With the increasing utilization of braze repair in the gas turbine industry, the properties of braze joints under simulated service conditions become vital in selecting braze repair over other processes. While braze repair has often been claimed to deliver mechanical properties equivalent to that of the parent material, this is largely based on the results of tensile or accelerated creep tests for most gas turbine hot section components failure occurs as a result of thermal fatigue or thermomechanical fatigue. The damage that occurs under such conditions cannot be assessed from tensile or creep testing. This study was undertaken to characterize the fatigue properties of narrow and wide gap brazed X-40 cobalt-based superalloy and compare these properties to that of the X-40 parent material. Butt joint narrow gap and wide gap specimens were vacuum brazed using BNi-9 braze alloy. X-40 and IN-738 were used as additive materials in wide gap braze joints. To characterize the fatigue properties of the braze joints and parent material, isothermal fatigue tests were conducted at and under load control using a fully reversed sinusoidal wave form having stress amplitude of 75% of the yield strength of the parent material. The braze specimens were fatigue tested in the as-brazed condition. The fatigue test results showed that the fatigue lives of the brazed specimens were lower than that of the parent material, particularly for the narrow gap samples and wide gap samples containing IN-738 additive alloy. All fatigue failures in the brazed samples occurred in the braze joints. An analysis of the fracture surfaces using a scanning electron microscope revealed that porosity was the major contributing factor to fatigue failures in the wide gap braze joints. The testing life debit observed in the narrow gap braze samples can be attributed to the presence of brittle boride phases in the braze joint. This study also included examination of techniques for reducing the aforementioned porosity and presence of brittle intermetallic phases.
Skip Nav Destination
Article navigation
September 2011
Research Papers
Fatigue Properties of Narrow and Wide Gap Braze Repaired Joints
Thomas Henhoeffer,
Thomas Henhoeffer
Liburdi Turbine Services Incorporated
, Dundas, ON L9H 7K4, Canada
Search for other works by this author on:
Xiao Huang,
Xiao Huang
Department of Mechanical and Aerospace Engineering,
Carleton University
, Ottawa, ON K1S 5B6, Canada
Search for other works by this author on:
Scott Yandt,
Scott Yandt
Institute for Aerospace Research,
National Research Council
, Ottawa, ON K1A 0R6, Canada
Search for other works by this author on:
Peter Au
Peter Au
Institute for Aerospace Research,
National Research Council
, Ottawa, ON K1A 0R6, Canada
Search for other works by this author on:
Thomas Henhoeffer
Liburdi Turbine Services Incorporated
, Dundas, ON L9H 7K4, Canada
Xiao Huang
Department of Mechanical and Aerospace Engineering,
Carleton University
, Ottawa, ON K1S 5B6, Canada
Scott Yandt
Institute for Aerospace Research,
National Research Council
, Ottawa, ON K1A 0R6, Canada
Peter Au
Institute for Aerospace Research,
National Research Council
, Ottawa, ON K1A 0R6, CanadaJ. Eng. Gas Turbines Power. Sep 2011, 133(9): 092101 (7 pages)
Published Online: April 15, 2011
Article history
Revised:
July 15, 2010
Received:
July 15, 2010
Online:
April 15, 2011
Published:
April 15, 2011
Citation
Henhoeffer, T., Huang, X., Yandt, S., and Au, P. (April 15, 2011). "Fatigue Properties of Narrow and Wide Gap Braze Repaired Joints." ASME. J. Eng. Gas Turbines Power. September 2011; 133(9): 092101. https://doi.org/10.1115/1.4002824
Download citation file:
Get Email Alerts
Cited By
On Leakage Flows In A Liquid Hydrogen Multi-Stage Pump for Aircraft Engine Applications
J. Eng. Gas Turbines Power
A Computational Study of Temperature Driven Low Engine Order Forced Response In High Pressure Turbines
J. Eng. Gas Turbines Power
The Role of the Working Fluid and Non-Ideal Thermodynamic Effects on Performance of Gas Lubricated Bearings
J. Eng. Gas Turbines Power
Tool wear prediction in broaching based on tool geometry
J. Eng. Gas Turbines Power
Related Articles
Case Studies of Fatigue Life Improvement Using Low Plasticity Burnishing in Gas Turbine Engine Applications
J. Eng. Gas Turbines Power (October,2006)
Life Prediction Method of CC and DS Ni Base Superalloys Under High Temperature Biaxial Fatigue Loading
J. Eng. Gas Turbines Power (November,2010)
High-Temperature Fatigue/Creep/Environment Interactions in Compressor Alloys
J. Eng. Gas Turbines Power (January,2003)
Coupled Thermomechanical Fatigue Tests for Simulating Load Conditions in Cooled Turbine Parts
J. Eng. Gas Turbines Power (May,2012)
Related Proceedings Papers
Related Chapters
In Situ Observations of the Failure Mechanisms of Hydrided Zircaloy-4
Zirconium in the Nuclear Industry: 20th International Symposium
Fatigue Testing of Hydrogen-Exposed Austenitic Stainless Steel Welded Samples
International Hydrogen Conference (IHC 2012): Hydrogen-Materials Interactions
A Novel Low Frequency Fatigue Testing Method in High Pressure Hydrogen Environment
International Hydrogen Conference (IHC 2016): Materials Performance in Hydrogen Environments