| 摘要 |
A method of fastening two structural members 48, 50 comprises the steps of: providing a sleeve 12 including a central channel 22 and a first diameter, inserting a bushing 14 comprising a tapered end 26 and portion spaced 28 apart from the tapered end 26 into the sleeve 12, where the portion 28 includes a second diameter which exceeds the first diameter of the sleeve 12. The method further includes inserting the sleeve 12 into an opening within one of the two structural members 48, 50 and securing the two structural members 48, 50 together. The two structural members 48, 50 may be aircraft parts. |
