B63B2021/504

Fairing and Method
20190203852 · 2019-07-04 ·

A fairing device and method for the reduction of vortex-induced vibrations or motions, the minimization of drag about a substantially cylindrical element immersed in a fluid medium, comprising; a fairing rotatably mounted about the cylindrical element, the fairing comprising a shell with a mainly cylindrical cross-sectional shape with an outer diameter (D) following the outer diameter of the cylindrical element from an upward stagnation point of 0 degrees to at least 90 degrees, and which at 90 degrees continues as two fin-like portions in an aft direction, further comprising that the fin-like portions are convexly curved aft of 90 degrees thus tapering towards each other and defining a tail end opening or gap less than the fairing standoff height. A method for mounting, storage, and deployment of the fairing device is also disclosed.

Flow modification device, system, and method

A flow modification device connectable to a generally cylindrical element adapted for immersion in a fluid medium, the device comprising an elongate body having a length and a generally circular cross-section; a plurality of raised body portions disposed about and extending along the length of the elongate body, the raised body portions being arranged generally parallel to a longitudinal axis of the body and having a height between 2% and 10% of a diameter of the body; and an aperture extending through the length of the elongate body, the aperture being adapted to receive the generally cylindrical element such that the flow modification device is arranged about the cylindrical element. The plurality of raised body portions are adapted to reduce vortex-induced vibration and/or drag on the cylindrical element when the device is connected to the cylindrical element and the connected device and cylindrical element are immersed in the fluid medium and there is relative movement between the connected device and cylindrical element and the fluid medium.

Fairing and method
10274107 · 2019-04-30 · ·

A fairing device for the reduction of vortex-induced vibrations or motions, and for minimizing the drag about a substantially cylindrical element immersed in a fluid medium, comprising; a fairing rotatably mounted about the cylindrical element, the fairing comprising a shell with a mainly cylindrical cross-sectional shape with an outer diameter (D) following the outer diameter of the cylindrical element from an upward stagnation point of 0 degrees to at least +/90 degrees, and which at +/90 degrees continues as two fin-like portions in an aft direction, whereby the fin-like portions are convexly curved aft of +/90 degrees thus tapering towards each other and are defining a tail end opening or gap less than the fairing standoff height. A method for mounting, storage, and deployment of the fairing device is also disclosed.

Minimizing movements of offshore wind turbines
12128995 · 2024-10-29 · ·

Techniques are disclosed herein for minimizing movement of an offshore wind turbine. Using the technologies described, a wind turbine may be mounted on a marine platform that is constructed and deployed to reduce environmental loads (e.g., wind, waves, . . . ) on the platform in both shallow and deep water. In some configurations, a fully restrained platform (FRP) is configured to support a wind turbine. According to some examples, moorings are attached to the FRP and/or the structure of the wind turbine structure to reduce movement in six degrees of freedom.

A CYLINDRICAL ELEMENT ADAPTED TO REDUCE VORTEX-INDUCED VIBRATION AND/OR DRAG

A generally cylindrical element adapted for immersion in a fluid medium, the cylindrical element comprising an elongate body having a length and a generally circular cross-section, and a plurality of raised body portions disposed about and extending along the length of the elongate body, the raised body portions being arranged generally parallel to a longitudinal axis of the body and having a height between 2% and 10% of a diameter of the body. The plurality of raised body portions are adapted to reduce vortex-induced vibration and/or drag on the cylindrical element when the cylindrical element is immersed in the fluid medium and there is relative movement between the cylindrical element and the fluid medium.

FLOW MODIFICATION DEVICE, SYSTEM, AND METHOD

A flow modification device connectable to a generally cylindrical element adapted for immersion in a fluid medium, the device comprising an elongate body having a length and a generally circular cross-section; a plurality of raised body portions disposed about and extending along the length of the elongate body, the raised body portions being arranged generally parallel to a longitudinal axis of the body and having a height between 2% and 10% of a diameter of the body; and an aperture extending through the length of the elongate body, the aperture being adapted to receive the generally cylindrical element such that the flow modification device is arranged about the cylindrical element. The plurality of raised body portions are adapted to reduce vortex-induced vibration and/or drag on the cylindrical element when the device is connected to the cylindrical element and the connected device and cylindrical element are immersed in the fluid medium and there is relative movement between the connected device and cylindrical element and the fluid medium.

TWIN-FIN FAIRING
20180135666 · 2018-05-17 ·

A fairing (1) for improving fluid flow around a circular-cylindrical object comprises a first fairing-element (11) and a second fairing-element (12), which are releasable relative to one another. The fairing-elements are easy to manufacture, compactly stackable, and easy to install around the object. In installed condition, the first fairing-element and the second fairing-element are mutually connected in circumferential direction of the fairing, while forming a twin-fin fairing, which reduces vortex-induced vibrations around the object, while providing favourable flow resistance, and without performing galloping motions.

MINIMIZING MOVEMENTS OF OFFSHORE WIND TURBINES
20250010957 · 2025-01-09 ·

Techniques are disclosed herein for minimizing movement of an offshore wind turbine. Using the technologies described, a wind turbine may be mounted on a marine platform that is constructed and deployed to reduce environmental loads (e.g., wind, waves, . . . ) on the platform in both shallow and deep water. In some configurations, a fully restrained platform (FRP) is configured to support a wind turbine. According to some examples, moorings are attached to the FRP and/or the structure of the wind turbine structure to reduce movement in six degrees of freedom.

Two-piece U-shaped fairing

A vortex-induced vibration (VIV) suppression device including a fairing comprising a fairing body having a nose dimensioned to partially encircle an underlying tubular and a first arm and a second arm extending from the nose, wherein the nose, the first arm and the second arm are one integrally formed unit and the first arm and the second arm are spaced a distance from one another along their entire length so as to define a gap therebetween; and a securing element dimensioned to fit within the gap between the first arm and the second arm and secure the fairing to an underlying tubular. Methods for securing a U-shaped fairing to a tubular and manufacturing a U-shaped fairing are also disclosed.

Fairing having an offset opening

A fairing having a fairing body having a nose dimensioned to partially encircle an underlying tubular and having a fairing body axis; a stand-off region extending radially outward from the nose, wherein the stand-off region comprises a first side wall extending from one side of the nose and a second side wall extending from another side of the nose and toward the first side wall; a tail flange extending radially outward from the stand-off region, the tail flange having a substantially planar member comprising a first portion adjacent the stand-off region and a second portion radially outward to the first portion; and an opening formed within one of the nose or the stand-off region, wherein the opening is parallel to the fairing body axis and the opening is modifiable between an open configuration and a closed configuration.