| 摘要 |
An aircraft power distribution system according to an exemplary aspect of the present disclosure includes, among other things, a power source 14, a load 20, 22, and a power distribution panel 12 receiving power from the power source 14 and selectively providing power to the load 20, 22. The power source 14 is connected to the power panel by a lug 40 having a heat sink portion 62. The heat sink portion 62 has at least one increased dimension relative to the remainder of the lug 40. |
