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).
Graph plotting heat dissipated to the cooler versus oil discharge through bearings for a 6 Cylinder Falcon engine at different compression ratios.
| Identifier | ExFiles\Box 179b\3\ img316 | |
| Date | 8th February 1933 guessed | |
| Hs{Lord Ernest Hives - Chair} 351. HEAT DISSIPATED TO COOLER TO KEEP INLET OIL AT 65°C CRANKCASE IN STILL AIR. TESTS MADE ON 6 CYL. FALCON UNIT. 2250 R.P.M. FULL THROTTLE. Y-Axis Label: B. Th. Us / MIN. X-Axis Label: OIL DISCHARGE THROUGH BEARINGS LBS/MIN. Curve Labels: 8 TO 1 COMPn RATIO 6 TO 1 COMPn RATIO Annotation: BAFFLES FITTED TO PISTONS TO PREVENT OIL SPLASHING ON THE HOT CROWNS. 8 TO 1 COMPn RATIO. | ||