A low-temperature composite
gas cylinder design method comprises the following steps: 1, designing laying parameters; 2, calculating the normal-temperature strength and the low-temperature strength ofthe
gas cylinder by utilizing a grid theory, judging whether the normal-temperature strength and the low-temperature strength meet requirements or not, if not, returning to the step 1, and if yes, entering a step 3; 3, establishing a finite
element model for the
gas cylinder, calculating the stress state of the lining of the gas cylinder under normal temperature and low temperature
working pressure, the stability of the lining under normal temperature and low temperature zero pressure and the stress in the
fiber direction of the outermost layer of the winding layer under low temperature
working pressure, and judging whether the Mises stress of the lining under normal temperature and low temperature
working pressure does not exceed the
yield limit of the material; judging whether the lining structure is complete and stable at normal temperature and low temperature and zero pressure; judging whether the stress in the
fiber direction of the outermost layer of the winding layer is not greater than sigma d1 / n under low-temperature working pressure; if yes, the gas cylinder design meets the requirement; otherwise, if the design of the gas cylinder does not meet the requirements, redesign is needed. The design is comprehensive, and it can be guaranteed that the gas cylinder performance meets the requirement.