Propulsion and Power Plants
Аuthors
1*, 2, 1**1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. JSC «Gazprom», 16 Nametkina St., Moscow, GSP-7, 117997, Russian
*e-mail: agulnik@mai.ru
**e-mail: igor6fhsrby@yandex.ru
Abstract
Methods of calculation of losses of efficiency of the axial turbine with the driving wheel with a bandage are analysed at a partial supply, results of a complex pilot study of axial turbines are presented at change of gaps and a number of parameters, settlement research and on the received results is carried out them formulas for turbines with a working wheel with a bandage are corrected.Keywords:
axial turbine stage, experiments, gaps, bandage, partial supply
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