Method for fabricating measuring comb utilized to measure e.g. pressure in air flow of experimental turbojet in e.g. military aircraft, involves installing and welding measuring units at outlet of internal pipes

摘要

The method involves realizing a monoblock measuring comb body comprising a set of cavities forming internal pipes emerging from a face of the measuring comb body. The comb body comprises measuring units utilized to measure parameters of air flow of an experimental turbojet. The measuring units are welded at an outlet of the internal pipes, and realization step of the comb body is carried out by laser fusion method.