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Tests with longer connecting rods to address over-run vibrations in an EAC engine.


Identifier  ExFiles\Box 72\1\  scan0154
Date  1st May 1924
  
R.R. 493A (20H) (D.A. 652 20-3-24) J.B.D.

Y9030
Expl. No. 9550 9030
REF: Hs {Lord Ernest Hives - Chair} 2/LGS.5.24.

EXPERIMENTAL REPORT.

S E C R E T.

To R. {Sir Henry Royce} from Hs. {Lord Ernest Hives - Chair}
c. to CJ. RG. {Mr Rowledge}
c. to DA. {Bernard Day - Chassis Design} E. {Mr Elliott - Chief Engineer}
c. to BY. {R.W. Bailey - Chief Engineer} WOR. {Arthur Wormald - General Works Manager}

EAC. ENGINE - OVER-RUN VIBRATIONS.

We have carried out tests with longer connecting
rods (Hawk(Aero Engine) engine type) fitted to the above engine.

The rods were changed over twice & in order to
confirm the results.

The longer rods do make the engine appreciably
smoother on retard, but there was still left a slight
period of much reduced amplitude at the same speed.

We are preparing to test the longer rods in
conjunction with the stiffer engine coupling shaft on
a second EAC. engine which is rather a worse example
for over-run vibrations.

Hs. {Lord Ernest Hives - Chair}
  
  
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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