Email RIS file
Bookmark
Report an Issue

Turbine disc sealing assembly [electronic resource].

Published
Washington, D.C. : United States. Dept. of Energy, 2013.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy
Additional Creators
National Energy Technology Laboratory (U.S.), United States. Department of Energy, and United States. Department of Energy. Office of Scientific and Technical Information
Access Online

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Free-to-read Unrestricted online access
Summary
A disc seal assembly for use in a turbine engine. The disc seal assembly includes a plurality of outwardly extending sealing flange members that define a plurality of fluid pockets. The sealing flange members define a labyrinth flow path therebetween to limit leakage between a hot gas path and a disc cavity in the turbine engine.
Report Numbers
E 1.99:8,388,310
8,388,310
Subject(s)
Note
Published through SciTech Connect.
03/05/2013.
"8,388,310"
"12/022,302"
Diakunchak, Ihor.
Funding Information
FC26-05NT42644
View MARC record | catkey: 23492096