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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).
Test report on a roller propellor shaft sliding joint, detailing wear issues and proposing a change in material.

Identifier  ExFiles\Box 87\3\  scan0018
Date  15th November 1934
  
x237

To E.{Mr Elliott - Chief Engineer}
c. to Da.{Bernard Day - Chassis Design}
c. to By.{R.W. Bailey - Chief Engineer}
c. to Hdy.{William Hardy}

Hs{Lord Ernest Hives - Chair}/Gry.{Shadwell Grylls}S/KW.15.11.34.

Roller Propellor Shaft Sliding Joint.

Tests on this joint to N.Sch.3647 show that under a torque of 150 lbs/ft. the end load required to slide the joint is about 15 lbs. compared with 150 lbs. of the ordinary joint.

After a few thousand miles on the road the rollers had worn slight ridges on the thrust faces of the sliding member. These ridges naturally prevent easy sliding of the joint and we shall try making this part in nitrided V.C.M.

This joint will run 10,000 miles on S-B-IV.

Hs{Lord Ernest Hives - Chair}/Gry.{Shadwell Grylls}
  
  


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