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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).
Calculations for end thrust and its horizontal component along a bushing.

Identifier  ExFiles\Box 83\2\  scan0251
Date  23th February 1938
  
-2-

23rd. February 1938.

B.III.
Mms. abt. b.

145 x 5.6 = add. end thrust in top lever x 10

∴ Additional end thrust = 81.3

∴ Horizontal component along bushing

= 81.3 Cos 67½

= 31.3 lb.

Rm{William Robotham - Chief Engineer}/Mr.Kennington.
  
  


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