Method for creating a transition from an edge of an add-on part mounted on the outer surface of a rotor blade

US12180924B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12180924-B2
Application numberUS-202017435558-A
CountryUS
Kind codeB2
Filing dateMar 9, 2020
Priority dateMar 8, 2019
Publication dateDec 31, 2024
Grant dateDec 31, 2024

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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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Abstract

Official abstract text for this publication.

A method for creating a transition from an edge of an add-on part mounted on the outer surface of a rotor blade, including the steps:delimiting an application area on the rotor blade surface and the add-on part to be covered by a sealant compound with a thin and smooth masking tape;dispensing of the sealant on the application area;distribution of the sealant;removing the masking tape; andsmoothening of a sealant transition step with a flexible tool, is provided.A wind turbine rotor blade is also provided.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for creating a transition from an edge of an add-on part mounted on an outer surface of a rotor blade, the method comprising: delimiting an application area on the outer surface and the add-on part to be covered by a sealant compound with a thin and smooth masking tape; dispensing of the sealant compound on the application area; distributing the sealant compound; removing the masking tape; and smoothening a sealant transition step with a flexible tool. 2. The method according to claim 1 , wherein the sealant compound is formed to overlap the edge of the add-on. 3. The method according to claim 1 , wherein the distributing the sealant compound is achieved by using a toothed spatula of a flexible material, for levelling the sealant compound after the sealant compound has been dispensed to the application area, further wherein teeth of the toothed spatula have a distance between 1 to 2 mm and/or a height between 0.2 to 5 mm. 4. The method according to claim 1 , wherein the flexible tool is a second spatula, with a Shore A hardness bigger than 30 and/or smaller than 70. 5. The method according to claim 1 , wherein the flexible tool comprises a silicone material, with a cross-section profile adapted to the application and a low energy surface preventing adhesion of the sealing material. 6. The method according to claim 1 , wherein the flexible tool comprises a tip where there is an intended contact area with the sealant compound, and a number of grooves running parallel to the tip and/or a number of fins at an opposite end of the tip. 7. The method according to claim 1 , wherein the masking tape has a thickness less than 0.2 mm. 8. The method according to claim 1 , wherein the dispensing of the sealant compound is achieved by bead or spray application, by roll application or using a swirl process, by application of the sealant compound in a serpentine line overlapping transition, on both the add-on and the outer surface, or in a straight line on the add-on and/or the outer surface. 9. The method according to claim 1 , wherein after distributing the sealant compound and before removing the masking tape, the sealant compound is smoothed with a tool, moved in a longitudinal direction of the blade, further wherein the tool is designed to meet a profile of the blade, with a curvature that matches that of a blade leading edge profile. 10. The method according to claim 1 , wherein the sealant compound is fluid enough to flow into gaps and surface crevices formed during application of the add-on, and to ensure a smooth finish, further wherein: the sealant compound has a surface tension being lower than a surface free energy of the blade surface; and/or the sealant compound has a sufficient resistance to the peel forces occurring on respective surfaces over an entire service life of the blade, bigger than 2 N/mm, and/or the sealant compound has a tensile strength of bigger than 4 MPa and/or smaller than 8 MPa; and/or the sealant compound has an elongation at break bigger than 80% and/or smaller than 130%; and/or the sealant compound has a Young's Modulus bigger than 8 MPa and/or smaller than 150 MPa; and/or the sealant compound has a maximum size of solid particles, filler particles, agglomerates of filler particles, gel particles, in the sealing material both in a liquid as well as hardened or cross-linked state is limited to max. 200 μm. 11. The method according to claim 1 , wherein before dispensing of the sealant compound on the application area a filler is first applied along the edge, further wherein the filler is a quick-setting adhesive and/or a high-viscosity adhesive, and the sealant compound is applied over the cured or hardened filler. 12. The method according to claim 1 , wherein the sealant compound comprises a same material as an adhesive used for fixing the add-on on the outer surface.

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What does patent US12180924B2 cover?
A method for creating a transition from an edge of an add-on part mounted on the outer surface of a rotor blade, including the steps:delimiting an application area on the rotor blade surface and the add-on part to be covered by a sealant compound with a thin and smooth masking tape;dispensing of the sealant on the application area;distribution of the sealant;removing the masking tape; andsmooth…
Who is the assignee on this patent?
Siemens Gamesa Renewable Energy As
What technology area does this patent fall under?
Primary CPC classification F03D1/0675. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 31 2024 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).