Induction pipe arrangements for various engines and proposing fuel distribution tests.
| Identifier | ExFiles\Box 183\M22\ img240 | |
| Date | 29th December 1922 | |
| S.R. 235a (100 T) S.H. 159 (1-8-20) G. {Mr Griffiths - Chief Accountant / Mr Gnapp} 2800 INDUCTION PIPES - H-N o SEAGULL(Experimental EAC.1 aka Export chassis, Phantom I engine) ORIGINAL TO HS. {Lord Ernest Hives - Chair} EY. FROM R DEC 29 1922 c. to CJ. BJ. RG. {Mr Rowledge} RECEIVED RE. HAWK(Aero Engine)-NORTHCLIFFE R5/M27.12.22. X3408 X4305 We are very pleased with the behaviour of the induction pipe on the Hawk(Aero Engine)-Northcliffe, and we should not lightly depart from the principles involved in this arrangement. It is the one we propose to try for "Seagull(Experimental EAC.1 aka Export chassis, Phantom I engine)" though we believe the still more simple arrangement as applied to Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) would be satisfactory if sufficient heat is added directly after the carburetter, such as around the throttle valve. Distribution, in both aero engines and car engines, both hot and cold, with good and bad petrol should be one of the most important features to study, and we should get some standard tests with standard badness of fuel. R. {Sir Henry Royce} | ||
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).