Patent ID: 8690453

Claim:
A plug/socket arrangement, in particular of an electrical or optical plug connector of an aircraft or spacecraft, comprising: a housing; at least one insert which can be received in the housing; a releasable connection means which is adjustable between a locked position, in which the insert and the housing are locked to one another, and an unlocked position, in which the insert and the housing are not locked to one another; and an adjustment member which is adjustable between an inoperative position, in which the adjustment member is not operatively connected to the connection means, and a release position, in which the adjustment member is operatively connected to the connection means for releasing the locked position into the unlocked position of the connection means, wherein the adjustment member is formed as a clamp having at least one pressure projection comprising at least one pressure portion, the adjustment member comprising two actuation portions which are spaced apart by a gap when the adjustment member is in the inoperative position, the actuation portions resting against one another and the gap being closed when the adjustment member is in the release position.