LPSC (M)/PT/04/2013-14 (sl No 3) - ISRO
LPSC (M)/PT/04/2013-14 (sl No 3) - ISRO
LPSC (M)/PT/04/2013-14 (sl No 3) - ISRO
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5.2 External surface: The external surface shall be subject to extra shot<br />
blasting to achieve surface condition as per “Preparation grade B Sa 2½”<br />
and surface finish to “15µm Ra”. The treatment shall be followed by<br />
painting with 2 coats of anti-corrosion paint of 70µm layer thickness.<br />
Surface finish of vessels after shot blasting shall be measured and details<br />
may be provided. The painting shall be French grey.<br />
6. End connections:<br />
Flanged ends on both sides as given in Drg <strong>No</strong>. S<strong>PT</strong>F/HPC/01/<strong>2013</strong><br />
7. Marking:<br />
The cylinder shall be stamped with permanent and clearly visible<br />
identification marks at an accessible location by steel stamps. The details<br />
such as water capacity, filling pressure at 15 0 C, hydraulic test pressure,<br />
material of construction, manufacturer’s serial number, date of inspection<br />
and inspector’s stamp shall be marked.<br />
8. Tests:<br />
The following tests shall be performed.<br />
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Material test for physical and chemical properties.<br />
Hardness test.<br />
Magnetic particle examination on the dished ends.<br />
Liquid penetrant examination on the bore of the dished ends.<br />
Internal and external surface examination.<br />
Tare mass measurement.<br />
Water capacity measurement.<br />
Hydraulic stretch test as per DOT 173.34 (the hydraulic test pressure<br />
shall be as per the code but not less than 1.5 times the filling<br />
pressure at 15 0 C)<br />
Ultrasonic test for flaw detection.<br />
Dimensional check.<br />
Wall thickness measurement by ultra sonic probe at identified points<br />
(The location of the measurement points shall be either permanently<br />
marked on the gas cylinders or sketched on a drawing with reference<br />
to a fixed point on the cylinder)<br />
Dye penetrant test at all the weld joints of the flanges.<br />
Hydro test of manifold assembly at 1.5 times of MAWP.