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The disappointing bump test results for Firths springs on the Goshawk 11.


Identifier  ExFiles\Box 52\2\  Scan026
Date  17th January 1922
  
X4429

To H. {Arthur M. Hanbury - Head Complaints} from Hs. {Lord Ernest Hives - Chair}
c. to CJ.
c. to R. {Sir Henry Royce}
c. to De.
c. to BY. {R.W. Bailey - Chief Engineer}
c. to EP. {G. Eric Platford - Chief Quality Engineer}
c. to Wor. {Arthur Wormald - General Works Manager}
c. to Wd. {Mr Wood / Mr Whitehead}

Hs {Lord Ernest Hives - Chair} 1/LG17.1.22.

FIRTHS SPRINGS FOR GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) 11.
X2628 (crossed out)
X4429
X4219

Under pressure from us, Messrs. Firths have recently supplied us with a number of top leaves for the front and rear springs of Goshawk(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) 11. We have tested these springs on the Bump test - the results are disappointing. So far we have broken four top leaves - they have run for -

15 1/4 hours.
11 1/4 "
8 1/2 "
2 1/4 "

The average life of the Woodhead spring is approx. 12 1/2 hours - it varies between 9 1/4 and 16 hours.

It will be seen that we are much worse off with Firths springs.

BY. {R.W. Bailey - Chief Engineer} is taking up the question of material and treatment with the makers.

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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