This report gives some load distribution along face width of main gear from tooth root strain measured by strain gauges. Measurement was made under 1/4, 2/4, 3/4 and 4/4 load of main propulsion turbine with the vessel at both ballasted and fully loaded draft.
Consequence of measurement were follows.
(1) Max. load sharing ratio was 1.7.
(2) Pattern of load distribution along face width was a little different from the calculated one.
(3) The draft of vessel or the load of main propulsion turbine reflected scarcely on the pattern of load distribution along face width.
(4) Max. tooth root stress of main gear was about 30kg/mm
2, and this value was about 23% larger than that calculated by AGMA formula and about 9% larger by HAND BOOK OF MECHANICAL INDUSTRIES (fifth edition) .
While, in order to examine the influence of line shaft alignment to the load distribution along face width, measurement was made at the condition of the steady bearing shifting 0.7mm upward and 0.3mm downward from the original position. In consequence, it seemed that the position of steady bearing reflect scarcely on the load distribution along face width.
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