z-logo
open-access-imgOpen Access
Improving the design of the seal gaps in the flow of the pumping unit GTK-10-4.
Author(s) -
Виктор Перевезенцев,
Максим Шилин
Publication year - 2015
Publication title -
bulletin of bryansk state technical university
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.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom