发明名称 ROLLING BEARING IN AIRCRAFT
摘要 Disclosed is a single-row or multi-row rolling bearing (1, 2) comprising thin-walled bearing races (3, 4, 5) which are made of a martensitic, fully hardened steel and have the following characteristics: a surface hardness (7, 7a) of = 613 HV (56 HRC) in the area of the bearing face; a core hardness (8) of = 285 HV (28 HRC); a difference (<) of = 150 HV (9HRc) 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; and a ratio of = 20 between the diameter of a partial circle Tk and the diameter of a rolling element DW.
申请公布号 WO2004040026(A2) 申请公布日期 2004.05.13
申请号 WO2003DE03603 申请日期 2003.10.29
申请人 FAG KUGELFISCHER AG;KREISELMEIER GERHARD;SEBALD WILHELM;EBERT FRANZ JOSEF 发明人 KREISELMEIER GERHARD;SEBALD WILHELM;EBERT FRANZ JOSEF
分类号 C21D9/40;F16C19/16;F16C19/18;F16C33/58;F16C33/62 主分类号 C21D9/40
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