NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Braze Repair Possibilities for Hot Section Gas Turbine PartsOverlay braze repair is a good technique for restoring aircraft vanes and industrial blades and vanes. The negative effects of the intermetallic phase, formed during the overlay braze process, can be reduced in such a way that the mechanical properties - creep rupture, strength and ductility - can be achieved close to the properties of the base materials. The elimination of the negative effects can be achieved by a combination of careful selection of the chemistries of the repair materials and the application of the correct procedures for cleaning and heat cycle.
Document ID
19950013261
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
G Marijnissen (Interturbine Holding Lomm, Netherlands)
R van Gestel (Elbar Lomm, Netherlands)
Date Acquired
August 16, 2013
Publication Date
November 1, 1994
Publication Information
Publication: Erosion, Corrosion and Foreign Object Damage Effects in Gas Turbines
Publisher: North Atlantic Treaty Organization
ISBN: 9283600053
DOI: 10.14339/AGARD-CP-558
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
AGARD-CP-558
Meeting Information
Meeting: Propulsion and Energetics Panel (PEP) Symposium
Location: Rotterdam
Country: NL
Start Date: April 25, 1994
End Date: April 28, 1994
Sponsors: North Atlantic Treaty Organization
Accession Number
95N19677
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19950013237Collected WorksErosion, Corrosion and Foreign Object Damage Effects in Gas Turbines [Les consequences de l'endommagement des turbines I gaz par erosion, corrosion et objets étrangers]
No Preview Available