Accession Number : ADA119829
Title : Material Characterization. Part B. Mechanical Properties of Two Metal Matrix Composite Materials.
Descriptive Note : Interim technical rept. 1 Oct 77-30 Jun 80,
Corporate Author : GENERAL ELECTRIC CO CINCINNATI OH AIRCRAFT ENGINE BUSINESS GROUP
Personal Author(s) : Emery,Susan A
PDF Url : ADA119829
Report Date : May 1982
Pagination or Media Count : 49
Abstract : This report describes mechanical property data collected in support of a fan blade analysis model. The development of the blade model is part of a foreign object damage (FOD) study of jet engine fan blades. Use of the properties in the model allows one to evaluate potential fan blade materials. Part A of this report contains a discussion of the mechanical property tests conducted on two metallic materials: 410 stainless steel and 8A1-1Mo-1V titanium. These two materials were selected because of their use in the J-79 blade and F-101 blade, respectively. Part B of the report contains a discussion of mechanical property tests conducted on the two composite components of a hybrid composite blade: boron/2024 aluminum and stainless steel wire mesh/2024 Aluminum. These two composites are used in the hybrid composite APSI blade. Quasi-static tensile tests and torsional tests were conducted on unidirectional specimens for the two composites indicated above.
Descriptors : *Composite materials, *Metals, *Matrix materials, *Mechanical properties, *Fan blades, Jet engines, Ingestion(Engines), Static tests, Tensile strength, Modulus of elasticity, Poisson ratio, Shear properties, Failure(Mechanics), Strain(Mechanics), Unidirectional, Thickness, Rods, Stainless steel, Boron compounds, Aluminum alloys, Titanium alloys, X rays, Equations, Birds, Ice, Sand
Subject Categories : Aircraft
Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE