发明名称 LINTEL STRUCTURE FOR AIRCRAFT FUSELAGE AND FUSELAGE COMPRISING SUCH A LINTEL
摘要 <p>An aircraft fuselage comprises a structure, considered in respect of all or part of the fuselage, with fuselage upper panels (12) constituting an upper part of the fuselage and a fuselage bottom structure (13) constituting a lower part of the fuselage. Openings (24, 25) in the structure of the fuselage are intended for the installation of windows or doors for exiting the fuselage. Furthermore, the fuselage upper panels (12) and the fuselage bottom structure (13) form fuselage sub-structures that are assembled with one another via at least one lintel (20) in which all or some of the openings (24, 25) intended for installing the exit doors or windows are formed.</p>
申请公布号 WO2016009075(A1) 申请公布日期 2016.01.21
申请号 WO2015EP66485 申请日期 2015.07.17
申请人 STELIA AEROSPACE 发明人 DUCOURNAU, HERVÉ;PRUDENT, ALAIN;GAUCHET, FLORIAN
分类号 B64C1/06;B64C1/08;B64C1/14 主分类号 B64C1/06
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