公开(公告)号：US12090723B2

公开(公告)日：2024-09-17

申请号：US18039942

申请日：2021-12-20

申请人： LM WIND POWER A/S

发明人： Jelmer Cnossen ,  Paul Todd

IPC分类号： B29D99/00 ,  F03D1/06 ,  F03D80/00

CPC分类号： B29D99/0028 ,  F03D1/0675 ,  F03D1/069 ,  F03D80/005 ,  F05B2240/3042 ,  F05B2260/96

摘要： A method for manufacturing a shell 36 and 38, is disclosed. The method includes laying one or more layers of fibres, on a surface of a mould 9 to form at least a portion of a shell half structure 36 and 38. A first panel 11 defined with noise reduction members 11a is positioned adjacent to the one or more layers of fibres on the surface of the mould 9. Further, resin is infused through the one or more layers of fiber and the first panel 11 and is subsequently cured to obtain the shell half structure 36 or 38, where the first panel 11 with noise reduction members 11a adheres to the shell half structure 36 and 38 upon curing the infused resin.

公开(公告)号：US12060863B2

公开(公告)日：2024-08-13

申请号：US18225536

申请日：2023-07-24

申请人： NEWTECH GROUP CO., LTD.

发明人： Kunlun Tan ,  Yelin Liu ,  Gaoyu Bai ,  Qiuping Du ,  Lei Cao ,  Juncheng Chen

IPC分类号： F03D1/06 ,  B29C65/48

CPC分类号： F03D1/0682 ,  F03D1/0675 ,  F03D1/0684 ,  B29C65/48 ,  F03D1/069 ,  F05B2240/302

摘要： A chordwise segment connection structure for wind turbine blades includes: a blade body including a pressure side and a suction side; a leading edge shell and a trailing edge shell formed by the skin of the pressure side and the suction side along the chord length of the blade, the pressure side and the suction side being each provided with a spar cap; and a shear web provided in a cavity of the blade body and extending between the pressure side and the suction side to support the spar cap; wherein the spar caps on the pressure side and the suction side are bonded and fixed to a skin structure where the leading edge shell and the trailing edge shell are spliced, so that the leading edge shell and the trailing edge shell are spliced with the spar caps to form the profile of the wind turbine blade.

公开(公告)号：US20240200530A1

公开(公告)日：2024-06-20

申请号：US18544040

申请日：2023-12-18

申请人： Wobben Properties GmbH

发明人： Dimitrios Bekiropoulos ,  Christoph Scheit ,  Jochen Stemberg

IPC分类号： F03D1/06

CPC分类号： F03D1/069 ,  F05B2230/23 ,  F05B2230/60 ,  F05B2240/301 ,  F05B2240/3042 ,  F05B2250/12 ,  F05B2260/96

摘要： Some embodiments relate to a rotor blade of a wind turbine, a wind turbine having a rotor blade and a method for optimizing a rotor blade. Some embodiments relate to a rotor blade of a wind turbine, wherein the rotor blade has a leading edge, a trailing edge, a suction side and a pressure side, and extends in a longitudinal direction of a rotor blade between a root end and a tip end, wherein a direct connection between the leading edge and the trailing edge is termed the chord line and the length thereof is termed the chord length, wherein the rotor blade has at least one airfoil element, wherein the at least one airfoil element is arranged at the trailing edge with a proximal portion adjoining a trailing edge region and projects from the trailing edge with a distal portion having a projecting direction, which is oriented substantially parallel to the direction of the chord length, wherein the at least one airfoil element has an airfoil element thickness in a direction perpendicular to the projecting direction, wherein the at least one airfoil element has a pressure side airfoil side facing the pressure side and a suction side airfoil side facing the suction side, wherein the at least one airfoil element has a cross-section substantially orthogonal to the projecting direction, characterized in that the cross-section of the at least one airfoil element has at least one local minimum of the airfoil element thickness, wherein the airfoil element thickness in the cross-section on both sides of the local minimum has a larger value.

公开(公告)号：US20240295210A1

公开(公告)日：2024-09-05

申请号：US18572234

申请日：2022-06-28

申请人： Vestas Wind Systems A/S

发明人： Rens Christiaan Verhoef ,  Gurmukh Singh

IPC分类号： F03D1/06

CPC分类号： F03D1/0688 ,  F03D1/069 ,  F05B2240/303 ,  F05B2240/304

摘要： The present disclosure provides a blade for a wind turbine, where the blade extends in a lengthwise direction between a root end and a tip end of the blade. The blade comprises a leeward shell portion and a windward shell portion, each extending in a chordwise direction between a leading edge of the blade and a trailing edge of the blade. A first windward reinforcement structure and a first leeward reinforcement structure are arranged internally within the blade and engage the windward and the leeward shell portion, respectively. The first windward and first leeward reinforcement structures extend in the lengthwise direction of the blade and have a thickness in the thickness direction of the blade. The respective thicknesses of the first leeward reinforcement structure and the first windward reinforcement structure decrease towards the tip end in the lengthwise direction in a first section of the blade; and at at least one position along the length of the blade, the decrease of the thickness of the first leeward reinforcement structure is staggered with respect to the decrease of the thickness of the first windward reinforcement structure.

公开(公告)号：US20240035441A1

公开(公告)日：2024-02-01

申请号：US18264227

申请日：2021-10-11

申请人： ZHUZHOU TIMES NEW MATERIAL TECHNOLOGY CO., LTD.

发明人： Xuebin FENG ,  Binbin HOU ,  Hang DENG ,  Jiehua HU ,  Jiangang ZHAO ,  Jun YANG ,  Chaoyi PENG ,  Sheng FAN ,  Penghui LIU

IPC分类号： F03D1/06

CPC分类号： F03D1/069 ,  F05B2280/40 ,  F05B2280/6003 ,  F05B2280/702 ,  F05B2230/40 ,  F05B2230/20 ,  F05B2240/304

摘要： The present disclosure provides a wind turbine blade with an improved trailing edge structure and a manufacturing method thereof. The wind turbine blade includes an upper shell, a lower shell, and a trailing edge, where a trailing edge bonding region enclosed by the upper shell, the lower shell and the trailing edge is filled with composite materials, and the composite materials are discontinuous in an airfoil chordwise direction. The manufacturing method includes the following steps: S1: manufacturing reinforcements with a same cross-sectional shape as the trailing edge filling region for composite materials; and S2: integrally molding the reinforcements, a fiber fabric and the upper shell, providing the lower shell, combining the upper shell and the lower shell, and performing heating for curing and molding. The discontinuous filling structure reduces usages of the adhesive and the reinforcements of the composite materials. The small web can improve a strength of the trailing edge region, and reduce a bonding width of the trailing edge. Therefore, the present disclosure realizes a light weight of the wind turbine blade.

公开(公告)号：US20240209830A1

公开(公告)日：2024-06-27

申请号：US18531818

申请日：2023-12-07

申请人： Vestas Wind Systems A/S

发明人： Stephen Randall ,  Gurmukh Singh

IPC分类号： F03D1/06 ,  F03D13/10

CPC分类号： F03D1/0675 ,  F03D1/0688 ,  F03D1/069 ,  F03D13/10 ,  F05B2220/30 ,  F05B2230/60 ,  F05B2240/221

摘要： A wind turbine blade comprising a leeward shell portion and a windward shell portion, each of the shell portions extending in a chordwise direction between a leading edge and a trailing edge of the wind turbine blade; a leading reinforcement arrangement comprising at least a leading leeward reinforcement structure engaging the leeward shell portion and a leading windward reinforcement structure engaging the windward shell portion; and a trailing reinforcement arrangement comprising at least a trailing leeward reinforcement structure engaging the leeward shell portion and a trailing windward reinforcement structure engaging the windward shell portion. The trailing windward reinforcement structure has a first stiffness in the lengthwise direction and the trailing leeward reinforcement structure has a second stiffness in the lengthwise direction, wherein the first stiffness is greater than the second stiffness at a chordwise plane of the wind turbine blade.

公开(公告)号：US12018638B2

公开(公告)日：2024-06-25

申请号：US18018321

申请日：2021-06-30

申请人： GE WIND ENERGY GMBH ,  LM WIND POWER A/S ,  BLADE DYNAMICS LIMITED

发明人： Benoit Petitjean ,  Guannan Wang ,  Andreas Herrig ,  Jeremy Hurault ,  Dongke Sun

IPC分类号： F03D1/06

CPC分类号： F03D1/0633 ,  F03D1/0642 ,  F03D1/0645 ,  F03D1/06495 ,  F03D1/0681 ,  F03D1/069 ,  F05B2240/3042 ,  F05B2260/96

摘要： A trailing edge panel is configured to be attached to a trailing edge of a wind turbine blade and includes a base element and a number of protruding aerodynamic elements. The base element has an attachment part configured to be attached to and extend from the trailing edge of the wind turbine blade and to an upstream position on a first blade side of the wind turbine blade. The base element further has a serrated part extending from the second side of the attachment part and configured to project out from the trailing edge of the wind turbine blade, wherein the serrated part comprises a number of serrations, including a first serration and a second serration. The number of protruding aerodynamic elements, including a first protruding aerodynamic element, includes a first protruding part attached to the serrated part of the base element.

公开(公告)号：US11939948B2

公开(公告)日：2024-03-26

申请号：US17924675

申请日：2021-05-11

申请人： LM WIND POWER A/S ,  LM WIND POWER R&D (HOLLAND) B.V. ,  BLADE DYNAMICS LIMITED

发明人： Manish Mukherjee ,  Laszlo Bartha ,  Aydin Raeis Hosseiny ,  Sigmund Wenningsted

IPC分类号： F03D1/06

CPC分类号： F03D1/0675 ,  F03D1/069 ,  F05B2240/304 ,  F05B2250/711 ,  F05B2250/712 ,  F05B2280/4003

摘要： Disclosed is a blade shell section of a wind turbine blade, such as wind turbine blade with a flatback section. The blade shell section extends in a longitudinal direction from a first shell section position to a second shell section position. The blade shell section comprises a first laminate layer forming the outer surface of the blade shell section and a second laminate layer forming the inner surface of the blade shell section. The blade shell section further comprising a first shell section and a corner shell section between the contour shell section and the flatback shell section.