B64C31/06

WIND ENERGY PARK WITH AIRBORNE WIND ENERGY SYSTEMS AND A DIRECT CURRENT (DC) INTERNAL GRID

The present invention relates to wind energy park connected to an electrical grid, having airborne wind energy systems (AWES), e.g. with kites. The wind energy park has an electrical DC network connecting the plurality of AWES and a grid converter unit for converting DC to AC, and transmit AC to the electrical grid. The wind energy park control unit controls the AWES to produce electrical power to the electrical grid by alternating between a power production phase, and a recovery phase so to balance the supply of power to the electrical grid according a demanded setpoint. An advantage is that the grid converter may be smaller, as compared to an AC network, because the power is evened out with the negative power from the AWES being in recovery phase. In this way, the invention stabilizes the grid and has a grid forming capability.

Kite control bar with integrated back trim line tensioning means
11059578 · 2021-07-13 · ·

A kite control bar having a tensioning member anchored to the bar end float and secured to the trim line. The tensioning member is capable of expanding and contracting. The tensioning member has a default state which is either an expanded state or a contracted state. When an adjusting force is exerted upon the trim line, the tensioning member is drawn into another of the expanded state or the contracted state. When the adjusting force is released, the tensioning member tends to return to the default state. This biases the trim line to force excess trim line out of the bar end float.

Invertible aircraft

A rotorcraft including a fuselage, one or more motor-driven rotors for vertical flight, and a control system. The motors drive the one or more rotors in either of two directions of rotation to provide for flight in either an upright or an inverted orientation. An orientation sensor is used to control the primary direction of thrust, and operational instructions and gathered information are automatically adapted based on the orientation of the fuselage with respect to gravity. The rotors are configured with blades that invert to conform to the direction of rotation.

CONTROL DEVICE FOR CONTROLLING A KITE STEERING ARRANGEMENT
20200377229 · 2020-12-03 ·

A control device for controlling a kite steering arrangement, including a base, a control bar support extending downward on the base, a control bar pivot point mounted displaceably about the control bar support, a pair of interconnecting members extending between opposing end regions of the control bar and the base upper the control bar support, a tensioning mechanism, a base pivot point, a base rotator for allowing rotation of the base about a vertical axis thereof, a manipulator that manipulates the base pivot point and base rotator, and a communicator, that communicates adjustment of the interconnecting members to the kite steering arrangement. The length aspect of the interconnecting members is adjusted by pivoting the control bar about the control bar pivot point and/or by displacement of the control bar pivot point relative the control bar support.

CONTROL DEVICE FOR CONTROLLING A KITE STEERING ARRANGEMENT
20200377229 · 2020-12-03 ·

A control device for controlling a kite steering arrangement, including a base, a control bar support extending downward on the base, a control bar pivot point mounted displaceably about the control bar support, a pair of interconnecting members extending between opposing end regions of the control bar and the base upper the control bar support, a tensioning mechanism, a base pivot point, a base rotator for allowing rotation of the base about a vertical axis thereof, a manipulator that manipulates the base pivot point and base rotator, and a communicator, that communicates adjustment of the interconnecting members to the kite steering arrangement. The length aspect of the interconnecting members is adjusted by pivoting the control bar about the control bar pivot point and/or by displacement of the control bar pivot point relative the control bar support.

Wind harvesting systems and methods

Various embodiments of the present disclosure provide wind harvesting systems and methods using crosswind power kites and methods for launching crosswind power kites into wing-borne flight, for generating electricity through such flights, and for landing or retrieving such crosswind power kites.

Wind harvesting systems and methods

Various embodiments of the present disclosure provide wind harvesting systems and methods using crosswind power kites and methods for launching crosswind power kites into wing-borne flight, for generating electricity through such flights, and for landing or retrieving such crosswind power kites.

Kite leading edge and sports kite
10843097 · 2020-11-24 · ·

A kite leading edge has a tubular structure having a first curve in a span-wise direction and a second curve a chord-wise direction. The tubular structure is formed by a plurality of panels joined together at seams including at least a first longitudinal seam running in the span-wise direction of the tubular structure. At least a portion of the first longitudinal seam defines a first partial helical path about the circumference of the tubular structure.

Kite leading edge and sports kite
10843097 · 2020-11-24 · ·

A kite leading edge has a tubular structure having a first curve in a span-wise direction and a second curve a chord-wise direction. The tubular structure is formed by a plurality of panels joined together at seams including at least a first longitudinal seam running in the span-wise direction of the tubular structure. At least a portion of the first longitudinal seam defines a first partial helical path about the circumference of the tubular structure.

A METHOD FOR CONTROLLING AN AIRBORNE OBJECT COUPLED TO A WIND TURBINE
20200362814 · 2020-11-19 ·

A method of controlling an airborne object (2), such as a kite or a glider, is disclosed. The airborne object (2) may be an airborne energy generating system. The airborne object (2) is coupled to a part of a wind turbine (1), such as a nacelle (4), a tower (3) or a foundation, via a cable (7). At least one parameter related to movements (8) of the tower (3) of the wind turbine (1) is measured, and a cable force (9) of the cable (7) acting on the wind turbine (1) is adjusted, based on the at least one measured parameter. Thereby the tower movements (8) can be counteracted and fatigue can be reduced.