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Tests conducted on an aero engine petrol pump.


Identifier  WestWitteringFiles\N\July1925-September1925\  Scan322
Date  29th September 1925
  
R.R. 493 (40 H) (SL 42 12-7-23). J.H., D. {John DeLooze - Company Secretary}
ORIGINAL
EXPERIMENTAL REPORT.
COPIES TO: (R)(CJ)(BJ)(WOR {Arthur Wormald - General Works Manager} )(By)(E)(DA {Bernard Day - Chassis Design} )(EP {G. Eric Platford - Chief Quality Engineer} ) PNMOYR (RG {Mr Rowledge} )
Expl. No. 7409 / X4535
REF. Hs {Lord Ernest Hives - Chair} 3/LG29.9.25.
OBJECT OF TEST.
Tests on R-R aero engine Petrol Pump.
TESTER.
A. {Mr Adams} A. {Mr Adams} Rubbra.
CONDITIONS.
Hangar test.
SUMMARY OF TEST.
The relief valve on the pump was a failure. When the relief valve was done away with the pump worked very satisfactorily. Without the relief valve the pump works better than the R.A.E. type petrol pump - see report Hs {Lord Ernest Hives - Chair} /TAG/LG27.6.25. We consider the improvement is due to the method of oiling the pump gears.
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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