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Hiduminium information


Six cylinder, 5 litre, all-Hiduminium engine for the Armstrong Siddeley Special

The Hiduminium alloys or R.R. alloys are a series of high-strength, high-temperature aluminium alloys, developed for aircraft use by Rolls-Royce ("RR") before World War II.[1] They were manufactured and later developed by High Duty Alloys Ltd.[1] The name Hi-Du-Minium is derived from that of High Duty Aluminium Alloys.

The first of these Hiduminium alloys was termed 'R.R.50' .[1] This alloy was first developed for motor-racing pistons,[2] and was only later adopted for aircraft engine use. It was a development of the earlier Y alloy, the first of the nickel-containing light aluminium alloys.[3] These alloys are one of the three main groups of high-strength aluminium alloys, the nickel-aluminium alloys having the advantage of retaining strength at high temperatures, making them particularly useful for pistons.

A Rolls-Royce R engine
Publicité dans La France Libre - octobre 1944.
  1. ^ a b c Camm, Frederick (January 1944). "R.R. Alloys". Dictionary of Metals and Alloys (3rd ed.). p. 102.
  2. ^ Camm, Frederick (January 1944). "Hiduminium". Dictionary of Metals and Alloys (3rd ed.). p. 58.
  3. ^ Murphy, A. J. (1966). "Materials in Aircraft Structures". The Journal of the Royal Aeronautical Society. 70 (661): 117. doi:10.1017/S0001924000094021. ISSN 0368-3931. S2CID 114130292.

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