3.1.1 Components
are to be manufactured and tested in accordance with the requirements
of the Rules for the Manufacture, Testing and Certification
of Materials (hereinafter referred to as the Rules for Materials).
3.1.2 The
specified minimum tensile strength of forgings for shafts is to be
selected within the following general limits:
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Carbon and carbon-manganese
steel – 400 to 760 N/mm2 (41 to 77,5 kgf/mm2). See also
Vol 2, Pt 3, Ch 2, 4.4 Screwshafts and tube shafts 4.4.1.
-
Alloy steel –
not exceeding 800 N/mm2 (82 kgf/mm2) and for
other forgings not exceeding 1100 N/mm2.
3.1.3 Where
it is proposed to use alloy steel, details of the chemical composition,
heat treatment and mechanical properties are to be submitted for approval.
3.1.4 Where
shafts may experience vibratory stresses close to the permissible
stresses for transient operation, the materials are to have a specified
minimum tensile strength of 500 N/mm2 (51 kgf/mm2).
3.1.5 Where materials with greater specified or actual tensile strengths than the
limitations given above are used, reduced shaft dimensions or higher permissible
vibration stresses are not acceptable when derived from the formulae used in Vol 2, Pt 3, Ch 2, 4.2 Intermediate shafts, Vol 2, Pt 3, Ch 2, 4.4 Screwshafts and tube shafts and
Vol 2, Pt 5, Ch 1, 3.2 Limiting stress in propulsion shafting unless, for intermediate shafts only, it is verified
that the materials exhibit a similar fatigue life to conventional steels through
compliance with the requirements in Vol 2, Pt 3, Ch 2, 6 Approval of alloy steel used
for intermediate shaft material.
3.1.7 In the
selection of materials for shafts, keys, locking nuts etc. consideration
is to be given to their compatibility with the proposed propeller
material.
3.1.8 Where
shafts are manufactured from composite material the process is to
be approved.