CPC B64D 37/30 (2013.01) [B64C 3/26 (2013.01); B64D 37/32 (2013.01)] | 18 Claims |
1. An aircraft assembly, comprising:
an aircraft panel;
a channel attached to the aircraft panel;
a fuel line for carrying cryogenic fuel, the fuel line disposed in the channel; and
a sealed containment space around the fuel line for containing cryogenic fuel leaked from the fuel line, the containment space defined between the channel, the fuel line, and the aircraft panel; and,
wherein the cryogenic fuel line is spaced from the channel.
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