|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/039.163; 060/788; 060/802|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 2|
A gas turbine engine arrangement comprises a first gas turbine engine, a second gas turbine engine, a differential gearbox and an electrical generator. The differential gearbox has a first input drive, a second input drive and an output drive. The output drive of the differential gearbox is arranged to drive the electrical generator via an external, accessory, gearbox. The external, accessory, gearbox drives other accessories. The first gas turbine is arranged to drive the first input drive of the differential gearbox and the second gas turbine engine is...
1. A gas turbine engine arrangement comprising a first gas turbine engine, a power unit, a differential gearbox and at least one electrical generator, the differential gearbox having a first input drive, a second input drive and an output drive,wherein the differential gearbox comprises a sun gear, a plurality of planet gears, and an annulus gear, wherein the planet gears mesh with the sun gear and the annulus gear and the planet gears are rotatably mounted on a carrier,wherein the first input drive is affixed to one of the sun gear, the annulus gear, or...