A newly-developed
aviation electronic product hardware comprehensive FMECA method comprises the first step of defining a
system to be analyzed, the second step of determining fault
modes and reasons of appointed
layers of a product based on a fault information
database, fault mechanism analyzing and a fault module
exposure test method, the third step of acquiring fault effects based on a fault
simulation analytical method, the fourth step of carrying out the quantification
hazard analysis, taking the
multiple fault effects caused by the redundancy design into consideration and providing a quantification
hazard analyzing method based on the
multiple fault effects, and the fifth step of
filling in an FMECA table and filling the fault
modes, the reasons, the effect and the
hazard degree all of which are acquired through analyzing into the FMECA table. The newly-developed
aviation electronic product hardware comprehensive FMECA method is a hardware FMECA method based on the fault information
database, fault mechanism analyzing, fault mode
exposure testing, fault simulating and analyzing and the
multiple fault effects, and is capable of providing more objective quantification for design and analyze workers and providing a basis for the
design improvement on electronic products.