Add to ORKGAdvanced disk structural concepts were employed to improve the cyclic lives and reliability of turbine disks. Analytical studies were conducted to evaluate bore-entry disks as potential replacements for the existing first-stage turbine disks in the CF6-50 and JT8D-17 engines. Results of low cycle fatigue, burst, fracture mechanics, and fragment energy analyses are summarized for the advanced disk designs and the existing disk designs, with both conventional and advanced disk materials. Other disk concepts such as composite, laminated, link, multibore, multidisk, and spline disks were also evaluated for the CF6-50 engine
Turbine disks are required to operate at a high temperature environment and rotate at high velocity ...
Flywheel safety and containment design technology are discussed. The effects of axial loading result...
In support of the preliminary evaluation of various engine technologies, a methodology has been deve...
Results of analytical studies to improve the low cycle fatigue lives and reliability of turbine disk...
An analytical study was performed on a novel disk design to replace the existing high-pressure turbi...
An analytical study was conducted on a bore entry cooled turbine disk for the first stage of the JT8...
Over the past decade, aircraft readiness rates have declined, spare parts have been in short supply,...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Design considerations, objectives, and approaches used in containing rotor burst debris are discusse...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
Two series of low cycle fatigue (LCF) test data for two groups of different aircraft gas turbine eng...
Environmental attack has the potential to limit turbine disk durability, particularly in next genera...
Turbine disks are required to operate at a high temperature environment and rotate at high velocity ...
Flywheel safety and containment design technology are discussed. The effects of axial loading result...
In support of the preliminary evaluation of various engine technologies, a methodology has been deve...
Results of analytical studies to improve the low cycle fatigue lives and reliability of turbine disk...
An analytical study was performed on a novel disk design to replace the existing high-pressure turbi...
An analytical study was conducted on a bore entry cooled turbine disk for the first stage of the JT8...
Over the past decade, aircraft readiness rates have declined, spare parts have been in short supply,...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Design considerations, objectives, and approaches used in containing rotor burst debris are discusse...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
Two series of low cycle fatigue (LCF) test data for two groups of different aircraft gas turbine eng...
Environmental attack has the potential to limit turbine disk durability, particularly in next genera...
Turbine disks are required to operate at a high temperature environment and rotate at high velocity ...
Flywheel safety and containment design technology are discussed. The effects of axial loading result...
In support of the preliminary evaluation of various engine technologies, a methodology has been deve...