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; Aeroplane v 82 n 2127 Apr 25 1952 p 494-7; Aviation Week v 56 n 26 June 30 1952 p 21-2, 24-6, 29, 32)


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    Title :

    Application of titanium to aircraft engines


    Additional title:

    Iron Age


    Contributors:

    Published in:

    Iron Age ; 169 , n 20


    Publication date :

    1952


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Application of titanium to aircraft engines

    Hanink, H.H. | Engineering Index Backfile | 1952


    Application of titanium to aircraft engines

    Hanink, H.H. | Engineering Index Backfile | 1952


    APPLICATION OF TITANIUM TO AIRCRAFT ENGINES

    HANINK, H. H. | SAE Technical Papers | 1952


    Application of titanium to aircraft engines

    Hanink, H.H. | Engineering Index Backfile | 1952


    Application of titanium to aircraft engines

    Hanink, H.H. | Engineering Index Backfile | 1952