Rolls-Royce Archives
         « Prev  Box Series  Next »        

Test data on the thermal efficiency and power of the 40/50 test engine at low compression, including a heat balance analysis.


Identifier  WestWitteringFiles\K\September1923\  Scan26
Date  12th July 1923 guessed
  
SHEET 2. LOW COMPRESSION (PRESENT STD.)

THERMAL EFFICIENCY, POWER ETC. OF THE 40/50 RR. TEST ENGINE.
COMPRESSION RATIO 3.9 - ENGINE CLEAN - FUEL 'SHELL' NO.2.
S.G. .752. CAL. {Mr Calvert} VALUE (LOWER) 19,000 B.Th.U's/LB.

[TABLE 1]
R.P.M. | Fuel pts. hr. | Pts. HP. hr. | B.H.P. | I.H.P. | HP. req. drive motor. | Jacket water. °C Inlet.Outlet. | Lbs. water min. | B.Th.U's. min. to water. | Mech. effcy.
500 | 18.09 | 0.78 | 23.1 | | 4 | 57.75 | 80 | 41 | 1660 |
750 | 26.27 | 0.78 | 33.67 | | 5.5 | 58 | 78 | 62.5 | 2250 |
1000 | 32.14 | 0.706 | 45.42 | | 8 | 61 | 81 | 82.5 | 2970 |
1250 | 40.45 | 0.71 | 56.75 | | 11.5 | 64.5 | 81.5 | 103.5 | 3167 |
1500 | 46.75 | 0.70 | 66.25 | | 15.5 | 65 | 80 | 126 | 3402 |
1750 | 52.9 | 0.71 | 74.75 | | 20 | 66.5 | 80.5 | 150 | 3780 |
2000 | 58.53 | 0.75 | 77.29 | | 26 | 70.5 | 83 | 177 | 3982 |

HEAT BALANCE.

[TABLE 2]
R.P.M. | 500 | 750 | 1000 | 1250 | 1500 | 1750 | 2000
Thermal equt. work done. | 980 | 1428 | 1927 | 2407 | 2809 | 3171 | 3278
Loss to engine friction. | 169 | 233 | 339 | 488 | 636 | 847 | 1103
Heat loss to jackets. | 1660 | 2250 | 2970 | 3167 | 3402 | 3780 | 3982
Ht. loss through exh. & radiation by difference. | 2577 | 3909 | 4332 | 5978 | 7073 | 7952 | 9067
Heat supplied. | 5386 | 7820 | 9568 | 12040 | 13920 | 15750 | 17430
  
  
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).


Copyright Sustain 2026, All Rights Reserved.    whatever is rightly done, however humble, is noble
An unhandled error has occurred. Reload 🗙