|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F16D-011/04 F02C-007/36 F16D-028/00 F02C-007/32 F16D-023/12 F16D-001/10|
|우선권정보||FR-11 56023 (2011-07-04)|
|§371/§102 date||20140103 (20140103)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 8|
A gas turbine AGB has a front lateral face, a rear lateral face opposite from the front lateral face, and a peripheral rim closing the box. At least one gear train is mounted in the AGB and is made up of a plurality of gearwheels meshing together, and designed to be coupled to a drive shaft for driving an accessory. The AGB further comprises, mounted between a central shaft carrying each gearwheel and the drive shaft, a decoupling unit for decoupling the accessory and constituted by a dog clutch having axial teeth co-operating with complementary teeth of...
1. A gas turbine accessory gear box (AGB), comprising: a front lateral face;a rear lateral face opposite from the front lateral face;a peripheral rim extending between the front and rear lateral faces;a gear train including a plurality of gearwheels meshing together, one of the gearwheels being carried by a central shaft held at each end thereof by a respective rolling bearing, the central shaft being coupled to a drive shaft for driving an accessory; anddecoupling means, mounted between said central shaft and said drive shaft, for decoupling said access...