A vertical takeoff and flying at a constant altitude are performed using an aircraft. The aircraft includes a fuselage, a left arm (attached to the fuselage), a right arm (attached to the fuselage), a left float (attached to the left arm), a right float (attached to the right arm), and a plurality of rotors. The plurality of rotors includes a left inner rotor and a right inner rotor (attached at a fixed angle to a top surface of the left float and the right float, respectively) and a left outer rotor and a right outer rotor (attached at a fixed angle to a top surface of the distal end of the left arm and the right arm, respectively).

A vertical takeoff and flying at a constant altitude are performed using an aircraft. The aircraft includes a fuselage, a left arm (attached to the fuselage), a right arm (attached to the fuselage), a left float (attached to the left arm), a right float (attached to the right arm), and a plurality of rotors. The plurality of rotors includes a left inner rotor and a right inner rotor (attached at a fixed angle to a top surface of the left float and the right float, respectively) and a left outer rotor and a right outer rotor (attached at a fixed angle to a top surface of the distal end of the left arm and the right arm, respectively).

A retrofittable float with an underwater camera attachment for unmanned aerial vehicles allows an unmanned aerial vehicle (UAV) to traverse over a body of water while recording images and/or video of the underwater environment. The retrofittable float with an underwater camera attachment includes a flotation device, a plurality of mounting brackets, an underwater scope, and at least one underwater illumination light. The flotation device attaches to the UAV via the plurality of mounting brackets. The plurality of mounting brackets is configured to align the center of gravity of the UAV with the center of buoyancy of the flotation device, thereby reducing the risk of capsizing. Once securely mounted, the camera of the UAV is positioned pointing into the underwater scope. The underwater scope allows the camera to record images and/or videos of the underwater environment. Finally, the at least one underwater illumination light is used to increase visibility.

A retrofittable float with an underwater camera attachment for unmanned aerial vehicles allows an unmanned aerial vehicle (UAV) to traverse over a body of water while recording images and/or video of the underwater environment. The retrofittable float with an underwater camera attachment includes a flotation device, a plurality of mounting brackets, an underwater scope, and at least one underwater illumination light. The flotation device attaches to the UAV via the plurality of mounting brackets. The plurality of mounting brackets is configured to align the center of gravity of the UAV with the center of buoyancy of the flotation device, thereby reducing the risk of capsizing. Once securely mounted, the camera of the UAV is positioned pointing into the underwater scope. The underwater scope allows the camera to record images and/or videos of the underwater environment. Finally, the at least one underwater illumination light is used to increase visibility.

An aircraft which includes a float-wing having a leading edge, a trailing edge, and an airfoil shape to produce aerodynamic lift when the float-wing flows through air at a lift-producing angle of attack in a forward flight mode of operation. The float-wing further includes a submersible portion that includes at least the trailing edge and which is constructed of materials and in a shape selected to produce a buoyancy force sufficient to prevent at least a non-submersible portion of the aircraft from being submersed under conditions in which the aircraft is in a waterborne non-flight position in which at least the trailing edge of the float-wing is submersed but at least the non-submersible portion of the aircraft is not submersed.

The invention relates to a propulsion device comprising a platform that is arranged so as to accommodate a passenger and cooperates with a thrust unit comprising a main nozzle, advantageously oriented from the bow to the stern of the device, and two secondary nozzles that are lateral and are positioned essentially at the bow of the propulsion device. The secondary nozzles are mounted so as to be mobile about a transverse axis so as to be moved by actuators controlled by a processing unit that implements a method for controlling the secondary nozzles, thus providing automatic control assistance to the passenger.

The invention relates to a propulsion device comprising a platform that is arranged so as to accommodate a passenger and cooperates with a thrust unit comprising a main nozzle, advantageously oriented from the bow to the stern of the device, and two secondary nozzles that are lateral and are positioned essentially at the bow of the propulsion device. The secondary nozzles are mounted so as to be mobile about a transverse axis so as to be moved by actuators controlled by a processing unit that implements a method for controlling the secondary nozzles, thus providing automatic control assistance to the passenger.

An aircraft having a longitudinal axis determining a fore-aft direction, comprising at least two floats configured to support the aircraft on a ground medium located below the floats with a ground-facing side of the floats, wherein each float comprises: a first support wheel and a second support wheel, the first support wheel being located within the float further in the fore direction than the second support wheel, wherein at least the first support wheel is located within the float so that it protrudes partly out of the ground-facing side of the float; wherein the first support wheel protrudes out of the ground-facing side of the float so that an angle between a first line z1 tangential to a float profile line, intersecting the float profile line in front of the first support wheel on the ground-facing side, which has the smallest angle with respect to the horizontal axis of the float, and which intersects the profile line within a circle C concentric with the first support wheel and of a radius 2R being two times larger than a radius R of the first support wheel, the first line z1 intersecting the circumference of the first support wheel in point B, and a second line z2 tangential to the circumference of the first support wheel point B, wherein the first line z1 and the second line z2 are comprised within the same, vertical plane, which is parallel to the fore-aft direction, is comprised in a range 145-175.

A flying machine frame structural body including: a frame that surrounds a flying machine body including a rotating blade, and to which the flying machine body is fixed; and plural wheels that are rotatably supported by the frame.

A flying machine frame structural body including: a frame that surrounds a flying machine body including a rotating blade, and to which the flying machine body is fixed; and plural wheels that are rotatably supported by the frame.