Accession Number : ADD001724
Title : Non-Abradable Turbine Seal.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Profant,Daniel
Report Date : 03 Jun 1975
Pagination or Media Count : 4
Abstract : The patent relates to a non-abradable turbine seal for use between the blade member and surrounding shroud of the turbine engine. The seal may take on a variety of configurations, any one of which constructed to allow deformation thereof by the blade member, either because of rotor growth or shroud eccentricities. The seals are made of oxidation resistant compressible or crushable materials in the form of thin metallic foil, pads, ceramic hollow spheres or thin walled tubing.
Descriptors : *Gas turbines, *Turbine blades, *Seals(Stoppers), *Patents, Deformation, Sealed systems, Wear resistance, Turbine parts
Subject Categories : Adhesives, Seals and Binders
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE