Problems analyzed that must be solved before titanium may be widely used, are its high cost, creep properties, fatigue strength, etc; possibility of 40% saving in deadweight indicated when using titanium alloys in crankshaft and connecting rods of reciprocating aircraft engine, in place of alloy steel; illustrations. (See also Soc Automotive Engrs -- J v 60 n 8 Aug 1952 p 25-30; Automotive Industries v 107 n 1 July 1 1952 p 72, 82, 84, 94; Iron Age v 169 n 20 May 15 1952 p 121-5; Aviation Week v 56 n 26 June 30 1952 p 21-2, 24-6, 29, 32)
Application of titanium to aircraft engines
Aeroplane
Aeroplane ; 82 , n 2127
1952
4 pages
Article (Journal)
English
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Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|APPLICATION OF TITANIUM TO AIRCRAFT ENGINES
SAE Technical Papers | 1952
|Application of titanium to aircraft engines
Engineering Index Backfile | 1952
|