Patent ID: 8967530
Filing Date: 2015-03-03
Classification: B64D,F03D,F05B,Y02E

Abstract:
1. A power generation system for integration into an aircraft fuselage, the power generation system comprising: a secondary power supply device, comprising: at least one actuation device that is functionally connected with the opening and closing device for generating an opening or closing signal for the same; and an opening function switching device that is functionally coupled with a power generation monitoring device, wherein the opening function switching device is also functionally connected via a control cable with the unlocking device; wherein the opening function switching device is configured such that in an initial state the opening function switching device activates the unlocking device electrically with the first signal strength, with which the unlocking device locks the covering device; and wherein on receipt of a power requirement signal from the power generation monitoring device the opening function switching device activates the unlocking device electrically with the second signal strength, with which the unlocking device unlocks the covering device.