Search academic texts

Information × Registration Number 0306U001098, 0105U000212 , R & D reports Title Physical bases of increase of bearing ability blades compressor GTD by application of integrated hardening. popup.stage_title Провести аналіз основних експлуатаційних пошкоджень та технологічних мікродефектів. Провести дослідження характеристик поверхневого шару лопаток компресора після комплексного зміцнення. Head Yatcenko Viktor Kuzmich, Registration Date 26-01-2006 Organization Zaporizhzhia National Technical University popup.description2 The object of the research is compressor blades of titanium alloy ВТ8М of engines ТВ3-117 and ТВЗ-117 ВМА-СБМ1. The purpose of the research is realization analysis of the main operational damages and technological micro defects of compressor blades and the research of surface layer characteristics. The results of the research are the list and peculiarities characteristic to main operational damages and technological micro defects, which reduce bearing ability of compressor blades of helicopter's engines, as well as laws forming of blanket characteristics after application of integrated processing of compressor blades of titanium alloy. The field of application is manufacturing firms of the aero-enginebuilding field. Product Description popup.authors popup.nrat_date 2020-04-02 Close