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Blueprint comparing two rear leaf spring designs, one with 5 plates and the other with 6 plates.


Identifier  ExFiles\Box 154\1\  scan0046
Date  26th January 1933
  
REAR SPRING TO ROLLS-ROYCE DRG F.B. 22 5-PLATES. 750 LBS LOAD. 4" DEFLECTION DUE TO LOAD. 25". 19 1/2". 8 5/8". 9". 20 3/8". TOTAL DEPTH 1.45". MAINPLATE .30 THICK. RANGE OF STRESS TO THE LOADED POSITION 25.0 TONS PER SQ. IN. SEAT 3.575". FRONT EYE. REAR EYE. 1 1/8" MAX TAPER 3". A. {Mr Adams} REAR SPRING TO ROLLS-ROYCE DRG F.B. 22 6-PLATES. 750 LBS LOAD. 4" DEFLECTION DUE TO LOAD. 25". 16". 7 1/8". 8". 17". TOTAL DEPTH 1.65". MAINPLATE .29 THICK. RANGE OF STRESS TO THE LOADED POSITION 24.1 TONS PER SQ. IN. SEAT 3.575". FRONT EYE. REAR EYE. 1 1/8" MAX TAPER 3". B. REFERENCE ROLLS-ROYCE LETTER DATED 24TH JAN 1933. SCALE HALF FULL SIZE. DRAWING No 82. THOS. FIRTH & JOHN BROWN LTD. SPRING DEPARTMENT. TINSLEY. SHEFFIELD. 26TH JANUARY 1933.
  
  
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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