发明名称 AIRCRAFT WITH OPTIMISED UTILITY VOLUME AND METHOD FOR OPTIMISING THE UTILITY VOLUME OF AN AIRCRAFT
摘要 An aircraft including a fuselage including a cabin to accommodate persons and/or a load, and a propulsion system. The propulsion system includes at least one tank and/or one combustion chamber, wherein part of the propulsion system can be used as an extension of the cabin to accommodate persons and/or a load, the part of the propulsion system lying adjacent the cabin and separated from the cabin by a partition.
申请公布号 EP2051904(B1) 申请公布日期 2013.07.10
申请号 EP20070802665 申请日期 2007.08.16
申请人 AIRBUS 发明人 SMITH, GARRETT
分类号 B64C1/00;B64D37/04;B64G1/40 主分类号 B64C1/00
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