发明名称 BEARING FAILURE INDICATOR
摘要 <p>The invention provides a bearing failure indication arrangement comprising a bearing having an inner and outer race, a first part arranged to be attached in fixed relation to either the bearing inner race or bearing outer race, a failure indicator arranged in fixed relation to both the first part and either the bearing inner race or the bearing outer race, the failure indicator constructed so that if relative movement occurs between the first part and the bearing race to which it is attached, the failure indicator responds to the relative movement thereby indicating failure of the bearing. The failure indicator is particularly adapted for use in aircraft structures and indicates full of partial bearing failure by means of movement and/or deformation of the indicator.</p>
申请公布号 WO2007132159(A1) 申请公布日期 2007.11.22
申请号 WO2007GB01608 申请日期 2007.05.03
申请人 AIRBUS UK LIMITED;BLADES, PAUL;BURNESS, RICHARD, JOHN, HENRY 发明人 BLADES, PAUL;BURNESS, RICHARD, JOHN, HENRY
分类号 F16C19/52;F16C11/04;F16C35/063;G01M13/04 主分类号 F16C19/52
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