Zobrazeno 1 - 10
of 10
pro vyhledávání: '"P. T. Kantzos"'
Publikováno v:
International Journal of Fatigue. 150:106328
Machining parameters can influence fatigue life by altering residual stresses, cold work and surface roughness. A study was performed to examine the effect of various broaching machining parameters on high temperature fatigue lives of a nickel-based
Publikováno v:
Volume 7A: Structures and Dynamics.
An isothermal model for creep rupture prediction of equiaxed gas turbine airfoils is presented. It provides a family of curves linear in log-log space between applied tensile stress and rupture time. Each curve represents a specific temperature. The
Publikováno v:
International Journal of Fatigue. 33:1111-1117
An innovative procedure is presented here for determining the minimum low cycle fatigue (LCF) life of turbine disk bores under multiaxial states of stress. The procedure statistically combines multiaxial data from spin pit tests with the data from un
Publikováno v:
International Journal of Fatigue. 33:414-426
Mechanical property requirements vary with location in nickel-based superalloy disks. To maximize the associated mechanical properties, heat treatment methods have been developed for producing tailored microstructures. In this study, a specialized he
Autor:
T. Biles, Tim Gabb, Robert L. Barrie, Jack Telesman, P. T. Kantzos, A. Prescenzi, Peter J. Bonacuse
Publikováno v:
Materials Science and Engineering: A. 474:71-81
The fatigue lives of modern powder metallurgy disk alloys can be reduced over an order of magnitude by cracking at inherent non-metallic inclusions. The objective of this work was to study the effectiveness of shot peening in suppressing LCF crack in
Publikováno v:
Journal of Failure Analysis and Prevention. 7:56-65
Increasing service temperatures of gas turbine engines can improve performance and efficiency. Therefore, advanced alloys are being considered for higher-temperature applications than previously encountered. To support these higher-temperature applic
Publikováno v:
Practical Failure Analysis. 3:55-59
There is a need to increase the temperature capability of superalloy turbine disks to allow higher operating temperatures in advanced aircraft engines. When modifying processing and chemistry of disk alloys to achieve this capability, it is important
Publikováno v:
Volume 7A: Structures and Dynamics.
In a previous paper, a criterion for multiaxial lifing of turbine disk bores made from a nickel base super alloy, DP-718, was substantiated using results from spin pit testing of mini disks. In this paper, another turbine and compressor disk alloy, A
Publikováno v:
Superalloys 2012
Mechanical property requirements vary with location in nickel-based superalloy disks. In order to maximize the associated mechanical properties, heat treatment methods have been developed for producing tailored grain microstructures. In this study, f
Publikováno v:
Superalloys 2008 (Eleventh International Symposium).
The Versatile Affordable Advanced Turbine Engine (VAATE) program has been supporting the development of Alloy 10, a gasatomized powder metal (PM) superalloy. Funding for the program was provided by U.S. Air Force Research Laboratory (AFRL). Honeywell