OS-C501
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Offshore Standard DNV-<strong>OS</strong>-<strong>C501</strong>, November 2013<br />
Sec.11 Fabrication – Page 169<br />
3 Processing steps<br />
3.1 General<br />
3.1.1 Bending of composites shall be avoided. A minimum bending radius shall be defined if the process<br />
requires bending of materials.<br />
3.1.2 Materials and components shall not be exposed to point-loads. All possible point loads shall be evaluated<br />
and it shall be ensured that they will not damage the material.<br />
3.1.3 The working conditions are important when producing composite parts. Ambient temperature ranges<br />
shall be defined and production areas should be well ventilated. Dust, fumes, chemicals etc. may influence<br />
curing conditions or may attack the material later during service. The working conditions shall be defined.<br />
3.1.4 Humidity shall be controlled at places where chemical reactions occur. If humidity cannot be controlled<br />
its effect shall be evaluated.<br />
3.2 Raw materials<br />
3.2.1 All raw materials shall be traceable for applications with normal and high safety class.<br />
3.3 Storage of materials<br />
3.3.1 The manufactures recommended storage conditions should be followed. All materials shall be stored in<br />
clean and dry environments.<br />
3.3.2 Fibres should be stored in a clean environment, preferably wrapped up.<br />
3.3.3 Resins and other chemicals should be stored in tight containers or tanks.<br />
3.3.4 All resins and chemicals shall not be used after their shelf life has expired.<br />
3.3.5 Some foam cores have internal gases from the production process that diffuse out with time. Such cores<br />
shall be stored long enough to allow the gases to diffuse out. Core skin delaminations may be the result if the<br />
gases remain in the core.<br />
3.3.6 When taking materials out of storage it is important that they reach the same temperature as in the<br />
production facility while inside their sealed storage bag or container. This step prevents the formation of<br />
humidity on the materials.<br />
3.4 Mould construction<br />
3.4.1 The word moulds is interpreted in this section in a wide sense, covering many processes. Laying tables,<br />
mandrels and vacuum bags are considered as moulds or parts of moulds.<br />
3.4.2 Moulds should match all tolerances required by the design.<br />
3.4.3 Sharp corners and discontinuities at joining points should be avoided.<br />
3.4.4 The surface finish shall be as specified. It shall be demonstrated that the mould surface finish can produce<br />
components with the required surface finish of the component.<br />
3.4.5 Compatibility of mould release agents with the material and further operations should be considered.<br />
Especially adhesive joining or re-lamination may be effected by residues of mould release agents on the surface<br />
of the component. This applies for mould release agents that were applied to the mould and for mould release<br />
agents that were added to the resin.<br />
3.4.6 The structural stability of moulds or mandrels should be ensured.<br />
3.4.7 Possible deformations of the moulds should be considered in the design. The structure should be able to<br />
withstand all resulting loads and strains.<br />
3.4.8 If moulds are heated a controlled distribution of temperature shall be ensured.<br />
3.4.9 If a vacuum is applied inside the mould (or some bag), it shall be ensured that no leaks exist. The vacuum<br />
shall be measured far away from the point where the vacuum is pulled. Large moulds may require more than<br />
one measurement point.<br />
3.4.10 When removing the part from the mould large stresses and deformations may be induced, especially if<br />
the component got stuck somewhere. These effects should be avoided or at least carefully controlled. Possible<br />
stresses or strains due to these operations should be considered in the design. If such a situation occurs<br />
accidentally the loads shall be estimated and the component shall be reanalysed.<br />
DET NORSKE VERITAS AS