Author: Stephen D. Antolovich
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
The LCF(Low Cycle Fatigue) behavior of Ni base superalloys was studied both for smooth and notched test bars. The primary research material was Rene 80 which finds application in turbine blades used in the temperature range of 650-982 C (1200-1800 F). The smooth bar LCF behavior was studied in the as-heat treated condition and also after exposure for 100h at 982 C, either under a stress of 97 MPa (14 ksi) or OMPa. Test conditions included continuous cycling at different strain rates as well as 90 second hold periods at either maximum or minimum strain. The primary test temperatures were 871 C (1600 F) and 982 C (1800 F). It was found that prior exposure greatly reduces the fatigue life. Since these experiments tend to duplicate actual engine conditions, use of data obtained using as-heat treated specimens may be very non-conservative to predict lives of actual components. The test results correlated very well with a model for LCF which is based on the concept that cracks initiate at a critical combination of oxide depth and stress. The notch LCF problem was also studied. A computer model for calculating local stresses and strains was developed. In addition to the Rene 80 studies, some initial smooth bar LCF studies were carried out using Rene 77.
Microstructural Effects and Fatigue Life Predictions of Notched and Un-notched Ni Base Superalloys at Elevated Temperatures
Author: Stephen D. Antolovich
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
The LCF(Low Cycle Fatigue) behavior of Ni base superalloys was studied both for smooth and notched test bars. The primary research material was Rene 80 which finds application in turbine blades used in the temperature range of 650-982 C (1200-1800 F). The smooth bar LCF behavior was studied in the as-heat treated condition and also after exposure for 100h at 982 C, either under a stress of 97 MPa (14 ksi) or OMPa. Test conditions included continuous cycling at different strain rates as well as 90 second hold periods at either maximum or minimum strain. The primary test temperatures were 871 C (1600 F) and 982 C (1800 F). It was found that prior exposure greatly reduces the fatigue life. Since these experiments tend to duplicate actual engine conditions, use of data obtained using as-heat treated specimens may be very non-conservative to predict lives of actual components. The test results correlated very well with a model for LCF which is based on the concept that cracks initiate at a critical combination of oxide depth and stress. The notch LCF problem was also studied. A computer model for calculating local stresses and strains was developed. In addition to the Rene 80 studies, some initial smooth bar LCF studies were carried out using Rene 77.
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
The LCF(Low Cycle Fatigue) behavior of Ni base superalloys was studied both for smooth and notched test bars. The primary research material was Rene 80 which finds application in turbine blades used in the temperature range of 650-982 C (1200-1800 F). The smooth bar LCF behavior was studied in the as-heat treated condition and also after exposure for 100h at 982 C, either under a stress of 97 MPa (14 ksi) or OMPa. Test conditions included continuous cycling at different strain rates as well as 90 second hold periods at either maximum or minimum strain. The primary test temperatures were 871 C (1600 F) and 982 C (1800 F). It was found that prior exposure greatly reduces the fatigue life. Since these experiments tend to duplicate actual engine conditions, use of data obtained using as-heat treated specimens may be very non-conservative to predict lives of actual components. The test results correlated very well with a model for LCF which is based on the concept that cracks initiate at a critical combination of oxide depth and stress. The notch LCF problem was also studied. A computer model for calculating local stresses and strains was developed. In addition to the Rene 80 studies, some initial smooth bar LCF studies were carried out using Rene 77.
Microstructural Effects and Fatigue Life Predictions of Notched and Un-notched Nickel Base Superalloys at Elevated Temperatures
Author: Stephen D. Antolovich
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
The low cycle fatigue (LCF) of Rene 80 has been investigated at 1400, 1600 and 1800 F. Emphasis has been placed on the 1800 F studies using smooth bar (continuous cycling and 90 sec hold time) and notch LCF specimens. The detailed transmission electron microscopy shows that at 1600 and 1800 F the dislocation debris is independent of test rate over two orders of magnitude. The test results can not be explained in terms of the conventional approaches to high temperature LCF for which damage is assumed to result from creep/fatigue interactions. Instead, it is suggested that the important damage mechanism is an interaction between the deformation mode and the environment. Based on that understanding a model is developed for crack propagation at elevated temperatures and a similar model is being developed for crack initiation. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
The low cycle fatigue (LCF) of Rene 80 has been investigated at 1400, 1600 and 1800 F. Emphasis has been placed on the 1800 F studies using smooth bar (continuous cycling and 90 sec hold time) and notch LCF specimens. The detailed transmission electron microscopy shows that at 1600 and 1800 F the dislocation debris is independent of test rate over two orders of magnitude. The test results can not be explained in terms of the conventional approaches to high temperature LCF for which damage is assumed to result from creep/fatigue interactions. Instead, it is suggested that the important damage mechanism is an interaction between the deformation mode and the environment. Based on that understanding a model is developed for crack propagation at elevated temperatures and a similar model is being developed for crack initiation. (Author).
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1018
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1018
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 870
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 870
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 228
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 228
Book Description
Fatigue Life
Author: V. S. Goel
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 440
Book Description
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 440
Book Description
Aerospace Structural Metals Handbook
Author:
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 828
Book Description
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 828
Book Description
CAB
Author:
Publisher:
ISBN:
Category : Ceramics
Languages : en
Pages : 528
Book Description
Publisher:
ISBN:
Category : Ceramics
Languages : en
Pages : 528
Book Description
Metals Abstracts
Author:
Publisher:
ISBN:
Category : Metallurgy
Languages : en
Pages : 1602
Book Description
Publisher:
ISBN:
Category : Metallurgy
Languages : en
Pages : 1602
Book Description
Aerospace Structural Metals Handbook
Author: Belfour Stulen, Inc. Mechanical Properties Data Center
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 860
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 860
Book Description