| 摘要 |
The invention relates to an adapter for a connector in an aircraft power supply system that is designed to permit the supply of power onboard aircraft, comprising pins (16, 18, 20) that are positioned in the aircraft, especially extending outward from a base plate (22), onto which sockets of the adapter may be pushed. In order to enable the rapid replacement or repair in the case of damage to a pin, it is proposed that an exchangeable adapter (24) be positioned on and fastened to the pins (16, 18, 20) in the aircraft, and that the adapter be comprised of a receptacle base (38) with contact elements (26, 28, 36), which are designed, in the area nearest the pins, at one end as sleeves or sockets designed to take up the pins, and at the other end to extend beyond the receptacle base and correspond dimensionally to the pins.
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