Recommending longer inlet cams and new low-stress valve springs for various aero engines.
| Identifier | ExFiles\Box 106\5\ scan0011 | |
| Date | 13th August 1927 | |
| X5060 RG. {Mr Rowledge} Hs. {Lord Ernest Hives - Chair} from R. {Sir Henry Royce} BY. {R.W. Bailey - Chief Engineer} c. to BJ. R1/M13.8.27. PHANTOM, GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)), CONDOR(Aero Engine) X.3822 X.8060 FALCON(Aero Engine). X.2993 X.5060 X.3616 Unless we know of some disadvantage of the longer inlet cam it should be used on all engines, because it reduces the risk of detonations at slower, and makes the valve spring situation easier. All new valve springs that are being made should be of low max. stress type, or at least with better figure of merit, by our formula not less than 1. From our latest investigations, to obtain the best figure of merit in a given valve spring space we find the 50% range type the best. Condor(Aero Engine) E.15421 and DES.96. are particularly bad ones which must be avoided at once. 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).