0
Article ? AI-assigned paper type based on the abstract. Classification may not be perfect — flag errors using the feedback button. Tier 2 ? Original research — experimental, observational, or case-control study. Direct primary evidence. Human Health Effects Policy & Risk Sign in to save

High Sensitive Methods for Health Monitoring of Compressor Blades and Fatigue Detection

The Scientific World JOURNAL 2013 26 citations ? Citation count from OpenAlex, updated daily. May differ slightly from the publisher's own count. Score: 40 ? 0–100 AI score estimating relevance to the microplastics field. Papers below 30 are filtered from public browse.
Mirosław Witoś

Summary

Researchers reviewed diagnostic approaches for detecting compressor blade fatigue, presenting methods for identifying low-cycle, high-cycle, and very-high-cycle fatigue modes along with the role of polycrystalline defects and surface finish in fatigue initiation. The study addresses practical maintenance challenges in identifying early-stage blade fatigue before catastrophic failure.

The diagnostic and research aspects of compressor blade fatigue detection have been elaborated in the paper. The real maintenance and overhaul problems and characteristic of different modes of metal blade fatigue (LCF, HCF, and VHCF) have been presented. The polycrystalline defects and impurities influencing the fatigue, along with their related surface finish techniques, are taken into account. The three experimental methods of structural health assessment are considered. The metal magnetic memory (MMM), experimental modal analysis (EMA) and tip timing (TTM) methods provide information on the damage of diagnosed objects, for example, compressor blades. Early damage symptoms, that is, magnetic and modal properties of material strengthening and weakening phases (change of local dislocation density and grain diameter, increase of structural and magnetic anisotropy), have been described. It has been proven that the shape of resonance characteristic gives abilities to determine if fatigue or a blade crack is concerned. The capabilities of the methods for steel and titanium alloy blades have been illustrated in examples from active and passive experiments. In the conclusion, the MMM, EMA, and TTM have been verified, and the potential for reliable diagnosis of the compressor blades using this method has been confirmed.

Sign in to start a discussion.

More Papers Like This

Article Tier 2

Corrosion Fatigue Analysis in Power Steam Turbine Blade

Researchers studied corrosion fatigue of steam turbine blades, finding saline environments caused pitting corrosion that accelerated crack initiation and reduced fatigue life.

Article Tier 2

Review of Fatigue Crack Initiation Mechanisms Development and Monitoring in the Very High Cycle Fatigue Regime

This review covers how fatigue cracks initiate and grow in materials under very high cycle loading conditions, with implications for engineering design. Understanding material fatigue mechanisms helps develop longer-lasting products that reduce the need for replacement, thereby reducing manufacturing waste and plastic use.

Article Tier 2

Highly Sensitive Nonlinear Identification to Track Early Fatigue Signs in Flexible Structures

Researchers developed a physics-based and data-driven nonlinear system identification approach for detecting and tracking early fatigue damage in flexible aluminum structures subjected to vibration. The method estimates nonlinear parameters including geometric stiffness and cubic damping as a function of fatigue cycles, enabling real-time structural health monitoring.

Article Tier 2

Methodology for Application of Damage Mechanics Approach to Model High Temperature Fatigue Damage Evolution in a Turbine Disc Superalloy

Researchers developed a damage mechanics methodology to model high-temperature fatigue damage evolution in a turbine disc superalloy, addressing the absence of established standards for this approach. Testing at 650°C enabled characterization of cyclic damage accumulation and material strength deterioration, providing a lifing framework for assessing fatigue life in aeroengine gas turbine components.

Article Tier 2

Fatigue Failure Assessment in Ultrasonic Test Based on Temperature Evolution and Crack Initiation Mechanisms

This study examined how temperature changes and crack formation can be used to detect fatigue failure in materials during ultrasonic testing. Researchers found that thermal imaging can identify fatigue damage earlier than conventional methods. The work advances non-destructive testing techniques for structural materials.

Share this paper