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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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