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 |
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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