Pictorial and schematic diagrams of the Condor battery ignition system.
| Identifier | ExFiles\Box 180\M2\M2.1\ img005 | |
| Date | 25th June 1918 | |
| To BV FROM E DA {Bernard Day - Chassis Design} Copy to EH EFC {E. Fowler Clarke - Electrical Engineer} HT CONNECTION CONDENSER IF IT WERE DECIDED LATER TO USE A SIMPLE EARTHED SYSTEM THIS WOULD BE ACCOMPLISHED BY MAKING EARTH CONNECTIONS AT POINTS MARKED E SWITCH BATTERY CONTACT BREAKER CONDENSER PICTORIAL & DIAGRAMATIC SCHEMES OF LOW TENSION CIRCUIT NOTE - LT CIRCUIT IS NOT EARTHED COIL SWITCH & BALANCE RESISTANCE BATTERY CONDOR(Aero Engine) BATTERY IGNITION 25-6-18 H.C.E. | ||
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).