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Performance data report comparing the average of 8 R.A.E. pumps with an original R.A.E. pump on a Condor engine.


Identifier  WestWitteringFiles\N\July1925-September1925\  Scan11
Date  22th June 1925
  
-2-

Pump speed = .204 : 1
on the Condor(Aero Engine) engine.

AVERAGE OF 8 RAE. PUMPS.

REF.
Expl. No.
EXPERIMENTAL REPORT.
R.R. 493A (50H) (D.B. 175 25-9-24) J.H.D.

| Engine. R.P.M. Condor(Aero Engine). | Pump R.P.M. | Delivery. galls. min. | Does not start to pump until R.P.M = pump speed. | Slow speed continues pumping at R.P.M. | Time taken to start delivering. |
|---|---|---|---|---|---|
| 696 | | | 142.5 | | 20 secs. |
| 2200 | 449 | 77.3 | | | |
| 2000 | 408 | 71.7 | | | |
| 1900 | 388 | 64.5 | | | |
| 392 | | | | 80 | |

R.A.E. ORIGINAL PUMP No. 109 - fitted on Condor(Aero Engine) engine.

| | | | | | |
|---|---|---|---|---|---|
| 715 | | | 146 | | 2 mins. 30secs. |
| 2200 | 449 | 66 | | | |
| 2000 | 408 | 60 | | | |
| 1900 | 388 | 57 | | | |
| 514.7 | | | | 105 stops pumping. | |

Hs {Lord Ernest Hives - Chair} /TAG.
22. 6. 25
  
  
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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