Turbo engine, in particular a turbine for an airplane, characterized in that the turbo engine (100) is coupled with an energy harvesting device (30) comprising at least one thermoelectric device (10) for producing electric energy from temperature differences in the turbo engine (100) and / or at least one kinetic energy converter (40) for the conversion of vibrational energy into electric energy and wherein the energy harvesting device (30) is coupled to a control system (20) of the turbo engine (100) as a redundant electric energy supply and / or the at least one kinetic energy converter (40) providing a means for reducing the vibrational energy of the turbo engine (100). The invention also relates to an energy harvesting device and a method for energy harvesting.
Turbo engine with an energy harvesting device, energy harvesting device and a method for energy harvesting
Turbomaschine mit Energiegewinnungsvorrichtung, Energiegewinnungsvorrichtung und Verfahren zur Energiegewinnung
Turbomachine avec dispositif de récupération d'énergie, dispositif de récupération d'énergie et procédé de récupération d'énergie
2015-05-06
Patent
Electronic Resource
English
British Library Online Contents | 2012
British Library Online Contents | 2012