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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).
Table of measurements and tolerances for main and auxiliary switch unit gaps.

Identifier  ExFiles\Box 60\2\  Scan057
Date  25th February 1932
  
25. 2. 32.

MAIN AND AUXILIARY SWITCH UNIT GAP TABLES.

SCHEME OR UNIT :- .L

MAIN SWITCH
Position of Switch. Air gap at core centre. Core to Armature Stop. Copper gap (first blade to make). Carbon gap.

Off .084+4 .090+5 -3 .062+4 .025+5

Carbons just in contact. .071+1 -3 .074+2 .040 0

Coppers just in contact. .047 -2 .045 0 0

Full on. .010 -2 0 0 0

Mutual gaps :-
Full off .015+3
Full on .010+2

AUXILIARY SWITCH
Position. Air gap at core Gap between pole face & min. airgap. Gap at Upper contact Gap at lower contact

Off .060 .060 0 .017

Just making lower contact. .050 .048 .014 0

Full on. .010 -2 0 .070 0

Hs {Lord Ernest Hives - Chair} /wst.
  
  


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