To provide a cryogenic tank (10) for an aircraft (30) enabling a tank access for maintenance and repair services of equipment inside the tank onboard the aircraft (30).SOLUTION: An access opening (44) is closed by a removable closure (48) including a multi-wall panel (56) which is vacuum-insulated and which is designed and fitted to a multi-tank wall (42) such that the heat ingress into the cryogenic tank (10) is minimized and such that no vacuum is impacted by opening and closing the removable closure (48).SELECTED DRAWING: Figure 2
【課題】航空機(30)に搭載されたタンク内の機器のメンテナンスおよび修理サービスのためタンクアクセスできる航空機(30)のための極低温タンク(10)を提供すること。【解決手段】アクセス開口部(44)は、真空断熱された多重壁パネル(56)を含む取り外し可能な閉鎖部(48)によって閉じられており、この多重壁パネルは、極低温タンク(10)への熱の侵入が最小限に抑えられ、取り外し可能な閉鎖部(48)の開閉によって真空が影響されないように、多重タンク壁(42)に設計され取り付けられている。【選択図】図2
CRYOGENIC TANK WITH ACCESS OPENING, AND AIRCRAFT EQUIPPED THEREWITH
アクセス開口部を備えた極低温タンクおよびそれを備えた航空機
12.12.2024
Patent
Elektronische Ressource
Japanisch
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