The present disclosure relates to a fuel cell system and an aircraft equipped with a fuel cell system. The aircraft may have a fuselage elongated in a front-rear direction, a front horizontal stabilizer towards a front of the fuselage, main wings extending to opposite sides of the fuselage, a rear horizontal stabilizer towards a rear of the fuselage, the fuel cell system rear to the main wings and a controller. The fuel cell system may be configured to provide electrical energy for driving a motor on each of the main wings. The controller may be configured to cause transmission of electrical energy from the fuel cell system to the motor. A center of gravity of the aircraft may be near front edges of the main wings. A flow rate of air into the fuel cell system may be controlled in response to an outside air condition.
AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM
2024-01-25
Patent
Electronic Resource
English
AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM AND THRUST CONTROL METHOD
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