Gas Turbine Monitoring – Stator Vane Cracking

12.6.3.4 Remedies for HCF Damage [Aeroengine Safety]

Minimising The Cost of Gas Turbine Failure Through Performance

12.6.3.3 Damage due to HCF [Aeroengine Safety]

Parametric Analysis of Variable Stator Vane System in Gas Turbines

Nozzle Vane - an overview

Analysis of the effects of simplifications on the state of loads

Asset Management - Specialized Protection

25.2.2.1 Outer indications: Visual, noise, smell, temperatures and

21.1 Limits of reparability [Aeroengine Safety]

Generator Stators & Field Rewinds Plus Modified Hot Gas Path

Hardness test results of the fractured turbine blade.

Advances in inspection technologies benefit users – Combined Cycle

Crack and Erosion on the leading and trailing edge