DocumentCode :
2743982
Title :
Tools available for implementing AVIP
Author :
Steinberg, Dave S.
Author_Institution :
Litton Guidance & Control Syst., Woodland Hills, CA, USA
fYear :
1988
fDate :
32477
Firstpage :
23
Lastpage :
31
Abstract :
Consideration is given to analysis and design techniques that are presently available for evaluating the mechanical design integrity of electronic equipment for reliable operation in severe thermal, vibration, and shock environments. These techniques can be considered as the tools that are required to implement an avionics integrity program (AVIP) successfully. These tools are a knowledge of fatigue damage, physical properties of materials, and methods for determining thermal and vibration forces and stresses. It is shown how these tools can be used to ensure the mechanical design integrity and reliability of the avionic equipment required to operate in harsh military environments for extended time periods
Keywords :
aircraft instrumentation; design engineering; fatigue; military systems; reliability; thermal shock; thermal stresses; vibrations; AVIP; analysis; avionic equipment; avionics integrity program; design; electronic equipment; fatigue damage; mechanical design integrity; military environments; reliability; shock environments; stresses; thermal stresses; vibration; Aerospace electronics; Control systems; Creep; Electronic equipment; Equations; Fatigue; Frequency; Temperature; Thermal stresses; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Dayton Chapter Symposium, 1988. Avionics Integrity Program., Ninth Annual IEEE/AESS
Conference_Location :
Dayton, OH
Type :
conf
DOI :
10.1109/DAYTON.1988.76014
Filename :
76014
Link To Document :
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