发明申请
US20120006937A1 REAR PART OF AN AIRCRAFT INCLUDING AN ENGINE SUPPORT STRUCTURE ASSEMBLED SO AS TO OSCILLATE ON THE FUSELAGE
有权
航空器的后部分包括发动机支撑结构，因此要摆放在FUSELAGE上
- 专利标题： REAR PART OF AN AIRCRAFT INCLUDING AN ENGINE SUPPORT STRUCTURE ASSEMBLED SO AS TO OSCILLATE ON THE FUSELAGE
- 专利标题（中）： 航空器的后部分包括发动机支撑结构，因此要摆放在FUSELAGE上
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申请号： US13257628申请日： 2010-03-29
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公开(公告)号： US20120006937A1公开(公告)日： 2012-01-12
- 发明人: Laurent Lafont , Jean-Michel Saucray , Esteban Quiroz-Hernandez , Jerome Antypas , Mathieu Bonnet , Frederic Journade
- 申请人： Laurent Lafont , Jean-Michel Saucray , Esteban Quiroz-Hernandez , Jerome Antypas , Mathieu Bonnet , Frederic Journade
- 申请人地址： FR TOULOUSE
- 专利权人： AIRBUS OPERATIONS (INC AS A SOCIETE PAR ACT SIMPL)
- 当前专利权人： AIRBUS OPERATIONS (INC AS A SOCIETE PAR ACT SIMPL)
- 当前专利权人地址： FR TOULOUSE
- 优先权： FR0951959 20090330
- 国际申请： PCT/FR2010/050566 WO 20100329
- 主分类号： B64C1/16
- IPC分类号： B64C1/16 ; B64D27/02 ; B64D27/26
摘要：
A rear part of an aircraft including two connecting rods positioned symmetrically on either side of a median vertical plane, wherein each connecting rod has an end mounted on a support structure of the engines and another end mounted on the fuselage, wherein this part is configured to allow, by rotation of the connecting rods around their axes of rotation, an oscillating movement of limited amplitude of the assembly formed by the support structure and the engines, relative to the fuselage, through the first and second fuselage openings.