Repairing Gas Turbine Hot Section Airfoils Today

821487

02/01/1982

Event
Aerospace Congress and Exposition
Authors Abstract
Content
The team approach to development and application of repair techniques for gas turbine hot section airfoils can be effective in achieving goals of product safety, conservation of critical materials, thermal protection and operational cost control. This concept is explored and various repair techniques and processes are described as well as is their interrelation. Included is the application of hot-isostatic-pressing, diffusion joining, controlled chamber tungsten inert gas welding, electrical discharge machining, laser drilling, electro-chemical machining, abrasive flow machining, airfoil replacement and blade tip sulfidation repair. Protective coatings considered are low pressure plasma spray, physical vapor deposition, platinum aluminide pack coating and overcoating. An example of cost effectiveness is presented.
Repair engineering can extend useful life of hot section airfoils without compromising safety, critical materials and cost considerations.
Meta TagsDetails
DOI
https://doi.org/10.4271/821487
Pages
8
Citation
Wilkens, J., "Repairing Gas Turbine Hot Section Airfoils Today," SAE Technical Paper 821487, 1982, https://doi.org/10.4271/821487.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
821487
Content Type
Technical Paper
Language
English