|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 : 1 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. A system comprising: an unmanned aerial vehicle comprising: a propeller, anda rotor motor configured to drive rotation of the propeller;an energy source configured to provide electrical energy to the rotor motor, the energy source being a hybrid energy generation system including an engine coupled to a generator;an electronic device detachable from the unmanned aerial vehicle; anda cable configured to electrically connect the unmanned aerial vehicle to the electronic device;wherein the electronic device includes the energy source, andwherein the syste...