Engine Truss Mount Analysis
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Applied Mechanics Division © 1987-2012 Mercer Engineering Research Center 135 Osigian Blvd. • Warner Robins, GA 31088 info@merc-mercer.org • www.merc-mercer.org • 478.953.6800 Truss Mount Finite Element Mesh Predicted Truss Mount Stresses Due to Loading MERC Engineer Reviewing Truss Mount MERC re-evaluated aircraft engine truss mount grind out limits for corrosion and mechanical damage. MERC determined that the grind out limits could be increase significantly, based on static strength and damage tolerance analysis. This provided the customer with significant savings by extending the life of the parts.Engine Truss Mount Analysis
 
Engine Truss Mount AnalysisEngine Truss Mount Analysis