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From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
Letter suggesting the use of a fusible alloy instead of mercury for cooling aeroplane engine spark plugs.

Identifier  ExFiles\Box 34\2\  Scan112
Date  25th May 1918
  
I.
F.R.
M.D. 28 MAY 1918
7 Churchill Terrace,
Holywood,
Co. Down.
25th May, 1918
Sir,
I believe that the sparking plug used on aeroplane engines is liable to become overheated.
I believe that if the mercury used for cooling were replaced by a fusible alloy the evil effects of the heating would be diminished.
If a suitable alloy were used it should be possible to have the alloy solid at the colder parts of the plug & liquid at the hotter. If this could be arranged it would mean that there would be continuous fusion & condensation solidification; in such a case the transference of heat to the radiating fins would be far more rapid than it could possibly be by conduction alone.
Should the sparking plug not work as I anticipate I think it would still
  
  


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