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Structural fatigue life prediction tech landscape 2026

Structural Fatigue Life Prediction Technology Landscape 2026 — PatSnap Insights
Innovation Intelligence

Structural fatigue life prediction is undergoing a fundamental architectural shift — from empirical damage rules to physics-constrained machine learning — mapped across 60+ patent and literature records spanning 2004 to 2025. Chinese institutions account for approximately 65% of recent filings, while Boeing, GE, and Rolls-Royce hold the deepest application-specific IP in the West.

PatSnap Insights Team Innovation Intelligence Analysts 12 min read
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Reviewed by the PatSnap Insights editorial team ·

The Three Technology Pillars Defining the Field

Structural fatigue life prediction encompasses the methods, models, and systems used to estimate when engineering components will fail under cyclic loading — and within the 60+ patent and literature records spanning 2004 to 2025 analyzed for this landscape, the field resolves into three principal technical pillars. Each addresses a different part of the prediction problem: physics provides the mechanistic foundation, machine learning extracts patterns from sensor data at scale, and hybrid models combine the strengths of both to achieve the extrapolation reliability required for safety-critical deployment.

60+
Patent & literature records analyzed (2004–2025)
65%
Of patent records from CN-jurisdiction filers in this dataset
21
CN patents among 32 records with identifiable jurisdictions
2023–25
Peak filing period for hybrid physics-ML models

The first pillar — physics-based damage modeling — is rooted in established frameworks such as the Palmgren-Miner linear damage rule, Paris-Erdogan crack growth laws, continuum damage mechanics (CDM), and energy density methods. These are well-represented in foundational literature dating from 2010 to 2020 and remain the primary reference framework for regulatory compliance in aviation and nuclear applications, according to published standards from EASA and structural integrity guidelines issued by ASTM International.

The second pillar — data-driven and machine learning models — encompasses support vector machines (SVM), gradient boosting, random forests, convolutional neural networks (CNN), long short-term memory (LSTM) networks, and Gaussian process regression (GPR). These dominate the most recent filings from 2020 to 2025 in this dataset and have been validated on diverse component populations ranging from GCr15 bearing steel in ultra-high-cycle regimes to PLA/TPU functionally graded materials under cyclic loading.

Remaining Useful Life (RUL) Prediction Defined

Remaining useful life (RUL) prediction estimates how much operational time a component has before it reaches a failure threshold under cumulative fatigue loading. A 2014 literature survey on Through-life Engineering Services (TES) formally classified RUL prediction techniques and mapped failure mechanisms to prediction approaches — providing the field’s first systematic taxonomy and laying the conceptual groundwork for modern hybrid prognostics architectures.

The third pillar — hybrid physics-informed data models — integrates sensor signals with mechanistic degradation models, Wiener-process stochastic frameworks, and mission-profile-aware life estimators. This cluster is explicitly identified as the fastest-growing segment in the 2023–2025 filing period within this dataset. Representative examples include Novity Inc.’s WO 2024 filing, which separates degradation into phases and applies machine learning only during the accelerated degradation phase, and Siemens Industry Software NV’s FEA-to-SWT-to-ML pipeline (US 2023), which uses finite element analysis-computed Smith-Watson-Topper parameters to train fatigue life prediction models grounded in physical surface mechanics.

The hybrid physics-informed data model cluster — integrating sensor signals with mechanistic degradation models and Wiener-process stochastic frameworks — is the fastest-growing segment in structural fatigue life prediction patent filings during the 2023–2025 period, based on analysis of 60+ patent and literature records spanning 2004 to 2025.

Two Decades of Innovation: From Palmgren-Miner to Deep Learning

The patent and literature publication dates in this dataset span 2004 to 2025, revealing a multi-decade technology arc with clear maturity inflection points that track the broader availability of computational power, sensor miniaturization, and machine learning frameworks.

Figure 1 — Structural Fatigue Life Prediction: Patent Filing Activity by Era (2004–2025)
Structural Fatigue Life Prediction Patent Filing Activity by Era (2004–2025) 0 5 10 15 Approx. filings ~5 ~12 ~35 Early Foundations 2004–2014 Mid-Stage 2015–2021 High Activity 2022–2025 Physics-based foundations ML integration begins Hybrid & PIML dominance
Approximate filing volumes by era within the 60+ record dataset: the 2022–2025 period accounts for roughly 35 records — more than the two preceding eras combined — driven primarily by Chinese academic-industrial filers working on hybrid and deep learning architectures.

The early foundations era (2004–2014) established the computer-assisted life tracking paradigm. Mitsubishi Heavy Industries filed a gas turbine component life management system as early as 2004 in the Canadian jurisdiction, linking operating history to crack growth limits for superalloy turbine components. Oracle International Corporation introduced the concept of accumulative stress parameters driving degradation models in US filings from 2011–2012. NASA published a decomposition technique in 2014 that separated the RUL problem into feature-to-damage and operational-conditions-to-damage-rate mappings — an architectural concept underlying many current hybrid approaches.

The mid-stage development era (2015–2021) saw established OEMs deepen their domain-specific IP. Rolls-Royce Corporation filed fracture mechanism map systems targeting turbine engine dwell conditions across US and EP jurisdictions (2015 and 2018). General Electric and GE Infrastructure Technology filed turbine component creep-life impact systems with physics-statistical hybrid outputs (US, WO, EP 2017–2019). Boeing’s first aircraft maintenance induction patents using onboard sensor-derived fatigue metrics appeared in US filings in 2020 and 2021. Deep learning approaches began appearing at scale from 2021, with Harbin Institute of Technology filing distributed fault prediction systems using degradation state architectures.

“Chinese institutions account for approximately 65% of patent records in this dataset, with filing dates concentrated in 2023–2025 — covering axes spindles, gearboxes, bearings, aerospace mechanisms, vector thrusters, electro-hydraulic actuators, and coating-substrate systems.”

The recent high-activity period (2022–2025) is defined by the volume and breadth of Chinese academic-industrial filings and the maturation of hybrid physics-ML architectures among Western technology companies. Siemens Industry Software NV’s machine-learning-based fatigue response prediction using FEA-generated virtual surface profiles and SWT parameters (WO 2021, US 2023) represents the most technically sophisticated Western hybrid filing in this dataset. Boeing’s maintenance induction system received continued active filings through 2025, demonstrating sustained R&D investment in fleet-level fatigue monitoring — a building block for aircraft digital twin deployments.

Gradient boosting machine learning models trained on ultra-high-cycle fatigue (UHCF) data for GCr15 bearing steel produced only one outlier beyond the triple error band, according to a 2023 literature study benchmarking gradient boosting and random forest models on UHCF metallic material datasets.

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Geographic and Assignee Landscape: Where the IP Is Being Filed

Among the 32 patent records with identifiable jurisdictions in this dataset, China (CN) dominates with 21 patents — approximately 65% of records — concentrated in 2023–2025 filings from universities, state-affiliated research institutes, and emerging technology companies. The United States accounts for 11 patents, held primarily by established aerospace, industrial, and software OEMs. PCT international (WO) filings number 3, indicating multinational coverage intent. EP (Europe) accounts for 2 filings, both from General Electric and Rolls-Royce, and CA (Canada) accounts for 1 filing from Mitsubishi Heavy Industries.

Figure 2 — Structural Fatigue Life Prediction Patent Jurisdiction Distribution (32 records with identified jurisdictions)
Structural Fatigue Life Prediction Patent Jurisdiction Distribution — CN, US, WO, EP, CA 0 10 21 21 11 3 2 1 CN US WO EP CA China United States PCT/WO Europe Canada
CN-jurisdiction filings account for 21 of 32 identifiable records (approximately 65%), dominated by Chinese universities and state-affiliated research institutes filing in the 2023–2025 period — compared to 11 US patents held primarily by Boeing, GE, Rolls-Royce, NEC, Oracle, and NASA.

The assignee landscape reveals a clear bifurcation in IP strategy. A small number of large Western OEMs — Boeing, GE, Rolls-Royce — hold deep, application-specific patents tied to particular component types: aircraft load-bearing joint areas, turbine creep-fatigue interaction, and engine disc dwell crack growth respectively. These are narrow but defensible patents where the specificity of the application makes them difficult to design around without entering the same domain. Siemens, Novity, Fanuc, Oracle, and NASA each hold single distinctive filings covering niche but important sub-fields, including robot joint cable fatigue estimation (Fanuc, US 2019) and the transferable hybrid prognostics framework that operates across application domains (Novity, WO 2024).

On the Chinese side, the ecosystem is broad and methodologically diverse. Institutions active in this dataset include Harbin Institute of Technology, Shanghai University, Yanshan University, Zhejiang University of Technology, Nanjing University of Technology, Central South University, Qingdao University of Technology, and Chongqing University — spanning aerospace mechanisms, heavy gearboxes, electro-hydraulic actuators, bearings, rotating machinery degradation, and deep learning architectures for multiaxial fatigue. According to innovation intelligence databases maintained by WIPO, China’s share of global mechanical engineering patent filings has grown substantially through 2024, consistent with the pattern observed in this dataset.

Key finding: IP strategy bifurcation

Innovation in structural fatigue life prediction is split between a small number of large Western OEMs holding deep, application-specific patents (Boeing: aircraft joints; GE: turbine creep-fatigue; Rolls-Royce: dwell crack growth) and a large and growing Chinese academic-industrial ecosystem producing broad, methodologically diverse filings — approximately 65% of patent records in this dataset originate from CN-jurisdiction filers.

Application Domains: Aerospace, Turbomachinery, Wind, and Beyond

Aerospace and aviation represent the largest single-domain cluster in this dataset by patent count. Boeing holds multiple active US patents for fleet-level structural fatigue monitoring of aircraft load-bearing joint areas using onboard sensor arrays, with filings active from 2020 through 2025. Applications span commercial aircraft maintenance scheduling and airworthiness management. The Shenyang Aircraft Design and Research Institute (AVIC) has filed a CN 2023 patent targeting aircraft structural detail fatigue life under superimposed high-cycle and low-cycle loadings — addressing a specific failure mode in combat aircraft structural design. Shanghai University filed BiLSTM-based rolling prediction of health indicators for space mechanism components under temperature stress relaxation (CN 2025).

Power generation and turbomachinery require thermomechanical fatigue (TMF) and creep-fatigue interaction modeling at high temperatures. GE Infrastructure Technology’s US 2017 filing generates physics-statistical hybrid life prediction models for turbine components. Tianjin University’s US 2023 filing combines pure creep and pure fatigue data to iteratively calculate oxidative, creep, and fatigue damage via a dichotomy method. Komatsu Ltd. filed a thermal fatigue life prediction system in CN 2025 that detects temperature cycles and plastic strain amplitude per cycle for construction and industrial machinery components. Mitsubishi Heavy Industries’ 2004 CA filing — the earliest in this dataset — established the paradigm of linking gas turbine operating history to crack growth limits in superalloy components.

Wind turbine blade fatigue presents distinct challenges: variable amplitude loading, large composite structures, and difficult offshore inspection access. Shenyang University of Technology’s US 2023 filing uses intrinsic dissipated energy and residual stiffness to generate S-N curves for composite spars containing manufacturing wrinkle defects — a common quality control challenge in blade production. A 2023 literature review examined durability and damage tolerance analysis (DADTA) frameworks adapted from aerospace specifically for wind blade trailing edge life management, reflecting the cross-domain technology transfer pattern noted by research institutions including those affiliated with NREL.

Heavy Industrial Machinery, Marine, and Robotics

Large bearings, gearboxes, spindles, and pumped storage units are active targets for Chinese academic and industrial filers. Qingdao University of Technology (CN 2025) filed a multi-scale fatigue feature extraction and dual-source fusion prediction model for high-power heavy-duty gearbox RUL. Okada Intelligent (Jiangsu) Co., Ltd. (CN 2025) filed multi-scenario feature vector fatigue damage accumulation modeling with dynamic operating condition switching for machine tool spindles. Nanjing University of Technology (CN 2025) filed a multi-model driven approach combining BiGRU data models with load-life mechanistic models for extra-large bearings across three degradation stages with mutually updating loss functions.

Marine and offshore structures are addressed through stochastic fracture mechanics approaches. A 2013 literature study applied Paris-Erdogan and Palmgren-Miner stochastic frameworks to petrochemical pipeline RUL estimation. Ocean University of China (CN 2024) filed a polynomial regression-based 3D crack front reconstruction method for marine structural fatigue assessment. A 2020 literature review examined the Unified Fatigue Life Prediction (UFLP) method for marine structures, incorporating all crack growth rate sensitivity factors into a single integrated fracture mechanics model. In robotics, Fanuc Corporation (US 2019) filed a life prediction apparatus for robot joint cables using encoder information from actuators — demonstrating how structural fatigue prediction has extended from macro-scale structures to electromechanical subcomponents.

The Boeing Company holds 4 active US patents for fleet-level structural fatigue monitoring of aircraft load-bearing joint areas using onboard sensor arrays, with patent filings spanning 2020 through 2025 — making it the highest-volume assignee in the structural fatigue life prediction dataset analyzed for this landscape.

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Six Emerging Directions Shaping Fatigue Prediction Through 2026

Based on filings dated 2023–2025 in this dataset, six forward vectors are actively forming the next generation of structural fatigue life prediction technology — each addressable through distinct R&D investment priorities.

1. Physics-Informed Machine Learning (PIML) Integration

Novity Inc.’s WO 2024 filing explicitly builds degradation models that integrate physics and machine learning by separating degradation into phases and applying ML only during the accelerated degradation phase where physics-based models lose accuracy — enabling the model to be transferred across different application domains. Siemens Industry Software NV’s FEA-to-SWT-to-ML pipeline (US 2023) achieves physical grounding by computing Smith-Watson-Topper parameters from virtual surface profiles generated through finite element analysis, then using these physics-derived inputs to train surface fatigue life prediction models. Yanshan University’s EHA system (PreDyn-ST model, CN 2025) visualizes spatiotemporal degradation dynamics with physical mechanism interpretation — specifically targeting electro-hydraulic actuators in aerospace applications.

2. Multi-Scenario and Mission-Profile-Aware Life Prediction

Okada Intelligent (Jiangsu) Co., Ltd. (CN 2025) and East China Jiaotong University (CN 2025) both address dynamic operating condition switching — constructing multi-dimensional feature contribution matrices and fatigue response curves for components transitioning between different load regimes. East China Jiaotong University introduces stress ratio and strength degradation coefficient into a nonlinear cumulative damage model for multi-level loading scenarios, directly addressing variable duty cycle equipment in manufacturing and transportation.

3. Explainable AI (XAI) for Degradation Assessment

Zhejiang University of Technology (CN 2024, CN 2025) explicitly targets interpretable rotating machinery life assessment, using Graph Convolutional Networks (GCN) with Wiener-process stochastic models and building loss functions centered on prediction uncertainty. This reflects regulatory pressure for auditability in safety-critical applications — a requirement increasingly signaled in structural integrity frameworks published by bodies including the FAA for aviation and the European nuclear sector for pressure vessel monitoring.

4. Coating-Substrate and Advanced Material Fatigue Systems

Sun Yat-sen University (CN 2025) filed a coating-substrate fatigue life prediction system that separately models uncoated base material, pre-cracked coated base material, and post-cracked coated base material using statistical volume element microstructure representations. The damage metric used is cyclic accumulated plastic slip, targeting aerospace thermal barrier coatings and industrial protective coatings — a regime not addressed by classical S-N or bulk crack growth approaches.

5. Fleet-Level Digital Twin Integration for Aircraft

Boeing’s continued active filings through 2025 (US 2025) demonstrate sustained investment in fleet-scale structural monitoring via onboard sensor networks at common load-bearing joint areas, with regression models connecting fatigue metrics to usage metrics across multiple in-service aircraft simultaneously. This sensor-prediction architecture is the foundational building block for aircraft structural digital twin deployments — a direction consistent with programs tracked by aerospace standards bodies including SAE International.

6. Ultra-High-Cycle and Long-Life Regime Prediction

East China University of Science and Technology (US 2024) addresses the UHCF regime — defined as beyond 10^8 cycles — under extreme environmental conditions by establishing defect-matrix-environment interaction mechanisms and environmental weakening coefficients. This regime is not adequately covered by classical S-N curves or Paris-Erdogan crack growth approaches, which were validated predominantly on low-cycle and high-cycle fatigue data. A 2023 literature study benchmarked gradient boosting and random forest models specifically on UHCF data for GCr15 bearing steel, with gradient boosting producing only one outlier beyond the triple error band across the full dataset.

Strategic Implications for R&D and IP Teams

The structural fatigue life prediction landscape presents five concrete strategic implications for R&D leaders, patent counsel, and product development teams entering or operating in this space.

Physics-ML hybrid models are becoming the industry standard. Pure data-driven models are being superseded by architectures that inject physical constraints — SWT parameters, Paris law crack growth rates, Wiener process priors — to improve extrapolation reliability and reduce training data requirements. R&D teams should prioritize hybrid model development over standalone deep learning architectures.

Freedom-to-operate analysis in China is mandatory. With approximately 65% of patent records in this dataset originating from CN-jurisdiction filers — spanning universities, state-affiliated research institutes, and emerging companies — IP strategists entering the space should conduct freedom-to-operate analysis specifically in China, particularly for rotating machinery, spindle fatigue, bearing life, and sensor-integrated prognosis systems, where filing density in 2023–2025 is highest.

Application-specific specialization is the dominant commercial IP strategy. Leading OEMs — Boeing, GE, Rolls-Royce — hold narrow but defensible patents tied to specific component types rather than broad method patents. Entrants should identify underserved component categories or material classes — such as composite-metal hybrid structures or additive manufactured parts — to find white space not yet claimed by either Western OEMs or Chinese academic filers.

“Uncertainty quantification is a mandatory requirement for deployment in safety-critical markets. Multiple 2021–2025 filings explicitly incorporate uncertainty bounds, confidence scores, or prediction variance as core outputs — not as optional enhancements.”

Uncertainty quantification is a mandatory requirement. Multiple 2021–2025 filings — from Zhejiang University of Technology, East China Jiaotong University, and Yanshan University — explicitly incorporate uncertainty bounds, confidence scores, or prediction variance as core outputs. Product developers targeting safety-critical markets in aviation, nuclear, and offshore must include probabilistic life estimates rather than point predictions to meet regulatory auditability requirements.

Sensor integration is the enabling infrastructure bottleneck. From Boeing’s onboard sensor arrays (2020–2025) to Fanuc’s encoder-based cable fatigue estimator (2019) to the Qingdao-Harbin vector thruster system (2025), the quality of fatigue life prediction is increasingly constrained by sensor placement, data fusion architecture, and edge-compute capability. Sensor integration and embedded signal processing are equally critical R&D investment areas alongside the prediction algorithms themselves.

Dataset Scope Note

This landscape is derived from a targeted set of 60+ patent and literature records retrieved across focused searches spanning 2004 to 2025. It represents a snapshot of innovation signals within this dataset only and should not be interpreted as a comprehensive view of the full industry or as a complete freedom-to-operate analysis. A full competitive intelligence study using the complete PatSnap patent database will identify additional filings not captured in this snapshot.

Frequently asked questions

Structural fatigue life prediction — key questions answered

The three principal clusters are: (1) physics-based damage modeling using frameworks such as the Palmgren-Miner rule, Paris-Erdogan crack growth laws, and continuum damage mechanics; (2) data-driven and machine learning models including SVM, gradient boosting, CNN, LSTM, and Gaussian process regression; and (3) hybrid physics-informed data models that integrate sensor signals with mechanistic degradation models and stochastic frameworks. The hybrid cluster is identified as the fastest-growing segment in 2023–2025 filings within this dataset.

Within the 60+ patent and literature dataset analyzed, The Boeing Company leads with 4 US patents focused on aircraft fleet structural monitoring. GE / GE Infrastructure Technology and Rolls-Royce Corporation each hold 3 filings covering turbine creep-fatigue life and crack growth prediction respectively. NEC Corporation / NEC Laboratories also holds 3 filings on physical system aging profiling. Chinese institutions collectively account for approximately 65% of patent records, concentrated in 2023–2025.

Pure data-driven models are being superseded by hybrid architectures that inject physical constraints — such as SWT parameters, Paris law crack growth rates, and Wiener process priors — to improve extrapolation reliability and reduce training data requirements. Examples from this dataset include Siemens Industry Software NV’s FEA-to-SWT-to-ML pipeline (US 2023) and Novity Inc.’s phase-separated degradation model (WO 2024), which applies ML only during the accelerated degradation phase where physics-based models lose accuracy.

Among 32 patent records with identifiable jurisdictions in this dataset, CN (China) accounts for 21 patents — approximately 65% of records — concentrated in 2023–2025 filings from universities, state-affiliated research institutes, and emerging companies. The US accounts for 11 patents, WO (PCT international) for 3, EP (Europe) for 2, and CA (Canada) for 1 filing from Mitsubishi Heavy Industries.

Remaining useful life (RUL) prediction estimates how much operational time a component has before reaching a failure threshold under cumulative fatigue loading. A 2014 literature survey on Through-life Engineering Services formally classified RUL prediction techniques and mapped failure mechanisms to prediction approaches, providing the field’s first systematic taxonomy. Accurate RUL prediction enables condition-based maintenance scheduling that avoids both premature component replacement and catastrophic in-service failure — critical for aviation, power generation, and marine infrastructure operators.

Six forward vectors are active based on 2023–2025 patent filings in this dataset: (1) physics-informed machine learning integration; (2) multi-scenario and mission-profile-aware life prediction for variable duty cycle equipment; (3) explainable AI (XAI) for degradation assessment to meet regulatory auditability requirements; (4) coating-substrate and advanced material fatigue systems targeting thermal barrier coatings; (5) fleet-level digital twin integration for aircraft using onboard sensor networks; and (6) ultra-high-cycle fatigue (UHCF) prediction beyond 10^8 cycles under extreme environmental conditions.

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References

  1. Overview of Remaining Useful Life Prediction Techniques in Through-life Engineering Services — Literature, 2014
  2. A Review on Fatigue Life Prediction Methods for Metals — Literature, 2016
  3. Fatigue Life Prediction Method Based on Support Vector Machine — Shanghai Maritime University, 2012, CN
  4. A Method for Managing Lifespans of High Temperature Gas Turbine Components — Mitsubishi Heavy Industries, 2004, CA
  5. Decomposition Technique for Remaining Useful Life Prediction — NASA (US Government), 2014, US
  6. Using Fracture Mechanism Maps to Predict Time-Dependent Crack Growth Behavior Under Dwell Conditions — Rolls-Royce Corporation, 2018, US
  7. Systems and Methods for Determining Operational Impact on Turbine Component Creep Life — GE Infrastructure Technology LLC, 2017, US
  8. Maintenance Induction for Aircraft — The Boeing Company, 2020, US
  9. Maintenance Induction for Aircraft — The Boeing Company, 2025, US
  10. System and Method for Fatigue Response Prediction — Siemens Industry Software NV, 2023, US
  11. Transferable Hybrid Prognostics Based on Fundamental Degradation Modes — Novity, Inc., 2024, WO
  12. Life Prediction Apparatus — Fanuc Corporation, 2019, US
  13. Multi-Model Driven Life Prediction Method for Extra-Large Bearings at Different Degradation Stages — Nanjing University of Technology, 2025, CN
  14. A Real-Time Remaining Fatigue Life Prediction Approach Based on a Hybrid Deep Learning Network — Literature, 2023
  15. Machine Learning-Based Fatigue Life Prediction of Functionally Graded Materials Using Material Extrusion Technology — Literature, 2023
  16. Ultra-High-Cycle Fatigue Life Prediction of Metallic Materials Based on Machine Learning — Literature, 2023
  17. Gaussian Process for Machine Learning-Based Fatigue Life Prediction Model Under Multiaxial Stress-Strain Conditions — Literature, 2022
  18. A Probabilistic Fatigue Framework to Enable Location-Specific Lifing for Critical Thermo-mechanical Engineering Applications — Literature, 2021
  19. Durability and Damage Tolerance Analysis Approaches for Wind Turbine Blade Trailing Edge Life Prediction — Literature, 2023
  20. Recent Developments on the Unified Fatigue Life Prediction Method Based on Fracture Mechanics and its Applications — Literature, 2020
  21. Anti-Fatigue and Safety Control Method for Ultra-Long Life Service Structures Under Extreme Environment — East China University of Science and Technology, 2024, US
  22. Explainable Full-Lifecycle Service Performance Degradation Assessment Method for Rotating Machinery — Zhejiang University of Technology, 2024, CN
  23. Method and System for Predicting Creep-Fatigue Life of Structural Part of Thermal Power Unit — Tianjin University, 2023, US
  24. WIPO — World Intellectual Property Organization (patent filing trend data)
  25. ASTM International — Structural integrity and fatigue standards
  26. FAA — Federal Aviation Administration (structural integrity and airworthiness frameworks)
  27. NREL — National Renewable Energy Laboratory (wind turbine structural fatigue research)
  28. SAE International — Aerospace structural digital twin and fatigue standards
  29. PatSnap Patent Analytics — Innovation intelligence platform for IP and R&D teams
  30. PatSnap Competitive Intelligence — Technology landscape and competitor monitoring

All data and statistics in this article are sourced from the references above and from PatSnap‘s proprietary innovation intelligence platform. The patent and literature dataset analyzed comprises 60+ records spanning 2004 to 2025 and represents a snapshot of innovation signals only — not a comprehensive industry survey.

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