|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-027/08 B64C-039/02 B64C-027/00 B64D-001/08 B64D-001/22 B64D-027/02 B64D-027/24 B64D-033/08 B64F-003/02 G05D-001/10|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 13|
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: a propeller;a rotor motor to drive rotation of the propeller;a hybrid energy generation system comprising a rechargeable battery configured to provide electrical energy to the rotor motor,an engine configured to generate mechanical energy,a generator configured to convert the mechanical energy generated by the engine into electrical energy, anda flexible coupling device that directly couples a rotor of the engine to the generator, the flexible coupling device including a heat transfer system disposed between the ...