Abstract: A power distribution arrangement, especially in an aircraft, includes plural power sources, a power line having plural power supply strands connected to the power sources, plural power consumer groups each including plural power consuming devices, and branch lines respectively connecting the power line with the power consumer groups. A respective allocation unit selectively interconnects the power consuming devices of each group with selected individual branch line strands of the branch lines. A status unit acquires information regarding the respective operating status of the power sources and the power line strands, and conveys corresponding information regarding a power failure on any power line strand to a central power control unit, which correspondingly transmits control commands over a control bus to the respective allocation units.

Abstract: The climate in one or more aircraft cabin zones is controlled to achieve a minimal use of fresh air and an optimal use of recirculation air while satisfying official regulation requirements and avoiding freeze-ups in the air duct system of commercial aircraft. For this purpose temperature sensors ascertain a plurality of different actual temperature informations at different locations in the air supply system. Valve position sensors provide actual flow volume information from one or more valve locations. An r.p.m., volumetric flow or differential pressure sensor provides actual blower r.p.m., volumetric flow or differential pressure information. A CPU compares the actual information with rated information stored in a memory or entered through a keyboard to provide control signals, including closed loop control and/or open loop control signals, to a blower or blowers, a valve or valves, and to at least one air conditioner.