DocumentCode
1769902
Title
Highly Accelerated Life Testing for avionics devices
Author
Catelani, Marcantonio ; Ciani, Lorenzo
Author_Institution
Dept. of Inf. Eng., Univ. of Florence, Florence, Italy
fYear
2014
fDate
29-30 May 2014
Firstpage
418
Lastpage
422
Abstract
In avionics application one of the most important competition factors is the reliability, given that the failure occurrence may leads to a critical state for the functioning of the aircraft. Some avionics apparatus are intolerant of failures, as lives may depend on the reliable functioning of equipment. Highly Accelerated Life Testing (HALT) is a time compression testing protocol that utilizes a step stress approach in subjecting products to varied thermal and vibration stresses. It is used to uncover design limitations and weaknesses in the preliminary design phase, helping designers to find and fix errors before they occur during the application in the field. The goal of HALT testing is to break the product by subjecting the test unit to progressively higher stress levels, incorporating thermal dwells, rapid temperature transitions, varied vibration stresses, and a combination of temperature and vibration to precipitate inherent defects. In this paper the HALT process related to an avionic equipment is described and a specific test plant is discussed.
Keywords
aircraft testing; avionics; failure analysis; life testing; reliability; thermal stresses; vibrations; HALT testing; avionic equipment; avionics devices; failure occurrence; highly accelerated life testing; reliability; step stress approach; temperature transitions; test plant; thermal dwells; thermal stresses; time compression testing protocol; vibration stresses; Aerospace electronics; Life estimation; Reliability engineering; Stress; Testing; Vibrations; HALT; Highly Accelerated Life Testing; avionics; reliability;
fLanguage
English
Publisher
ieee
Conference_Titel
Metrology for Aerospace (MetroAeroSpace), 2014 IEEE
Conference_Location
Benevento
Type
conf
DOI
10.1109/MetroAeroSpace.2014.6865961
Filename
6865961
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