Abstract: A system comprising a device or the device itself for measuring temperatures, comprising a sensor array plate, comprising on a first surface at least one temperature sensor arranged on at least one tongue that is surrounded by a cut-out leaving a bridge to the sensor array plate, wherein the at least one sensor has on both sides' spacer and a second surface opposite the first surface for connection to at least one operating plate of a thermocycler; and a pressure plate, comprising fins at the side for connection to the sensor array plate that align with the spacer of the sensor array plate when a pressure plate is arranged onto a sensor array plate.

Abstract: An air gap between a main flap and an adjacent aircraft portion is closed an auxiliary flap. The auxiliary flap (8) has a hinging axis (9) extending substantially in parallel to the aerodynamic flow along aircraft portions adjacent to the auxiliary flap. With the aid of the auxiliary flap an aerodynamically improved transition zone is provided between the aircraft portion and the main flap.