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Graph plotting combustion volume distribution and flame travel for a D.H. Aero Engine.


Identifier  ExFiles\Box 127\4\  scan0096
Date  24th February 1938
  
COMBUSTION VOLUME DISTRIBUTION
MOTOR: D. {John DeLooze - Company Secretary} H. {Arthur M. Hanbury - Head Complaints} AERO ENGINE
ESTIMATED B.M.E.P.
COMPRESSION RATIO
MAX RATIO LOCATION
6.5 6 5
COMPRESSION RATIO
% VOLUME INCREASE IN PER CENT
RATIO
% TRAVEL INCREASE
FLAME VOLUME IN PER CENT
FLAME TRAVEL PER CENT
MAX RATIO
PER B.M.E.P.
90
105
120
FEB 24 1938
A
R.H.Y / 12/11/36
W.S.
FORM T-D
COPYRIGHTED 1934 ALEX TAUB
  
  
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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