A number of materials issues related to the design of piping and support components in high-temperature fluidized bed combustor systems were examined. These issues included the availability of long-time design data on structural materials, the general character of the creep and stress rupture behavior, the performance of weldments, and the assessment of damage accumulation. Emphasis was placed on alloy 800H, but several other alloys were briefly examined for use at temperatures above 816°C (1500°F). It was concluded that the character of the creep curve ranged significantly with chemistry, processing variables, and environment, and that the specification of design allowable stresses and life estimation techniques must be approached with caution for service above 816°C (1500°F).
Skip Nav Destination
Article navigation
April 1994
Research Papers
Criteria for Design With Structural Materials in Combined-Cycle Applications Above 815°F
R. W. Swindeman,
R. W. Swindeman
Oak Ridge National Laboratory, Oak Ridge, TN 37831
Search for other works by this author on:
D. L. Marriott
D. L. Marriott
Stress Engineering Services, Cincinnati, OH 45246
Search for other works by this author on:
R. W. Swindeman
Oak Ridge National Laboratory, Oak Ridge, TN 37831
D. L. Marriott
Stress Engineering Services, Cincinnati, OH 45246
J. Eng. Gas Turbines Power. Apr 1994, 116(2): 352-359 (8 pages)
Published Online: April 1, 1994
Article history
Received:
March 3, 1993
Online:
April 24, 2008
Citation
Swindeman, R. W., and Marriott, D. L. (April 1, 1994). "Criteria for Design With Structural Materials in Combined-Cycle Applications Above 815°F." ASME. J. Eng. Gas Turbines Power. April 1994; 116(2): 352–359. https://doi.org/10.1115/1.2906827
Download citation file:
Get Email Alerts
Cited By
Study Of Tandem Rotor Dual Wake Interaction With Downstream Stator Under Unsteady Numerical Approach
J. Eng. Gas Turbines Power
An Efficient Uncertainty Quantification Method Based on Inter-Blade Decoupling for Compressors
J. Eng. Gas Turbines Power (April 2025)
Experimental Design Validation of a Swirl-Stabilized Burner With Fluidically Variable Swirl Number
J. Eng. Gas Turbines Power (April 2025)
Experimental Characterization of a Bladeless Air Compressor
J. Eng. Gas Turbines Power (April 2025)
Related Articles
Creep Lifetime Prediction of Alloy 617 Using Black Box Machine Learning Approach
J. Eng. Gas Turbines Power (April,2025)
Evaluation of the Creep Rupture Behavior of Alloy 690 Steam Generator Tubes Considering the Pressure Ramp Rate
J. Pressure Vessel Technol (February,2022)
Evaluation of Creep-Fatigue Damage Interaction in HK40 Alloy
J. Mech. Des (March,1993)
A Review on Current Status of Alloys 617 and 230 for Gen IV Nuclear Reactor Internals and Heat Exchangers
J. Pressure Vessel Technol (August,2009)
Related Proceedings Papers
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Basic Concepts
Design & Analysis of ASME Boiler and Pressure Vessel Components in the Creep Range
Section III: Subsections NC and ND — Class 2 and 3 Components
Companion Guide to the ASME Boiler and Pressure Vessel Code, Volume 1, Fourth Edition