Fatigue　life　prediction　method　based　on　stress　normalization　was　proposed　to　reduce　the　infiuence　of　material　property　dispersion　on　life　for　CFRC　(carbon　fibre　reinforced　composites).　In　order　to　consider　the　effect　of　temperature　on　fatigue　damage,　a　temperature　infiuence　factor　was　introduced　into　the　fatigue　limit　equation　and　the　life　prediction　method　under　variable　amplitude　loading　at　high　temperature.　Combined　with　the　rainfiow　cycle　counting　and　Miner　linear　damage　accumulation　rule,　the　proposed　fatigue　life　prediction　method　was　verified　by　the　experimental　results　of　composite　multidirectional　laminates　under　constant　amplitude　and　variable　amplitude　loadings　at　various　temperatures,　and　the　prediction　errors　are　within　a　factor　of　5.