Generally, an inventive aircraft (1) having at least a first lift body (2) and a second lift body (3) each controllably configurable to correspondingly generate an amount of lift (4) sufficient to remain aloft at a first elevation (5) and a second elevation (6) a sufficient distance apart (7) to subject the first lift body (2) and the second lift body (3) to sufficiently disparate fluid flow characteristics (8) to propel the aircraft (1).
Aircraft lift and propulsion from disparate air flows
2019-06-25
Patent
Electronic Resource
English