发明名称 PIVOT PIN FOR A TURBINE ENGINE COMPRISING A RING FOR RECOVERING A FLOW OF LUBRICATING OIL WITH A PLURALITY OF LUBRICATING OIL DISCHARGE PORTS
摘要 A journal configured to be driven in rotation in a housing of a turbine engine, or for an aircraft, the journal including: a circumferential main body including plural ventilation openings configured to allow plural axial airflows to circulate from upstream to downstream in the turbine engine, two consecutive ventilation openings being connected by a connecting segment, and a circumferential ring for recovering a flow of lubrication oil, which ring is rigidly connected to the main body and is radially inside the ventilation openings, the recovery ring including plural radial discharge openings for allowing plural radial flows of oil to be discharged towards the outside, each discharge opening being radially aligned with a connecting segment of the main body to allow each flow of oil to be discharged between the airflows.
申请公布号 US2015147157(A1) 申请公布日期 2015.05.28
申请号 US201314408425 申请日期 2013.06.12
申请人 SNECMA 发明人 Fontanel Eddy Stephane Joel;Rossi Giuliana Elisa;Bouiller Philippe Pierre Vincent;Da Costa Emmanuel;Foll Julien
分类号 F01D25/18 主分类号 F01D25/18
代理机构 代理人
主权项
地址 Paris FR