| 发明名称 |
ПИЛОН КРЕПЛЕНИЯ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ ДЛЯ ЛЕТАТЕЛЬНОГО АППАРАТА |
| 摘要 |
The structure has a rigid structure (10) comprising a set of half rings (30) arranged in order to delimit conjointly a part of a cylindrical imaginary surface (32) of a circular section. The half rings are centered on a longitudinal axis (34) of the imaginary surface. The rigid structure (10) has a central case (20) extending parallel to the axis of the imaginary surface. An independent claim is also included for an aircraft. |
| 申请公布号 |
RU2007107930(A) |
申请公布日期 |
2008.09.10 |
| 申请号 |
RU20070107930 |
申请日期 |
2005.08.03 |
| 申请人 |
ЭРБЮС ФРАНС (FR) |
发明人 |
ДЬОШОН Лионель (FR);ДЮРАН Жером (FR) |
| 分类号 |
B64D27/26 |
主分类号 |
B64D27/26 |
| 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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