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 US2010170997(A1) 申请公布日期 2010.07.08
申请号 US20070377031 申请日期 2007.08.16
申请人 AIRBUS 发明人 SMITH GARRETT
分类号 B64G1/60;B64C1/00;B64C1/18;B64C1/20;B64D9/00;B64D11/00;B64D11/06;B64D13/00;B64D37/04;B64G1/40 主分类号 B64G1/60
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