Tooling for manufacturing an aeronautical part and a method for manufacturing the aeronautical part using this tooling

Abstract

The invention relates to a tool (6) for manufacturing an aeronautical part, the tool comprising two rigid shells (62, 64) assembled to define a cavity (60) for receiving a fibrous preform (520), wherein at least one of the shells comprises a through opening (800), and an elastically deformable membrane (82) extending at the level of this opening and defining a first injection compartment (880) opening into the cavity, and a second compaction compartment (882) separated from the cavity by the membrane. The tool further comprises at least one first port (804) connected to the first compartment and configured to be connected to a resin source, and at least one second port (884, 886) connected to the second compartment and configured to be connected to a compaction fluid source. Figure 6 (for the abstract)