A seal system for a gas turbine engine includes a ceramic matrix composite (CMC) seal arc segment and a carrier supporting the CMC seal arc segment. The CMC seal arc segment defines radially inner and outer sides and has an abradable layer disposed on the radially outer side. There is a cooling cavity radially between the carrier and the abradable layer. The carrier includes a ridge that projects into a groove in the abradable layer and provides a labyrinth seal that partitions the cooling cavity into sub-cavities.

A method for producing a split rotor blade, a method for connecting a split rotor blade, a rotor blade, a rotor blade segment, a rotor, a wind power plant, and a production device for producing rotor blades. A method for producing a split rotor blade, comprising: providing a rotor blade having a spar cap and an extension in the longitudinal direction from a blade root region to a blade tip; making at least one groove in the spar cap, the groove being arranged in a first connection region of the rotor blade, and a portion of the main extension direction of the groove being oriented parallel to the longitudinal direction; splitting the rotor blade, in the first connection region, into a rotor blade section facing the blade root and a rotor blade section facing away from the blade root, a first groove section being arranged in the rotor blade section facing the blade root and a second groove section being arranged in the rotor blade section facing away from the blade root.

An enclosure structure, and an aerodynamic configuration adjuster arranged on an outer surface of same are provided. The aerodynamic configuration adjuster is of a grid structure capable of surrounding the enclosure structure, and the grid structure comprises a plurality of grid cells, at least some of grid cells have bevel edges, and the attack angle of a fluid is changed when the fluid passes over the bevel edges. The aerodynamic configuration adjuster changes the aerodynamic configuration of the fluid, and thus the resistance coefficient becomes smaller such that a pressure differential between the pressures at a incident flow surface and a back surface of the enclosure structure is reduced, thereby reducing a forward resistance; and in addition, due to a smaller resistance coefficient, the amplitude of a transverse vortex-induced resonance can also be reduced, thereby reducing vibration.

A Vortex-shedding-arrangement, which is prepared to be arranged on a tower of a wind turbine, is provided. Embodiments of the invention even relate to a tower, which is equipped with the Vortex-shedding-arrangement and to a method to equip the tower with the Vortex-shedding-arrangement. The Vortex-shedding-arrangement according to embodiments of the invention is arranged and prepared to be connected to a surface of a tower. The Vortex-shedding-arrangement is prepared to reduce Vortex-induced-vibrations, acting on the tower and its structure, during the tower-transportation. The vortex shedding arrangement comprises vortex shedding elements and at least one shrink foil. The at least one shrink foil is prepared to fix and to position the vortex shedding elements at specific positions at the tower surface by heat applied to the shrink foil.

A rotor blade assembly for a wind turbine. The rotor blade assembly includes a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a blade tip and a blade root. The rotor blade assembly also includes at least one noise reducer secured at the trailing edge. The noise reducer(s) includes at least one serration having a base portion and at least one side edge feature extending from the base portion. Further, the base portion extends along a first plane. The side edge feature(s) extends out of the first plane so as to reduce vortices generated by the serration(s).

A wind tunnel system increasing wind flow into and out of a wind turbine is presented. T the wind tunnel system has a wind turbine. The wind turbine converts kinetic energy from wind to electrical energy. The wind tunnel system has a wind inception system that has a netting, a pole and a skin. The wind inception center is useful for increasing wind to the wind turbine. The wind tunnel system further has a wind disperser. The wind disperser receives outputted wind from the wind turbine and disperses the received outputted wind from the wind turbine.

The present disclosure is directed to a rotor blade that includes a shell defining an interior cavity. The rotor blade also includes exterior surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge. Each of the pressure side, the suction side, the leading edge, and the trailing edge extends between a tip and a root. The shell defines a span and a chord. A shear web is positioned in the interior cavity and coupled to the shell. The shear web includes a lattice structure.

A hydroelectric power plant for a water stream includes an electromechanical converter and a turbine driving the converter. The turbine includes two vertical supports parallel to the flow and, between the supports, driving blades moved by the hydrodynamic lift forces, connected at each end to a drive component. The turbine further includes wheels driven by the drive component and assembled on the supports. The hydroelectric power plant includes at least first, second, and third travel areas where each drive component extends rectilinearly, the leading edges of the blades being arranged horizontally plus or minus 5 at least in the first and second travel areas. Each support includes guides and each blade includes elements abutting against the guides.

In an embodiment, a molding apparatus for a turbine blade includes first and second mold compartments defining a mold cavity when in a closed position, at least one of the first and second mold compartments including a micro-structured surface facing an interior of the mold cavity. The micro-structured surface includes an array of V-shaped channels, and the V-shaped channels have a maximum height of 200 micrometers. A turbine blade including integral micro-structured riblets and method for making the turbine blade is also provided.

A Vortex-shedding-arrangement, which is prepared to be arranged on a tower of a wind turbine, is provided. Embodiments of the invention even relate to a tower, which is equipped with the Vortex-shedding-arrangement and to a method to equip the tower with the Vortex-shedding-arrangement.

The Vortex-shedding-arrangement according to embodiments of the invention is arranged and prepared to be connected to a surface of a tower. The Vortex-shedding-arrangement is prepared to reduce Vortex-induced-vibrations, acting on the tower and its structure, during the tower-transportation. The vortex shedding arrangement comprises vortex shedding elements and at least one shrink foil. The at least one shrink foil is prepared to fix and to position the vortex shedding elements at specific positions at the tower surface by heat applied to the shrink foil.