发明名称 BEARING FOR ROCKET TURBO PUMP
摘要 PROBLEM TO BE SOLVED: To reduce wear caused by sliding contact between a cage and a guide race ring of a bearing for a rocket turbo pump. SOLUTION: In the bearing for a rocket turbo pump in which an inner ring 1 and an outer ring 2 are formed of martensitic stainless steel and at least a surface layer portion of the cage 4 is formed of PTFE, an inner diameter surface 2a of the outer ring 2 for guiding the cage 4 is processed to have an arithmetical means roughness value Ra of surface roughness not larger than 0.2μm. It is thus possible to largely reduce the wear caused by the sliding contact of the cage 4 with the outer ring 2, as compared with the prior art. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006057744(A) 申请公布日期 2006.03.02
申请号 JP20040240662 申请日期 2004.08.20
申请人 NTN CORP 发明人 ITO TAKASHI;NOZAKI MASAYUKI;NAKAMURA SHOHEI
分类号 F16C33/64;F02K9/60;F04D29/046;F16C19/16;F16C33/38;F16C33/62 主分类号 F16C33/64
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