Open AccessInvestigation of methods for equalizing the flow parameters in the axial compressor intake flare
Author(s) -
А. Е. Зарянкин,
Т. Падашмоганло,
Maryna Postnikova
Publication year - 2020
Publication title -
izvestiâ vysših učebnyh zavedenij. problemy ènergetiki
Language(s) - English
Resource type - Journals
eISSN - 2658-5456
pISSN - 1998-9903
DOI - 10.30724/1998-9903-2019-21-6-72-83
Subject(s) - inlet , flare , gas compressor , mechanics , axial compressor , turbine , flow (mathematics) , physics , centrifugal compressor , angular velocity , engineering , acoustics , aerospace engineering , mechanical engineering , classical mechanics
The problem of ensuring a uniform velocity field at the air inlet to the first stage of the gas turbine compressor SGT5-2000E with an angular inlet path, that contains an inlet filter, a silencer and an angular intake flare, is considered. Based on the mathematical modeling of the flow in this flare, it was found that the maximum speed at the compressor inlet is 36% higher than the average flow rate. It leads to the fact that the range of stable operation of the compressor seriously narrows. To solve this problem, it is proposed to change the intake flare design so that a newly developed effective damper of uneven velocity fields is installed in its flow part. Studies have shown that in this way the nonuniformity coefficient was reduced from the above 36% to 6%.