JP3576262B2 - GFRP-made wind turbine blade capable of predicting fracture and method of predicting its fracture - Google Patents
GFRP-made wind turbine blade capable of predicting fracture and method of predicting its fracture Download PDFInfo
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Description
【0001】
【産業上の利用分野】
本発明は、風力発電用の破壊予知可能型GFRP製風車翼に関する。
【0002】
【従来の技術】
風力発電用の風車翼としては、従来、図2(A)縦断面図及び同図(B)B−B斜視断面図に示すように、翼形形状を作る外皮1,2と、主として強度部材となる長方形枠状断面を有する長尺筒状材であるボックス状断面の主桁3及び中間充填材となる発泡ウレタン4,5から構成された翼が使用されている。ここで、外皮1,2と主桁3は、軽量・高強度化及び低コスト化の観点からGFRP(Grass Fiber Reinforced Plastic)が用いられている。
【0003】
【発明が解決しようとする課題】
この種の発電用風車の翼は、発電効率の向上の点から、例えば、250KW級の風車の場合、翼の長さは約12m,回転直径は約28m程度になるというように、大型化の傾向にある。そのため、翼材料としては、軽量化及び高強度化の観点からプラスチック系の複合材料(FRP)が用いられている。
また、風車の翼は、風を受け回転することにより遠心力による引張荷重を受けるとともに繰り返しの曲げ荷重を受ける。また、最近は少なくとも10年以上の耐久性を保証しなければならないため、翼の疲労損傷に対する信頼性の確保が必要となっている。
そのため、翼の疲労強度の確保が必要であるが、風車用GFRP翼は長さが10mを越える大型の製品であるため製造上のばらつきがあり、これまでに装置設置後5年前後で翼が折損し飛散した例が何件か報告されている。 翼が疲労損傷により回転中に破壊し、その先端が折損飛散した場合、長さが5〜10m,重量が何百kgもあるものが遠心力により飛散するので、周囲の構造物あるいは人への衝突を考えた場合、非常に危険であり大きな問題となる。したがって、少なくとも翼が折損し飛散する前にその損傷情報を捉え、運転中(翼回転中)の折損事故だけは確実に防止することが非常に重要なのである。
【0004】
本発明はこのような事情に鑑みて提案されたもので、翼の内部的損傷を早期に検知して翼の折断〜飛散等の事故が回転中に発生することを防止することができる安全な破壊予知可能型GFRP風車翼及びその破壊予知方法を提供することを目的とする。
【0005】
【課題を解決するための手段】
そのために請求項1の発明の破壊予知可能型GFRP製風車翼は、翼根から翼先端までの翼の全長にわたって延びるボックス状断面を有する長尺主桁の前端面,後端面にそれぞれ発泡ウレタンからなる前縁翼部,後縁翼部を翼の全長にわたって突設するとともに、同前縁翼部,同後縁翼部,同主桁の外面を全長にわたって外皮により接着被覆してなるGFRP製の風車翼において、上記主桁の背面,腹面とその外皮とを接着した接着層中に埋設され、それぞれ翼根部から翼先端にわたって連続的に張装された小断面の細線又は長箔からなる翼の全長を単位長として多重折りされた1本の長尺導電性線状材を備えたことを特徴としている。
【0006】
請求項2の発明の破壊予知可能型GFRP製風車翼は、請求項1に記載された破壊予知可能型GFRP製風車翼において、翼根部に格納された複数の抵抗測定用端子を設け、上記長尺導電性線状材の両端をそれぞれ上記各抵抗測定用端子に接続したことを特徴としている。
【0007】
請求項3の発明の破壊予知可能型GFRP製風車翼は、請求項1に記載された破壊予知可能型GFRP製風車翼において、複数の翼根部の回転中心ボスに同軸的に並設された複数のスリップリング及び同各スリップリングにそれぞれ当接するブラシを備え、風車の回転中に常時上記各長尺導電性線状材の抵抗値を測定可能としたことを特徴としている。
【0008】
請求項4の発明のGFRP製風車翼の破壊予知方法は、請求項1に記載された破壊予知可能型GFRP製風車翼の破壊予知方法であって、定期的に風車翼の稼働を停止し、上記長尺導電性線状材の電気抵抗を測定して、その測定値の変化に基づいて翼の破壊を予知することを特徴としている。
【0009】
【作用】
このような構成によれば、翼の内部に埋設する導電性材料の形態は、GFRP翼材の強度を損なわないような細線状あるいは薄板状のもので、例えば金属繊維や箔あるいはカーボン繊維などである。また、埋め込む位置は、運転時の翼の派生応力が最も高く変形歪み量が大きい部分の表層近傍、例えば、外皮と主桁の間の接着層内がよい。
本発明においては、翼内部に配設した導電性材料の電気抵抗を測定することにより、翼の僅かな損傷を検知することができ、稼働中における翼の折断〜飛散という最悪の事故を起こす前に、対策を施すことができる。
【0010】
【実施例】
本発明を250KW級の発電風車に適用した一実施例を図面について説明すると、図1はその風車翼の横断面図を示す斜視図である。
【0011】
上図において、図2と同一の符号はそれぞれ同図と同一の部材を示し、本発明が図2の構造と大きく相違するところは主桁〜外皮間の接着層部に、線径φ1.5mmの銅線を主桁3の背面,腹面とその外皮1との間の接着層6,7中に埋設的に翼先端から翼根まで連続的に張装したことにある。
【0012】
この試作翼の腹側から外皮,接着層(銅線部を含む)、主桁を含む大型の疲労試験片(長さ;600mm,幅;120mm,板あつ;20mm)を切出し、加工後の試験片の銅線の電気抵抗を測定した結果、1.6〜1.7μΩ・cmであった。
【0013】
次に、この電気抵抗の測定後、引張の疲労試験を実施した。引張負荷応力は、0.3〜3.0kg/mm2 の繰り返しとし、銅線の電気抵抗測定では連続的に記録をとった。
その結果、繰り返し回数が2×106 回を越えたところで銅線の電気抵抗が∞となり銅線が破断したことが確認された。
そこで、試験片の詳細な観察を行ったところ、試験片中央部に微細な亀裂が多数発生しており、その中の一つは、長さ約5mm程度のもので深さは試験片の肉厚の1/3まで進展しており、この部分で埋め込まれた銅線が破断していることが判明した。
【0014】
以上のことから、GFRP翼の主桁〜外皮間の接着層部に翼先端から翼根にわたって導電性を有する複数の連続線を張装し、その電気抵抗を測定することにより、翼の折損,飛散という最悪の事態を起こす前に、上記導電性抵抗線の損傷を検知して対策を施すことが可能であることが確認できた。
なお、連続線を翼の腹面,背面及び又は前縁,後縁に沿って翼全長にわたって布設しておくことにより、損傷が腹面,背面のいずれで起きるか前縁,後縁のいずれで起きるかの別も検知できる。
【0015】
【発明の効果】
このような本発明によれば、翼内部に長手方向に全長を多重に折り曲げた形で張装埋設した長尺の導電性材料の電気抵抗を測定することにより、翼の初期損傷を検知でき、翼の折損さらに飛散という最悪の事態を起こす前に対策を施すことができる。また、これまでかなりの費用をかけて行ってきた翼の定期的な損傷検査(目視検査,非破壊検査)を実施する必要もなくなるため、保守検査費用が大幅に削減できる。
【0016】
要するに、請求項1の発明の破壊予知可能型GFRP製風車翼によれば、翼根から翼先端までの翼の全長にわたって延びるボックス状断面を有する長尺主桁の前端面,後端面にそれぞれ発泡ウレタンからなる前縁翼部,後縁翼部を翼の全長にわたって突設するとともに、同前縁翼部,同後縁翼部,同主桁の外面を全長にわたって外皮により接着被覆してなるGFRP製の風車翼において、上記主桁の背面,腹面とその外皮とを接着した接着層中に埋設され、それぞれ翼根部から翼先端にわたって連続的に張装された小断面の細線又は長箔からなる翼の全長を単位長として多重折りされた1本の長尺導電性線状材を備えているので、翼の内部的損傷を早期に検知して翼の折断〜飛散等の事故が回転中に発生することを防止することができる安全な破壊予知可能型GFRP風車翼及びその破壊予知方法を得るから、本発明は産業上極めて有益なものである。
【0017】
請求項2の発明の破壊予知可能型GFRP製風車翼によれば、請求項1に記載された破壊予知可能型GFRP製風車翼において、翼根部に格納された複数の抵抗測定用端子を設け、上記長尺導電性線状材の両端をそれぞれ上記各抵抗測定用端子に接続するようにしたので、翼の内部的損傷を早期に検知して翼の折断〜飛散等の事故が回転中に発生することを防止することができるとともに、その導電性線状材の抵抗値を測定することが容易である安全な破壊予知可能型GFRP風車翼を得るから、本発明は産業上極めて有益なものである。
【0018】
請求項3の発明の破壊予知可能型GFRP製風車翼によれば、請求項1に記載された破壊予知可能型GFRP製風車翼において、複数の翼根部の回転中心ボスに同軸的に並設された複数のスリップリング及び同各スリップリングにそれぞれ当接するブラシを備え、風車の回転中に常時上記各長尺導電性線状材の抵抗値を測定可能としたので、翼の内部的損傷を早期に検知して翼の折断〜飛散等の事故が回転中に発生することを防止することができ、翼の回転中でもその電気抵抗値を測定することができ、定期検査を実施する必要をなくし保守コストを大幅に削減することができる安全な破壊予知可能型GFRP風車翼を得るから、本発明は産業上極めて有益なものである。
【0019】
請求項4の発明のGFRP製風車翼の破壊予知方法によれば、請求項1に記載された破壊予知可能型GFRP製風車翼の破壊予知方法であり、定期的に風車翼の稼働を停止し、上記長尺導電性線状材の電気抵抗を測定して、その測定値の変化に基づいて翼の破壊を予知するようにしたので、翼の内部的損傷を早期に検知して翼の折断〜飛散等の事故が回転中に発生することを防止することができる安全な破壊予知可能型GFRP風車翼の破壊予知方法を得るから、本発明は産業上極めて有益なものである。
【図面の簡単な説明】
【図1】本発明を250KW出力の風力発電用翼車に適用した実施例のGFRP試作翼の横断面を示す斜視図である。
【図2】従来の発電用風車のFRP翼を示し、同図(A)はFRP翼の断面図、同図(B)はそのB−B横断面を示す斜視図である。
【符号の説明】
1 背側外皮(GFRP)
2 腹側外皮(GFRP)
3 主桁(GFRP)
4 後縁翼部発泡ウレタン
5 前縁翼部発泡ウレタン
6 背側接着層(GFRP)
7 腹側接着層(GFRP)
8 前縁(リーディングエッジ)
9 後縁(トレーリングエッジ)
10 背側銅線(φ1.5mm)
11 腹側銅線(φ1.5mm)[0001]
[Industrial applications]
The present invention relates to a wind turbine blade made of GFRP that can be predicted to be broken for wind power generation.
[0002]
[Prior art]
Conventionally, as wind turbine blades for wind power generation, as shown in FIG. 2 (A) longitudinal sectional view and FIG. 2 (B) BB perspective sectional view,
[0003]
[Problems to be solved by the invention]
In order to improve the power generation efficiency, for example, a 250 kW class wind turbine blade has a blade of about 12 m and a rotating diameter of about 28 m in order to improve power generation efficiency. There is a tendency. Therefore, a plastic composite material (FRP) is used as the blade material from the viewpoint of weight reduction and high strength.
In addition, the blades of the windmill receive a tensile load due to centrifugal force and a repeated bending load by rotating and receiving the wind. In addition, since durability of at least 10 years has recently been required to be guaranteed, it is necessary to ensure reliability against blade fatigue damage.
Therefore, it is necessary to ensure the fatigue strength of the blades. However, since the GFRP blades for wind turbines are large products with a length of more than 10 m, there is a variation in manufacturing. Several broken and scattered cases have been reported. If the wing breaks during rotation due to fatigue damage and its tip breaks and scatters, centrifugal force causes the wing to be scattered due to centrifugal force. Considering a collision is very dangerous and a big problem. Therefore, it is very important to at least capture the damage information before the wing breaks and scatters, and to reliably prevent only the breakage accident during operation (while the wing is rotating).
[0004]
The present invention has been proposed in view of such circumstances, and it is possible to detect internal damage of a wing at an early stage and to prevent an accident such as breakage or scattering of the wing from occurring during rotation. An object of the present invention is to provide a GFRP wind turbine blade capable of predicting fracture and a method of predicting its fracture.
[0005]
[Means for Solving the Problems]
For this purpose, the wind turbine blade made of GFRP with predictable fracture according to the first aspect of the present invention has a long main girder having a box-shaped cross section extending over the entire length of the blade from the blade root to the tip of the blade. The leading edge wing and the trailing edge wing protrude over the entire length of the wing, and the outer surfaces of the leading edge wing, the trailing edge wing, and the main girder are adhesively coated with a skin over the entire length. In a wind turbine blade, a wing made of a thin wire or a long foil having a small cross section, which is embedded in an adhesive layer that bonds the back surface and the abdominal surface of the main girder to the outer skin and is continuously stretched from the blade root portion to the blade tip, respectively. The present invention is characterized in that one long conductive linear material that is multiply folded with the entire length as a unit length is provided.
[0006]
According to a second aspect of the present invention , there is provided a wind turbine blade made of a predictable fracture type GFRP according to the first aspect of the present invention , wherein a plurality of resistance measurement terminals stored in a blade root portion are provided. It is characterized in that both ends of the measuring conductive wire are connected to the respective terminals for resistance measurement.
[0007]
The wind turbine blade made of GFRP with predictable fracture according to the invention of
[0008]
The method for predicting the destruction of a GFRP wind turbine blade according to the invention of
[0009]
[Action]
According to such a configuration, the form of the conductive material embedded in the wing is a thin wire or thin plate that does not impair the strength of the GFRP wing material, such as metal fiber, foil, or carbon fiber. is there. The embedding position is preferably in the vicinity of the surface of the portion where the induced stress of the blade during operation is the highest and the amount of deformation is large, for example, in the adhesive layer between the outer skin and the main girder.
In the present invention, by measuring the electric resistance of the conductive material disposed inside the wing, slight damage to the wing can be detected, and before the worst accident of breaking or scattering of the wing during operation is caused. In addition, measures can be taken.
[0010]
【Example】
One embodiment in which the present invention is applied to a 250 kW class wind turbine will be described with reference to the drawings. FIG. 1 is a perspective view showing a cross-sectional view of the wind turbine blade.
[0011]
In the figure, the same reference numerals as in FIG. 2 each represent the same members of the same figure, when the present invention is greatly different from the structure of Figure 2 in the adhesive layer portion between the main girder-hull, wire diameter φ1.5mm certain copper back of the
[0012]
From the ventral side of this prototype wing, cut out a large fatigue test piece (length: 600 mm, width: 120 mm, plate thickness: 20 mm) including the outer skin, adhesive layer (including copper wire), and main girder, and test after processing As a result of measuring the electric resistance of one copper wire, it was 1.6 to 1.7 μΩ · cm.
[0013]
Next, after measuring the electric resistance, a tensile fatigue test was performed. The tensile load stress was 0.3 to 3.0 kg / mm 2 repeatedly, and the electrical resistance of the copper wire was continuously recorded.
As a result, when the number of repetitions exceeded 2 × 10 6 , the electric resistance of the copper wire became Δ and it was confirmed that the copper wire was broken.
Then, when the specimen was observed in detail, many fine cracks were generated at the center of the specimen. One of them was about 5 mm long and the depth was the thickness of the specimen. It has grown to 1/3 of the thickness, and it was found that the embedded copper wire was broken at this portion.
[0014]
In view of the above, a plurality of conductive lines having conductivity from the blade tip to the blade root are mounted on the adhesive layer between the main girder and the outer skin of the GFRP blade, and the electrical resistance is measured. It has been confirmed that before the worst case of scattering occurs, it is possible to detect damage to the conductive resistance wire and take a countermeasure.
By laying a continuous line along the entire length of the wing along the abdominal surface, the back surface and / or the leading and trailing edges of the wing, whether the damage occurs on the abdominal surface, the back surface, or on the leading or trailing edge Can also be detected.
[0015]
【The invention's effect】
According to the present invention, it is possible to detect the initial damage of the wing by measuring the electric resistance of a long conductive material stretched and buried in a form in which the entire length is bent multiple times in the longitudinal direction inside the wing, Countermeasures can be taken before the worst case of wing breakage and splashing occurs. In addition, there is no need to perform regular damage inspection (visual inspection, non-destructive inspection) of the wing, which has been performed at a considerable cost, so that maintenance inspection costs can be significantly reduced.
[0016]
In short, according to the wind turbine blade made of GFRP with predictable fracture according to the first aspect of the present invention, foam is formed on the front end face and the rear end face of a long main girder having a box-shaped cross section extending from the root to the tip of the blade. A GFRP formed by projecting a leading edge wing portion and a trailing edge wing portion made of urethane over the entire length of the wing, and adhesively coating the outer surfaces of the leading edge wing portion, the trailing edge wing portion, and the main girder with a skin over the entire length. Wind turbine blades, which are embedded in an adhesive layer that adheres the back and abdominal surfaces of the main girder to the outer skin, and are each composed of a small-section thin wire or long foil that is continuously stretched from the blade root to the blade tip. full length single elongated conductive linear member multiplexed folded so Bei Eteiru as a unit length of the blade, by detecting the internal damage of the blade at an early stage accident Oridan-scattering and the like of the blade during rotation Safety that can be prevented from occurring From getting destroyed predictable type GFRP wind turbine blade and fracture prediction method, the present invention is extremely useful industrially.
[0017]
According to the wind turbine blade made of predictable fracture type GFRP of the invention of
[0018]
According to the wind turbine blade made of predictable fracture type GFRP according to the invention of
[0019]
According to the method for predicting destruction of a GFRP wind turbine blade according to the invention of
[Brief description of the drawings]
FIG. 1 is a perspective view showing a cross section of a prototype GFRP blade of an embodiment in which the present invention is applied to a wind turbine for wind power generation having a power of 250 kW.
FIG. 2 shows an FRP blade of a conventional wind turbine for power generation, wherein FIG. 2 (A) is a cross-sectional view of the FRP blade, and FIG. 2 (B) is a perspective view showing a BB transverse section thereof.
[Explanation of symbols]
1 dorsal skin (GFRP)
2 Ventral outer skin (GFRP)
3 Main girder (GFRP)
4 Trailing edge wing urethane foam 5 Leading edge
7 Ventral adhesive layer (GFRP)
8 Leading edge
9 Trailing edge (trailing edge)
10. Back copper wire (φ1.5mm)
11 ventral copper wire (φ1.5mm)
Claims (4)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9454595A JP3576262B2 (en) | 1995-03-28 | 1995-03-28 | GFRP-made wind turbine blade capable of predicting fracture and method of predicting its fracture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9454595A JP3576262B2 (en) | 1995-03-28 | 1995-03-28 | GFRP-made wind turbine blade capable of predicting fracture and method of predicting its fracture |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH08261135A JPH08261135A (en) | 1996-10-08 |
| JP3576262B2 true JP3576262B2 (en) | 2004-10-13 |
Family
ID=14113288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9454595A Expired - Fee Related JP3576262B2 (en) | 1995-03-28 | 1995-03-28 | GFRP-made wind turbine blade capable of predicting fracture and method of predicting its fracture |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3576262B2 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20040073461A (en) * | 2001-12-08 | 2004-08-19 | 우벤 알로이즈 | Rotor Blade of a Wind Power Installation, Comprising a Warning Light |
| DE10259680B4 (en) | 2002-12-18 | 2005-08-25 | Aloys Wobben | Rotor blade of a wind turbine |
| ES2255454B1 (en) | 2004-12-15 | 2007-07-01 | Gamesa Eolica, S.A. | PARARRAYOS SYSTEM FOR AEROGENERATOR SHOVEL. |
| JP4969098B2 (en) | 2005-12-21 | 2012-07-04 | 三菱重工業株式会社 | Windmill lightning protection device, method of assembling the lightning protection device, windmill blade including the lightning protection device, and windmill including the windmill blade |
| JP6440367B2 (en) * | 2014-02-27 | 2018-12-19 | 三菱重工業株式会社 | Wind turbine blade damage detection method and wind turbine |
| KR101581229B1 (en) * | 2014-08-22 | 2015-12-30 | 삼성중공업 주식회사 | Fabricating method of blade for wind turbine |
| KR102422918B1 (en) * | 2021-11-22 | 2022-07-21 | 한국기계연구원 | Monitoring device and method for blades of wind generator |
-
1995
- 1995-03-28 JP JP9454595A patent/JP3576262B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH08261135A (en) | 1996-10-08 |
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