| 摘要 |
PROBLEM TO BE SOLVED: To provide a distribution system that facilitates reduction of size and space necessary for installation of a fluid distribution system in an aircraft to decrease weight, installation time and cost.SOLUTION: A method includes providing a first distribution line configured to channel a fluid in a first direction 204, and coupling at least one internal support member 208 to an outer surface of the first distribution line. The at least one internal support member includes a plurality of support legs extending radially outward from the at least one internal support member. The method also includes aligning a second distribution line concentrically with and circumscribing the first distribution line. The second distribution line is configured to channel the fluid in an opposite second direction 206. The method further includes coupling the plurality of support legs to an inner surface of the second distribution line. |
