Accession Number : AD0164673
Title : Fixture for Tensile and Stress Rupture Testing of Turbine Blades.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Struthers,John O. ; Miller,John A. ; Boucher,Raymond R.
Report Date : 09 APR 1974
Pagination or Media Count : 3
Abstract : The patent describes a fixture to hold turbine blades, too small for conventional test-bar testing methods, which grasps the root and tip end of the blade. The fixture is formed of a suitable metal alloy and is molded to fit the blade tip and root, and is adapted to be secured to the testing machine.
Descriptors : *Gas turbine blades, *Test equipment, *Patents, Tensile properties, Stresses
Subject Categories : Test Facilities, Equipment and Methods
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE