Abstract: A thickness inspection method inspects the thickness of a part having a hollow shape by using tooling enabling a counter-shape to be molded that matches said hollow shape. The method includes putting the part into place on a support secured to the tooling, locking the part in place, and filling the hollow shape with a molding material in order to form the counter-shape. The method also includes solidifying the molding material, acquiring 3D images of the external surface of the part and of the support, and removing the part from the support in order to leave only the counter-shape on the support. The method also includes acquiring 3D images of the outside surface of the counter-shape and of the support, and superposing and processing the 3D images in order to obtain various dimensions of the part enabling its thickness to be inspected.

Abstract: Tooling for removing sand from a turbine engine, such as an airplane turbojet, the tooling including at least one endoscopic display device including a display and a duct having light guide and image transmission device mounted therein, a suction device having a suction device connected to a suction duct fastened to the duct of a display device, and a plasma jet generator device including a plasma torch connected to gas supply and electricity power supply suitable for operating the plasma torch, the plasma torch being fastened to the duct of an above-mentioned display device.

Abstract: A thickness inspection method inspects the thickness of a part having a hollow shape by using tooling enabling a counter-shape to be molded that matches said hollow shape. The method includes putting the part into place on a support secured to the tooling, locking the part in place, and filling the hollow shape with a molding material in order to form the counter-shape. The method also includes solidifying the molding material, acquiring 3D images of the external surface of the part and of the support, and removing the part from the support in order to leave only the counter-shape on the support. The method also includes acquiring 3D images of the outside surface of the counter-shape and of the support, and superposing and processing the 3D images in order to obtain various dimensions of the part enabling its thickness to be inspected.

Abstract: Tooling for removing sand from a turbine engine, such as an airplane turbojet, the tooling including at least one endoscopic display device including a display and a duct having light guide and image transmission device mounted therein, a suction device having a suction device connected to a suction duct fastened to the duct of a display device, and a plasma jet generator device including a plasma torch connected to gas supply and electricity power suitable for operating the plasma torch, the plasma torch being fastened to the duct of an above-mentioned display device.