2.3.1 Relevant
data covering the following topics is to be submitted.
2.3.2
Service
Profile. The machinery power/speed operational envelope indicating
all the intended operational points applicable to the class notation,
and any short term high power operation.
2.3.3
Classification
rating:
-
The following operational
parameters are to be taken, using the design conditions for the intended
Class Notation:
- Total barometric pressure, in bar.
- Temperature of engine room, or suction air, in oC.
- The relative humidity, in per cent.
- Temperature of sea water, or charge air coolant inlet, in oC.
-
For unrestricted
service, the following operational parameters ambient reference conditions
are to be taken:
- Total barometric pressure, at 1000mb.
- Temperature of engine room or suction air, at 45oC.
- Relative humidity, at 60 per cent.
- Temperature of sea water or charge air coolant inlet, at 32oC.
2.3.4
Short
term high power operation. Where the propulsion machinery is
being considered for short term high power operation, full details
of the power, speed and time intervals together with fatigue endurance
calculations, and documentary evidence indicating the suitability
of the component design under these conditions and for the intended
class notation are required. The following are to be considered; prime
mover, gearbox, flexible coupling, vibration dampers, shafting and
propeller.
-
The accrued number
of load cycles and the percentage component overload are to be those
recommended by the designers.
-
Excessive overload
may require the interval between surveys to be reduced.
-
Machinery is to be
maintained in accordance with the manufacturers' requirements.
2.3.5
Damper
and Flexible Coupling characteristics. Documentary evidence
that the characteristics have been verified.
2.3.6
Machinery
Fastening.
-
Documentary evidence
and calculations indicating that machinery is securely mounted for
the accelerations to be expected during service.
-
Calculations that
mountings of large masses such as main engines, auxiliary engines,
lift fans and electrical equipment can withstand the design collision
acceleration according to Pt 9, Ch 1, 5.2 Collision load 5.2.1 without
fracturing.
-
Natural frequency
calculation of resilient mounted machinery.
-
For non-metallic
machinery chocks:
-
Resin type.
-
The effective area and minimum thickness
of the chocks.
-
The total deadweight loading of machinery.
-
The thrust load, where applicable, that will
be applied to the chocked item.
-
The loading to be applied to the holding-down
bolts.
-
The material of the holding-down bolts.
-
The number, thread size, and waisted shank
diameter (where applicable) of the holding-down bolts.
2.3.7
Manuals.
The operation and maintenance manuals.
2.3.8
Failure
Mode and Effect Analysis. Where required for high speed craft,
an FMEA is to be carried out covering the following systems:
-
Main and auxiliary
machinery systems, and their controls.
-
Steering systems.
-
Electrical systems.
2.3.9
Fatigue
Strength Analysis. Where undertaken as an alternative to the
requirements of the individual Chapters, fatigue strength analysis
of components indicating a factor of safety of 1,5 at the design loads
based on a suitable fatigue failure criteria. The effects of stress
concentrations, material properties and operating environment are
to be taken into account.