发明名称 Rolling bearing in aircraft
摘要 A single-row or multi-row rolling bearing comprising thin-walled bearing races which are made of a martensitic, through hardened steel and have the following characteristics: a surface hardness of >=613 HV (56 HRC) in the area of the bearing face; a core hardness of >=285 HV (28 HRC); a difference of >=150 HV (9 HRc) between the surface hardness and the core hardness. The core hardness is reached at a depth ranging between 8 percent of the diameter of the rolling elements and 90 percent of the wall thickness on the bottom of the track. There is a ratio of >=20 between the diameter of a pitch circle T<SUB>k </SUB>and the diameter of a rolling element D<SUB>W</SUB>.
申请公布号 US2006165329(A1) 申请公布日期 2006.07.27
申请号 US20050533043 申请日期 2005.05.23
申请人 KREISELMEIER GERHARD;SEBALD WILHELM;EBERT FRANZ J 发明人 KREISELMEIER GERHARD;SEBALD WILHELM;EBERT FRANZ J.
分类号 C21D9/40;F16C33/62;F16C19/16;F16C19/18;F16C33/58 主分类号 C21D9/40
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