An aircraft includes a fuselage extending in a front-rear direction of the aircraft, main wings extending from sides of the fuselage, a fuel cell system located adjacent to a rear of the fuselage with respect to the main wings and configured to apply driving force to a nacelle located on each of the main wings, and a controller configured to transmit electrical energy applied from the fuel cell system to the nacelle. A center of gravity of the aircraft is located in the fuselage close to front ends of the main wings, and a flow rate of air flowing into the fuel cell system is controlled in response to an outside air condition of the aircraft.
AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM AND THRUST CONTROL METHOD
2024-01-25
Patent
Electronic Resource
English
System for controlling braking of aircraft equipped with thrust reversal system
European Patent Office | 2021
|European Patent Office | 2020
|