Patent ID: 11958619
Assignee: RPS AEROSPACE S.R.L.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 0:
1. A remote piloted aircraft comprising a primary propulsion unit with at least one engine to put in rotation a plurality of propellers and a main control unit comprising at least one receiver to receive commands from a remote control unit,
wherein the aircraft has a secondary flight assembly to intervene in case of failure or emergency of the aircraft,
wherein the secondary flight assembly is provided with an additional control unit to process data relevant to the flight and which includes an additional receiver to receive commands from a further remote control unit,
wherein in case of failure or emergency, the additional control unit will generate, as a response to failure or emergency, an activation command to activate a first device for the expulsion of an upper wing placed in a first compartment of the aircraft and to inflate a lower wing housed in a second compartment of the aircraft, and also to generate an interdiction command of the primary propulsion unit,
wherein the lower wing is inflated by compressed fluid contained in a tank of the aircraft,
wherein the upper wing is maneuverable by the further remote control unit,
wherein the lower wing is shaped to cooperate with the upper wing for the stability of the flight of the aircraft,
wherein the lower wing when inflated is positioned underneath the aircraft.