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Requesting instructions for Goshawk II engine cams based on Goshawk I valve lift curves.


Identifier  WestWitteringFiles\F\January1921\  Scan80
Date  28th January 1921
  
ORIGINAL
ES/G27/A/21. 3
To: Dr. from E. {Mr Elliott - Chief Engineer} [Dr. is struck through]
Copy to N.L. [Struck through]
E.H. [Struck through]
R.W. [Struck through]
EFC. {E. Fowler Clarke - Electrical Engineer} X.4229
RE "GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II" CAMS.
Will you kindly instruct for "Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II" engine cams which will give the movement prescribed by the "Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) I" valve lift curves Lec.1048/1050 with the mechanism shown on drawing Lec.1332.
[Stamp: E. {Mr Elliott - Chief Engineer} EFC {E. Fowler Clarke - Electrical Engineer} RECEIVED JAN 20 1922]
[Stamp: D RECEIVED 28 JAN 1921]
  
  
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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