| CPC B64D 37/30 (2013.01) [B64C 39/10 (2013.01); B64C 2039/105 (2013.01)] | 19 Claims |

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1. An aircraft with at least a multi-walled fuel
tank, the aircraft comprising: a blended wing body; and
the at least a multi-walled fuel tank attached to the blended wing body and configured to store liquified gas fuel, wherein the at least a fuel tank further comprises:
an inner wall;
an outer wall; and
an interstitial volume between the inner wall and the outer wall comprising of at least a reflective film layer and at least a structural insulation layer, wherein the at least a structural layer is divided into blocks, wherein the interstitial volume comprises a gap located between the blocks of the at least a structural insulation layer; and
at least a vent fluidly connected to the interstitial volume, wherein the at least a vent is further connected to the gap, and configured to vent gas from the gap at a purge flow rate sufficient to maintain a fuel gas concentration within the interstitial volume below a threshold gas concentration.
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