Aircraft cooling system with fluid and pressure-tight pipe...

Pipe joints or couplings – Temperature responsive joint element; e.g. – shrunk fit

Reexamination Certificate

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C285S226000, C285S229000

Reexamination Certificate

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06843515

ABSTRACT:
A cooling system in an aircraft has fluid flow pipe sections that are mounted to the aircraft structure. The pipe sections have pipe ends that form part of pipe junctions. The two pipe ends of a pipe junction are facing each other and are surrounded by a shrunk hose member of a shrinkable material which overlaps both pipe ends in a fluid- and pressure-tight manner.

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