This invention relates to the field of high-pressure
gas cylinder safety assessment technology, specifically to a method for estimating the burst strength of a high-pressure
hydrogen cylinder with a plastic-lined, fully carbon
fiber-wound liner. The high-pressure
hydrogen cylinder with a plastic-lined, fully carbon
fiber-wound liner consists of a plastic liner, a spirally wound carbon
fiber layer, and a circumferentially wound carbon
fiber layer. The inner
diameter of the plastic liner is D0, and its outer
diameter is D1. The outer
diameter of the spirally wound layer is D2, and the outer diameter of the circumferentially wound layer is D3. The plastic liner includes front and rear end sections and a central cylindrical section. The spirally wound layer is fully wound on the end sections and the cylindrical section, while the circumferentially wound layer is only wound on the cylindrical section. The fiber winding adopts geodesic winding theory, and the
internal pressure is entirely borne by the fibers. By analyzing and estimating the maximum stress in the circumferential and meridional directions of the fibers under
internal pressure, the burst strength of the
gas cylinder can be estimated. This invention, through its method for calculating the burst strength of gas cylinders, provides a more convenient, intuitive, and rapid method for predicting the burst strength of gas cylinders.