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Performance estimate comparing a Goshawk II motor applied to a Goshawk I engine with a different reduction ratio.


Identifier  WestWitteringFiles\G\August1921\  Scan65
Date  30th August 1921
  
To R. {Sir Henry Royce} from EFC. {E. Fowler Clarke - Electrical Engineer} ORIGINAL EFC {E. Fowler Clarke - Electrical Engineer} 1/T30.8.21.
c.c. to CJ.
c.c. to E. {Mr Elliott - Chief Engineer}
c.c. to Da. {Bernard Day - Chassis Design}
c.c. to Da {Bernard Day - Chassis Design} /T. } at W. Wittering.

X.4384 - "GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II" MOTOR APPLIED TO
"GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) I" ENGINE.

We attach table showing our estimate of the
performance of the Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II motor as applied to Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) I
engine with a reduction ratio of 14.4 instead of 8.4 as
on Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II.

It will be seen that the relative performances
should be approximately in accordance with the following
table :-

Quantity. Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II. Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) I.
Motor volts. 9.26 10.1
Amperes. 137 95.5
Electrical H.P. 1.63 1.29
Motor speed. 810 1363
Engine speed. 96.5 94.5
B.H.P. .85 .835
Efficiency. 50% 64.6%

It will be remembered that the calculations
of the performances are made for these for the Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II
engine in a quite cold condition, so that in nearly every
case of starting the figures of operation here cited for
Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II are modified to more nearly those corresponding
to Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) I engine.

EFC. {E. Fowler Clarke - Electrical Engineer}

R R 322v (100 1) (2' H 168' 10-12-30) O 2071
  
  
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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