The invention relates to a novel anti-falling airplane and an anti-falling control method. The novel anti-falling airplane comprises a machine body and a machine base which are connected through a movable buckle. The machine body comprises a flight deck, a passenger cabin and a tail wing. The machine base comprises a warehouse, a fuel tank, a landing gear, a power device and wings. The tail wing is connected to the tail end of the machine body through movable buckles. A propeller anti-falling system driving the machine body to take off is arranged on the top of the passenger cabin. An anti-falling backlash device is arranged at the bottom of the passenger cabin. The novel anti-falling airplane further comprises a control system arranged in the flight deck. When the airplane comes across the accident in air, the control system unlocks the movable buckles to throw the machine base and the tail wing away and controls the propeller anti-falling system and the anti-falling backlash device to run to enable the machine body to safely land. According to the novel anti-falling device, it can be guaranteed that the airplane can safely land when the serious accident happens, and broad application prospects are achieved.
Novel anti-falling airplane and anti-falling control method
02.12.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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