A fractured motor shaft of an air cooler was sent to the laboratory to analyse the cause of failure. Investigation revealed that the shaft has failed by fatigue. Multiple fatigue cracks have originated at the fillet of the change of section and progressed over about 90% of the shaft cross section before giving way to torsional overload failure. The fatigue crack initiation appears to be due to stress concentrations arising from the sharp edges of the undercut at the fillet of the change of section. The problem appears to have further aggravated due to superimposed bending stresses on the shaft
A failed reduction gear shaft of indigenous rotary engine was sent to this laboratory for investigat...
The 9th stage turbine blade has failed by fatigue. The fatigue crack had initiated at the fillet of ...
Fractured 1st stage compressor blade and LPTR shaft belonging to an aeroengine were brought to the l...
A fractured motor shaft of an air cooler was sent to the laboratory to analyse the cause of failure....
The damaged/failed compressor stator and rotor blades of an aeroengine were analyzed. All the blades...
All the compressor stator blades of aeroengine referred to the laboratory were found to have failed ...
The cause for the failure of an air compressor has been investigated. It was found that a pre-existi...
There was an incidence to an aircraft wherein the pilot heard a loud bang on accelerating throttle t...
The hold down bolt of the fans of an air cooler has failed by fatigue. Investigation showed that jam...
AbstractThis paper investigates the failure of a rocker arm shaft of a passenger car. The shaft fail...
Following an incidence in an aeroengine, two compressor stator blades belonging to stage II and III ...
A fractured Air Turbine Starter (ATS) quill shaft was forwarded to the laboratory for analysis. The ...
A few fractured bolts recovered from an in flight incident of an aircraft were received for analysi...
AbstractThis paper reports the results of failure analysis of a two high gearbox shaft of a gearbox ...
Three failed compressor rotor blades, one from first stage and the other two from second stage, bel...
A failed reduction gear shaft of indigenous rotary engine was sent to this laboratory for investigat...
The 9th stage turbine blade has failed by fatigue. The fatigue crack had initiated at the fillet of ...
Fractured 1st stage compressor blade and LPTR shaft belonging to an aeroengine were brought to the l...
A fractured motor shaft of an air cooler was sent to the laboratory to analyse the cause of failure....
The damaged/failed compressor stator and rotor blades of an aeroengine were analyzed. All the blades...
All the compressor stator blades of aeroengine referred to the laboratory were found to have failed ...
The cause for the failure of an air compressor has been investigated. It was found that a pre-existi...
There was an incidence to an aircraft wherein the pilot heard a loud bang on accelerating throttle t...
The hold down bolt of the fans of an air cooler has failed by fatigue. Investigation showed that jam...
AbstractThis paper investigates the failure of a rocker arm shaft of a passenger car. The shaft fail...
Following an incidence in an aeroengine, two compressor stator blades belonging to stage II and III ...
A fractured Air Turbine Starter (ATS) quill shaft was forwarded to the laboratory for analysis. The ...
A few fractured bolts recovered from an in flight incident of an aircraft were received for analysi...
AbstractThis paper reports the results of failure analysis of a two high gearbox shaft of a gearbox ...
Three failed compressor rotor blades, one from first stage and the other two from second stage, bel...
A failed reduction gear shaft of indigenous rotary engine was sent to this laboratory for investigat...
The 9th stage turbine blade has failed by fatigue. The fatigue crack had initiated at the fillet of ...
Fractured 1st stage compressor blade and LPTR shaft belonging to an aeroengine were brought to the l...