Patent ID: 8091203

Claim:
A method comprising: providing a liner comprising an alloy high pressure hydrogen gas storage tank, the liner having first and second open ends with a first inner diameter and a first outer diameter; providing alloy caps having an outer surface with multiple axially offset ribs with spaces therebetween, the spaces having a second outer diameter which is slightly less than the first inner diameter, the ribs having a third outer diameter slightly greater than the first inner diameter; providing alloy collars having a second inner diameter which is less than the first outer diameter; bringing the liner to a first temperature about 200-250° C., bringing the caps to a second temperature about −196 to 10° C., and bringing the collars to a third temperature about 350-400° C.; placing at least a portion of the caps inside the open ends while the liner is at or near the first temperature and while the caps are at or near the second temperature; placing at least a portion of the collars over the open ends while the liner is at or near the first temperature and while the collars are at or near the third temperature bringing the liner, the caps, and the collars to a room temperature which is less than the third temperature and which is greater than the second temperature; winding an interwoven pre-peg multiple layer unidirectional fiber sheet comprising a resin and having at least an intermediate carbon fiber layer and an outer glass fiber layer, the fiber sheet having a pre-sized axial width equal to an axial length of the liner and end assemblies comprising the installed caps and collars, the sheet having an inner surface contacting an outer surface of the liner and end assemblies; and curing the resin to permanently adhere the fiber sheet to the liner and to the end assemblies.