Stress and Fatigue Characteristics for Fan Blade Locking Pins in High Bypass Modern Jet Engines

 Stress and Fatigue Characteristics for Fan Blade Locking Pins in High Bypass Modern Jet Engines

The fan blade locking pin in a high-bypass modern jet engine is a critical component subjected to various stresses and fatigue conditions.

Parameter	Description	Key Findings
Material Properties	Typically made of high-strength alloys like titanium (e.g., Ti-48Al-2Cr-2Nb) or intermetallic compounds.	Offers excellent high-temperature performance but can experience fretting fatigue at contact interfaces under cyclic loads.
Stress Sources	Centrifugal forces, aerodynamic forces, and vibrational loads.	Aerodynamic forces increase stress levels by 18% compared to centrifugal forces alone. Stress concentration areas are near the root or stiffener joints.
Stress Distribution	Axial, radial, and circumferential stresses vary along the locking pin geometry.	Maximum equivalent stresses occur near root or stiffener areas under combined aerodynamic and centrifugal loads.
Fatigue Mechanisms	Fretting fatigue, thermal fatigue, and cyclic loading.	Fatigue cracks nucleate at high-contact-pressure zones and propagate under cyclic stress, as confirmed by FEA and experimental studies.
Operating Conditions	High rotational speeds and elevated temperatures.	Increased temperature weakens material properties, accelerating fatigue crack growth.
Fatigue Life Considerations	Dependent on load cycles, material selection, and design margins.	A 10–20% margin between excitation force frequency and natural frequency prevents resonance-induced fatigue failure.
Failure Modes	Crack initiation and propagation due to stress concentration or resonance effects.	Resonance leads to sharp stress increases, causing fatigue fractures in locking pins and nearby components.
Surface Treatment	Shot peening, nitriding, or coatings to enhance fatigue resistance.	Reduces crack initiation and improves surface hardness, extending service life.
Inspection Methods	Non-destructive testing (NDT), ultrasonic, eddy current, and acoustic emission monitoring.	Ensures structural integrity, detects early fatigue signs, and validates FEA predictions.

 

1. Critical Stress Areas: The root and stiffener joints of the locking pin experience the highest stress concentrations.
2. Impact of Aerodynamics: Coupled aerodynamic and centrifugal forces significantly amplify stress levels.
3. Fatigue Mitigation: Proper material selection, surface treatments, and resonance avoidance strategies enhance durability.
4. Monitoring & Testing: Advanced NDT techniques help detect early fatigue failures, ensuring safe operation.