This paper describes the results of a case study on the use of physics based prognosis to deal with the uncertainty of disc failures in a fleet of forty two W-101 turbines. The MIL-STD-1783 based damage tolerance analysis is used to predict a safe inspection interval for the design life expired discs. It is demonstrated that safe inspection interval limits based on traditional empirical methods are overly optimistic under creep crack propagation conditions and it is necessary to use physics based crack propagation models to make reliable life cycle management decisions. Physics based crack propagation approaches yield substantially more accurate results. It is further demonstrated that the use of sensitive inspection techniques at depot lev...
Gas turbine discs are heavily loaded due to centrifugal and thermal loads and are therefore designed...
This paper describes the destructive inspection analyses of cracks growing from firtree serrations o...
LecturePg. 105-110This paper describes the application of a fracture mechanics-based procedure for l...
Prognostics and health monitoring (PHM) technology needs to be developed to meet the challenges pose...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
The damage tolerance-based life prediction concepts proposed for gas turbine components are explaine...
Rotor discs for gas turbines are heavy components usually designed following a safe-life approach, w...
Major cost savings are possible through life extension of high-cost jet engine components until dama...
Life extension of high cost components until measurable damage is detected can result in marked redu...
This paper describes the destructive inspection analyses of cracks growing from firtree serrations o...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
Current Federal Aviation Administration (FAA) rotor design certification practices risk assessment u...
This paper reports the results of a demonstration computer program carried out to determine the infl...
This paper reports the results of a demonstration programme carried out to determine the influence o...
Turbine engine disk life prediction and understanding the associated risk remains a significant chal...
Gas turbine discs are heavily loaded due to centrifugal and thermal loads and are therefore designed...
This paper describes the destructive inspection analyses of cracks growing from firtree serrations o...
LecturePg. 105-110This paper describes the application of a fracture mechanics-based procedure for l...
Prognostics and health monitoring (PHM) technology needs to be developed to meet the challenges pose...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
The damage tolerance-based life prediction concepts proposed for gas turbine components are explaine...
Rotor discs for gas turbines are heavy components usually designed following a safe-life approach, w...
Major cost savings are possible through life extension of high-cost jet engine components until dama...
Life extension of high cost components until measurable damage is detected can result in marked redu...
This paper describes the destructive inspection analyses of cracks growing from firtree serrations o...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
Current Federal Aviation Administration (FAA) rotor design certification practices risk assessment u...
This paper reports the results of a demonstration computer program carried out to determine the infl...
This paper reports the results of a demonstration programme carried out to determine the influence o...
Turbine engine disk life prediction and understanding the associated risk remains a significant chal...
Gas turbine discs are heavily loaded due to centrifugal and thermal loads and are therefore designed...
This paper describes the destructive inspection analyses of cracks growing from firtree serrations o...
LecturePg. 105-110This paper describes the application of a fracture mechanics-based procedure for l...