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公开(公告)号：EP4393642A3
公开(公告)日：2024-09-11
申请号：EP23220614.4
申请日：2023-12-28
发明人： MORIN, Philippe , WHITTOM, Guillaume , HOANG, Canam , COLLETTE, Jean-Francois , NAULT, Pierre-Luc , DARSIGNY, Olivier , FORTIER, Guillaume , LAFORTUNE, David
IPC分类号： B24B19/14 , B24B19/26 , B24B21/16 , B24B21/20 , B24B27/00 , B24B49/16 , B24B51/00 , B24B37/005
CPC分类号： B24B19/14 , B24B19/26 , B24B51/00 , B24B49/16 , B24B21/165 , B24B27/0038 , B24B21/20 , B24B37/005 , B24B21/16
摘要： A manufacturing method includes controlling a robotic polishing device (46), at a controller (48), to polish a plurality of first zones (88A; 90A) of a bladed rotor (20) for an aircraft engine based on a first operating parameter associated with the robotic polishing device (46). An exterior (56) of the bladed rotor (20) includes the first zones (88A; 90A) and a plurality of second zones (88B-F; 90B-F). The first zones (88A; 90A) are distributed circumferentially about an axis (22) of the bladed rotor (20) in a first array. The second zones (88B-F; 90B-F) are distributed circumferentially about the axis (22) of the bladed rotor (20) in a second array. The method further includes controlling the robotic polishing device (46), at a controller (48), to polish the second zones (88B-F; 90B-F) using the robotic polishing device (46) based on a second operating parameter. The second operating parameter for the robotic polishing device (56) is different than the first operating parameter.
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公开(公告)号：EP4393642A2
公开(公告)日：2024-07-03
申请号：EP23220614.4
申请日：2023-12-28
发明人： MORIN, Philippe , WHITTOM, Guillaume , HOANG, Canam , COLLETTE, Jean-Francois , NAULT, Pierre-Luc , DARSIGNY, Olivier , FORTIER, Guillaume , LAFORTUNE, David
CPC分类号： B24B19/14 , B24B19/26 , B24B51/00 , B24B49/16 , B24B21/165 , B24B27/0038 , B24B21/20
摘要： A manufacturing method includes controlling a robotic polishing device (46), at a controller (48), to polish a plurality of first zones (88A; 90A) of a bladed rotor (20) for an aircraft engine based on a first operating parameter associated with the robotic polishing device (46). An exterior (56) of the bladed rotor (20) includes the first zones (88A; 90A) and a plurality of second zones (88B-F; 90B-F). The first zones (88A; 90A) are distributed circumferentially about an axis (22) of the bladed rotor (20) in a first array. The second zones (88B-F; 90B-F) are distributed circumferentially about the axis (22) of the bladed rotor (20) in a second array. The method further includes controlling the robotic polishing device (46), at a controller (48), to polish the second zones (88B-F; 90B-F) using the robotic polishing device (46) based on a second operating parameter. The second operating parameter for the robotic polishing device (56) is different than the first operating parameter.
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