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The production of the 'Goshawk' 11 Coil for battery ignition, detailing wire specifications and winding instructions.


Identifier  ExFiles\Box 45\4\  Scan007
Date  2nd February 1922
  
H.R. 235c (10 T) (S.J 194.9.6.21).

x2079a

RECEIVED 8 FEB 1922 EFC {E. Fowler Clarke - Electrical Engineer}

BY {R.W. Bailey - Chief Engineer} /WER11/EF9. 2. 22.

"GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine))" 11. COIL FOR BATTERY IGNITION
SECTION 8140.

We have released the above unit for production less the following parts:-

Primary Winding ( for our latest instructions to the Experimental Dept., see BY {R.W. Bailey - Chief Engineer} /WER2/EF16.1.22)

Secondary " (for our latest instructions to the Experimental Dept., see BY {R.W. Bailey - Chief Engineer} /WER5/EF27. 1.22)

Regarding the secondary winding we propose using all the 43 S.W.G. enamel coated covered wired that is in stock, after that any future orders will of course be to the standard wire i.e.,44 S.W.G.

We hope to shortly hear from you that the coils wound with the above windings are O.K. so that we may release the wire for production purposes.

BY {R.W. Bailey - Chief Engineer} /WER.
W.R.
  
  
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).


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