Under the complex coupled effect of temperature and load fields, the internal stress state of carbon fiber reinforced polymers (CFRP) composites and its components undergo unpredictable changes, which greatly affects the accuracy and lifespan. In this study, the M55J-carbon fiber/cyanate ester (M55J-CF/CE) composites was used as the research object, which the bending strength and deflection experiment under high-low temperatures was performed, the strength decreases and the deflection value increases with the temperature rises was obtained, and provided parameters selection basis for the stress relaxation experiment research. Based on this, the stress relaxation experiment studies under high and low temperatures (-150°C ∼ +180°C) and initial loads (400 N, 800 N, and 1200 N) were carried out, and the high-temperature relaxation and low-temperature rebound relaxation variation law induced by the temperature-load-configuration was obtained. Furthermore, the constitutive parameters under the action of temperature and load were corrected based on the time-hardening model (THM), and the stress distribution prediction and evolution law research were carried out in combination with FEM. The research results show that temperature has the highest sensitivity to stress relaxation, and the relaxation trends caused by different loads are identical, the experiment maximum stress relaxation rate under the coupling effect of temperature and load is 58%, and the simulation prediction model error is <10%. Additionally, the cyclic angle laminate compared with single angle laminate shows an effect of ‘bias pressure mitigation leapfrog’ relaxation behavior, then the influence of layup angle, temperatures and initial loads to the stress relaxation mechanism were revealed.
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