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: A flap such as an aileron or a landing flap is operatively secured to the rear edge of an aircraft wing in such a manner that the wing construction itself may be thin in the direction perpendicularly to the central plane of the wing and as compared to the prior art wing structures. For this purpose a coupling plate extending vertically is secured to the bottom of the flap. The coupling plate provides two journal points arranged substantially vertically one above the other. The upper journal point is connected to the wing. The lower journal point is connected to a rocker drive. A drive piston rod is connected through crank levers to rotate the coupling plate in the manner of a four journal drive.