A floating moving device includes a first rotation unit, a second rotation unit, a third rotation unit, a fourth rotation unit, and a fifth rotation unit. A fourth adjustment unit adjusts a direction of a fourth impeller such that a rotation axis of the fourth impeller is parallel to at least an up-down direction at a takeoff time. A fifth adjustment unit adjusts a direction of a fifth impeller such that a rotation axis of the fifth impeller is parallel to the up-down direction at the takeoff time. A first adjustment unit adjusts a position of a first wheel such that the first wheel comes into contact with the ground until the takeoff is performed. A second adjustment unit adjusts a position of a second wheel such that the second wheel comes into contact with the ground until the takeoff is performed.

A floating moving device includes a first rotation unit, a second rotation unit, a third rotation unit, a fourth rotation unit, and a fifth rotation unit. A fourth adjustment unit adjusts a direction of a fourth impeller such that a rotation axis of the fourth impeller is parallel to at least an up-down direction at a takeoff time. A fifth adjustment unit adjusts a direction of a fifth impeller such that a rotation axis of the fifth impeller is parallel to the up-down direction at the takeoff time. A first adjustment unit adjusts a position of a first wheel such that the first wheel comes into contact with the ground until the takeoff is performed. A second adjustment unit adjusts a position of a second wheel such that the second wheel comes into contact with the ground until the takeoff is performed.

The present invention relates to a glide bomb and methods of use thereof for use with an unmanned or manned aerial vehicle or for operative deployment. In one form, the glide bomb is configured to be carried and released by an unmanned aerial vehicle (“UAV”) for flight towards a selected target. The glide bomb includes an elongate body having a nose and an opposed tail aligned along a longitudinal axis; a payload; a pair of wings extendable from opposed sides of the body for producing lift, said wings configured to be selectively moveable between a retracted position and an extended position; and two or more tail control surfaces operatively associated with the tail of the body for at least pitch and yaw control.

An aircraft wing having a fixed wing and a wing tip device at the tip of the fixed wing is disclosed. The wing tip device being movable relative to the fixed wing between flight and ground configurations, the aircraft wing having a locking mechanism including a locking bore and a locking pin, the locking mechanism being configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing, and wherein the locking pin is configured such that it has a replaceable tip.

An aircraft wing having a fixed wing and a wing tip device at the tip of the fixed wing is disclosed. The wing tip device being movable relative to the fixed wing between flight and ground configurations, the aircraft wing having a locking mechanism including a locking bore and a locking pin, the locking mechanism being configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing, and wherein the locking pin is configured such that it has a replaceable tip.

A foldable aerial vehicle may take the form of a flying wing. The flying wing includes port and starboard wings having port and starboard root and tip portions. The port and starboard root and tip portions are hinged one to another so that the span axes of all of the root and tip portions are parallel in the stowed condition and so that the tip portions are separated by the root portions in the deployed condition to define the flying wing. The wings are not symmetrical about the longitudinal axis of the vehicle, with the span axes of the root and tip portions being stepped from one wing tip to the other. Folding winglets are disposed on opposing wing tips, with the higher winglet extending in an upward direction and the lower winglet extending in the downward direction.

A foldable aerial vehicle may take the form of a flying wing. The flying wing includes port and starboard wings having port and starboard root and tip portions. The port and starboard root and tip portions are hinged one to another so that the span axes of all of the root and tip portions are parallel in the stowed condition and so that the tip portions are separated by the root portions in the deployed condition to define the flying wing. The wings are not symmetrical about the longitudinal axis of the vehicle, with the span axes of the root and tip portions being stepped from one wing tip to the other. Folding winglets are disposed on opposing wing tips, with the higher winglet extending in an upward direction and the lower winglet extending in the downward direction.

Foldable aircraft wings are disclosed. An example aircraft includes a foldable wing having a fixed wing portion, a foldable wing portion and a hinge to pivotally couple the foldable wing portion relative to the fixed wing portion. The hinge includes a wing transition portion including wing hinge ribs and wing stub ribs, respective ones of the wing hinge ribs coupled to corresponding respective ones of the wing stub ribs. The hinge also includes a tip transition portion including tip hinge ribs, where respective ends of the tip hinge ribs positioned between corresponding respective ones of the wing hinge ribs and the wing stub ribs.

Foldable aircraft wings are disclosed. An example aircraft includes a foldable wing having a fixed wing portion, a foldable wing portion and a hinge to pivotally couple the foldable wing portion relative to the fixed wing portion. The hinge includes a wing transition portion including wing hinge ribs and wing stub ribs, respective ones of the wing hinge ribs coupled to corresponding respective ones of the wing stub ribs. The hinge also includes a tip transition portion including tip hinge ribs, where respective ends of the tip hinge ribs positioned between corresponding respective ones of the wing hinge ribs and the wing stub ribs.

An adjustable foil having a suction surface and a pressure surface. The foil comprises an adjustable internal frame comprising a base, a plurality of articulately connected sections forming the suction surface of the foil, arranged consecutively from the leading edge of the foil to the trailing edge of the foil, and a plurality of frame struts, each articulately connected to the base and to a section of the plurality of sections. The foil is movable from a collapsed configuration to an expanded configuration by rotating the frame struts with respect to the base.