Maintenance in Service of High Temperature Parts
Abstract
Partial contents: Military Maintenance Policies and Procedures for High Temperature Parts; Engine Depot Maintenance Repair Technology; Maintenance Problems in Gas Turbine Components at the Royal Naval Aircraft Yard, Fleetlands; Maintenance Experience with Civil Aero Engines; Engine Component Retirement for Cause; Defects and Their Effect on the Behaviour of Gas Turbine Discs; A titanium Silicon Coating for Gas Turbine Blades; Influence des Traitements de Protection Sur les Properties Mechaniques des Pieces en Superalliage; Reconditionnement de Pieces Fixes du Turbine par Brasage Diffusion; Rejuvenation of used Turbine Blades by Hot Isostatic Pressing and Reheat Treatment; HIP processing - Potentials and Applications; Regeneration of the Creep Properties of a Cast Ni-Cr-Base Alloy; Repair and Regeneration of Turbine Blades, Vanes and Discs; A New Approach to the Weldability of Nickel-Base, As-Cast and Powder Metallurgy Superalloys; and Comments on the Maintenance in Service of High Temperature Components in Aircraft Jet Engines.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1982
- Accession Number
- ADA112549
Entities
Organizations
- AGARD