Section
1 General requirements
1.1 Application
1.2 Definition of symbols
1.2.1 The symbols used in the various formulae in Vol 2, Pt 8, Ch 2, 2 Cylindrical shells and drums subject to internal pressure to Vol 2, Pt 8, Ch 2, 7 Standpipes and branches inclusive, unless
otherwise stated, are defined as follows, and are applicable to the specific part of the
pressure vessel under consideration:
d
|
= |
diameter
of hole, or opening, in mm |
r
i
|
= |
inside knuckle radius, in mm |
r
o
|
= |
outside knuckle radius, in mm |
t
|
= |
minimum
thickness, in mm |
D
i
|
= |
inside diameter, in mm |
D
o
|
= |
outside diameter, in mm |
R
i
|
= |
inside radius, in mm |
R
o
|
= |
outside radius, in mm |
T
|
= |
design temperature, in °C |
c |
= |
corrosion allowance in mm for design and operating condition taking into account
the intended life cycle; a minimum corrosion allowance of 0,75 mm is to be used,
any deviation is to be agreed with LR taking into consideration the material type,
service fluid, design and operating conditions. The corrosion allowance is to be
added to the calculated Rule thickness as well as to the minimum thickness
specified by the Rules. |
1.2.2 Where reference is made to calculated or actual plate thickness for the
derivation of other values, these thicknesses are to be minus the corrosion allowance
(c).
1.3 Design pressure
1.3.1 The
design pressure is the maximum permissible working pressure, and is
to be not less than the highest set pressure of any relief valve.
1.3.2 Calculations
made to determine the scantlings of the pressure parts are to be based
on the design pressure, adjusted where necessary to take account of
pressure variations corresponding to the most severe operational conditions.
1.3.3 It is
desirable that there should be a margin between the normal pressure
at which the pressure vessel operates and the lowest pressure at which
any relief valve is set to lift, to prevent unnecessary lifting of
the relief valve.
1.4 Metal temperature
1.4.1 The
metal temperature, T, used to evaluate the allowable
stress, s, is to be taken as the actual metal temperature
expected under operating conditions for the pressure part concerned,
and is to be stated by the manufacturer when plans of the pressure
parts are submitted for consideration.
1.4.2 The
design temperature, T, for calculation purposes is to
be not less than 50ºC.
1.5 Classification of fusion welded pressure vessels
1.5.1 For
Rule purposes, pressure vessels are graded as Class 1 where the shell
thickness exceeds 38 mm.
1.5.2 For
Rule purposes, pressure vessels are graded as Class 2/1 and Class
2/2 if they comply with the following conditions:
-
where the design pressure exceeds 1, 72 MPa; or
-
where the metal
temperature exceeds 150°C; or
-
where the design pressure, in MPa, multiplied by the actual thickness
of the shell, in mm, exceeds 15,7; or
-
where the shell
thickness does not exceed 38 mm.
1.5.3 For
Rule purposes, Class 3 pressure vessels are to have a maximum shell
thickness of 16 mm, and are pressure vessels not included in Classes
1, 2/1 or 2/2.
1.5.4 Pressure
vessels which are constructed in accordance with Classes 2/1, 2/2
or 3 standards (as indicated above) will, if manufactured in accordance
with the requirements of superior Class, be approved with the scantlings
appropriate to that Class.
1.5.5 Pressure
vessels which only have circumferential fusion welded seams, will
be considered as seamless with no Class being assigned. Preliminary
weld procedure tests and non-destructive examination for the circumferential
seam welds should be carried out for the equivalent Class as determined
by Vol 2, Pt 8, Ch 2, 1.5 Classification of fusion welded pressure vessels 1.5.1, Vol 2, Pt 8, Ch 2, 1.5 Classification of fusion welded pressure vessels 1.5.2 and Vol 2, Pt 8, Ch 2, 1.5 Classification of fusion welded pressure vessels 1.5.3
1.5.6 In special
circumstances relating to service conditions, materials, operating
temperature, the carriage of dangerous gases and liquids, etc. it
may be required that certain pressure vessels be manufactured in accordance
with the requirements of a superior Class.
1.5.8 Hydraulic
testing is required for all classes of pressure vessels.
1.6 Plans
1.6.1 Plans
of pressure vessels are to be submitted in triplicate for consideration
where all the conditions in (a) or (b) are satisfied:
-
The vessel contains
vapours or gases, e.g. air receivers, hydrophore or similar vessels
and gaseous CO2 vessels for fire-fighting, and
p
V > 60
p > 0,1
V > 100
V = volume (litres) of gas or vapour space
-
The vessel contains
liquefied gases, or flammable liquids
p > 0,7
V > 100
V = volume (litres)
p is as defined in Vol 2, Pt 8, Ch 2, 1.2 Definition of symbols 1.2.1
1.6.2 Plans
of full constructional features of the vessel and dimensional details
of the weld preparations for longitudinal and circumferential seams
and attachments, together with particulars of the welding consumables
and of the mechanical properties of the materials, are to be submitted
before construction is commenced.
1.7 Materials
1.7.2 The specified minimum tensile strength of carbon and carbon-manganese steel plates, pipes, forgings and castings is to be
within the general limits of 340 to 520 N/mm2.
1.7.3 The specified minimum tensile strength of low alloy steel plates, pipes, forgings and castings is to be within the general
limits of 400 to 500 N/mm2, and pressure vessels made in these steels are to be either seamless or Class 1 fusion welded.
1.7.4 Where it is proposed to use materials other than those specified in the
Rules for the Manufacture, Testing and Certification of Materials, July 2022, details of the chemical compositions, heat treatment and mechanical properties are to be submitted for approval. In such
cases, the values of the mechanical properties used for deriving the allowable stress are to be subject to agreement by LR.
1.8 Allowable stress
1.8.1 The
term ‘allowable stress’, σ, is the stress to be used
in the formulae for the calculation of scantlings of pressure parts.
1.8.2 The
allowable stress, s, is to be the lowest of the following
values:
where
E
t
|
= |
specified minimum lower yield stress or 0,2 per cent proof stress
at temperature, T for carbon and carbon-manganese steels.
In the case of austenitic steels, the 1,0 per cent proof stress at
temperature, T, is to be used
|
R
20
|
= |
specified minimum tensile strength at room temperature |
S
R
|
= |
average stress to produce rupture in 100 000 hours at temperature, T
|
1.9 Joint factors
1.9.1 The
following joint factors are to be used in the equations in Vol 2, Pt 8, Ch 2, 2 Cylindrical shells and drums subject to internal pressure, where applicable. Fusion
welded pressure parts are to be made in accordance with Vol 2, Pt 1, Ch 4 Requirements for Fusion Welding of Pressure Vessels and Piping
Class of pressure vessel
|
Joint factor
|
Class 1
|
1,0
|
Class 2/1
|
0,85
|
Class 2/2
|
0,75
|
Class 3
|
0,60
|
1.9.2 The
longitudinal joints for all Classes of vessels are to be butt joints.
Circumferential joints for Class 1 vessels are also to be butt welds.
Circumferential joints for Classes 2/1, 2/2 and 3 vessels should also
be butt joints with the following exceptions:
-
Circumferential
joints for Classes 2/1, 2/2 and 3 vessels may be of the joggle type
provided neither plate at the joints exceeds 16 mm thickness.
-
Circumferential
joints for Class 3 vessels may be of the lap type provided neither
plate at the joint exceeds 16 mm thickness nor the internal diameter
of the vessel exceeds 610 mm.
For typical acceptable methods of attaching flat ends, see
Figure 1.8.2 Toroidal furnace headers and Figure 1.9.1 Typical attachment of unflanged flat end plates to shell .
For
typical acceptable methods of attaching dished ends, see
Figure 2.8.1 Typical attachment of dished ends to cylindrical shell
1.9.3 Where
a pressure vessel is to be made of alloy steel, particulars of the
welding consumables to be used, including typical mechanical properties
and chemical composition of the deposited weld metal, are to be submitted
for approval.
1.10 Pressure parts of irregular shape
1.11 Adverse working conditions
1.11.1 Where
working conditions are adverse, special consideration may require
to be given to increasing the scantlings derived from the formulae.
In this connection, where necessary, account should also be taken
of any excess of loading resulting from:
-
impact loads,
including rapidly fluctuating pressures,
-
weight of the
vessel and normal contents under operating and test conditions,
-
superimposed
loads, such as other pressure vessels, operating equipment, insulation,
corrosion-resistant or erosion-resistant linings and piping,
-
reactions of
supporting lugs, rings, saddles or other types of supports, or
-
the effect of
temperature gradients on maximum stress.
|