| 摘要 |
<p>A hubcap (60) for an aircraft wheel (56) includes an internal spider (80) which engages an anti-skid transducer (30) located in the wheel hub. The hubcap (60) is constructed of one piece and has a conical configuration to provide increased strength as well as increased airflow inside the hubcap (60) for improved heat dissipation. <IMAGE></p> |
