|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-035/04 B64D-027/02 B64C-027/22 B64C-029/00 B64C-001/14 B64C-027/52 B64C-039/02 B64D-017/24 B64D-017/34 B64D-017/62 B64D-017/80 B64D-031/00 B64C-027/26 B64C-027/28 B64C-027/82 B64D-017/64|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 12|
An aircraft may have a fuselage, a left wing extending from the fuselage, a right wing extending from the fuselage, a tail section extending from a rear portion of the fuselage, and a first engine and a second engine operably connected by a common driveshaft, wherein the first and second engines are configured for freewheeling such that if one of the first and second engines loses power the other of the first and second engines continues to power the aircraft.
1. An aircraft comprising: a fuselage having a longitudinal axis;a first engine disposed in said fuselage;a second engine disposed in said fuselage;said first and second engines being operably connected to a common driveshaft traversing through said first and second engines and having an axis of rotation oriented transverse to said longitudinal axis of said fuselage;a first propeller operably connected to said common driveshaft; anda second propeller operably connected to said common driveshaft;wherein said first and second engines are configured for fre...