Physics of Failure models are mathematically derived, deterministic models based on knowledge of failure mechanisms and the root causes of failures. Failure rates are predicted based on stresses, material properties, individual use and environmental conditions. Fixed Vanes are primarily used in fluid machines (turbines, pumps, and windmills etc.) and in aircraft (control surfaces) apart from a variety of other uses. Reliability for vanes is considered to be static, i.e. the reliability function is invariant of time. Failures are defined to be those set of data points wherein the stress random variable experienced by the component exceeds the strength random variable of the material of the component. Static models are used in events where failures occur due to (nearly) instantaneous loads and are not a consequence of any previous effects/ history. This research text utilizes the Physics of Failures approach to quantitatively predict the Reliability of Fixed Vanes for a range of applications and environments. Only the primary/ dominant failure mode is targeted in this text.
[1]
R. Oppermann.
Strength of materials, part 2, advanced theory and problems
,
1941
.
[2]
Ronald L. Huston,et al.
Practical Stress Analysis in Engineering Design
,
1982
.
[3]
A. Preussger,et al.
Reliability qualification of semiconductor devices based on physics‐of‐failure and risk and opportunity assessment
,
2002
.
[4]
Ted L. Lomax.
Structural loads analysis for commercial transport aircraft : theory and practice
,
1996
.
[5]
Singiresu S Rao,et al.
Reliability-Based Design
,
1992
.
[6]
M. J. Cushing,et al.
Comparison of electronics-reliability assessment approaches
,
1993
.
[7]
Lawrence G. Katz.
CLIMATOLOGICAL PROBABILITY OF AIRCRAFT ICING
,
1967
.
[8]
Efrén Moreno Benavides,et al.
Reliability-based design
,
2012
.