发明名称 Fuselage arrangement for airplane
摘要 An aircraft fuselage with a shape elongated along a longitudinal axis X along a longitudinal axis of the aircraft that determines a direction toward the front along a direction of motion of the aircraft in flight. A front section with straight cross sections widening relative to the X axis, located at the front of the fuselage and ending in the front of the fuselage in a fuselage nose, and delimited at the rear by a cross section for joining to a rear part of the fuselage behind the front section. The front section includes a cockpit located above a floorboard between a cockpit bulkhead to the rear and a front base to the front.
申请公布号 US8308108(B2) 申请公布日期 2012.11.13
申请号 US20090494919 申请日期 2009.06.30
申请人 CAZALS OLIVIER;GENTY DE LA SAGNE JAIME;AIRBUS OPERATIONS SAS 发明人 CAZALS OLIVIER;GENTY DE LA SAGNE JAIME
分类号 B64C1/00 主分类号 B64C1/00
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