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Camshaft comparison between the Eagle Vlll and Eagle lX models.


Identifier  WestWitteringFiles\N\July1925-September1925\  Scan155
Date  25th September 1924
  
R.R. 493A (50H) (D.B. 175 25-9-24) J.H.D.

EXPERIMENTAL REPORT. -2- Expl. No. REF: Hs {Lord Ernest Hives - Chair} /TAG/LG26.8.25.

is fitted with Eagle(Aero Engine) lX. camshafts, which have 24° overlap,
that there is a big increase in power over the Eagle(Aero Engine) Vlll type
camshaft which has no overlap. The Eagle(Aero Engine) Vlll. curve is very
flat, and drops heavily from 2050 r.p.m. whereas the other
curve continues to rise, and is still rising at 2300 r.p.m. but
has a tendency to flatten.

The increase at 2300 r.p.m. = 78 B.HP. over the Eagle(Aero Engine)
Vlll. camshaft.

Note :- On each of these curves a small timing diagram is given
shewing the inlet opening and closing (the exhaust timing is
standard) position for the respective camshafts they represent,
also a small sketch intended to convey an idea of the induction
system layouts.

The B.HP. figures are corrected for barometer and
temperature on all the curves.

CURVE 11. CAMSHAFT COMPARISON.

The engine was fitted with :-
(1) Eagle(Aero Engine) Vlll. camshafts (no overlap)
(2) " lX " (24° " )
(3) " lX Carburetters and induction system.
(4) Standard pistons 5.27 to 1.

The fitting of the Eagle(Aero Engine) lX. type carburetters and
induction system has the effect, when used in conjunction with
the Eagle(Aero Engine) Vlll. camshafts, of giving a straight curve with
increased H.P. up to 2130 r.p.m. after which there is a sudden
droop as in Curve 1. With the Eagle(Aero Engine) lX. (overlap) camshaft,
the curve continues to rise at 2300 r.p.m. without any 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).


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