INSTALLATION FOR PRELIMINARY TESTS afterburner turbofan ENGINE

摘要

The invention relates to mechanical engineering, in particular to facilities for ground testing afterburning chambers (FC) of aircraft gas turbine engines, and improves the accuracy of results obtained when tested. Installation for the pretest augmentor of a gas turbine engine comprises equipment that generates the flow of the working body, wherein, the equipment that generates the working fluid flow configured as a turbocharger bypass turbomachine, the said device comprises a reservoir for air bleed from the outer contour to the atmosphere and an adapter with a lattice fixed profiles, installed in a test for the turbine to be tested afterburner. Fig.