Wind Turbine Blade Inspection Intelligence
Evaluates blade condition from drone or ground-based visual inspection and produces a structured damage assessment across seven failure modes.
When to Use
Load this skill when the user wants to:
- - Assess blade health from drone inspection images or written findings
- Classify damage type and severity on a 1-5 scale per blade and per zone
- Determine whether a turbine should continue operating, be scheduled for repair, or shut down
- Generate a structured blade inspection report with repair recommendations
Blade Zones
| Zone | Span | Description |
|---|
| Root | 0-33% | Highest structural loads, bolted connection area |
| Mid |
33-66% | Transition zone, moderate aerodynamic load |
| Tip | 66-100% | Highest velocity, most erosion-prone, lightning receptor area |
Surfaces: Leading Edge (LE), Trailing Edge (TE), Suction Side (SS), Pressure Side (PS)
Damage Type Definitions
| Damage Type | Description | Typical Location |
|---|
| Surface crack | Gelcoat or laminate cracks, linear fractures | LE, TE, root transition |
| Erosion / wear |
Material loss, pitting, roughening | LE tip zone |
| Lightning damage | Burn marks, punctures, receptor damage | Tip, receptor area |
| Lamination/structural | Delamination, fiber exposure, buckling, dents | Any zone |
| Debonding | Bond line separation at LE, TE, or shear web | LE, TE, internal |
| Ice accumulation | Ice buildup on surface or edges | Any zone |
| General visual anomaly | Discoloration, contamination, coating loss | Any zone |
Severity Scale
| Severity | Label | Description | Action |
|---|
| 1 | Healthy | No damage or cosmetic marks only | Continue normal operation |
| 2 |
Minor | Early erosion, superficial cracks, coating loss | Increase inspection frequency |
| 3 | Moderate | Gelcoat breach, early debonding, defined damage | Repair within 1-3 months |
| 4 | Significant | Structural involvement, active debonding, lightning | Repair within 2-4 weeks |
| 5 | Critical | Fiber exposure, structural breach, delamination | Immediate shutdown required |
Procedure
- 1. Collect inputs: blade IDs, inspection method, findings per blade per zone per surface.
- Classify each finding by damage type.
- Assign severity per finding using the severity scale.
- Determine overall blade severity as the highest finding for that blade.
- Determine turbine-level severity as the highest across all blades.
- Apply damage-specific rules:
- Lightning damage: minimum Severity 4 until OEM confirms otherwise.
- Debonding at LE or TE over 300 mm: escalate to Severity 4.
- Any confirmed fiber exposure: minimum Severity 4.
- Erosion with full gelcoat loss over 500 mm span at tip: Severity 4.
- Active ice accumulation: always Severity 4.
- 7. Generate output report using the format below.
Output Format
=== BLADE INSPECTION REPORT ===
ASSET : [Turbine ID]
SITE : [Site name]
INSPECTION : [Date / Method]
BLADES : [Number inspected]
BLADE [ID]:
Zone/Surface : [e.g., Tip / Leading Edge]
Damage Type : [e.g., Erosion]
Description : [e.g., Deep pitting ~600 mm span, gelcoat fully lost]
Severity : [1-5] - [Label]
BLADE [ID] OVERALL SEVERITY: [1-5] - [Label]
TURBINE-LEVEL SEVERITY : [1-5] - [Label]
SHUTDOWN RECOMMENDATION: [Yes / No / Conditional]
REPAIR PRIORITY:
- [e.g., Blade 2 tip LE erosion - schedule LEP repair within 6 weeks]
MONITORING STRATEGY:
- [e.g., Monthly drone re-inspection for all blades]
ESCALATION TRIGGERS:
- [e.g., Debond length exceeds 500 mm - shutdown for repair]
- [e.g., SCADA vibration or imbalance alarms - ground turbine]
Damage-Specific Guidance
Erosion: Progresses from roughening to pitting to gelcoat loss to fiber exposure. Repair with Leading Edge Protection (LEP) tape or coating. Severity 3-4 causes measurable energy production loss.
Lightning: Always notify OEM. Minor visible damage may hide internal delamination. Do not assume safe to operate until specialist confirms.
Debonding: LE debonding causes aerodynamic noise and vibration. TE debonding starts at tip and progresses toward root. Bond line gap over 300 mm is Severity 4.
Lamination/Structural: Fiber exposure is always Severity 4 minimum. Dents or buckling without fiber exposure is Severity 3.
Ice: Active ice requires immediate grounding due to rotor imbalance and ice throw risk. After melting, inspect surface for underlying damage.
Pitfalls
- - Do not classify erosion from low-resolution images. Ask for close-up zone-specific photos.
- Lightning damage is always higher priority than it looks. Treat as Severity 4 until proven otherwise.
- Debonding can be invisible from drone imagery. If SCADA shows imbalance alarms, flag potential hidden debonding.
- Active ice is a safety hazard. Recommend immediate grounding.
- Assess each blade independently. Damage distribution is rarely uniform across all three blades.
Verification
After generating the report, confirm with the user:
- - Does the severity match the inspector's on-site assessment?
- Are all three blades accounted for?
- Are there SCADA alarms (vibration, imbalance, power curve deviation) correlating with findings?
- Is there a previous inspection report for trend comparison?
风力发电机叶片检测智能分析
根据无人机或地面目视检测结果评估叶片状况,并针对七种失效模式生成结构化的损伤评估报告。
使用场景
当用户需要以下操作时,可加载此技能:
- - 根据无人机检测图像或书面检查结果评估叶片健康状况
- 按叶片和区域对损伤类型和严重程度进行1-5级分级
- 确定风机应继续运行、安排维修或停机
- 生成包含维修建议的结构化叶片检测报告
叶片区域
| 区域 | 跨度 | 描述 |
|---|
| 根部 | 0-33% | 结构载荷最大,螺栓连接区域 |
| 中部 |
33-66% | 过渡区域,中等气动载荷 |
| 尖部 | 66-100% | 速度最高,最易侵蚀,接闪器区域 |
表面:前缘(LE)、后缘(TE)、吸力面(SS)、压力面(PS)
损伤类型定义
| 损伤类型 | 描述 | 典型位置 |
|---|
| 表面裂纹 | 胶衣或层压板裂纹,线性断裂 | 前缘、后缘、根部过渡区 |
| 侵蚀/磨损 |
材料损失,点蚀,表面粗糙化 | 前缘尖部区域 |
| 雷击损伤 | 烧痕,穿孔,接闪器损坏 | 尖部、接闪器区域 |
| 层压/结构损伤 | 分层,纤维暴露,屈曲,凹陷 | 任何区域 |
| 脱粘 | 前缘、后缘或剪切腹板处的粘接线分离 | 前缘、后缘、内部 |
| 积冰 | 表面或边缘的冰积聚 | 任何区域 |
| 一般视觉异常 | 变色,污染,涂层脱落 | 任何区域 |
严重程度分级
| 严重程度 | 标签 | 描述 | 行动 |
|---|
| 1 | 健康 | 无损伤或仅有外观标记 | 继续正常运行 |
| 2 |
轻微 | 早期侵蚀,表面裂纹,涂层脱落 | 增加检测频率 |
| 3 | 中等 | 胶衣破损,早期脱粘,明确损伤 | 1-3个月内维修 |
| 4 | 显著 | 结构涉及,活跃脱粘,雷击 | 2-4周内维修 |
| 5 | 严重 | 纤维暴露,结构破损,分层 | 需立即停机 |
操作流程
- 1. 收集输入:叶片编号、检测方法、每个叶片每个区域每个表面的检查结果。
- 按损伤类型对每个检查结果进行分类。
- 使用严重程度分级为每个检查结果分配严重等级。
- 将单个叶片的整体严重程度确定为该叶片检查结果中的最高等级。
- 将风机级别的严重程度确定为所有叶片中的最高等级。
- 应用损伤特定规则:
- 雷击损伤:最低严重等级4,直至OEM确认其他情况。
- 前缘或后缘脱粘超过300毫米:升级至严重等级4。
- 任何确认的纤维暴露:最低严重等级4。
- 尖部跨度超过500毫米的完全胶衣脱落侵蚀:严重等级4。
- 活跃积冰:始终为严重等级4。
- 7. 使用以下格式生成输出报告。
输出格式
=== 叶片检测报告 ===
资产 : [风机编号]
场站 : [场站名称]
检测 : [日期 / 方法]
叶片 : [检测数量]
叶片 [编号]:
区域/表面 : [例如,尖部 / 前缘]
损伤类型 : [例如,侵蚀]
描述 : [例如,深度点蚀约600毫米跨度,胶衣完全脱落]
严重程度 : [1-5] - [标签]
叶片 [编号] 整体严重程度: [1-5] - [标签]
风机级别严重程度 : [1-5] - [标签]
停机建议: [是 / 否 / 视情况而定]
维修优先级:
- [例如,叶片2尖部前缘侵蚀 - 在6周内安排前缘保护维修]
监测策略:
- [例如,所有叶片每月进行无人机复检]
升级触发条件:
- [例如,脱粘长度超过500毫米 - 停机维修]
- [例如,SCADA振动或不平衡报警 - 风机停机]
损伤特定指导
侵蚀:从表面粗糙化发展到点蚀,再到胶衣脱落,最终纤维暴露。使用前缘保护(LEP)胶带或涂层进行维修。严重等级3-4会导致可测量的发电量损失。
雷击:始终通知OEM。轻微的可见损伤可能隐藏内部分层。在专家确认之前,不要假设可以安全运行。
脱粘:前缘脱粘会引起气动噪音和振动。后缘脱粘从尖部开始并向根部发展。粘接线间隙超过300毫米为严重等级4。
层压/结构损伤:纤维暴露始终至少为严重等级4。无纤维暴露的凹陷或屈曲为严重等级3。
积冰:活跃积冰因转子不平衡和抛冰风险需立即停机。融冰后,检查表面是否存在潜在损伤。
常见误区
- - 不要根据低分辨率图像分类侵蚀。要求提供特写区域照片。
- 雷击损伤的优先级始终高于其外观所示。在证实其他情况前,按严重等级4处理。
- 脱粘在无人机图像中可能不可见。如果SCADA显示不平衡报警,标记潜在的隐藏脱粘。
- 活跃积冰是安全隐患。建议立即停机。
- 独立评估每个叶片。损伤分布很少在所有三个叶片上均匀。
验证
生成报告后,与用户确认:
- - 严重程度是否与检查员的现场评估一致?
- 是否涵盖了所有三个叶片?
- 是否存在与检查结果相关的SCADA报警(振动、不平衡、功率曲线偏差)?
- 是否有之前的检测报告用于趋势比较?