Properties, Weldability, and Applications of Modern Wrought Heat-Resistant Alloys for Aerospace and Power Generation Industries

Author:

Rowe M. D.1,Ishwar V. R.1,Klarstrom D. L.1

Affiliation:

1. Haynes International, Inc., 1020 W. Park Avenue, Kokomo, IN 46904-9013

Abstract

Alloy selection and alloy design both require consideration of an array of material attributes, including in-service properties, weldability, and fabricability. Critical properties of modern heat-resistant alloys for gas turbine applications include high-temperature strength, thermal stability, oxidation resistance, and fatigue resistance. In this paper, the properties of 12 solid-solution-strengthened and six age-hardenable heat-resistant alloys are compared. Weldability is an important attribute and can be a major limiting factor in the use of certain alloys. Weldability test methods are discussed, and the resistance of alloys to solidification cracking and strain-age cracking is compared. The use of weldability testing in the development of modern heat-resistant alloys is discussed with several examples cited. Finally, alloy selection for gas turbine components is outlined, taking into account both alloy properties and fabricability.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference16 articles.

1. Effects of Aging on the Low Cycle Fatigue Behavior of Three Solid-Solution-Strengthened Superalloys;Klarstrom

2. Srivastava, S. K. , 1996, Haynes International Technical Report No. 13866.

3. Studies on Repair Welding Age-Hardenable Nickel-Base Alloys;Lepkowski;Weld. J. (Miami, FL, U. S.)

4. Welding Evaluation of High Temperature Sheet Materials by Restrained Patch Testing;Weiss;Weld. J. (Miami, FL, U. S.)

5. Practical Solutions to Strain-Age Cracking of Rene 41;Thompson;Weld. J. (Miami, FL, U. S.)

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