发明名称 Cryogenic fuel tanks for use in aircraft structures
摘要 Cryogenic fuels tanks (218, 220) for use in airfoil-shaped aircraft structures (1200) are disclosed herein. An example apparatus disclosed herein an airfoil-shaped structure (1200) disposed outboard of a fuselage of an aircraft (100). The example apparatus also includes a first cryogenic fuel tank (118) disposed inside the airfoil-shaped structure (1200).
申请公布号 EP2848520(A1) 申请公布日期 2015.03.18
申请号 EP20140184139 申请日期 2014.09.09
申请人 THE BOEING COMPANY 发明人 BARMICHEV, SERGEY D.;SANKRITHI, MITHRA M.K.V.;STUHR, VICTOR K.
分类号 B64C3/34;B64D37/04;B64D37/30 主分类号 B64C3/34
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