A method of manufacturing a shell of a wind turbine blade

US2023249421A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2023249421-A1
Application numberUS-202118015166-A
CountryUS
Kind codeA1
Filing dateJul 8, 2021
Priority dateJul 10, 2020
Publication dateAug 10, 2023
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A method of manufacturing a shell (36 and 38) of a wind turbine blade (10) is disclosed. The method comprises providing a mould (9) having a marker (11) at pre-determined locations. One or more layers of fiber fabrics are provided on surface of the mould (9) to form a shell half structure (36 and 38). Resin is infused through the one or more layers of fiber fabrics and subsequently cured to obtain the shell half structure (36 and 38). A reference portion (19) is marked on the shell half structure (36 and 38) to assemble one or more components on the shell half structure (36 and 38), by detecting a location of the marker (11) in the mould (9) by a detection device (13). The above method facilitates accurate positioning of component such as shear webs (7).

First claim

Opening claim text (preview).

1 . A method of manufacturing a shell ( 36 and 38 ) of a wind turbine blade ( 10 ), the method comprises: providing a mould ( 9 ) having a marker ( 11 ) at pre-determined locations; laying one or more layers of fiber fabrics on surface of the mould ( 9 ) to form a shell half structure ( 36 and 38 ); infusing resin through the one or more layers of fiber fabrics and subsequently curing the same to obtain the shell half structure ( 36 and 38 ); marking a reference portion ( 19 ) on the shell half structure ( 36 and 38 ) to assemble one or more components in the shell half structure ( 36 and 38 ), by detecting a location of the marker ( 11 ) in the mould ( 9 ) by a detection device ( 13 ) wherein the detection device ( 13 ) is a radar type detection device. 2 . The method according to claim 1 , wherein the marker ( 11 ) is provided along a length of the mould ( 9 ) in a continuous or segmented manner. 3 . The method according to claim 1 , wherein the marker ( 11 ) is metallic or non-metallic strip. 4 . The method according to claim 1 , wherein the location of the marker ( 11 ) is detected by positioning the detection device ( 13 ) on the surface of the shell half structure ( 36 and 38 ). 5 . The method according to claim 1 , wherein the reference portion ( 19 ) on the surface of the shell half structure ( 2 ) are made at a distance ranging from 500 mm to 3000 mm along the surface of the shell half structure ( 2 ). 6 . The method according to claim 1 , wherein the reference portion ( 19 ) on the surface of the shell half structure ( 2 ) is continuous. 7 . The method according to claim 1 , wherein the marker ( 11 ) is made of at least one of steel or aluminum. 8 . The method according to claim 1 , wherein the one or more components positioned on the shell half structure ( 2 ) with reference to the detected position of the marker ( 11 ) includes a shear web ( 7 ), box beam, spar beam and box spar. 9 . A method of manufacturing a wind turbine blade ( 10 ) having a profiled contour including a pressure side ( 36 ) and a suction side ( 38 ), and a leading edge ( 18 ) and a trailing edge ( 20 ) with a chord having a chord length extending therebetween, the wind turbine blade ( 10 ) extending in a spanwise direction between a root end and a tip end, the method comprises: providing a mould ( 9 ) having a marker ( 11 ) at pre-determined locations; laying one or more layers of fiber fabrics, on surface of the mould ( 9 ) to form a first shell half structure ( 36 ) and a second shell half structure ( 38 ) separately; infusing resin through the one or more layers of fiber fabrics with a resin and subsequently curing the same to obtain the first and the second shell half structure ( 36 and 38 ); marking a reference portion ( 8 ) on at least one of the first shell half and the second shell half structure ( 36 and 38 ), by detecting a location of the marker ( 11 ) in the mould ( 9 ) using a detection device ( 13 ); fixing a shear web ( 7 ) with reference to the marked reference position ( 19 ) in an inner surface ( 17 ) of at least one of the first shell half structure ( 36 ) and the second shell half structure ( 38 ); joining the first shell half structure ( 36 ) with the second shell half structure ( 38 ) to obtain a wind turbine blade ( 10 ); 10 . The method according to claim 9 , wherein the marker ( 11 ) is provided along a length of the mould ( 9 ) in a continuous or segmented manner. 11 . The method according to claim 9 , wherein the marker ( 11 ) is metallic or non-metallic strip. 12 . The method according to claim 9 , wherein the location of the marker ( 11 ) is detected by positioning the detection device ( 3 ) on the surface of the shell half structure ( 36 and 38 ). 13 . The method according to claim 9 , wherein the detection device ( 13 ) is a radar type detection device. 14 . The method according to claim 9 , wherein the reference portions ( 19 ) on the surface of the shell half structure ( 2 ) are made at a distance ranging from 500 mm to 3000 mm along the surface of the shell half structure ( 5 ). 15 . The method according to claim 9 , wherein the reference portion ( 19 ) on the surface of the shell half structure ( 2 ) is continuous. 16 . The method according to claim 9 , wherein the marker ( 11 ) is made of at least one of steel or aluminum. 17 . The method according to claim 9 , wherein the layers of fiber fabrics on the mould ( 9 ) include aramid fiber fabrics, glass fiber fabrics, carbon fiber fabrics or hybrid fiber fabrics made of glass and carbon. 18 . A mould ( 9 ) for manufacturing a shell ( 36 ) of a wind turbine blade ( 10 ), the mould ( 9 ) comprising: an inner surface ( 21 ) and an outer surface ( 23 ), wherein the inner surface ( 21 ) is defined by an aerodynamic shape of the wind turbine blade ( 10 ) and extends in a spanwise direction; at least one marker ( 11 ) embedded within the inner surface ( 21 ) of the blade shell ( 36 and 38 ) at a predetermined depth from the inner surface ( 21 ) of the blade shell ( 36 and 38 ), wherein, the location of the marker ( 11 ) is detectable by a detection device ( 13 ) for positioning a component on an inner surface ( 17 ) of the blade shell ( 36 and 38 ), wherein the detection device ( 13 ) is a radar type detection device. 19 . The mould ( 9 ) according to claim 18 , wherein the at least one marker ( 11 ) is integrally laid in the mould ( 9 ) or positioned in a groove defined in the inner surface ( 17 ) of the mould ( 9 ). 20 . The mould ( 9 ) according to claim 18 , wherein the predetermined depth from the inner surface ( 17 ) ranges from about 20 mm to about 150 mm. 21 . A system for determining a reference position in a wind turbine blade ( 10 ) to mount one or more components on the shell half structure ( 36 and 38 ), the system comprising: a mould ( 9 ) according to claim 18 ; and a detection device ( 13 ) configured to detect the location of at least one marker ( 11 ) in the mould ( 9 ) by positioning a detection device ( 13 ) on the surface of a shell half structure ( 36 and 38 ), wherein the detection device ( 13 ) is a radar type detection device.

Assignees

Inventors

Classifications

  • B29C70/541Primary

    Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement (positioning inserts in moulds B29C33/12; lay-up on a mould B29C70/30) · CPC title

  • in the form of positioning marks · CPC title

  • and impregnating by vacuum or injection · CPC title

  • hollow blades · CPC title

  • Producing blades or the like, e.g. blades for turbines, propellers, or wings · CPC title

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What does patent US2023249421A1 cover?
A method of manufacturing a shell (36 and 38) of a wind turbine blade (10) is disclosed. The method comprises providing a mould (9) having a marker (11) at pre-determined locations. One or more layers of fiber fabrics are provided on surface of the mould (9) to form a shell half structure (36 and 38). Resin is infused through the one or more layers of fiber fabrics and subsequently cured to obt…
Who is the assignee on this patent?
Lm Wind Power As
What technology area does this patent fall under?
Primary CPC classification B29C70/541. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Aug 10 2023 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).