The invention relates to a propulsion system (150) comprising an electric motor (108) whose output drives a propeller (110), and a reversible fuel cell (250) comprising a cathode and an anode connected to the electric motor (108), a supply line (256) conne...

The method involves determining a pitch angle limiting value representative of a maximum admissible angle of incidence, depends on a set of flight parameters and aircraft configurations. A maximum angle of incidence pointer (33) indicating pitch angle limi...

The seat consists of a back (2) with a headrest (4) and a base in two sections (12, 14). The rear section (14) of the seat base is able to move between an upper and a lower position, and the front section (12) is attached to it by connecting bars (26, 28)....

The luggage locker consists of a hinged box (12) inside a housing (14) under the lifting base (2) of a seat. The box pivots about a horizontal axis (6), adopting an inclined position inside the housing while the luggage (26) is inserted or removed and lyin...