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Graph showing the variation in angular deflection versus torque for a Kestrel engine's reduction gear spring coupling.


Identifier  ExFiles\Box 179\2\  img262
Date  5th February 1932
  
KESTREL(Aero Engine) ENGINES
CURVE 283'F'
REDUCTION GEAR SPRING COUPLING - D.F.S. 1335
VARIATION IN ANGULAR DEFLECTION OF VARIOUS UNITS
WITH INCREASING TORQUE, MEASURED IN DEGREES OF CRANKSHAFT MOVEMENT
ORIGINAL SPRINGS E.36802
Y-AXIS: ANGULAR DEFLECTION - CRANKSHAFT DEGREES
X-AXIS: TORQUE APPLIED TO PROP SHAFT LBS-FT
PLOT LINES:
- PROP SHAFT
- SPRING DRIVE TO REDN GEAR
- FRONT END OF C.SHAFT
STAMP: G.P. 5.2.32
  
  
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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