|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/012.2; 244/007.A; 244/034.A|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 5|
VTOL micro-aircraft comprising a first and a second ducted rotor mutually aligned and distanced according to a common axis and whose propellers are driven in rotation in mutually opposite directions. Between the two ducted rotors are positioned a fuselage and a wing system formed by wing profiles forming an X or an H configuration and provided with control flaps.
1. Vertical Take-Off and Landing micro-aircraft comprising:a first ducted rotor and a second ducted rotor mutually aligned and distanced according to a common axis and each including a propeller rotatable within a respective annular cowling, a fuselage positioned along said common axis between said first and second rotors and bearing said propellers at opposite ends of the fuselage, first and second motorised means positioned at said ends of the fuselage to drive the propellers of said first and second rotor in mutually opposite directions of rotation, a...