now doing this at work, Friday id PhD afternoon though
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@ -587,7 +587,8 @@ number={2},
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@INPROCEEDINGS{FMEAmultiple653556,
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@INPROCEEDINGS{FMEAmultiple653556,
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author={Price, C.J. and Taylor, N.S.},
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author={Price, C.J. and Taylor, N.S.},
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booktitle={Reliability and Maintainability Symposium, 1998. Proceedings., Annual}, title={FMEA for multiple failures},
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booktitle={Reliability and Maintainability Symposium, 1998. Proceedings., Annual},
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title={FMEA for multiple failures},
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year={1998},
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year={1998},
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month={jan},
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month={jan},
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volume={},
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volume={},
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@ -892,8 +892,13 @@ failures\footnote{Multiple simultaneous failures are taken to mean failures that
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Detection periods are typically determined for the process under control. For instance, for a flame detector in an industrial burner this
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Detection periods are typically determined for the process under control. For instance, for a flame detector in an industrial burner this
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is typically one second.~\cite{en298}}.
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is typically one second.~\cite{en298}}.
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%
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%
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Work has been performed using component failure statistics to
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Multiple failures may cause the same system level failure (i.e. two separate failures
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offer the more likely multiple failures~\cite{FMEAmultiple653556} for analysis.
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could cause the same system failure, and in combination still cause the same failure), this
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can be termed a common failure result.
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%
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Work has been performed using component failure statistics and logic to
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offer selected---by virtue of statistical likelihood and common failure result reduction---multiple failures for analysis
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and consideration by an investigating engineer~\cite{FMEAmultiple653556}.
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%
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%
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%We now compound the multiple symptoms from one {\bc} {\fm} possibility
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%We now compound the multiple symptoms from one {\bc} {\fm} possibility
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%with the merging of Markov chains.
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%with the merging of Markov chains.
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@ -906,7 +911,7 @@ meaning the additional failures might have to be analysed with respect to the ch
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%for the the results of an FMEA line of reasoning.
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%for the the results of an FMEA line of reasoning.
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Because multiple failures mean dealing with changed topologies
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Because multiple failures mean dealing with changed topologies
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the objective criteria is additionally complicated with the subjective
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the objective criteria is additionally complicated with the subjective
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adding another layer of complication.
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adding yet another layer of complication.
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%
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%
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%
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%
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Traditional FMEA has the translation from an objective to subjective
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Traditional FMEA has the translation from an objective to subjective
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@ -1137,7 +1142,7 @@ is given in section~\ref{sec:resistortolerance}.
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\item \textbf{FMECA - Criticality} Emphasis on minimising the effect of critical systems failing; % Military/Space
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\item \textbf{FMECA - Criticality} Emphasis on minimising the effect of critical systems failing; % Military/Space
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\item \textbf{FMEDA - Statistical Safety} Statistical analysis giving Safety Integrity Levels;
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\item \textbf{FMEDA - Statistical Safety} Statistical analysis giving Safety Integrity Levels;
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\item \textbf{DFMEA - Design or Static/Theoretical} Approval of safety critical systems using FMEA and single or double failure prevention;% EN298/EN230/UL1998
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\item \textbf{DFMEA - Design or Static/Theoretical} Approval of safety critical systems using FMEA and single or double failure prevention;% EN298/EN230/UL1998
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\item \textbf{SFMEA - Software FMEA --- only used in highly critical systems at present}
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\item \textbf{SFMEA - Software FMEA} --- Usage not enforced by most current standards~\cite{en298,en230,en61508}. %only used in highly critical systems at present.
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\end{itemize}
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\end{itemize}
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@ -1567,7 +1572,17 @@ so that the entry can be more easily reviewed or revisited/audited. % than a tra
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%
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%
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Because FMEA is traditionally performed with one entry per component {\fm}, full reasoning descriptions
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Because FMEA is traditionally performed with one entry per component {\fm}, full reasoning descriptions
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are rare.
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are rare.
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This means that re-use, review and checking of traditional analysis must often be started from `cold'.
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%
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Another effect on a one entry per failure mode model, is that the terminology
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may be inconsistent. Failure symptoms, although being the same at a system level, may be
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given different names in the same project.
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%
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These factors mean that re-use, review and checking of traditional analysis can often be started from `cold'.
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%
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Work has been performed to assist in incremental FMEA production by use of a software tool
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which in conjunction with circuit simulation
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and a database of component failure modes (providing consistency in terminology)
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speeds up the FMEA process~\cite{incrementalfmea}.
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%
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%
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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@ -46,6 +46,7 @@ of the era when FMEA methodologies were invented.
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With FMEA it is very difficult to perform %impossibility of performing
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With FMEA it is very difficult to perform %impossibility of performing
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meaningful
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meaningful
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multiple failure analysis~\cite{FMEAmultiple653556,maikowski}.
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multiple failure analysis~\cite{FMEAmultiple653556,maikowski}.
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%
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The main reasons for this are that in electronics, each failure
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The main reasons for this are that in electronics, each failure
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can introduce a circuit topology change and state explosion
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can introduce a circuit topology change and state explosion
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means there can be extremely large numbers of double failures to check.
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means there can be extremely large numbers of double failures to check.
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@ -225,7 +226,7 @@ This property is examined in section~\ref{sec:theoreticalperfmodel}.
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A comparison complexity order, or reasoning distance, of $O(N^2)$
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A comparison complexity order, or reasoning distance, of $O(N^2)$
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could be seen as desirable in an automated process such as a search algorithm,
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could be seen as desirable in an automated process such as a search algorithm,
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but here it is a time consuming manual process which
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but here it is a time consuming manual process which
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demands experienced and highly qualified personnel.
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demands experienced and highly qualified personnel~\cite{automatingFMEA1281774}.
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%
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%
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It is therefore desirable to reduce this order further.
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It is therefore desirable to reduce this order further.
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@ -258,7 +259,9 @@ Work has been performed using databases
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to track the relationships between variables
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to track the relationships between variables
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and system failure modes~\cite{procsfmeadb}, to %work has been performed to
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and system failure modes~\cite{procsfmeadb}, to %work has been performed to
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introduce automation into the FMEA process~\cite{appswfmea} and to provide code analysis
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introduce automation into the FMEA process~\cite{appswfmea} and to provide code analysis
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automation~\cite{modelsfmea}. Although the SFMEA and hardware FMEAs are performed separately,
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automation~\cite{modelsfmea}.
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%
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Although the SFMEA and hardware FMEAs are performed separately,
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some schools of thought aim for Fault Tree Analysis (FTA)~\cite{nasafta,nucfta} (top down - deductive)
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some schools of thought aim for Fault Tree Analysis (FTA)~\cite{nasafta,nucfta} (top down - deductive)
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and FMEA (bottom-up inductive)
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and FMEA (bottom-up inductive)
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to be performed on the same system to provide insight into the
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to be performed on the same system to provide insight into the
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@ -268,11 +271,17 @@ Subtle problems in embedded software are often due to interrupt contention causi
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corruption of variables: automated tools to aid the detection of this
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corruption of variables: automated tools to aid the detection of this
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are becoming available~\cite{concurrency_c_tool}.
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are becoming available~\cite{concurrency_c_tool}.
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%
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%
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Work has been performed to parse software, and to map source code statements as edges
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and variables as nodes, to form directed acyclic graphs~\cite{sfmea}, where failure mode propagation
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can be traced.
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%
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Although current software FMEA techniques
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Although current software FMEA techniques
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should give a better picture of the failure mode behaviour,
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should give a better picture of the failure mode behaviour,
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they are by no means a rigorous approach to tracing errors that may occur in hardware being followed
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they are by no means a rigorous approach to tracing errors that may occur in hardware being followed
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through to the top (and therefore ultimately controlling) layer of software.
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through to the top (and therefore ultimately controlling) layer of software.
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%
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%
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That is they do not offer an integrated software hardware failure mode model.
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%
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With the increasing use of micro-controllers in place of much analogue electronics
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With the increasing use of micro-controllers in place of much analogue electronics
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for most new designs of electronic product, the poor software integration capabilities of FMEA
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for most new designs of electronic product, the poor software integration capabilities of FMEA
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are now being seen as deficiencies.
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are now being seen as deficiencies.
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@ -509,8 +518,10 @@ getting too complicated for meaningful analysis using FMEA.
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%
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%
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\subsection{FMEA Criticism: Conclusions.}
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\subsection{FMEA Criticism: Conclusions.}
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%
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FMEA is a useful tool for basic safety --- it provides statistics on safety where field data is impractical ---
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FMEA is a useful tool for basic safety --- it provides statistics on safety where field data is impractical ---
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and is good with single failure modes linked to top level events.
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and is good with single failure modes linked to top level events.
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%
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FMEA has become part of the safety critical and safety certification industries.
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FMEA has become part of the safety critical and safety certification industries.
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%
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%
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SFMEA is in its infancy, and there are corresponding gaps in
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SFMEA is in its infancy, and there are corresponding gaps in
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@ -529,7 +540,7 @@ with a one step analysis stage.
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% \begin{itemize}
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% \begin{itemize}
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% \item Impossible to integrate Software and hardware models,
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% \item Impossible to integrate Software and hardware models,
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% \item State explosion problem exacerbated by increasing complexity due to density of modern electronics,
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% \item State explosion problem exacerbated by increasing complexity due to density of modern electronics,
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% \item Impossible to consider all multiple component failure modes~\cite{FMEAmultiple653556}
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% \item Impossible to consider all multiple component failure modes~\cite{FMEAmultbbbiple653556}
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% \end{itemize}
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% \end{itemize}
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%
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%
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%\subsection{FMEA - Better Methodology - Wish List}
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%\subsection{FMEA - Better Methodology - Wish List}
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@ -2,7 +2,7 @@
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\chapter{Detailed FMMD analyses}
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\chapter{Detailed FMMD analyses}
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For clarity the detailed workings of the FMMD analysis stages in many of the examples
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For clarity the detailed workings of the FMMD analysis stages in many of the examples
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in chapter 5 have been moved here for reference.
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in chapters ~\ref{sec:chap5}~and~\ref{sec:chap6} have been moved here for reference.
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\section{Bubba Oscillator FMMD analyses}
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\section{Bubba Oscillator FMMD analyses}
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@ -105,7 +105,7 @@ $$
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\end{tabular}
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\end{tabular}
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\end{table}
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\end{table}
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Collecting symptoms from table~\ref{tbl:bubbalargefg}, the {\dc} $ BubbaOscillator $ is created with the following failure modes:
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Collecting symptoms from table~\ref{tbl:bubbalargefg}, the {\dc} $ BubbaOscillator $ is created with the following failure modes:
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$$
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$$
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fm(BubbaOscillator) = \{ NO_{osc}, HI_{fosc} \} .
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fm(BubbaOscillator) = \{ NO_{osc}, HI_{fosc} \} .
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$$
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$$
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@ -124,7 +124,7 @@ $$
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\begin{table}[h+]
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\begin{table}[h+]
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\caption{BUFF45: Failure Mode Effects Analysis} % title of Table
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\caption{BUFF45: Failure Mode Effects Analysis} % title of Table
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\label{tbl:buff45}
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\label{tbl:buff45}
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\centering
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\begin{tabular}{|| l | l | c | c | l ||} \hline
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\begin{tabular}{|| l | l | c | c | l ||} \hline
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%\textbf{Failure Scenario} & & \textbf{BUFF45} & & \textbf{Symptom} \\
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%\textbf{Failure Scenario} & & \textbf{BUFF45} & & \textbf{Symptom} \\
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% & & & & \\
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% & & & & \\
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@ -132,8 +132,8 @@ $$
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\textbf{cause} & & \textbf{Effect} & & \\
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\textbf{cause} & & \textbf{Effect} & & \\
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\hline
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\hline
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FS1: $PHS45_1$ $0\_phaseshift$ & & phase shift low & & $0\_phaseshift$ \\
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FS1: $PHS45_1$ $0\_phaseshift$ & & no phase shift & & $0\_phaseshift$ \\
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FS2: $PHS45_1$ $no\_signal$ & & signal lost & & $NO_{signal}$ \\ \hline
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FS2: $PHS45_1$ $no\_signal$ & & signal lost & & $NO_{signal}$ \\ \hline
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%FS3: $PHS45_1$ $90\_phaseshift$ & & phase shift high & & $90\_phaseshift$ \\ \hline
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%FS3: $PHS45_1$ $90\_phaseshift$ & & phase shift high & & $90\_phaseshift$ \\ \hline
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FS3: $NIBUFF_1$ $L_{up}$ & & output high & & $NO_{signal}$ \\
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FS3: $NIBUFF_1$ $L_{up}$ & & output high & & $NO_{signal}$ \\
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@ -237,7 +237,7 @@ $$
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Collecting symptoms from table~\ref{tbl:phs225amp}, the {\dc} $PHS225AMP $ is created with the following failure modes:
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Collecting symptoms from table~\ref{tbl:phs225amp}, the {\dc} $PHS225AMP $ is created with the following failure modes:
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$$
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$$
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fm() = \{ 180\_phaseshift, NO\_signal \} .
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fm(PHS225AMP) = \{ 180\_phaseshift, NO\_signal \} .
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$$
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$$
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\clearpage
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\clearpage
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@ -349,7 +349,7 @@ $$
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FS1: $IC2$ $HIGH$ & & output perm. high & & HIGH \\
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FS1: $IC2$ $HIGH$ & & output perm. high & & HIGH \\
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FS2: $IC2$ $LOW$ & & output perm. low & & LOW \\
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FS2: $IC2$ $LOW$ & & output perm. low & & LOW \\
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FS3: $IC2$ $NOOP$ & & no current to output & & $NOOP$ \\
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FS3: $IC2$ $NOOP$ & & no current to output & & $NOOP$ \\
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FS4: $IC2$ $LOW\_SLEW$ & & delay signal & & $LOW\_{SLEW}$ \\ \hline
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FS4: $IC2$ $LOW\_SLEW$ & & delayed signal & & $LOW\_{SLEW}$ \\ \hline
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\end{tabular}
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\end{tabular}
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\end{table}
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\end{table}
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% \hline
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% \hline
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@ -382,7 +382,7 @@ $$
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\hline \hline
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\hline \hline
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FS1: $PD $ $HIGH$ & & output perm. low & & LOW \\
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FS1: $PD $ $HIGH$ & & output perm. low & & LOW \\
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FS2: $PD $ $LOW$ & & output perm. low & & HIGH \\ \hline
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FS2: $PD $ $LOW$ & & output perm. high & & HIGH \\ \hline
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\hline
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\hline
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FS3: $IC3$ $HIGH$ & & output perm. high & & HIGH \\
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FS3: $IC3$ $HIGH$ & & output perm. high & & HIGH \\
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@ -815,13 +815,8 @@ $$
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\subsection{ LEDOutput: Failure Mode Effects Analysis }
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\subsection{ LEDOutput: Failure Mode Effects Analysis }
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%
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{
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{
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\tiny
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\tiny
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\begin{table}[h+]
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\begin{table}[h+]
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@ -1017,14 +1012,14 @@ Some standards, notably EN298 only consider most types of resistor as failing in
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%FMD-97 gives 27\% OPEN and 3\% SHORTED, for resistors under certain electrical and environmental stresses.
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%FMD-97 gives 27\% OPEN and 3\% SHORTED, for resistors under certain electrical and environmental stresses.
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% FMD-91 gives parameter change as a third failure mode, luvvverly 08FEB2011
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% FMD-91 gives parameter change as a third failure mode, luvvverly 08FEB2011
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This example
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This example
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compromises and uses a 9:1 OPEN:SHORT ratio, for resistor failure.
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compromises and uses a 9:1 OPEN:SHORT ratio for resistor failure.
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%
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%
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Thus for this example resistors are expected to fail OPEN in 90\% of cases and SHORTED
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Thus for this example resistors are expected to fail OPEN in 90\% of cases and SHORTED
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in the other 10\%.
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in the other 10\%.
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A standard fixed film resistor, for use in a benign environment, non military specification at
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A standard fixed film resistor, for use in a benign environment, non military specification at
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temperatures up to {60\oc} is given a probability of 13.8 failures per billion ($10^9$)
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temperatures up to {60\oc} is given a probability of 13.8 failures per billion ($10^9$)
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hours of operation (see equation \ref{eqn:resistor}).
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hours of operation (see equation \ref{eqn:resistor}).
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In EN61508 terminology, this figure is referred to as a Failure in Time FIT\footnote{FIT values are measured as the number of
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In EN61508 terminology, this figure is referred to as a Failure in Time (FIT)\footnote{FIT values are measured as the number of
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failures per Billion (${10}^9$) hours of operation, (roughly 114,000 years). The smaller the
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failures per Billion (${10}^9$) hours of operation, (roughly 114,000 years). The smaller the
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FIT number the more reliable the component.}.
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FIT number the more reliable the component.}.
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%
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%
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@ -1065,7 +1060,7 @@ Thus thermistor, bead type, `non~military~spec' is given a FIT of 315.0.
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\frategloss
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\frategloss
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%Using the RIAC finding the following (table~\ref{tab:stat_single}) can be created which
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%Using the RIAC finding the following (table~\ref{tab:stat_single}) can be created which
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%presents the FIT values for all single failure modes.
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%presents the FIT values for all single failure modes.
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Using the above table~\ref{tab:stat_single} is presented which lists the FIT values for all single failure modes.
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Using the above; table~\ref{tab:stat_single} is presented which lists the FIT values for all single failure modes.
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%\glossary{name={FIT}, description={Failure in Time (FIT). The number of times a particular failure is expected to occur in a $10^{9}$ hour time period.}}
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%\glossary{name={FIT}, description={Failure in Time (FIT). The number of times a particular failure is expected to occur in a $10^{9}$ hour time period.}}
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\fmmdglossFIT
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\fmmdglossFIT
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%
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%
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@ -1087,6 +1082,7 @@ TC:4 $R_3$ OPEN & High Fault & Low Fault & 283.5 \\ \hline
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\hline
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\hline
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TC:5 $R_2$ SHORT & - & Low Fault & 1.38 \\
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TC:5 $R_2$ SHORT & - & Low Fault & 1.38 \\
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TC:6 $R_2$ OPEN & High Fault & High Fault & 12.42 \\ \hline
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TC:6 $R_2$ OPEN & High Fault & High Fault & 12.42 \\ \hline
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TC:6 $R_2$ OPEN & High Fault & High Fault & 12.42 \\ \hline
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\hline
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\hline
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\end{tabular}
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\end{tabular}
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\label{tab:stat_single}
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\label{tab:stat_single}
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@ -1098,8 +1094,9 @@ The FIT for the circuit as a whole is the sum of MTTF values for all the
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test cases. The Pt100 circuit here has a FIT of 342.6. This is an MTTF of
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test cases. The Pt100 circuit here has a FIT of 342.6. This is an MTTF of
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about $\approx 360$ years per circuit.
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about $\approx 360$ years per circuit.
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%
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%
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A probabilistic tree can now be drawn, with a FIT value for the overall Pt100
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A probabilistic tree can now be drawn, see figure~\ref{fig:stat_single}, with a FIT value for the overall Pt100
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circuit and FIT values for all its component fault modes. % from which it was calculated.
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circuit and
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FIT values for all its component fault modes. % from which it was calculated.
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%
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%
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From this it can be seen that the most likely fault is the thermistor going OPEN.
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From this it can be seen that the most likely fault is the thermistor going OPEN.
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%
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%
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@ -1145,7 +1142,7 @@ failures in the electronic examples from chapter~\ref{sec:chap5} in table~\ref{t
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The failure mode of most concern, the undetectable {\textbf{FLOATING}} condition,
|
The failure mode of most concern, the undetectable {\textbf{FLOATING}} condition,
|
||||||
requires that resistors $R_1$ and $R_2$ both fail.
|
requires that resistors $R_1$ and $R_2$ both fail.
|
||||||
%
|
%
|
||||||
Multiplying the MTTF probabilities for these types of resistor failing gives the MTTF for both failing.
|
Multiplying the MTTF probabilities for these types of resistor failing gives the MTTF for both failing simultaneously.
|
||||||
%
|
%
|
||||||
The FIT value of 12.42 corresponds to $12.42 \times {10}^{-9}$ failures per hour.
|
The FIT value of 12.42 corresponds to $12.42 \times {10}^{-9}$ failures per hour.
|
||||||
%
|
%
|
||||||
|
Loading…
Reference in New Issue
Block a user