Open AccessImproving the design of the seal gaps in the flow of the pumping unit GTK-10-4.
Author(s) -
Виктор Перевезенцев,
Виктор Перевезенцев,
Максим Шилин,
Максим Шилин
Publication year - 2015
Publication title -
vestnik brânskogo gosudarstvennogo tehničeskogo universiteta
Language(s) - English
Resource type - Journals
ISSN - 1999-8775
DOI - 10.12737/22746
Subject(s) - turbomachinery , seal (emblem) , honeycomb , mechanical engineering , honeycomb structure , gas turbines , flow (mathematics) , thermal , unit (ring theory) , engineering , mechanics , materials science , physics , aerospace engineering , mathematics , thermodynamics , composite material , art , visual arts , mathematics education
Describes the methods of modernization seal the radial clearance of the gas turbine by using the honeycomb structure at the periphery of the wheel. Discusses the gas-dynamic and thermal engineering problems using honeycomb seals in turbomachinery.