Patent ID: 11912435
Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 5:
6. The composite air vehicle system according to claim 1, including one of the following:
wherein each one of first air vehicle and the second air vehicle comprises a propulsion system configured for enabling the respective said first air vehicle or said second air vehicle to be independently operated under powered flight;
wherein each one of first air vehicle and the second air vehicle comprises a propulsion system configured for enabling the respective said first air vehicle or said second air vehicle to be independently operated under powered flight, and, wherein said propulsion system comprises a powered rotary drive coupled to at least one propeller;
wherein each one of first air vehicle and the second air vehicle comprises a propulsion system configured for enabling the respective said first air vehicle or said second air vehicle to be independently operated under powered flight, and, wherein said propulsion system comprises a powered rotary drive coupled to at least one propeller, and, wherein said at least one propeller is at least one of: at least one puller propeller; at least one pusher propeller; or
wherein each one of first air vehicle and the second air vehicle comprises a propulsion system configured for enabling the respective said first air vehicle or said second air vehicle to be independently operated under powered flight, and, wherein said propulsion system comprises a powered rotary drive coupled to at least one propeller, and, wherein said at least one propeller is at least one of at least one puller propeller and at least one pusher propeller, and, wherein said powered rotary drive includes at least one electric motor for providing torque to the propeller, or, wherein said powered rotary drive includes at least one fuel powered combustion engine for providing torque to the propeller.