A Wind Turbine Blade Manufacturing System and Method
US-2017043542-A1 · Feb 16, 2017 · US
US2023249421A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2023249421-A1 |
| Application number | US-202118015166-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 8, 2021 |
| Priority date | Jul 10, 2020 |
| Publication date | Aug 10, 2023 |
| Grant date | — |
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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).
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.
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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