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Blueprint for experimental piston ring type springs to replace plungers in a synchro-mesh system.


Identifier  ExFiles\Box 104\4\  scan0277
Date  11th March 1937
  
EXCEPT FOR THE 3 DETAILS QUOTED ALL OTHER PIECES ARE STANDARD TO 20/25 & BENTLEY.
3 HOLES, EQUALLY SPACED, IN EACH RING GROOVE.
WHEN ASSEMBLED AS SHOWN & WELL OILED THE INNER SLIDING PIECE SHOULD PULL OUT UNDER AN AXIAL LOAD OF 30-36 LBS. THIS IS THE FRICTIONAL DRAG WHEN THE RINGS ARE OUT OF THE GROOVES. SHOULD BE CHECKED BEFORE ASSEMBLING INTO A GEARBOX.
ANTI-RATTLERS & CAMS ARE UNALTERED.
SECTION AA. {D. Abbot Anderson}
NOTE THE SCHEME DELETES 6 PLUNGERS, 6 SPRINGS & 12 HOLES FROM THE INNER SLIDING PIECE & SUBSTITUTES 2 SPRING RINGS & THEIR GROOVES. NO LIGHTENING HAS BEEN DONE AS WE MERELY WISH TO TEST THE RINGS AT THIS STAGE. THE STRESS RANGE IN THE SPRINGS IS 77,200 - 102,000 LB/SQ".
EXPERIMENTAL PISTON RING TYPE SPRINGS
TO REPLACE PLUNGERS - SYNCHRO-MESH
SCALE 1/1
N&H 5065
RS. {Sir Henry Royce's Secretary} 458
RS. {Sir Henry Royce's Secretary} 456
RS. {Sir Henry Royce's Secretary} 457
RECEIVED W-ROYCE LTD HUCKNALL
d'Asworth 10/3/37
  
  
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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