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Increasing the power of the Eagle engine.


Identifier  WestWitteringFiles\N\July1925-September1925\  Scan153
Date  1st August 1925
  
R.R. 493 (40 H) (SL 42 12-7-23). J.H. D. {John DeLooze - Company Secretary}
EXPERIMENTAL REPORT.
COPIES TO: RCJ, BJ, WOR {Arthur Wormald - General Works Manager} , By. {R.W. Bailey - Chief Engineer} E. {Mr Elliott - Chief Engineer} EP. {G. Eric Platford - Chief Quality Engineer} BG
Expl. No. 22437
REF. Hs {Lord Ernest Hives - Chair} 7/LG28. 8. 25.
OBJECT OF TEST.
TESTER
Increase power of Eagle(Aero Engine) engine;
T.A. Gibson.
A. {Mr Adams} Rubbra.
CONDITIONS.
Test bench.
SUMMARY OF TEST.
It will be seen from the attached report and curves that the Eagle(Aero Engine) engine is capable of being boosted up to a considerable increase in H.P. It would appear that we have by no means exhausted the possibility of improvements in induction pipes. Valve timing could also be usefully investigated further.
Hs. {Lord Ernest Hives - Chair}
  
  
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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