The invention provides an aircraft with lift force and buoyancy, which relates to technologiesof engineering such as aviation, photovoltaics,air consignment, air communication monitoring, sports and the like. The aircraft comprises a wing body (2), an aircraft body (3), a taking body or taking cabin body (4), a propulsion system (5), a control system (6) and other sub bodies; the aircraft is characterized by further comprising a buoyancy gas (1) and a photovoltaic power generation system (10); the density of the buoyancy gas (1) is lower than that of the air; at least one of the wing body (2), the aircraft body (3) and the taking body or taking cabin body (4) comprises the buoyancy gas (1) and the photovoltaic power generation system (10). The aircraft with the lift force and the buoyancy, provided by the invention, is advantaged in that the aircraft is provided with both single buoyancy of the wing body (2) and double buoyancy of the wing body (2) and the aircraft body (3) so that the dead-weight and flight energy consumption of the aircraft are greatly reduced; and without consuming fuels, flight as well as vertical take-off and landing can be carried out with no time limit by using solar energy. Even though the aircraft suffers accidents such as collision, stopping, abrupt meteorological change and the like in the air, injuries of personnel, crashing of the cabin and damages of the aircraft cannot occur and the craft is very safe under effects of the buoyancy, the flexible wing body (2) and the aircraft body (3). The manufacturing cost of the aircraft with the lift force and the buoyancy, provided by the invention, is extremely low.
Aircraft with lift force and buoyancy
2015-10-28
Patent
Electronic Resource
English