Abstract: A manufacturing and assembly method of parts of an aircraft comprising the following several steps. Providing a first aircraft part comprising a receptor surface on which a coupling surface of a second aircraft part is to be assembled. Providing a model of the first and the second aircraft parts in their assembled position, the model of the second aircraft part comprising machining allowances in its coupling surface. Digitalizing the receptor surface of the first aircraft part. Positioning the digitalization in the computer model in the assembled position such that the digitalization of the receptor surface intersects the coupling surface of the second aircraft part. Obtaining a model of the second part in which the coupling surface fits the digitalized receptor surface. Mechanizing the second aircraft part.

Abstract: A catoptric imaging device for drill measuring comprising a laser guide, an imaging unit for converting optical image into image information, and processing the image information to obtain a drill measure, a catoptric assembly including a first conical surface, and a second surface including a frustoconical surface, wherein the first surface is arranged relative to the laser guide to reflect a cone beam onto an cross section of the drill to be measured, and wherein the smallest diameter of the frustoconical surface is larger than the largest diameter of the first surface to receive the cone beam reflections and reflect them towards the imaging unit, and wherein the imaging unit is arranged to receive an optical image from the frustoconical surface reflections to obtain a drill measure.

Abstract: A catoptric imaging device for drill measuring comprising a laser guide, an imaging unit for converting optical image into image information, and processing the image information to obtain a drill measure, a catoptric assembly including a first conical surface, and a second surface including a frustoconical surface, wherein the first surface is arranged relative to the laser guide to reflect a cone beam onto an cross section of the drill to be measured, and wherein the smallest diameter of the frustoconical surface is larger than the largest diameter of the first surface to receive the cone beam reflections and reflect them towards the imaging unit, and wherein the imaging unit is arranged to receive an optical image from the frustoconical surface reflections to obtain a drill measure.