in the air at an optimum altitude; (e) increasing the weight of the flight vehicle, reducing the buoyancy of the flight vehicle, or reducing the buoyancy of the flight vehicle while increasing the weight of the flight vehicle, by using a second floating control portion or a propulsion portion of the flight vehicle; and (f) disconnecting the connection between the flight vehicle and the mooring portion and retrieving the cable.
La présente invention concerne un procédé de fonctionnement d'un véhicule aérien comprenant les étapes consistant à : (a) faire voler un véhicule aérien en direction d'une partie d'amarrage située sous le véhicule aérien ; (b) amarrer le véhicule aérien au niveau de la partie d'amarrage en attachant le véhicule aérien à la partie d'amarrage à l'aide d'un câble ; (c) réduire le poids du véhicule aérien, augmenter sa flottabilité ou augmenter sa flottabilité tout en réduisant son poids à l'aide d'une première partie de commande flottante ; (d) faire flotter le véhicule aérien dans l'air à une altitude optimale ; (e) augmenter le poids du véhicule aérien, réduire sa flottabilité ou réduire sa flottabilité tout en augmentant son poids à l'aide d'une seconde partie de commande flottante ou d'une partie de propulsion du véhicule aérien ; puis (f) détacher l'attache entre le véhicule aérien et la partie d'amarrage et récupérer le câble.
본 발명은 (a) 비행체를 상기 비행체 하부에 위치하는 계류부 방향으로 비행시키는 단계, (b) 케이블에 의해 상기 비행체와 상기 계류부를 서로 연결하여 상기 비행체를 상기 계류부에 계류시키는 단계, (c) 제1부양조절부를 이용하여, 상기 비행체의 중량을 감소시키거나, 상기 비행체의 부력을 증가시키거나, 상기 비행체의 중량을 감소시키면서 상기 비행체의 부력을 증가시키는 단계, (d) 상기 비행체를 공중에 적정 고도로 부양시키는 단계, (e) 제2부양조절부 또는 상기 비행체의 추진부를 이용하여, 상기 비행체의 중량을 증가시키거나, 상기 비행체의 부력을 감소시키거나, 상기 비행체의 중량을 증가시키면서 상기 비행체의 부력을 감소시키는 단계 및 (f) 상기 비행체와 상기 계류부 간의 연결을 해제하고 상기 케이블을 회수하는 단계를 포함하는, 비행체 운용 방법을 제공한다.
FLIGHT VEHICLE OPERATING METHOD AND OPERATING SYSTEM USING SAME
PROCÉDÉ DE FONCTIONNEMENT D'UN VÉHICULE AÉRIEN ET SYSTÈME DE FONCTIONNEMENT L'UTILISANT
비행체 운용 방법 및 이를 이용하는 운용 시스템
14.12.2017
Patent
Elektronische Ressource
Koreanisch
IPC: | B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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