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公开(公告)号:US10138754B2
公开(公告)日:2018-11-27
申请号:US15348824
申请日:2016-11-10
IPC分类号: F01D21/00 , G01D11/24 , G01M15/14 , F01D5/14 , G01L15/00 , G01L19/14 , G01P5/165 , G01M9/06 , G01F1/46 , G01P5/10 , G01P5/14
摘要: The present invention relates to a device for measuring aerodynamic magnitudes (1) intended to be placed transversally in a flow passage (12, 13) of a turbine engine comprising: an upstream body (2) having a profile of general cylindrical shape defining a leading edge (5) a plurality of sensors (4), the instrumentation lines (45) of the sensors being placed in the body (2), the sensitive elements (41) of the sensors extending at the leading edge (5); a downstream fairing (3) mounted on the upstream body (2) and defining a trailing edge (6); the downstream fairing (3) comprising, in the longitudinal direction of the upstream body (2), several sections (35) fixed independently of each other to the body (2), two successive sections (35) being connected by a flexible junction (37).