Test bench figures for the Goshawk I engine's starting torque and advance.
| Identifier | ExFiles\Box 54\5\ Scan147 | |
| Date | 28th April 1921 | |
| x3985 To R from Hs {Lord Ernest Hives - Chair} ; c. to CJ. c. to BN. {W.O. Bentley / Mr Barrington} c. to E. {Mr Elliott - Chief Engineer} c. to Da. {Bernard Day - Chassis Design} c. to BY. {R.W. Bailey - Chief Engineer} Hs {Lord Ernest Hives - Chair} 9/LG28.4.21. X3481 X2949 X-3485 RE. GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) 1 ENGINE. We are running Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine))1 engine on the Test Bench. We have measured the torque necessary to turn this engine. Below are the figures:- Starting of Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) engine. (COLD) | Motor volts. | Amps. | R.P.M. speed. | Initial kick. | |--------------|-------|---------------|---------------| | 9.5 | 96 | 85 | 125 amps. | | 9.5 | 96 | 85 | -- | (HOT) | 10.65 | 47.0 | 140 | 80 amps. | | 10.65 | 48.0 | 145 | -. | 40/50 Starter Motor with total reduction of 12 to 1. We have also taken again the figures for the amount of advance required with the Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) engine. We have taken these figures by means of a drum fixed to the dynamometer shaft and taken a high tension wire from one of the plugs to this drum to mark exactly where the spark takes place. These figures can be taken as correct. The figures given in our Hs {Lord Ernest Hives - Chair} 5/LG14.4.21 should not be worked to. Contd. | ||
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).