发明申请
WO2020239470A1 LÈVRE D'ENTRÉE D'AIR DE NACELLE DE TURBOMACHINE COMPRENANT UN DISPOSITIF ACOUSTIQUE ET PROCÉDÉ DE FABRICATION D'UNE TELLE LÈVRE
审中-公开
基本信息:
- 专利标题: LÈVRE D'ENTRÉE D'AIR DE NACELLE DE TURBOMACHINE COMPRENANT UN DISPOSITIF ACOUSTIQUE ET PROCÉDÉ DE FABRICATION D'UNE TELLE LÈVRE
- 专利标题(英):AIR INTAKE LIP FOR A TURBOMACHINE NACELLE, COMPRISING AN ACOUSTIC DEVICE, AND METHOD FOR PRODUCING SUCH A LIP
- 申请号:PCT/EP2020/063536 申请日:2020-05-14
- 公开(公告)号:WO2020239470A1 公开(公告)日:2020-12-03
- 发明人: DIGEOS, Virginie, Emmanuelle, Anne-Marie , GONIDEC, Patrick
- 申请人: SAFRAN NACELLES
- 申请人地址: Route du Pont VIII 76700 GONFREVILLE-L'ORCHER FR
- 专利权人: SAFRAN NACELLES
- 当前专利权人: SAFRAN NACELLES
- 当前专利权人地址: Route du Pont VIII 76700 GONFREVILLE-L'ORCHER FR
- 代理机构: ARGYMA
- 优先权: FRFR1905563 20190527
- 主分类号: B64D33/02
- IPC分类号: B64D33/02 ; B64D15/04
The invention relates to an air intake lip (2a) of an aircraft turbomachine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the lip (2a) extending annularly about the X-axis and having an inner wall (21) facing the X-axis and an outer wall (22) which is opposite the inner wall (21), the inner wall (21) and the outer wall (22) being connected by an upstream wall (23) so as to delimit an annular cavity (20), the lip (2a) comprising an annular acoustic device (50) mounted in the annular cavity (20). The lip (2a) has a first module (M1), comprising the outer wall (22), the wall (23) and a front wall (24) forming an upstream portion of the inner wall (21), and a second module (M2), comprising the acoustic device (50) and a front skin (51) forming a downstream portion of the inner wall (21), the first module (M1) and the second module (M2) being secured together so that the front wall (24) and the front skin (51) together form the inner wall (21) of the lip (2a).
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64D | 用于与飞机配合或装到飞机上的设备;飞行衣;降落伞;动力装置或推进传动装置的配置或安装 |
------B64D33/00 | 其他类目不包含的动力装置部件或辅助设备在飞机内的布置 |
--------B64D33/02 | .进气口燃烧的 |