| 发明名称 |
REAR FUSELAGE SECTION OF AN AIRCRAFT |
| 摘要 |
A rear fuselage section of an aircraft comprises at least one closed frame constructed as a unitary body, and a horizontal tail plane comprising a box-type central element and two lateral torsion boxes, said horizontal tail plane trimmable with respect to a pivot axis. The horizontal tail plane is mounted at the closed frame and the pivot axis is contained in a horizontal plane below the lowest end of said closed frame. |
| 申请公布号 |
US2015034765(A1) |
申请公布日期 |
2015.02.05 |
| 申请号 |
US201414445537 |
申请日期 |
2014.07.29 |
| 申请人 |
Airbus Operations S.L. |
发明人 |
Gonzalez Gozalbo Alfonso;Llamas Sandin Raul Carlos |
| 分类号 |
B64C1/06;B64C25/00;B64C7/00;B64C1/10;B64C1/26;B64C9/00 |
主分类号 |
B64C1/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A rear fuselage section of an aircraft comprising:
at least one closed frame constructed as a unitary body, a horizontal tail plane comprising two lateral torsion boxes and a box-type central element configured to join the two lateral torsion boxes, said horizontal tail plane being trimmable with respect to a pivot axis, said horizontal tail plane being mounted at the closed frame, and the pivot axis being contained in a horizontal plane below a lowest end of said closed frame. |
| 地址 |
Getafe (Madrid) ES |
