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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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