Manufacture of a rotor blade for a wind turbine

US9931689B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9931689-B2
Application numberUS-201113822703-A
CountryUS
Kind codeB2
Filing dateOct 5, 2011
Priority dateOct 12, 2010
Publication dateApr 3, 2018
Grant dateApr 3, 2018

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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 and manufacturing unit for producing a rotor blade ( 5 ) of a wind turbine ( 1 ) from at least a first rotor blade element ( 11, 11′, 12, 12 ′) and a second rotor blade element ( 11, 11′, 12, 12 ′). The first rotor blade element ( 11, 11′, 12, 12 ′) and the second rotor blade element ( 11, 11′, 12, 12 ′) are positioned in the desired relative arrangement with respect to each other such that a joint gap ( 13 ) remains between the first rotor blade element ( 11, 11′, 12, 12 ′) and the second rotor blade element ( 11, 11′, 12, 12 ′). Adhesive is introduced into the joint gap ( 13 ) for joining the first rotor blade element ( 11, 11′, 12, 12 ′) and the second rotor blade element ( 11, 11′, 12, 12 ′).

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for producing a rotor blade ( 5 ) of a wind turbine ( 1 ), comprising the steps of: fastening a seal ( 14 , 122 ) to a second rotor blade element ( 12 , 12 ′) during production of the second rotor blade element ( 12 , 12 ′); positioning a first rotor blade element ( 11 , 11 ′) and the second rotor blade element ( 12 , 12 ′) in a desired relative arrangement with respect to each other such that a joint gap ( 13 ) remains between the first rotor blade element ( 11 , 11 ′) and the second rotor blade element ( 12 , 12 ′), wherein the seal ( 14 , 122 ) is fastened to the second rotor blade element ( 12 , 12 ′) before the second rotor blade element ( 12 , 12 ′) is positioned, and joining the first rotor blade element ( 11 , 11 ′) and the second rotor blade element ( 12 , 12 ′) by introducing an adhesive in a controlled manner into the joint gap ( 13 ), wherein the introduction of the adhesive into the joint gap ( 13 ) is regulated by controlling at least one of an adhesive quantity that is introduced per unit time and a movement of an adhesive application apparatus ( 20 ) along the joint gap ( 13 ), wherein the joint gap ( 13 ) is sealed along a second longitudinal side which extends opposite a first longitudinal side. 2. The method according to claim 1 , wherein the adhesive is introduced into the joint gap ( 13 ) at the first longitudinal side of the joint gap ( 13 ). 3. The method according to claim 1 , wherein the adhesive is introduced starting at one end of the joint gap ( 13 ) along a longitudinal extension of the joint gap ( 13 ) stepwise or continuously proceeding in the joint gap ( 13 ). 4. A wind turbine ( 1 ), comprising: a tower ( 2 ); a nacelle ( 3 ) disposed at a tip of the tower ( 2 ); and a rotor blade ( 5 ) according to claim 1 , wherein the rotor blade ( 5 ) is attached to the nacelle ( 3 ). 5. A manufacturing unit for joining a first rotor blade element ( 11 , 11 ′) and a second rotor blade element ( 12 , 12 ′) during production of a rotor blade ( 5 ) of a wind turbine ( 1 ), the manufacturing unit comprising: a first positioning device ( 15 ) that receives the first rotor blade element ( 11 , 11 ′); a second positioning device ( 16 ) that positions the second rotor blade element ( 12 , 12 ′) with respect to the first rotor blade element ( 11 , 11 ′) such that a gap ( 13 ) remains therebetween, wherein a seal ( 14 , 122 ) is fastened to the second rotor blade element ( 12 , 12 ′) during production of the second rotor blade element ( 12 , 12 ′) and before the second positioning device ( 16 ) positions the second rotor blade element ( 12 , 12 ′); an adhesive application apparatus ( 20 ) disposed at a first longitudinal side at one end of the joint gap ( 13 ), wherein the adhesive application apparatus ( 20 ) introduces an adhesive into the joint gap ( 13 ); and a sensor ( 22 ) that senses a filling degree of the adhesive in the joint gap ( 13 ), wherein the adhesive is introduced in a controlled manner into the joint gap ( 13 ), and wherein the sensor senses the filling degree of the adhesive in the joint gap ( 13 ) near a nozzle ( 21 ) for the adhesive, wherein the joint gap ( 13 ) is sealed along a second longitudinal side which extends opposite the first longitudinal side. 6. The manufacturing unit according to claim 5 , wherein the adhesive application apparatus ( 20 ) comprises the nozzle ( 21 ) for the adhesive, and wherein at least one of the adhesive application apparatus ( 20 ) and the nozzle ( 21 ) for the adhesive are movable along the first longitudinal side of the joint gap ( 13 ). 7. The manufacturing unit according to claim 5 , further comprising: a control device for the adhesive application apparatus ( 20 ) that regulates at least one of a cross sectional area of an outlet opening of the nozzle ( 21 ) for the adhesive, an adhesive pressure, a movement of the nozzle ( 21 ) for the adhesive along the joint gap ( 13 ), and movement of the adhesive application apparatus ( 20 ) along the joint gap ( 13 ). 8. The manufacturing unit according to claim 5 , wherein the adhesive application apparatus ( 20 ) mixes adhesive composed of at least two components.

Assignees

Inventors

Classifications

  • Joining from or joining on the inside (for making tubes by bending sheets and joining from the inside B29C53/387) · CPC title

  • with two right angles, e.g. for making T-shaped pieces, H-shaped pieces · CPC title

  • by gluing (gluing of plastics material B29C65/48) · CPC title

  • Cross-Sectional Technologies · mapped topic

  • B21K3/04Primary

    blades, e.g. for turbines; Upsetting of blade roots · CPC title

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What does patent US9931689B2 cover?
A method and manufacturing unit for producing a rotor blade ( 5 ) of a wind turbine ( 1 ) from at least a first rotor blade element ( 11, 11′, 12, 12 ′) and a second rotor blade element ( 11, 11′, 12, 12 ′). The first rotor blade element ( 11, 11′, 12, 12 ′) and the second rotor blade element ( 11, 11′, 12, 12 ′) are positioned in the desired relative arrangement with respect to each other such…
Who is the assignee on this patent?
Zeller Lenz Simon, Gunther Maik, Senvion Se
What technology area does this patent fall under?
Primary CPC classification B21K3/04. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 03 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). 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).