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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).
Testing the fitting and running of new CH. AVT.64 carburetters on a Falcon X engine.

Identifier  ExFiles\Box 42\3\  Scan013
Date  1st October 1926
  
S.S. 493 (40 H) (SL 42 12-7-23). J.H., D.{John DeLooze - Company Secretary}
X3841
EXPERIMENTAL REPORT. 1.10.26
COPIES TO: RCJ. BJ WOR.{Arthur Wormald - General Works Manager} Sy E Da.{Bernard Day - Chassis Design} EP.{G. Eric Platford - Chief Quality Engineer} PN.{Mr Northey} OY. (RG{Mr Rowledge})
Expl. No. 2917a
REF. Hs{Lord Ernest Hives - Chair}1/LG4.10.26
OBJECT OF TEST.
Testing the fitting and running of the new CH. AVT.64 carburetters in the Vee.
TESTER.
V.{VIENNA} Halliwell.
CONDITIONS.
2nd. Falcon X, (six-cyl. engine).
Compression ratio 6.1 to 1.
SUMMARY OF TEST.
The Claudel carburetters in the Vee. being fitted up. The inter-control for the butterfly throttles on each carburetter had to be removed as it fouls the present water jackets on the castings.
E.28308 castings were removed after a short run, being required on the 3rd. F.X. engine. The indications pointed to the fact that the sizes of jets as supplied with the carburetter were too small.
Hs{Lord Ernest Hives - Chair}/V.Halliwell.
  
  


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