Comparing carburettors and compression ratios on Eagle Vlll and Eagle IX engines.
| Identifier | WestWitteringFiles\N\July1925-September1925\ Scan157 | |
| Date | 1st August 1925 | |
| R.R. 493A (50H) (D.B. 175 25-9-24) J.H.D. EXPERIMENTAL REPORT. -4- Expl. No. REF: Hs {Lord Ernest Hives - Chair} /TAG/LG26.8.25. As in the previous curve the 4 Eagle(Aero Engine) Vlll carbs. are predominant at low speeds up to 2200 r.p.m. where the curve flattens out and crossing the Eagle(Aero Engine) lX. at 2280 r.p.m. - the Eagle(Aero Engine) lX. curve is still continuing to rise at 2300 r.p.m. The B.M.E.P. curves are very much better than those where the 5.27 to 1 pistons are fitted. CURVE V. {VIENNA} CARBURATTER COMPARISON 6.28 to 1. The engine was fitted with :- (1) Eagle(Aero Engine) lX. camshafts (overlap) (2) " Vlll carburetters and induction pipes. (3) " lX " " (4) Very high compression pistons 6.28 to 1. For these curves the range of speed was increased to 2400 r.p.m. As in the previous curves the Eagle(Aero Engine) Vlll. carbs. have the advantage at the lower speeds up to about 2265 m.p.m. and then flattens out crossing the other at 2265 r.p.m. Whereas with the Eagle(Aero Engine) lX. the peak of the curve appears to be much higher than 2400 r.p.m. CURVE Vl. {V. Lewis / Mr Valentine} COMPRESSION RATIO COMPARISON. These curves show the increased power obtained by increasing the compression ratios :- from 5.27 to 1 std. (1) to 6.09 to 1 and then - (2) to 6.28 to 1 (3) Eagle(Aero Engine) lX. camshafts. (4) " carburetters and induction pipes. With the 5.27 to 1 and 6.09 to 1 compression ratio the curves are practically parallel with a greater increase in power at higher speeds. 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).