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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).
Modifications to the Phantom II air inlet silencer to reduce power loss.

Identifier  ExFiles\Box 13\3\  03-page192
Date  28th January 1930
  
BY.{R.W. Bailey - Chief Engineer} FROM E.{Mr Elliott - Chief Engineer}
.17080
E2/M28.1.30.
Copy to SG.{Arthur F. Sidgreaves - MD}
Copy to HS.{Lord Ernest Hives - Chair}
PHANTOM 2. AIR INLET SILENCER.

We send you herewith a blueprint of LeC.2786.
shewing the above modified to reduce the power lost
which occurred with the original design.
We have reinstated the standard diameter of suction
chamber, air valve, and high speed choke.
The air supply passage to the air valve has
also been enlarged at the expanse of some height added to
the jet control and the suction chamber, but this has been
kept down to a minimum particularly to enable us to with-
draw these parts without fouling the induction pipe.
The completed drawing will follow shewing details
of the breather attachment to crankcase.

E.{Mr Elliott - Chief Engineer}
  
  


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