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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).
Trickle charging tests on a battery at various loads and rotational speeds.

Identifier  WestWitteringFiles\J\January1923\  Scan10
Date  1st January 1923
  
Contd. -4- EFCL/T3.1.23.

of suitable value
with the loads of resistance proper for the job, with the steady
trickle charging current to the battery with no load on the
system, remained fairly closely at the value 2 amperes.
In the colder condition this current would be slightly less.
It will be understood that we are referring to the trickle
charge given to a battery which is otherwise fully
charged, all plates being in such a condition as to gas
vigorously with the normal charging current. If the battery
were not up to this state of charge, then owing to its smaller
E.M.F., this trickle current would be materially increased.
Tests were made with the dynamo unit in an
intermediate condition of temperature (45°C) of putting on
loads of various values in steps for three different rotational
speeds, viz. 760, 1500 and 2250, and the results obtained
are in accordance with the following tables:-

Speed. Amp. load on Amp. delivery Resultant current
R.P.M. system. of dynamo unit. charging or discharg-
ing (-) battery.
0 1.2 1.2
1.0 2.0 1.0
760 2.0 2.75 .75
3.0 3.7 .7
4.0 4.6 .6
5.0 5.6 .6
6.0 6.6 .6
7.0 7.5 .5
8.0 8.45 .45
9.0 9.45 .45
10.0 10.45 .45
11.0 11.4 .4
12.0 12.3 .3
13.0 12.75 -.25
14.0 12.8 -1.2
15.0 13.0 -2.0


Contd.
  
  


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