发明名称 ROLLING BEARING FOR AIRCRAFT ENGINE
摘要 PROBLEM TO BE SOLVED: To prolong a usable time further by suppressing a temperature increase of a bearing in a dry-run status. SOLUTION: Friction heating inside the bearing is escaped to a housing 12 through an outer ring 3 by interposing heat conductive grease 6 containing heat conductive material between an outer diameter face of the outer ring 3 and an inner diameter face of the housing 12. Therefore, the temperature increase of a ball bearing 1 in the dry-run status can be suppressed, and the usable time is further prolonged. COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2008157365(A) 申请公布日期 2008.07.10
申请号 JP20060347530 申请日期 2006.12.25
申请人 NTN CORP 发明人 KOMATSUBARA SHINJI;ITO TAKASHI
分类号 F16C35/07;F16C19/06;F16C33/58;F16C37/00 主分类号 F16C35/07
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