发明名称 |
EPICYCLIC REDUCTION GEAR WITH FLUID TRANSFER PIPES, AND PROPELLER TURBOMACHINE FOR AN AIRCRAFT WITH SUCH A REDUCTION GEAR |
摘要 |
The epicyclic reduction gear comprises a planetary input shaft, planet gears meshing around said shaft and supported by a planet carrier, and two transverse sides. According to the invention, the reduction gear comprises at least one fluid transfer pipe suitable for being connected to a fluid supply source and passing through the planet carrier, being linked in rotation to same, from a first of said transverse sides of the reduction gear to a second of said transverse sides of the latter in order to open on the outside of the reduction gear and dispense the fluid. |
申请公布号 |
EP3030808(A1) |
申请公布日期 |
2016.06.15 |
申请号 |
EP20140790183 |
申请日期 |
2014.08.06 |
申请人 |
SNECMA |
发明人 |
CURLIER, AUGUSTIN;BOUDEBIZA, TEWFIK;CHARIER, GILLES, ALAIN |
分类号 |
F16H57/04 |
主分类号 |
F16H57/04 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|