By substituting aluminum forgings for steel, weight of flexible engine suspension for Pratt and Whitney R-4360 engine was reduced from 134 to 71.5 lb; mounting described; endurance life of link; conclusions from fatigue tests on 26 assemblies; redesign of link explained; it incorporates antifretting corrosion reliefs and chromic acid anodizing.
Fatigue life of aircraft engine mounting components
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 58 , n 4
1950
4 pages
Article (Journal)
English
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Fatigue Life Of Aircraft Engine Mounting Components
SAE Technical Papers | 1950
|Emerald Group Publishing | 2002