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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).
Calculation of the weight and polar moment of inertia for various engine components.

Identifier  ExFiles\Box 65\4\  scan0167
Date  4th November 1926 guessed
  
contd :- -2-

PART. WEIGHT. lbs. POLAR MOMENT OF INERTIA. (W/g K^2)

Crankshaft complete - 75.875 .06738 units.
Big end of conn. rod
(2.64 lbs. each -
total for six) - 15.84 .02579 "
Spring drive parts - 14.125 .01437 "
Flywheel complete with
clutch - 168.25 1.384 "


The spring drive parts do not include the slipper
wheels because being free to slip they do not add to the polar
inertia in this case. The equivalent rotating weight
of the conn. rods was found approximately by weighing the big
ends while supporting the other end horizontally and they were
of the loose shell type.

Having determined the stiffness of the shaft and
the inertia of the parts, we were able to estimate the fundamental
or free period of oscillation of the system, also the position
of the nodal point - by calculation.

The nodal point depends upon the disposition and
inertia of the various masses and in this particular case works
out at 1.6" from the flywheel end.

As the node is situated so near to the flywheel we
can, without introducing any serious error, assume the inertia of
the crankshaft to be replaced by an equivalent mass at the front
end. This equivalent mass would then have one-third the total
inertia of the crankshaft and would be added to the inertia of
the spring drive.
contd :-
  
  


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