|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-027/08 B64C-039/02 B64D-027/02 B64C-027/00 B64D-033/08 B64D-027/24 B64D-001/08 B64D-001/22 B64F-003/02 G05D-001/10|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 10|
An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator system comprises a rechargeable battery configured to provide power to the at least one rotor motor, a small engine configured to generate mechanical power, a generator motor coupled to the small engine and configured to generate AC power using the mechanical power generated by the small engine, a bridge rectifier configured to convert the AC power generated by the generator motor to DC power and provi...
1. An unmanned aerial vehicle comprising: at least one rotor motor configured to drive at least one propeller to rotate around an axis of rotation, rotation of the at least one propeller generating thrust and causing the unmanned aerial vehicle to fly;an electronic speed control configured to control an amount of power provided to the at least one rotor motor; anda micro hybrid generator system configured to provide power to the at least one rotor motor comprising: a rechargeable battery configured to provide power to the at least one rotor motor;a small...