The present invention relates to an aircraft having at least one wing, on which at least one propulsion unit is arranged, comprising at least one heat engine, especially a gas turbine, as well as an exhaust gas passage for conducting exhaust gas of the heat engine into and inside the wing.
LUFTFAHRZEUG MIT WÄRMEKRAFTMASCHINE UND EINRICHTUNG ZUR NUTZUNG DES ABGASES DER WÄRMEKRAFTMASCHINE
AIRCRAFT HAVING A HEAT ENGINE AND DEVICE FOR USING THE EXHAUST GASES FROM THE HEAT ENGINE
AÉRONEF COMPRENANT UN MOTEUR THERMIQUE ET DISPOSITIF POUR UTILISER LES GAZ D'ÉCHAPPEMENT DU MOTEUR THERMIQUE
2022-01-19
Patent
Electronic Resource
German
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
LUFTFAHRZEUG MIT WÄRMEKRAFTMASCHINE UND EINRICHTUNG ZUR NUTZUNG DES ABGASES DER WÄRMEKRAFTMASCHINE
European Patent Office | 2020
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