Abstract: Proposed is a self-optimizing, adaptive industrial chocolate production system (1), and method thereof. The system comprising a chocolate mass processing line (11) with at least dosing means (2), one or more mixers (3), one or more refiners (4), one or more conches (5), and liquefying and tempering means (6). Appropriate inter-dependent operational parameters of the various devices (2/3/4/5/6) are measured by real-time measuring devices and transmitted to a controller device 12. The measured inter-dependent operational parameters are mutually optimized and dynamically adjusted providing an optimal operation at least in terms of the characteristics of the end chocolate mass 7 and/or throughputs of the chocolate production line 11 and/or other operation conditions as energy consumption.

Abstract: Proposed is a self-optimizing, adaptive industrial chocolate production system (1), and method thereof. The system comprising a chocolate mass processing line (11) with at least dosing means (2), one or more mixers (3), one or more refiners (4), one or more conches (5), and liquefying and tempering means (6). Appropriate inter-dependent operational parameters of the various devices (2/3/4/5/6) are measured by real-time measuring devices and transmitted to a controller device 12. The measured inter-dependent operational parameters are mutually optimized and dynamically adjusted providing an optimal operation at least in terms of the characteristics of the end chocolate mass 7 and/or throughputs of the chocolate production line 11 and/or other operation conditions as energy consumption.

Abstract: A combination comprises an aircraft wing trailing edge section and an adjustment body. The adjustment body comprises a tapered cross section in a local chord axis direction of the wing trailing edge section, a lower adjustment body surface connected to a top surface of the aircraft wing trailing edge section and a back-end surface having a height. The adjustment body is positioned such that the back-end surface is flush with the trailing edge of the aircraft wing trailing edge section. Attaching the adjustment body onto a top surface of the wing trailing edge section leads to compensation of an offset rolling moment due to unavoidable structural shape deviations of the aircraft and eliminates additional structural reinforcement requirements on the trailing edge compared to edge wedges mounted on the bottom surface of trailing edges. The trailing edge section may comprise a flap.

Abstract: A blade bar (2) for a stripping system (10) for stripping a product from a roller in a roller mill, to a blade holding system (20), and to a stripping system (10). A pressure element (6) is provided for securing the blade in the blade bar, the pressure element is arranged within the blade bar. The blade bar (2) has a line (3) for conducting a fluid, by which pneumatic or hydraulic pressure can be built up in order to secure the stripping blade (1) on the blade bar (2).

Abstract: A combination comprises an aircraft wing trailing edge section and an adjustment body. The adjustment body comprises a tapered cross section in a local chord axis direction of the wing trailing edge section, a lower adjustment body surface connected to a top surface of the aircraft wing trailing edge section and a back-end surface having a height. The adjustment body is positioned such that the back-end surface is flush with the trailing edge of the aircraft wing trailing edge section. Attaching the adjustment body onto a top surface of the wing trailing edge section leads to compensation of an offset rolling moment due to unavoidable structural shape deviations of the aircraft and eliminates additional structural reinforcement requirements on the trailing edge compared to edge wedges mounted on the bottom surface of trailing edges. The trailing edge section may comprise a flap.