发明名称 SYSTEME D'ETANCHEITE DE LA CHAMBRE DE LUBRIFICATION ARRIERE D'UN TURBOREACTEUR
摘要 <p>The jet engine has a shaft (14) driven by a turbine (12) superimposed outside the shaft, which is supported by a rear rolling bearing (20) situated between the shaft and the turbine. The rolling bearing is housed in a lubricating chamber (24), which maintains oil mist. The chamber has an inner rotating part and an outer fixed part separated by a seal (40). A pressurized recovery chamber (26) surrounds the lubricating chamber and comprises another seal (48) situated radially with respect to the seal (40), where the seal (48) is situated downstream from a rotor (28) of the turbine.</p>
申请公布号 FR2889561(B1) 申请公布日期 2010.10.29
申请号 FR20050008232 申请日期 2005.08.02
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION SNECMA 发明人 BART JACQUES;ROUSSELIN STEPHANE
分类号 F02C7/06 主分类号 F02C7/06
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