| 摘要 |
An aircraft nacelle includes an air intake (40) that makes it possible to channel a stream of air (42) in the direction of a power plant (44), whereby the air intake (40) includes an inside pipe (48) that forms an aerodynamic surface (52) that is in contact with the stream of air (42) that is extended toward the rear by an aerodynamic surface (54) of a pipe (56) of the power plant, characterized in that it includes a support (66) of at least one measuring device (68), whereby the support (66), in annular form, is able to be inserted in a removable way between the air intake (40) and the power plant (44) and includes a so-called aerodynamic surface (70) that can ensure the continuity of the aerodynamic surfaces (52, 54) that are arranged downstream and upstream according to the direction of flow of the stream of air (42).
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