Life extension of high cost components until measurable damage is detected can result in marked reductions in total cycle costs. The life extension strategy for turbine disks is based upon nondestructive inspection to detect defects, usage and stress analysis to define requirements, and fracture mechanics analysis and testing to evaluate the severity of any defects under future usage. Because there are uncertainties and inaccuracies in the inspection, analysis, testing and definition of past and future usage, the selection of the optimum life extension strategy requires quantitative evaluation of the costs and risks associated with each uncertainty during life extension. This paper summarizes recent developments in the basic methodologies n...
The fir-tree-root-fillets of turbine blades are prone to fatigue cracking on the notch surfaces and ...
The ability to perform accurate remnant life predictions is crucial to ensure the integrity of engin...
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...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
This paper describes the results of a case study on the use of physics based prognosis to deal with ...
Turbine engine disk life prediction and understanding the associated risk remains a significant chal...
Over the past decade, aircraft readiness rates have declined, spare parts have been in short supply,...
LecturePg. 85-92The approach and methodology to life assessment/extension are described. Items consi...
There is an economic need to extend the fatigue life of turbine engine rotor disks. The probability ...
Current Federal Aviation Administration (FAA) rotor design certification practices risk assessment u...
The damage tolerance-based life prediction concepts proposed for gas turbine components are explaine...
Prognostics and health monitoring (PHM) technology needs to be developed to meet the challenges pose...
Historically, cyclic life limited gas turbine engine components have been retired when they reach an...
The fir-tree-root-fillets of turbine blades are prone to fatigue cracking on the notch surfaces and ...
The ability to perform accurate remnant life predictions is crucial to ensure the integrity of engin...
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...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
This paper describes the results of a case study on the use of physics based prognosis to deal with ...
Turbine engine disk life prediction and understanding the associated risk remains a significant chal...
Over the past decade, aircraft readiness rates have declined, spare parts have been in short supply,...
LecturePg. 85-92The approach and methodology to life assessment/extension are described. Items consi...
There is an economic need to extend the fatigue life of turbine engine rotor disks. The probability ...
Current Federal Aviation Administration (FAA) rotor design certification practices risk assessment u...
The damage tolerance-based life prediction concepts proposed for gas turbine components are explaine...
Prognostics and health monitoring (PHM) technology needs to be developed to meet the challenges pose...
Historically, cyclic life limited gas turbine engine components have been retired when they reach an...
The fir-tree-root-fillets of turbine blades are prone to fatigue cracking on the notch surfaces and ...
The ability to perform accurate remnant life predictions is crucial to ensure the integrity of engin...
Major cost savings are possible through life extension of high-cost jet engine components until dama...