|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/50 B64C-013/34 B64C-009/14 B64C-013/26|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 1 인용 특허 : 13|
A variable camber system for an aircraft may include a variable camber trim unit (VCTU) positioned between an inboard device and an outboard device. The inboard device and the outboard device may be mounted to at least one of a leading edge and a trailing edge of a wing. The VCTU may include a speed sum gearbox having an inboard shaft coupled to the inboard device and an outboard shaft coupled to the outboard device. The VCTU may additionally include a VCTU electric motor engaged to the speed sum gearbox. The VCTU electric motor may be selectively operab...
1. A variable camber system for an aircraft, comprising: a variable camber trim unit (VCTU) positioned between an inboard device and an outboard device mounted to at least one of a leading edge and a trailing edge of a wing, and including: a speed sum gearbox including: a sun gear coupled to an inboard shaft and surrounded by a plurality of planet gears, the planet gear supported on a carrier coupled to an outboard shaft, the planet gears engaged to an internal side of a ring gear, an external side of the ring gear engaged to a motor shaft, the inboard s...