| 摘要 |
<p>An aircraft propeller taper bore insert apparatus (100) includes an outer surface (101), the outer surface (101) dimensioned and configured to fit within an aircraft propeller taper bore or an aircraft propeller balancing tube, and an inner surface (102), the inner surface (102) defining an inner cavity (103) configured to receive a balancing medium (202), the inner surface (102) comprising a plurality of retention formations (104) arranged thereon, and the plurality of retention formations (104) being configured to support the balancing medium (202).</p> |
