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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).
Low depression carburettor experiments for the Phantom model, including a sketch of the adapted manifold.

Identifier  ExFiles\Box 66a\1\  scan0200
Date  3rd November 1927
  
To R.{Sir Henry Royce} from Hs{Lord Ernest Hives - Chair}/ACL.
c.c. to BJ. Wor.{Arthur Wormald - General Works Manager}
c.c. to RG.{Mr Rowledge} E.{Mr Elliott - Chief Engineer}
c.c. to DA.{Bernard Day - Chassis Design} BY.{R.W. Bailey - Chief Engineer}

X8080

Hs{Lord Ernest Hives - Chair}/ACL1/LG3.11.27.

PHANTOM CARBURETTERS - LOW DEPRESSION
EXPERIMENTS.

..We have carried out some experiments on the
Phantom with a single low depression carburetter with the object
of finding the dimensions of the choke and pipe which would give
a manifold depression of about one inch of mercury at a speed of
3000 r.p.m. and so improve the volumetric efficiency at these
higher speeds.

The induction manifold used was adapted from the
std. Phantom manifold by altering
the angle of the centre flange to
which the uptake pipe was bolted -
as shewn in this sketch. A 2" dia.
down pipe and throttle was used.

The carburetter
had a choke of 1.6" dia. and in
the centre of this was used a
Claudel diffuser of .700 dia.

The sketch below
shews the arrangement of the carburetter. The free area past
the diffuser in the choke was 1.625 sq.ins. or 51.8% of the
throttle bore area.

At 3000 r.p.m. full throttle the depression
in the uptake pipe was 2.3 ins. mercury - the power output was
110.8 B.HP. or 62.5 lbs/sq.in. B.M.E.P. contd :-

[Text from diagram]
STD MANIFOLD.
FLANGE FITTED AT DIFFERENT ANGLE
4"
8"
  
  


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