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>.
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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 |
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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