SlideShare a Scribd company logo
1 of 160
By : Mehdi Sibtain
Cryogenic processes
Introduction
 Program aimed at customized training for better
understanding of cryogenic process.
Agenda Day One
 Introduction to cryogenic process
 Cooling in a cryogenic process.
 Joule-Thomson effect.
 Inversion Temperature.
 Expansion in work producing process.
 Thermodynamic analysis of cryogenic
process.
Agenda Day
Two(morning)
 Thermodynamic cooling paths.
 Comparison of J-T & expander process.
 Safety in cryogenic process.
 Cold box configuration.
 Effect on metals.
Agenda Day Two
(Evening)
 Heat exchangers.
 Gas expanders.
 Separation system.
 PLANT VISIT
Agenda (Day-Three)
 He & N2 separation in NG System.
 Insulation.
 Cryogenic control valves.
 Instrumentation.
 Precautions during pre-commissioning.
 Operational precautions.
Agenda (Day-Four)
• Inert gas & Hydrogen recovery plants.
 FFC experience with cold boxes.
 Plant Visit.
 Conclusion.
Introduction to
cryogenics
 Cryogenic means the generation of cold.
 Considered to attain at <-101C
temperature.
 Based on the principle of liquefaction
separation of gases by decreasing the
temperature.
Benefits
 Low capital investment.
 Compact units requiring minimum space
for installation.
 Best possible recovery of valuable
components
 Production of higher heating value fuels.
 Economical production of rare gases .
Applications
 Separation of air for production of Oxygen
& Nitrogen.
 Production of liquid Hydrogen for Nuclear
weapons & space programs.
 Liquid Helium for space programs.
 Liquefied natural gas (LNG) plants.
Applications Contd..
 Liquid N2 for food preservation.
 In Biological application utilization of liquid
nitrogen cooled containers.
 In surgery for Parkinson's disease.
 Recovery of valuable feedstock from
natural gas streams, upgrading the heat
content of fuel gas.
 Purification of various gas streams
Properties of Cryogenic Fluids
 Boiling points less than 0oC.
 Critical temp. normally below ambient.
 Gases with high Joule-Thomson
coefficient.
 Higher non-ideality (polarity) of the gas
better it is for the cryogenic cooling.
 Inversion temperature above ambient
temperature.
Properties Contd..
 Shouldn’t solidify at the operating
temperature.
 Principles of mechanics &
thermodynamics at ambient temperature
also apply for cryogens.
 Except for H2 & He all have thermal
conductivities that increase as the
temperature is decreased.
Liquefaction and the
Liquid States
 Molecules in the gaseous state exhibit
opposing tendencies-dispersion &
aggregation..
 The intermolecular attractive forces
increase to definite maxima as the
distances between molecules are
diminished.
Liquefaction Contd..
 These conditions are brought about when
the temperature of a substance is
lowered,or
 When the molecules are crowded close
together I.e pressure is increased.
Liquefaction Contd..
 When the energy of attraction of one
molecule for another exceeds its kinetic
energy of translation, the molecules will
form a dense aggregation which is termed
a liquid.
Cooling in Cryogenic Process
 May be accomplished in several ways:
– Cooling at constant pressure, as in a heat
exchanger.
– Application of Joule Thomson effect by
expansion valve or throttling process.
– Expansion in an expansion engine.
– Cooling & Purification by evaporation
Cooling In A Heat Exchanger
 Requires a heat sink at a lower temperature.
 An external refrigeration system is required if
necessary.
 This method is used for pre-cooling the gas &
recovery of the low temperature from out going
streams.
 Operation at low temperature demands special
techniques for fabrication.
Joule-Thomson Effect
 Joule-Thomson studied the behavior of
gasses during expansion..
 It can be utilized in a cycle till the dew
point of a gas.
 Expansion causes decrease in the kinetic
energy of translation; the net result is
decrease in the temperature.
Throttling Process
 Processes at continuous flow in a pipe occurring
at condition approaching constant enthalpy.
 Flow through a porous plug or throttling valve
causes decrease in pressure due to resistance.
 If device is insulated & no shaft work is
produced then process is one of constant
enthalpy.
Joule-Thomson Coefficient
 It is the measure of temperature behavior of a
fluid during a throttling process.
 At constant enthalpy, it is ratio of the change in
temperature & pressure.
 This coefficient is a property of the gas.
 The value can be positive, negative, or zero.
 For ideal gas,  = 0 this means that there is
negligible change in temperature when ideal
gas flows through an insulated valve.
Coefficient Contd..
 For most gases  is positive at moderate
pressures & temperatures; that is, the gas
becomes cooler as it expands.
 Joule-Thomson coefficient represents the slope
of h = constant lines on a T-P diagram.
 Can be determined from the data of constant
pressure specific heat & P-V-T behavior.
Inversion Temperature
 Temperature at which J-T coefficient is zero.
 It is the temperature at point where a constant-
enthalpy line intersects the inversion line.
 The temperature at the intersection of P = 0 line
the upper part of the inversion line is called the
maximum inversion temperature.
 Slopes of the η= constant lines are negative
(η<0) at states to the right of the inversion line
and positive (η>0) to its left side.
Inversion Temp. Contd..
 Temperature of a fluid will increase during a
throttling process that takes place on the right-
hand side of the inversion line.
 Temperature will decrease during a throttling
process that takes place the left-hand side of
the inversion line.
 Cooling effect cannot be achieved by throttling
unless the fluid is below its maximum inversion
temperature.
Expansion in a Claude Process
 It is an isentropic process.
 Temperature of the fluid always decreases.
 Cooling does not depend on being below the
inversion temperature prior to expansion.
 Temperature drop is much higher for this
process than in isenthalpic expansion.
 Increasing the pressure drop ratio increases the
amount of heat removed.
Cooling By Flashing
 Flashing causes decrease in Partial pressure of
the component & temperature decreases as the
distance of the molecule increases.
 Pressure letdown effect on liquids serves
following benefits:
– Avoidance of two phase flow in piping / heat
exchangers.
– Better purification of due to high solubility.
Cryogenic Separation
 The constant-pressure path (1) approaches
the two-phase region.
 The isenthalpic expansion (3) will not result in
liquefaction unless the initial state is at a high
enough pressure and low enough
temperature for the constant-enthalpy line to
cut into the two-phase region.
 The isentropic process (2) does not require
an initial state at as high a pressure (at a
given temperature) for liquefaction.
Liquefaction of Air
 Can be explained from its enthalpy-pressure
data by reference to the TS diagram for air.
Achievement of Steady-State
 Maximum liquefaction is not obtained until
steady-state conditions are reached.
 which time an energy balance around the
separator, valve, and cooler gives
H6z + H8 (1-z) = H3
where the enthalpy quantities refer the
positions numbered in figure.
Claude - Process
 The flow scheme is the same as for the Joule-
Thomson expansion, except that an expansion
engine replaces the expansion valve.
 The energy balance becomes
 H6z + H8 (1 – z) + WS = H3
 If the operation is reversible and adiabatic, the
work is given by the expansion.
 WS = - (H5 – H4)
Thermodynamic Paths
 Liquefaction by joule-Thomson valve.
 Liquefaction by expansion engine.
 Liquefaction by expansion engine &
expansion valve .
Comparison
 Turbo-expander process has a far better
capacity for recovering liquids.
 Process design is complicated with
expanders
 Initial & operating cost are higher for
expander process.
Item
Specified
Condition
Heat Exchanger
Pressure drop (psia) shell side 5
Tube 5
Minimum Approach
Temperature, O F 15
Flash Separator
Pressure, psia 400
Turbo-expander
Discharge Pressure, psia 400
Efficiency, % 75
Specified Process Conditions For Joule-Thomson/Turbo-expander Process Comparison
Item
Calculated Process Conditions
Joule-Thomson
Turbo-
expander
Primary Separator
- Temperature, F -48 -45
- Liquid rate, moles/hr 119 182
Secondary Separator
(Turbo-expander)
- Temperature F - -112
- Liquid rate, moles / hr - 463
Heat Exchanger
- Temperature of
Feed out, F
-9 -45
- Power Generated in
Turbo Expander, hp
- 1316
Component Turbo-expender Joule-Thomson Turbo-expander
Incremental
Rec Moles/hr
Mols/hr %Rec Moles/hr %Rec
N2 0.88 0.80 0.07 0.06 0.81
C1 353.42 3.42 30.60 0.30 322.82
C2 103.18 30.26 10.22 3.00 92.96
C3 92.09 76.11 17.11 14.27 74.82
iC4 30.92 93.70 11.48 34.79 19.44
nC4 21.27 96.68 10.33 46.95 10.94
iC5 10.94 99.45 8.15 74.09 2.79
nC5 10.97 99.73 8.98 81.64 1.99
C6+ 22.00 100.00 21.74 98.92 0.26
645.68 118.85 526.83
C4+ Recovery 97% 61%
Physiological Hazards
 Severe cold "burns" may be inflicted if the
human body comes in contact.
 Damage to the skin or tissue is similar to tan
ordinary burn because the body is composed
mainly of water.
 The low temperature effectively freezes the
tissue damaging or destroying it.
Physiological Hazards Contd..
 Body can normally adjust for a heat loss of 95
J/m2s for an area of limited exposure.
 Freezing of facial tissue will occur in about
100 sec. if the heat loss is 2300 J/m2s.
Materials and Construction
Hazards
 Consider the ductility of the material
since low temperatures have the effect
of making some construction materials
brittle or less ductile.
 Exposure of low temperature stream on
to ordinary metals may result in material
failure.
Typical protections of cold box
 On high ΔP, closure of inlet valve(During
S/UP)
 Trip of unit at high inlet temperature to protect
exchanger.
 Closure of J-T valve / expander nozzle on low
flow of inlet gas to protect temperature
gradient.
 Trip of unit on low exit gases temperature.
Flammability and
Explosion Hazards
 Explosion requires an oxidant, a fuel and an
ignition source.
 The oxidizer will be oxygen available from a
leakage or condensation of air on cooled
surfaces and buildup as a solid with water.
 The ignition source may be a mechanical or
electrostatic spark, flame, impact heat by
kinetic effects, friction, chemical reaction.
Mixture Flammability
Limits (mol%)
Detonability Limits
H2 – air 4-75 20-65
H2 – O2 4-95 15-90
CH4 – air 5-15 6-14
CH4 – O2 5-61 10-50
Flammability & Detonability Limits of Hydrogen & Methane Gas
High – Pressure Hazards
 High pressure is obtained by gas
compression during liquefaction (if required).
 If this confined gas is suddenly released a line
a significant thrust may be experienced.
 Force generated by rupturing a 2.5 cm
diameter valve on a 13.9-Mpa pressurized
gas cylinder would be over 6670N.
 Adequate PSVs should be provided.
Cold Box
 Cold box is a group of multi fluid exchanger
cores assembled in a single structure.
 Designed for cooling upto very low
temperatures.
 These must be properly insulated for
approaching the adiabatic conditions.
Components of cold box
 Piping and liquid separators with low
temperature metallurgy.
 Coiled or plate-fin exchangers.
 Isenthalpic valves/ Expanders or both
 Separation or rectification columns (if
required).
 Instrumentation.
 Insulation.
Cryogenic Metallurgy
 Metals used for vessels and piping vary
with temperature.
 As temperature decreases most
mechanical properties—hardness, yield,
tensile and fatigue strength increase.
 Corrosion is of less concern.
 The problem is ductility.
 Linear expansion is important as well.
Ductile Properties
 Usual way of characterizing ductile properties
of metal is Charpy-notch or keyhole test.
 Notch sensitivity depends on crystal structure
of the metal.
 Austenitic stainless steels, high nickel steels,
aluminum, and copper all have face-centered
crystal structures.
 Aluminum is usually preferred over copper
because of its lighter weight.
Linear Expansion
 Coefficient of linear expansion for several
metals varies with temperature.
 The higher coefficients for aluminum and copper
raise the problem of providing for Expansion by
means of expansion loops, bellows type
connections, and the like.
Structural Properties
 Face-centered-cubic (fcc) metals and their
alloys are most often used in the construction of
cryogenic equipment.
 Al, Cu, Ni, their alloys and the austenitic
stainless steels are “fcc” and do not exhibit an
impact ductile-to-brittle transition at low
temperatures.
 The body-centered-cubic (bcc) metals and
alloys are undesirable for low temperature.
Structural Properties Contd..
 Fe, the martensitic steels (low carbon and the
400 series stainless steels), Mo and Nb. exhibit
a ductile-to-brittle transition at low temperatures.
 Hexagonal-close-packed (hcp) metals exhibit
mechanical properties intermediate between
those of the “fcc” and “bcc” metals.
Structural Properties Contd..
 Zr and pure Ti alloys with a “hcp” structure
have been used where weight reduction
and reduced heat leakage through the
material have been important.
 Small impurities of O, N, H, and C can
have a detrimental effect on the low
temperature ductility properties of Ti and
its alloys.
Properties non Metals
 Plastics increase in strength as the temperature
is decreased, but this is also accompanied by a
rapid decrease in elongation in a tensile test
and a decrease in impact resistance.
 Teflon and glass-reinforced plastic retain
appreciable impact resistance.
 The glass-reinforced plastics also have high
strength-to-weight and strength-to-thermal
conductivity ratios.
Properties non Metals Contd..
 Elastomers, become brittle at low
temperatures.
 Nevertheless, rubber, Mylar, and nylon
can be used for static seal gaskets
provided they are highly compressed at
room temperature prior to cooling.
Thermal Properties
 High-purity aluminum and copper exhibit high
thermal conductivity from 20 to 50 K.
 These peaks are rapidly suppressed with
increased impurity levels and cold work.
 Monel, Inconel, stainless steel & aluminum
alloys show a steady decrease in thermal
conductivity.
 All cryogenic liquid except hydrogen and helium
have thermal conductivities that increase as the
temperature is decreased.
Electrical Properties
 The electrical resistivity of most pure metallic
elements at ambient and moderately low
temperatures is approximately proportional to
the absolute temperature.
 At very low temperatures it approaches a
residual value almost independent of
temperature.
 For alloys it is largely independent of
temperature.
Heat Exchangers
Selection
 Small temperature difference between
inlet and exit streams to enhance
efficiency.
 Large surface area-to-volume ratio to
minimize heat leak.
 High heat transfer to reduce surface area.
 Low mass to minimize start-up time.
Selection Contd..
 Multi-channel capability to minimize the
number of exchangers.
 High-pressure capability to provide design
flexibility.
 Low or reasonable pressure drop to
minimize compression requirements.
 High reliability with minimal maintenance
to reduce shutdowns.
Tubular-fin Heat
Exchangers
 These heat exchangers are used as
gas-to-liquid heat exchangers.
Plate-fin Heat
Exchangers
 Plate-fin are about nine times as compact as
conventional shell-and-tube heat exchangers.
 Commonly fabricated from aluminum.
 These are stack of layer.
 Each layer consists of corrugated aluminum
sheets (fins) between flat aluminum
“separator” plates to form individual passage.
Plate-fin Exch. Contd..
 The stack, including the sidebars, is bonded
by a carefully controlled brazing process.
 Passages can be arranged for either cross
flow, countercurrent flow, concurrent flow, or
multi pass flow.
 The number of passages provided for each
stream can be varied to yield the required flow
rates and pressure drop.
Plate-fin Exch. Contd..
 Up to eight separate streams can be
accommodated in one core.
 Heat transfer area per unit volume is
around 2000 m2 / m3.
Applications
 The plate-fin type is primarily used for gas-to-
gas application and tube-fin exchangers for
liquid-air heat exchangers.
 In most of the application (in trucks, cars, and
airplanes), mass and volumes reduction are
particularly important.
 Widely used in cryogenic, energy recovery,
process industry, refrigeration, and air-
conditioning system.
Forms of Corrugated Sheets
 The plates are typically 0.5 to 1.0 mm thick and
the fins 0.15 to 0.75 mm thick.
 Fins give extra heat transfer area and structural
support to the flat plates.
 Most common types of fins are:
– Plain fin
– Plain-perforated fin
– Serrated fin (also called “lanced”, “interrupted”,
“louver” or “militantly”)
– Herringbone or wavy fin
Limitations
 The flow channels are small, which means
that the mass velocity also has to be small
(10 to 300 kg/[m2.s]) to avoid excessive
pressure drops.
 Plate-fin exchangers are restricted to
clean fluids.
Limitations Contd..
 Operation at low temperatures requires
removal of essentially all impurities that
are to be cooled.
 High operating temperature & differential
temperature are not allowed due to
brazing.
Gas Expanders
 There are four general types of expanders.
 Mostly expanders in low temperature services
are of the single-stage, radial wheel impeller.
 High efficiency of a turbo-expander requires
operation at near optimum speed.
 Optimum efficiency lies in the speed range of
10,000 to over 50,000 rpm.
Flow Control
 Flow through the turbo-expander is controlled
by variable stationary nozzles.
 These are mechanically arranged for an
outside manual or diaphragm control to vary
the clearances between the nozzles.
Shaft Seal
 The “oil-free” arrangement is widely used.
 An outward leakage of gas is permitted out of
each labyrinth seal.
 A continual stream of pressurized gas ( seal
gas) is introduced at a midpoint of each
labyrinth seal which leaks to atmosphere.
 This seal gas is injected at a rate slightly higher
than that leaking out through the seal thus
retaining the valuable process gas
Turbo-Expander Materials
 Expanders should have bearings
approx.10 times as strong as in similar
machines.
 Blade materials are selected based on
erosion resistance and ability to
withstand low temperature.
 Aluminum alloys are used in the
manufacture of expander wheels.
Separation System
 Utilized if the mixture to be separated is
essentially binary with a difference in
boiling points.
 Tray columns are utilized for the desired
separation.
Single column Separation
 It is a J-T liquefaction system with a
substitution of a rectification column for
the liquid reservoir.
 In a simple single-column process,
although the bottoms purity is high, the
top effluent stream is impure.
Linde Double-Column System
 Two rectification columns are placed one on top
of the other.
 Feed is introduced at an intermediate point.
 Condenser-evaporator at the top of the lower
column makes the arrangement a complete
reflux distillation column.
 Almost pure top & bottom products are
produced.
Linde System Contd..
 Condenser must condense light gas
vapor by evaporating liquid heavy
component.
 It is necessary to operate the lower
column at a higher pressure, while the
upper column at lower pressure.
Helium And Nitrogen Separation In
N G System
 Helium content of the natural gas plants
normally has varies upto 02 %
 Nitrogen content varies from 12 to 80%.
 The remainder of the natural gas is
methane, ethane, and heavier
hydrocarbons.
He & N2 Separation In NG
System Contd..
 Major constituents of NG have boiling
points very much different from that of
He, a distillation column is unnecessary.
 High separation can be accomplished
with condenser-evaporators.
 Expanders give better recovery but at
the expense of complexity of process.
Insulation
 To minimize radiative heat transfer, minimize
convective heat transfer and use only a
minimum of solid conductance media.
 In selection consider ruggedness, convenience,
volume, weight, ease of fabrication and
handling, thermal effectiveness and cost.
 Experimentally obtained apparent thermal
conductivity is used to characterize the thermal
effectiveness of various insulations.
Types of Insulation
 Cryogenic insulations have generally been
divided into five general categories:
 High vacuum, multilayer insulation,
powder, foam, and special insulations.
Vacuum Insulation
 Heat transport across an evacuated space
depends on the emissivity.
 The insertion of low-emissivity floating shields
within the evacuated space reduce the heat
transport by radiation.
 Radiant heat transfer is reduced to around one-
half of the rate without the shield, two shields
can reduce this to around one-fourth of the rate
without the shield.
Multilayer Insulation
 Consists of alternating layers of highly reflecting
material, such as aluminum foil or aluminized
Mylar, and a low-conductivity spacer material or
insulator, such as fiberglass mat or paper, glass
fabric, or nylon net, all under high vacuum.
 Degradation in thermal performance is caused
by presence of edge exposure to isothermal
boundaries, gaps, joints, fill and vent lines.
Powder Insulation
 It has the benefit of multiple floating
shields without incurring the difficulties of
awkward structural complexities.
 Amount of heat transport due to radiation
through the powders can be reduced by
the addition of metallic powders.
Foam Insulation
 Thermal conductivity is dependent upon
the bulk density of the insulation.
 Of all the foams, polyurethane and
polystyrene have received the widest use
at low temperatures.
 The major disadvantage is that they tend
to crack upon repeated thermal cycling
and lose their insulation value.
Selection of Insulation
 Many of the vessels contained in a “cold box”
use granular perlite.
 Wool felt might be used around maintenance
entrances.
 On transfer lines use urethane, perlite or
possibly vacuum jacketed lines.
 Polyurethane foam requires a vapor proof
outer jacket.
Cryogenic Control Valves
 The principal function of a J-T valve is to
obtain isenthalpic cooling.
 These valves are generally needle-type valves
modified for cryogenic operation.
 Normally these are made of SS-304 or SS-
321 material
 Have a protection sleeve around the body.
 The plugs are tapered & installed in a clean &
polished body for minimum friction.
Cryogenic Instrumentation
 Metals become brittle at low temperatures, so
the instrument literally falls apart.
 Elastomeric gasket and seals contract faster
than the surrounding metal parts, and the seal
often is lost.
 Even hermetically sealed instruments can
develop pin holes or cracks
 For cryogenic service, check integrity under
liquid N2.
Pressure Instrumentation
 Measured by the flush mounted pressure
transducer
 Consists of a force-summing device (below,
diaphragm, bourdon tube), an analog device
(strain gage, piezoelectric crystal, variable
distance between capacitor plates, and the like).
 Elements are likely to be made of different
materials (bronze diaphragm, stainless-steel
case, semiconductor strain gage), each will
react to the temperature change differently.
Pressure Instrumentation Contd..
 Very small pressure sensing elements
from a single semiconductor chip may be
used to reduce or eliminate temperature
gradients across the device.
 The single element nature of the pressure
gage assembly reduces differences in
materials of construction.
Liquid Level
 The measurements are made in the
conventional CPI approach using floats.
 Sight glasses cannot be used since cryogenic
fluid in it shall boil.
 The dielectric constant of cryogens is related to
their density.
 As liquid level rises, greater dielectric constant
of liquid causes capacitance to vary linearly.
 For best accuracy, should be calibrated in place.
Flow
 The measurement of cryogenic fluids is most
troublesome since it is a derived quantity.
 Normally these are avoided & flow is measured
by the liquid level transfer & measurement at
high temperature exit streams.
 Calibration has accuracy limitation.
Temperature
 The level & range of measurement need
consideration.
 Up to 20K favorite choice is platinum resistance
thermometer (PRT).
 Below 20k, semiconductor thermometers
(germanium, C, or Si based) are preferred.
 Their resistance increases as the temperature is
lowered, semiconductors are usually chosen for
temperatures from about 1 to 20 K.
Temperature Contd..
 For large range of say 1 to 400 K, diode
thermometers are recommended.
 Diode thermometers are very much
smaller and faster.
 Thermocouples are not used as the
thermoelectric power drops to a few µV/K.
Installation and Operation
 Transport and storage.
 Erection.
 Operation.
Transport and Storage
 Plate-fin heat exchangers are shipped
hermetically sealed to avoid ingress of moisture
or dust.
 Without N2-filling, silica gel will be inserted into
the headers to absorb any moisture.
 Inactive or dummy layers are normally closed
by self-sticking aluminum foils.
 Lifting and transportation only allowed on the
marked points and under use of suitable
devices. Protect the exchanger edges.
Measures at Arrival on-site
 Check for damages of the packing & block.
 Check the nitrogen pressure level.
 Check for any defects of stuck aluminum foils
and possible renewal.
 In case of any leakages or mechanical damage,
Vendor shall be informed.
 Carry out washing / drying if exchanger is not
sea worthy packed for sea freight batteries.
Storage
 Block should be stored within the original
packing. Otherwise plate-fin exchangers may be
stored upon square timbers.
 Protect from ambient influences (rain, dirt) by
suitable covering.
 Storage shall be in a position where aluminum
foils are seen on vertical.
 Should be stored in-house.
 Monitor pressure of nitrogen gas regularly.
 Check Sealing of inactive sections.
Installation
 The covers on nozzles or flanges shall be
removed only immediately before the
connection of nozzles to the piping system.
 Consider Exact Alignment .
 Piping has to be carefully cleaned and dried
before connecting to the heat exchangers.
 Install strainers at the inlet pipes.
 Before insulation work any existing temporary
nipples or gauges on dummy layers should be
removed
OPERATION
 Process fluids should be in steady flow.
 Deviations from the specified operation
conditions are only allowed, if there are no
appreciable changes in stream
compositions, temperatures and
pressures.
 Before starting, Nitrogen filling has to be
purged out by the process fluids.
Cooling & Warming up
 Avoid building up of thermal stresses.
 Avoid sudden temperature shocks and
under changes of stream temperatures.
 Cooling is allowed with designed gas only.
 Warming up with gas is allowed only after
draining all liquid out of the exchanger.
Allowable limits & Precautions
 Temperature difference between two streams in
the heat exchanger must not exceed 50 K.
 The temperature change of any stream must not
exceed 60 K/h and 2 K/min.
 Mass velocity on any side should never exceed
300 Kg/m2.s.
 Pressurization / de-pressurization rate to be
kept lower than 2 Kg/cm2/min.
Allowable limits Contd..
 Cold box cooling down speed should not
exceed 25oC / hr.
 During deriming transfer the cold only in one
direction to avoid excessive temperature
difference.
 Degree of drying is sufficient if equipment
temperature is 30oC and dew point is <–40oC.
 Strictly follow the design limits for temperature
and pressure.
Allowable limits Contd..
 Differential pressure of any side of plate-
fin exchanger should be controlled. Follow
vendor instructions about the same.
 Analyze Insulation chamber periodically.
 If leakage from cold box is detected,
inform Vendor, & shutdown/ preserve it.
General Operational Consideration
 The major design problem is assembling
accurate process & enthalpy data.
 The operating problems stem from In- adequate
design& temperature involved are:
– Freezing of liquids
– Protection of metals at low temperature
– Handling of highly volatile liquids
– Safety
– Mechanical failure
Freezing of Liquids
 Hydrocarbons heavier than propane are solids
below –1300C.
 CO2 & water freeze at –800C & O0C resp. H2S &
other contaminants solidifying on cold surface.
 Insulation should be continuously purged to
protect freezing on outer sides.
 Control dew point from upstream section .
 Perform warming up operations.
Hydrogen Recovery Unit
 Purpose :
 Removal of Ar, CH4 & N2
from synthesis gas.
Nitrogen Separation Plant
 The Nitrogen plant produces inert gas
(nitrogen) in purity, using the cryogenic
process.
 The source from which nitrogen is
produced is air.
Major Problems Encountered in HRU
 Fouling/choking of Cold Box Exchangers.
– Low regeneration of adsorbers
– High temperature of inlet gas.
– Upsets in NH3 recovery unit.
– Bellow leakages at V-4581A/B.
– Passing of inlet valve TV-45083.
 Inlet Strainer Choking.
 Failure of PV-45022 (Letdown Valve).
Major Problems in HRU Contd..
 Insulation Shell Pressure Monitoring and
Sampling.
 Condensation and Icing on External
Surfaces.
 No specialty for maintenance of fin
exchangers on site.
Deriming Operation Problems
• Deriming process is very slow.
– Drain valve #45112 line occasionally chokes.
– Warming rate control is sometimes
problematic.
– Temperature gradients limits were not
followed (occasionally).
– Procedure revised to improve the
understanding.
Areas of Concern
 There is no procedure available to carryout
following activities:
– Removal and refilling of perlite.
– Leak test of HRU cold box.
– Inspection of E-4552A/B and V-4583 etc.
– Repair of any damaged part including brazing
procedure and alignment of exchangers.
Areas of Concern Contd..
 Flow / Pressure Variations During
Adsorber Changeover.
 Sampling Points Sensing Tubing Blockage
N2 Plant Problems Encountered
 Turbine Flow Control nozzles sticking during
startup; resolved by repacking of valve.
 Nitrogen Plant Evaporation Pit Y-3919:
– Icing and condensate formation around the
pit.
– Seepage of water inside the pit and
solidfication.
– LS tracing around the pit was provided.
Nitrogen Plant Problems Contd..
 After T/A-2000 liquid N2 inventory dropped to
25.4% & level rise rate was slow. Probable
reason is low insulation level.
 Plant Tripping at Low Lube Oil Temperature.
 Refrigeration Unit Performance
Deterioration.
 Leakage From Storage Liquid Inlet Line
during commissioning.
Compounds
Critical Temperature
Tc (K) to
Critical Pressure
Pc (Atm)
Ammonia 405.5 111.3
Carbon dioxide 304.2 72.9
Hydrogen 33.3 12.8
Hydrogen Sulfied 373.6 88.9
Nitrogen 126.2 33.5
Oxygen 154.4 49.7
Sulfur dioxide 430.7 77.8
Water 647.3 218.2
Methane 190.7 45.8
Ethane 305.43 48.2
Propane 369.9 42.01
Plate-Fin Exchanger Parts
Separation Column
CRYOGENIC VALVES
Cold Box- Exchanger
Condenser-Evaporator
Cryogenic Process Principle.ppt
Cryogenic Process Principle.ppt
Cryogenic Process Principle.ppt
Cryogenic Process Principle.ppt
Cryogenic Process Principle.ppt
Cryogenic Process Principle.ppt
Cryogenic Process Principle.ppt

More Related Content

Similar to Cryogenic Process Principle.ppt

Refrigeration and Air Conditioning
Refrigeration and Air ConditioningRefrigeration and Air Conditioning
Refrigeration and Air Conditioningdineshucer
 
5- liquifaction.pdf
5- liquifaction.pdf5- liquifaction.pdf
5- liquifaction.pdfelsayedAmer7
 
IRJET- Study on Effect of Moisture Contain on Temperature
IRJET-  	  Study on Effect of Moisture Contain on TemperatureIRJET-  	  Study on Effect of Moisture Contain on Temperature
IRJET- Study on Effect of Moisture Contain on TemperatureIRJET Journal
 
Congelacion de pescado
Congelacion de pescadoCongelacion de pescado
Congelacion de pescadoorlandoes
 
Heat and thermodynamics - I / Dr. Mathivanan Velumani
Heat and thermodynamics -  I / Dr. Mathivanan VelumaniHeat and thermodynamics -  I / Dr. Mathivanan Velumani
Heat and thermodynamics - I / Dr. Mathivanan VelumaniMathivanan Velumani
 
Chapter_11.ppt RAC REFRIGERATOR.ppt
Chapter_11.ppt RAC REFRIGERATOR.pptChapter_11.ppt RAC REFRIGERATOR.ppt
Chapter_11.ppt RAC REFRIGERATOR.pptGeoffreyMichael1
 
Second law of thermodynamics
Second law of thermodynamicsSecond law of thermodynamics
Second law of thermodynamicsJaimin Patel
 
Refrigeration and air conditioning notes for gate
Refrigeration and air conditioning notes for gateRefrigeration and air conditioning notes for gate
Refrigeration and air conditioning notes for gateSoumith V
 
Refrigeration cycle
Refrigeration cycleRefrigeration cycle
Refrigeration cyclevidya Alex
 
Thermodynamics of thermal power plants
Thermodynamics of thermal power plantsThermodynamics of thermal power plants
Thermodynamics of thermal power plantsSugam Parnami
 
Thermodynamics chapter:7 Some Power and Refrigerator Cycle
Thermodynamics chapter:7 Some Power and Refrigerator Cycle Thermodynamics chapter:7 Some Power and Refrigerator Cycle
Thermodynamics chapter:7 Some Power and Refrigerator Cycle Ashok giri
 
REFRIGERATION AND AIR CONDITIONING
REFRIGERATION AND AIR CONDITIONINGREFRIGERATION AND AIR CONDITIONING
REFRIGERATION AND AIR CONDITIONINGDivakar Ketha
 
Introduction to Air Refrigeration for 3/4 B.Tech
Introduction to Air Refrigeration for 3/4 B.TechIntroduction to Air Refrigeration for 3/4 B.Tech
Introduction to Air Refrigeration for 3/4 B.Techmaheshchindanu5783
 
Basic Thermodynamics
Basic ThermodynamicsBasic Thermodynamics
Basic Thermodynamicssweetmpg
 

Similar to Cryogenic Process Principle.ppt (20)

Refrigeration and Air Conditioning
Refrigeration and Air ConditioningRefrigeration and Air Conditioning
Refrigeration and Air Conditioning
 
2
22
2
 
Thermal 08
Thermal 08Thermal 08
Thermal 08
 
5- liquifaction.pdf
5- liquifaction.pdf5- liquifaction.pdf
5- liquifaction.pdf
 
IRJET- Study on Effect of Moisture Contain on Temperature
IRJET-  	  Study on Effect of Moisture Contain on TemperatureIRJET-  	  Study on Effect of Moisture Contain on Temperature
IRJET- Study on Effect of Moisture Contain on Temperature
 
Joule thompson effect
Joule thompson effectJoule thompson effect
Joule thompson effect
 
Congelacion de pescado
Congelacion de pescadoCongelacion de pescado
Congelacion de pescado
 
liquifaction of gases.pdf
liquifaction of gases.pdfliquifaction of gases.pdf
liquifaction of gases.pdf
 
Thermodynamics - 203PHYS
Thermodynamics - 203PHYSThermodynamics - 203PHYS
Thermodynamics - 203PHYS
 
Heat and thermodynamics - I / Dr. Mathivanan Velumani
Heat and thermodynamics -  I / Dr. Mathivanan VelumaniHeat and thermodynamics -  I / Dr. Mathivanan Velumani
Heat and thermodynamics - I / Dr. Mathivanan Velumani
 
Chapter_11.ppt RAC REFRIGERATOR.ppt
Chapter_11.ppt RAC REFRIGERATOR.pptChapter_11.ppt RAC REFRIGERATOR.ppt
Chapter_11.ppt RAC REFRIGERATOR.ppt
 
Second law of thermodynamics
Second law of thermodynamicsSecond law of thermodynamics
Second law of thermodynamics
 
Refrigeration and air conditioning notes for gate
Refrigeration and air conditioning notes for gateRefrigeration and air conditioning notes for gate
Refrigeration and air conditioning notes for gate
 
Thermal 07
Thermal 07Thermal 07
Thermal 07
 
Refrigeration cycle
Refrigeration cycleRefrigeration cycle
Refrigeration cycle
 
Thermodynamics of thermal power plants
Thermodynamics of thermal power plantsThermodynamics of thermal power plants
Thermodynamics of thermal power plants
 
Thermodynamics chapter:7 Some Power and Refrigerator Cycle
Thermodynamics chapter:7 Some Power and Refrigerator Cycle Thermodynamics chapter:7 Some Power and Refrigerator Cycle
Thermodynamics chapter:7 Some Power and Refrigerator Cycle
 
REFRIGERATION AND AIR CONDITIONING
REFRIGERATION AND AIR CONDITIONINGREFRIGERATION AND AIR CONDITIONING
REFRIGERATION AND AIR CONDITIONING
 
Introduction to Air Refrigeration for 3/4 B.Tech
Introduction to Air Refrigeration for 3/4 B.TechIntroduction to Air Refrigeration for 3/4 B.Tech
Introduction to Air Refrigeration for 3/4 B.Tech
 
Basic Thermodynamics
Basic ThermodynamicsBasic Thermodynamics
Basic Thermodynamics
 

Recently uploaded

Call Girls Narol 7397865700 Independent Call Girls
Call Girls Narol 7397865700 Independent Call GirlsCall Girls Narol 7397865700 Independent Call Girls
Call Girls Narol 7397865700 Independent Call Girlsssuser7cb4ff
 
Risk Assessment For Installation of Drainage Pipes.pdf
Risk Assessment For Installation of Drainage Pipes.pdfRisk Assessment For Installation of Drainage Pipes.pdf
Risk Assessment For Installation of Drainage Pipes.pdfROCENODodongVILLACER
 
Introduction to Machine Learning Unit-3 for II MECH
Introduction to Machine Learning Unit-3 for II MECHIntroduction to Machine Learning Unit-3 for II MECH
Introduction to Machine Learning Unit-3 for II MECHC Sai Kiran
 
EduAI - E learning Platform integrated with AI
EduAI - E learning Platform integrated with AIEduAI - E learning Platform integrated with AI
EduAI - E learning Platform integrated with AIkoyaldeepu123
 
IVE Industry Focused Event - Defence Sector 2024
IVE Industry Focused Event - Defence Sector 2024IVE Industry Focused Event - Defence Sector 2024
IVE Industry Focused Event - Defence Sector 2024Mark Billinghurst
 
Artificial-Intelligence-in-Electronics (K).pptx
Artificial-Intelligence-in-Electronics (K).pptxArtificial-Intelligence-in-Electronics (K).pptx
Artificial-Intelligence-in-Electronics (K).pptxbritheesh05
 
What are the advantages and disadvantages of membrane structures.pptx
What are the advantages and disadvantages of membrane structures.pptxWhat are the advantages and disadvantages of membrane structures.pptx
What are the advantages and disadvantages of membrane structures.pptxwendy cai
 
Oxy acetylene welding presentation note.
Oxy acetylene welding presentation note.Oxy acetylene welding presentation note.
Oxy acetylene welding presentation note.eptoze12
 
CCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdf
CCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdfCCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdf
CCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdfAsst.prof M.Gokilavani
 
Concrete Mix Design - IS 10262-2019 - .pptx
Concrete Mix Design - IS 10262-2019 - .pptxConcrete Mix Design - IS 10262-2019 - .pptx
Concrete Mix Design - IS 10262-2019 - .pptxKartikeyaDwivedi3
 
Biology for Computer Engineers Course Handout.pptx
Biology for Computer Engineers Course Handout.pptxBiology for Computer Engineers Course Handout.pptx
Biology for Computer Engineers Course Handout.pptxDeepakSakkari2
 
An experimental study in using natural admixture as an alternative for chemic...
An experimental study in using natural admixture as an alternative for chemic...An experimental study in using natural admixture as an alternative for chemic...
An experimental study in using natural admixture as an alternative for chemic...Chandu841456
 
Architect Hassan Khalil Portfolio for 2024
Architect Hassan Khalil Portfolio for 2024Architect Hassan Khalil Portfolio for 2024
Architect Hassan Khalil Portfolio for 2024hassan khalil
 
Application of Residue Theorem to evaluate real integrations.pptx
Application of Residue Theorem to evaluate real integrations.pptxApplication of Residue Theorem to evaluate real integrations.pptx
Application of Residue Theorem to evaluate real integrations.pptx959SahilShah
 
Internship report on mechanical engineering
Internship report on mechanical engineeringInternship report on mechanical engineering
Internship report on mechanical engineeringmalavadedarshan25
 

Recently uploaded (20)

Call Girls Narol 7397865700 Independent Call Girls
Call Girls Narol 7397865700 Independent Call GirlsCall Girls Narol 7397865700 Independent Call Girls
Call Girls Narol 7397865700 Independent Call Girls
 
Risk Assessment For Installation of Drainage Pipes.pdf
Risk Assessment For Installation of Drainage Pipes.pdfRisk Assessment For Installation of Drainage Pipes.pdf
Risk Assessment For Installation of Drainage Pipes.pdf
 
Call Us -/9953056974- Call Girls In Vikaspuri-/- Delhi NCR
Call Us -/9953056974- Call Girls In Vikaspuri-/- Delhi NCRCall Us -/9953056974- Call Girls In Vikaspuri-/- Delhi NCR
Call Us -/9953056974- Call Girls In Vikaspuri-/- Delhi NCR
 
Introduction to Machine Learning Unit-3 for II MECH
Introduction to Machine Learning Unit-3 for II MECHIntroduction to Machine Learning Unit-3 for II MECH
Introduction to Machine Learning Unit-3 for II MECH
 
🔝9953056974🔝!!-YOUNG call girls in Rajendra Nagar Escort rvice Shot 2000 nigh...
🔝9953056974🔝!!-YOUNG call girls in Rajendra Nagar Escort rvice Shot 2000 nigh...🔝9953056974🔝!!-YOUNG call girls in Rajendra Nagar Escort rvice Shot 2000 nigh...
🔝9953056974🔝!!-YOUNG call girls in Rajendra Nagar Escort rvice Shot 2000 nigh...
 
EduAI - E learning Platform integrated with AI
EduAI - E learning Platform integrated with AIEduAI - E learning Platform integrated with AI
EduAI - E learning Platform integrated with AI
 
9953056974 Call Girls In South Ex, Escorts (Delhi) NCR.pdf
9953056974 Call Girls In South Ex, Escorts (Delhi) NCR.pdf9953056974 Call Girls In South Ex, Escorts (Delhi) NCR.pdf
9953056974 Call Girls In South Ex, Escorts (Delhi) NCR.pdf
 
IVE Industry Focused Event - Defence Sector 2024
IVE Industry Focused Event - Defence Sector 2024IVE Industry Focused Event - Defence Sector 2024
IVE Industry Focused Event - Defence Sector 2024
 
Artificial-Intelligence-in-Electronics (K).pptx
Artificial-Intelligence-in-Electronics (K).pptxArtificial-Intelligence-in-Electronics (K).pptx
Artificial-Intelligence-in-Electronics (K).pptx
 
What are the advantages and disadvantages of membrane structures.pptx
What are the advantages and disadvantages of membrane structures.pptxWhat are the advantages and disadvantages of membrane structures.pptx
What are the advantages and disadvantages of membrane structures.pptx
 
Oxy acetylene welding presentation note.
Oxy acetylene welding presentation note.Oxy acetylene welding presentation note.
Oxy acetylene welding presentation note.
 
CCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdf
CCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdfCCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdf
CCS355 Neural Network & Deep Learning Unit II Notes with Question bank .pdf
 
POWER SYSTEMS-1 Complete notes examples
POWER SYSTEMS-1 Complete notes  examplesPOWER SYSTEMS-1 Complete notes  examples
POWER SYSTEMS-1 Complete notes examples
 
Concrete Mix Design - IS 10262-2019 - .pptx
Concrete Mix Design - IS 10262-2019 - .pptxConcrete Mix Design - IS 10262-2019 - .pptx
Concrete Mix Design - IS 10262-2019 - .pptx
 
Biology for Computer Engineers Course Handout.pptx
Biology for Computer Engineers Course Handout.pptxBiology for Computer Engineers Course Handout.pptx
Biology for Computer Engineers Course Handout.pptx
 
young call girls in Rajiv Chowk🔝 9953056974 🔝 Delhi escort Service
young call girls in Rajiv Chowk🔝 9953056974 🔝 Delhi escort Serviceyoung call girls in Rajiv Chowk🔝 9953056974 🔝 Delhi escort Service
young call girls in Rajiv Chowk🔝 9953056974 🔝 Delhi escort Service
 
An experimental study in using natural admixture as an alternative for chemic...
An experimental study in using natural admixture as an alternative for chemic...An experimental study in using natural admixture as an alternative for chemic...
An experimental study in using natural admixture as an alternative for chemic...
 
Architect Hassan Khalil Portfolio for 2024
Architect Hassan Khalil Portfolio for 2024Architect Hassan Khalil Portfolio for 2024
Architect Hassan Khalil Portfolio for 2024
 
Application of Residue Theorem to evaluate real integrations.pptx
Application of Residue Theorem to evaluate real integrations.pptxApplication of Residue Theorem to evaluate real integrations.pptx
Application of Residue Theorem to evaluate real integrations.pptx
 
Internship report on mechanical engineering
Internship report on mechanical engineeringInternship report on mechanical engineering
Internship report on mechanical engineering
 

Cryogenic Process Principle.ppt

  • 1. By : Mehdi Sibtain Cryogenic processes
  • 2. Introduction  Program aimed at customized training for better understanding of cryogenic process.
  • 3. Agenda Day One  Introduction to cryogenic process  Cooling in a cryogenic process.  Joule-Thomson effect.  Inversion Temperature.  Expansion in work producing process.  Thermodynamic analysis of cryogenic process.
  • 4. Agenda Day Two(morning)  Thermodynamic cooling paths.  Comparison of J-T & expander process.  Safety in cryogenic process.  Cold box configuration.  Effect on metals.
  • 5. Agenda Day Two (Evening)  Heat exchangers.  Gas expanders.  Separation system.  PLANT VISIT
  • 6. Agenda (Day-Three)  He & N2 separation in NG System.  Insulation.  Cryogenic control valves.  Instrumentation.  Precautions during pre-commissioning.  Operational precautions.
  • 7. Agenda (Day-Four) • Inert gas & Hydrogen recovery plants.  FFC experience with cold boxes.  Plant Visit.  Conclusion.
  • 8. Introduction to cryogenics  Cryogenic means the generation of cold.  Considered to attain at <-101C temperature.  Based on the principle of liquefaction separation of gases by decreasing the temperature.
  • 9. Benefits  Low capital investment.  Compact units requiring minimum space for installation.  Best possible recovery of valuable components  Production of higher heating value fuels.  Economical production of rare gases .
  • 10. Applications  Separation of air for production of Oxygen & Nitrogen.  Production of liquid Hydrogen for Nuclear weapons & space programs.  Liquid Helium for space programs.  Liquefied natural gas (LNG) plants.
  • 11. Applications Contd..  Liquid N2 for food preservation.  In Biological application utilization of liquid nitrogen cooled containers.  In surgery for Parkinson's disease.  Recovery of valuable feedstock from natural gas streams, upgrading the heat content of fuel gas.  Purification of various gas streams
  • 12. Properties of Cryogenic Fluids  Boiling points less than 0oC.  Critical temp. normally below ambient.  Gases with high Joule-Thomson coefficient.  Higher non-ideality (polarity) of the gas better it is for the cryogenic cooling.  Inversion temperature above ambient temperature.
  • 13. Properties Contd..  Shouldn’t solidify at the operating temperature.  Principles of mechanics & thermodynamics at ambient temperature also apply for cryogens.  Except for H2 & He all have thermal conductivities that increase as the temperature is decreased.
  • 14. Liquefaction and the Liquid States  Molecules in the gaseous state exhibit opposing tendencies-dispersion & aggregation..  The intermolecular attractive forces increase to definite maxima as the distances between molecules are diminished.
  • 15. Liquefaction Contd..  These conditions are brought about when the temperature of a substance is lowered,or  When the molecules are crowded close together I.e pressure is increased.
  • 16. Liquefaction Contd..  When the energy of attraction of one molecule for another exceeds its kinetic energy of translation, the molecules will form a dense aggregation which is termed a liquid.
  • 17. Cooling in Cryogenic Process  May be accomplished in several ways: – Cooling at constant pressure, as in a heat exchanger. – Application of Joule Thomson effect by expansion valve or throttling process. – Expansion in an expansion engine. – Cooling & Purification by evaporation
  • 18. Cooling In A Heat Exchanger  Requires a heat sink at a lower temperature.  An external refrigeration system is required if necessary.  This method is used for pre-cooling the gas & recovery of the low temperature from out going streams.  Operation at low temperature demands special techniques for fabrication.
  • 19. Joule-Thomson Effect  Joule-Thomson studied the behavior of gasses during expansion..  It can be utilized in a cycle till the dew point of a gas.  Expansion causes decrease in the kinetic energy of translation; the net result is decrease in the temperature.
  • 20. Throttling Process  Processes at continuous flow in a pipe occurring at condition approaching constant enthalpy.  Flow through a porous plug or throttling valve causes decrease in pressure due to resistance.  If device is insulated & no shaft work is produced then process is one of constant enthalpy.
  • 21. Joule-Thomson Coefficient  It is the measure of temperature behavior of a fluid during a throttling process.  At constant enthalpy, it is ratio of the change in temperature & pressure.  This coefficient is a property of the gas.  The value can be positive, negative, or zero.  For ideal gas,  = 0 this means that there is negligible change in temperature when ideal gas flows through an insulated valve.
  • 22. Coefficient Contd..  For most gases  is positive at moderate pressures & temperatures; that is, the gas becomes cooler as it expands.  Joule-Thomson coefficient represents the slope of h = constant lines on a T-P diagram.  Can be determined from the data of constant pressure specific heat & P-V-T behavior.
  • 23. Inversion Temperature  Temperature at which J-T coefficient is zero.  It is the temperature at point where a constant- enthalpy line intersects the inversion line.  The temperature at the intersection of P = 0 line the upper part of the inversion line is called the maximum inversion temperature.  Slopes of the η= constant lines are negative (η<0) at states to the right of the inversion line and positive (η>0) to its left side.
  • 24. Inversion Temp. Contd..  Temperature of a fluid will increase during a throttling process that takes place on the right- hand side of the inversion line.  Temperature will decrease during a throttling process that takes place the left-hand side of the inversion line.  Cooling effect cannot be achieved by throttling unless the fluid is below its maximum inversion temperature.
  • 25. Expansion in a Claude Process  It is an isentropic process.  Temperature of the fluid always decreases.  Cooling does not depend on being below the inversion temperature prior to expansion.  Temperature drop is much higher for this process than in isenthalpic expansion.  Increasing the pressure drop ratio increases the amount of heat removed.
  • 26. Cooling By Flashing  Flashing causes decrease in Partial pressure of the component & temperature decreases as the distance of the molecule increases.  Pressure letdown effect on liquids serves following benefits: – Avoidance of two phase flow in piping / heat exchangers. – Better purification of due to high solubility.
  • 27. Cryogenic Separation  The constant-pressure path (1) approaches the two-phase region.  The isenthalpic expansion (3) will not result in liquefaction unless the initial state is at a high enough pressure and low enough temperature for the constant-enthalpy line to cut into the two-phase region.  The isentropic process (2) does not require an initial state at as high a pressure (at a given temperature) for liquefaction.
  • 28. Liquefaction of Air  Can be explained from its enthalpy-pressure data by reference to the TS diagram for air.
  • 29. Achievement of Steady-State  Maximum liquefaction is not obtained until steady-state conditions are reached.  which time an energy balance around the separator, valve, and cooler gives H6z + H8 (1-z) = H3 where the enthalpy quantities refer the positions numbered in figure.
  • 30. Claude - Process  The flow scheme is the same as for the Joule- Thomson expansion, except that an expansion engine replaces the expansion valve.  The energy balance becomes  H6z + H8 (1 – z) + WS = H3  If the operation is reversible and adiabatic, the work is given by the expansion.  WS = - (H5 – H4)
  • 31. Thermodynamic Paths  Liquefaction by joule-Thomson valve.  Liquefaction by expansion engine.  Liquefaction by expansion engine & expansion valve .
  • 32. Comparison  Turbo-expander process has a far better capacity for recovering liquids.  Process design is complicated with expanders  Initial & operating cost are higher for expander process.
  • 33. Item Specified Condition Heat Exchanger Pressure drop (psia) shell side 5 Tube 5 Minimum Approach Temperature, O F 15 Flash Separator Pressure, psia 400 Turbo-expander Discharge Pressure, psia 400 Efficiency, % 75 Specified Process Conditions For Joule-Thomson/Turbo-expander Process Comparison
  • 34. Item Calculated Process Conditions Joule-Thomson Turbo- expander Primary Separator - Temperature, F -48 -45 - Liquid rate, moles/hr 119 182 Secondary Separator (Turbo-expander) - Temperature F - -112 - Liquid rate, moles / hr - 463 Heat Exchanger - Temperature of Feed out, F -9 -45 - Power Generated in Turbo Expander, hp - 1316
  • 35. Component Turbo-expender Joule-Thomson Turbo-expander Incremental Rec Moles/hr Mols/hr %Rec Moles/hr %Rec N2 0.88 0.80 0.07 0.06 0.81 C1 353.42 3.42 30.60 0.30 322.82 C2 103.18 30.26 10.22 3.00 92.96 C3 92.09 76.11 17.11 14.27 74.82 iC4 30.92 93.70 11.48 34.79 19.44 nC4 21.27 96.68 10.33 46.95 10.94 iC5 10.94 99.45 8.15 74.09 2.79 nC5 10.97 99.73 8.98 81.64 1.99 C6+ 22.00 100.00 21.74 98.92 0.26 645.68 118.85 526.83 C4+ Recovery 97% 61%
  • 36. Physiological Hazards  Severe cold "burns" may be inflicted if the human body comes in contact.  Damage to the skin or tissue is similar to tan ordinary burn because the body is composed mainly of water.  The low temperature effectively freezes the tissue damaging or destroying it.
  • 37. Physiological Hazards Contd..  Body can normally adjust for a heat loss of 95 J/m2s for an area of limited exposure.  Freezing of facial tissue will occur in about 100 sec. if the heat loss is 2300 J/m2s.
  • 38. Materials and Construction Hazards  Consider the ductility of the material since low temperatures have the effect of making some construction materials brittle or less ductile.  Exposure of low temperature stream on to ordinary metals may result in material failure.
  • 39. Typical protections of cold box  On high ΔP, closure of inlet valve(During S/UP)  Trip of unit at high inlet temperature to protect exchanger.  Closure of J-T valve / expander nozzle on low flow of inlet gas to protect temperature gradient.  Trip of unit on low exit gases temperature.
  • 40. Flammability and Explosion Hazards  Explosion requires an oxidant, a fuel and an ignition source.  The oxidizer will be oxygen available from a leakage or condensation of air on cooled surfaces and buildup as a solid with water.  The ignition source may be a mechanical or electrostatic spark, flame, impact heat by kinetic effects, friction, chemical reaction.
  • 41. Mixture Flammability Limits (mol%) Detonability Limits H2 – air 4-75 20-65 H2 – O2 4-95 15-90 CH4 – air 5-15 6-14 CH4 – O2 5-61 10-50 Flammability & Detonability Limits of Hydrogen & Methane Gas
  • 42. High – Pressure Hazards  High pressure is obtained by gas compression during liquefaction (if required).  If this confined gas is suddenly released a line a significant thrust may be experienced.  Force generated by rupturing a 2.5 cm diameter valve on a 13.9-Mpa pressurized gas cylinder would be over 6670N.  Adequate PSVs should be provided.
  • 43. Cold Box  Cold box is a group of multi fluid exchanger cores assembled in a single structure.  Designed for cooling upto very low temperatures.  These must be properly insulated for approaching the adiabatic conditions.
  • 44. Components of cold box  Piping and liquid separators with low temperature metallurgy.  Coiled or plate-fin exchangers.  Isenthalpic valves/ Expanders or both  Separation or rectification columns (if required).  Instrumentation.  Insulation.
  • 45. Cryogenic Metallurgy  Metals used for vessels and piping vary with temperature.  As temperature decreases most mechanical properties—hardness, yield, tensile and fatigue strength increase.  Corrosion is of less concern.  The problem is ductility.  Linear expansion is important as well.
  • 46. Ductile Properties  Usual way of characterizing ductile properties of metal is Charpy-notch or keyhole test.  Notch sensitivity depends on crystal structure of the metal.  Austenitic stainless steels, high nickel steels, aluminum, and copper all have face-centered crystal structures.  Aluminum is usually preferred over copper because of its lighter weight.
  • 47. Linear Expansion  Coefficient of linear expansion for several metals varies with temperature.  The higher coefficients for aluminum and copper raise the problem of providing for Expansion by means of expansion loops, bellows type connections, and the like.
  • 48. Structural Properties  Face-centered-cubic (fcc) metals and their alloys are most often used in the construction of cryogenic equipment.  Al, Cu, Ni, their alloys and the austenitic stainless steels are “fcc” and do not exhibit an impact ductile-to-brittle transition at low temperatures.  The body-centered-cubic (bcc) metals and alloys are undesirable for low temperature.
  • 49. Structural Properties Contd..  Fe, the martensitic steels (low carbon and the 400 series stainless steels), Mo and Nb. exhibit a ductile-to-brittle transition at low temperatures.  Hexagonal-close-packed (hcp) metals exhibit mechanical properties intermediate between those of the “fcc” and “bcc” metals.
  • 50. Structural Properties Contd..  Zr and pure Ti alloys with a “hcp” structure have been used where weight reduction and reduced heat leakage through the material have been important.  Small impurities of O, N, H, and C can have a detrimental effect on the low temperature ductility properties of Ti and its alloys.
  • 51. Properties non Metals  Plastics increase in strength as the temperature is decreased, but this is also accompanied by a rapid decrease in elongation in a tensile test and a decrease in impact resistance.  Teflon and glass-reinforced plastic retain appreciable impact resistance.  The glass-reinforced plastics also have high strength-to-weight and strength-to-thermal conductivity ratios.
  • 52. Properties non Metals Contd..  Elastomers, become brittle at low temperatures.  Nevertheless, rubber, Mylar, and nylon can be used for static seal gaskets provided they are highly compressed at room temperature prior to cooling.
  • 53. Thermal Properties  High-purity aluminum and copper exhibit high thermal conductivity from 20 to 50 K.  These peaks are rapidly suppressed with increased impurity levels and cold work.  Monel, Inconel, stainless steel & aluminum alloys show a steady decrease in thermal conductivity.  All cryogenic liquid except hydrogen and helium have thermal conductivities that increase as the temperature is decreased.
  • 54. Electrical Properties  The electrical resistivity of most pure metallic elements at ambient and moderately low temperatures is approximately proportional to the absolute temperature.  At very low temperatures it approaches a residual value almost independent of temperature.  For alloys it is largely independent of temperature.
  • 55. Heat Exchangers Selection  Small temperature difference between inlet and exit streams to enhance efficiency.  Large surface area-to-volume ratio to minimize heat leak.  High heat transfer to reduce surface area.  Low mass to minimize start-up time.
  • 56. Selection Contd..  Multi-channel capability to minimize the number of exchangers.  High-pressure capability to provide design flexibility.  Low or reasonable pressure drop to minimize compression requirements.  High reliability with minimal maintenance to reduce shutdowns.
  • 57. Tubular-fin Heat Exchangers  These heat exchangers are used as gas-to-liquid heat exchangers.
  • 58. Plate-fin Heat Exchangers  Plate-fin are about nine times as compact as conventional shell-and-tube heat exchangers.  Commonly fabricated from aluminum.  These are stack of layer.  Each layer consists of corrugated aluminum sheets (fins) between flat aluminum “separator” plates to form individual passage.
  • 59. Plate-fin Exch. Contd..  The stack, including the sidebars, is bonded by a carefully controlled brazing process.  Passages can be arranged for either cross flow, countercurrent flow, concurrent flow, or multi pass flow.  The number of passages provided for each stream can be varied to yield the required flow rates and pressure drop.
  • 60. Plate-fin Exch. Contd..  Up to eight separate streams can be accommodated in one core.  Heat transfer area per unit volume is around 2000 m2 / m3.
  • 61. Applications  The plate-fin type is primarily used for gas-to- gas application and tube-fin exchangers for liquid-air heat exchangers.  In most of the application (in trucks, cars, and airplanes), mass and volumes reduction are particularly important.  Widely used in cryogenic, energy recovery, process industry, refrigeration, and air- conditioning system.
  • 62. Forms of Corrugated Sheets  The plates are typically 0.5 to 1.0 mm thick and the fins 0.15 to 0.75 mm thick.  Fins give extra heat transfer area and structural support to the flat plates.  Most common types of fins are: – Plain fin – Plain-perforated fin – Serrated fin (also called “lanced”, “interrupted”, “louver” or “militantly”) – Herringbone or wavy fin
  • 63. Limitations  The flow channels are small, which means that the mass velocity also has to be small (10 to 300 kg/[m2.s]) to avoid excessive pressure drops.  Plate-fin exchangers are restricted to clean fluids.
  • 64. Limitations Contd..  Operation at low temperatures requires removal of essentially all impurities that are to be cooled.  High operating temperature & differential temperature are not allowed due to brazing.
  • 65. Gas Expanders  There are four general types of expanders.  Mostly expanders in low temperature services are of the single-stage, radial wheel impeller.  High efficiency of a turbo-expander requires operation at near optimum speed.  Optimum efficiency lies in the speed range of 10,000 to over 50,000 rpm.
  • 66. Flow Control  Flow through the turbo-expander is controlled by variable stationary nozzles.  These are mechanically arranged for an outside manual or diaphragm control to vary the clearances between the nozzles.
  • 67. Shaft Seal  The “oil-free” arrangement is widely used.  An outward leakage of gas is permitted out of each labyrinth seal.  A continual stream of pressurized gas ( seal gas) is introduced at a midpoint of each labyrinth seal which leaks to atmosphere.  This seal gas is injected at a rate slightly higher than that leaking out through the seal thus retaining the valuable process gas
  • 68. Turbo-Expander Materials  Expanders should have bearings approx.10 times as strong as in similar machines.  Blade materials are selected based on erosion resistance and ability to withstand low temperature.  Aluminum alloys are used in the manufacture of expander wheels.
  • 69. Separation System  Utilized if the mixture to be separated is essentially binary with a difference in boiling points.  Tray columns are utilized for the desired separation.
  • 70. Single column Separation  It is a J-T liquefaction system with a substitution of a rectification column for the liquid reservoir.  In a simple single-column process, although the bottoms purity is high, the top effluent stream is impure.
  • 71. Linde Double-Column System  Two rectification columns are placed one on top of the other.  Feed is introduced at an intermediate point.  Condenser-evaporator at the top of the lower column makes the arrangement a complete reflux distillation column.  Almost pure top & bottom products are produced.
  • 72. Linde System Contd..  Condenser must condense light gas vapor by evaporating liquid heavy component.  It is necessary to operate the lower column at a higher pressure, while the upper column at lower pressure.
  • 73. Helium And Nitrogen Separation In N G System  Helium content of the natural gas plants normally has varies upto 02 %  Nitrogen content varies from 12 to 80%.  The remainder of the natural gas is methane, ethane, and heavier hydrocarbons.
  • 74. He & N2 Separation In NG System Contd..  Major constituents of NG have boiling points very much different from that of He, a distillation column is unnecessary.  High separation can be accomplished with condenser-evaporators.  Expanders give better recovery but at the expense of complexity of process.
  • 75. Insulation  To minimize radiative heat transfer, minimize convective heat transfer and use only a minimum of solid conductance media.  In selection consider ruggedness, convenience, volume, weight, ease of fabrication and handling, thermal effectiveness and cost.  Experimentally obtained apparent thermal conductivity is used to characterize the thermal effectiveness of various insulations.
  • 76. Types of Insulation  Cryogenic insulations have generally been divided into five general categories:  High vacuum, multilayer insulation, powder, foam, and special insulations.
  • 77. Vacuum Insulation  Heat transport across an evacuated space depends on the emissivity.  The insertion of low-emissivity floating shields within the evacuated space reduce the heat transport by radiation.  Radiant heat transfer is reduced to around one- half of the rate without the shield, two shields can reduce this to around one-fourth of the rate without the shield.
  • 78. Multilayer Insulation  Consists of alternating layers of highly reflecting material, such as aluminum foil or aluminized Mylar, and a low-conductivity spacer material or insulator, such as fiberglass mat or paper, glass fabric, or nylon net, all under high vacuum.  Degradation in thermal performance is caused by presence of edge exposure to isothermal boundaries, gaps, joints, fill and vent lines.
  • 79. Powder Insulation  It has the benefit of multiple floating shields without incurring the difficulties of awkward structural complexities.  Amount of heat transport due to radiation through the powders can be reduced by the addition of metallic powders.
  • 80. Foam Insulation  Thermal conductivity is dependent upon the bulk density of the insulation.  Of all the foams, polyurethane and polystyrene have received the widest use at low temperatures.  The major disadvantage is that they tend to crack upon repeated thermal cycling and lose their insulation value.
  • 81. Selection of Insulation  Many of the vessels contained in a “cold box” use granular perlite.  Wool felt might be used around maintenance entrances.  On transfer lines use urethane, perlite or possibly vacuum jacketed lines.  Polyurethane foam requires a vapor proof outer jacket.
  • 82. Cryogenic Control Valves  The principal function of a J-T valve is to obtain isenthalpic cooling.  These valves are generally needle-type valves modified for cryogenic operation.  Normally these are made of SS-304 or SS- 321 material  Have a protection sleeve around the body.  The plugs are tapered & installed in a clean & polished body for minimum friction.
  • 83. Cryogenic Instrumentation  Metals become brittle at low temperatures, so the instrument literally falls apart.  Elastomeric gasket and seals contract faster than the surrounding metal parts, and the seal often is lost.  Even hermetically sealed instruments can develop pin holes or cracks  For cryogenic service, check integrity under liquid N2.
  • 84. Pressure Instrumentation  Measured by the flush mounted pressure transducer  Consists of a force-summing device (below, diaphragm, bourdon tube), an analog device (strain gage, piezoelectric crystal, variable distance between capacitor plates, and the like).  Elements are likely to be made of different materials (bronze diaphragm, stainless-steel case, semiconductor strain gage), each will react to the temperature change differently.
  • 85. Pressure Instrumentation Contd..  Very small pressure sensing elements from a single semiconductor chip may be used to reduce or eliminate temperature gradients across the device.  The single element nature of the pressure gage assembly reduces differences in materials of construction.
  • 86. Liquid Level  The measurements are made in the conventional CPI approach using floats.  Sight glasses cannot be used since cryogenic fluid in it shall boil.  The dielectric constant of cryogens is related to their density.  As liquid level rises, greater dielectric constant of liquid causes capacitance to vary linearly.  For best accuracy, should be calibrated in place.
  • 87. Flow  The measurement of cryogenic fluids is most troublesome since it is a derived quantity.  Normally these are avoided & flow is measured by the liquid level transfer & measurement at high temperature exit streams.  Calibration has accuracy limitation.
  • 88. Temperature  The level & range of measurement need consideration.  Up to 20K favorite choice is platinum resistance thermometer (PRT).  Below 20k, semiconductor thermometers (germanium, C, or Si based) are preferred.  Their resistance increases as the temperature is lowered, semiconductors are usually chosen for temperatures from about 1 to 20 K.
  • 89. Temperature Contd..  For large range of say 1 to 400 K, diode thermometers are recommended.  Diode thermometers are very much smaller and faster.  Thermocouples are not used as the thermoelectric power drops to a few µV/K.
  • 90. Installation and Operation  Transport and storage.  Erection.  Operation.
  • 91. Transport and Storage  Plate-fin heat exchangers are shipped hermetically sealed to avoid ingress of moisture or dust.  Without N2-filling, silica gel will be inserted into the headers to absorb any moisture.  Inactive or dummy layers are normally closed by self-sticking aluminum foils.  Lifting and transportation only allowed on the marked points and under use of suitable devices. Protect the exchanger edges.
  • 92. Measures at Arrival on-site  Check for damages of the packing & block.  Check the nitrogen pressure level.  Check for any defects of stuck aluminum foils and possible renewal.  In case of any leakages or mechanical damage, Vendor shall be informed.  Carry out washing / drying if exchanger is not sea worthy packed for sea freight batteries.
  • 93. Storage  Block should be stored within the original packing. Otherwise plate-fin exchangers may be stored upon square timbers.  Protect from ambient influences (rain, dirt) by suitable covering.  Storage shall be in a position where aluminum foils are seen on vertical.  Should be stored in-house.  Monitor pressure of nitrogen gas regularly.  Check Sealing of inactive sections.
  • 94. Installation  The covers on nozzles or flanges shall be removed only immediately before the connection of nozzles to the piping system.  Consider Exact Alignment .  Piping has to be carefully cleaned and dried before connecting to the heat exchangers.  Install strainers at the inlet pipes.  Before insulation work any existing temporary nipples or gauges on dummy layers should be removed
  • 95. OPERATION  Process fluids should be in steady flow.  Deviations from the specified operation conditions are only allowed, if there are no appreciable changes in stream compositions, temperatures and pressures.  Before starting, Nitrogen filling has to be purged out by the process fluids.
  • 96. Cooling & Warming up  Avoid building up of thermal stresses.  Avoid sudden temperature shocks and under changes of stream temperatures.  Cooling is allowed with designed gas only.  Warming up with gas is allowed only after draining all liquid out of the exchanger.
  • 97. Allowable limits & Precautions  Temperature difference between two streams in the heat exchanger must not exceed 50 K.  The temperature change of any stream must not exceed 60 K/h and 2 K/min.  Mass velocity on any side should never exceed 300 Kg/m2.s.  Pressurization / de-pressurization rate to be kept lower than 2 Kg/cm2/min.
  • 98. Allowable limits Contd..  Cold box cooling down speed should not exceed 25oC / hr.  During deriming transfer the cold only in one direction to avoid excessive temperature difference.  Degree of drying is sufficient if equipment temperature is 30oC and dew point is <–40oC.  Strictly follow the design limits for temperature and pressure.
  • 99. Allowable limits Contd..  Differential pressure of any side of plate- fin exchanger should be controlled. Follow vendor instructions about the same.  Analyze Insulation chamber periodically.  If leakage from cold box is detected, inform Vendor, & shutdown/ preserve it.
  • 100. General Operational Consideration  The major design problem is assembling accurate process & enthalpy data.  The operating problems stem from In- adequate design& temperature involved are: – Freezing of liquids – Protection of metals at low temperature – Handling of highly volatile liquids – Safety – Mechanical failure
  • 101. Freezing of Liquids  Hydrocarbons heavier than propane are solids below –1300C.  CO2 & water freeze at –800C & O0C resp. H2S & other contaminants solidifying on cold surface.  Insulation should be continuously purged to protect freezing on outer sides.  Control dew point from upstream section .  Perform warming up operations.
  • 102. Hydrogen Recovery Unit  Purpose :  Removal of Ar, CH4 & N2 from synthesis gas.
  • 103. Nitrogen Separation Plant  The Nitrogen plant produces inert gas (nitrogen) in purity, using the cryogenic process.  The source from which nitrogen is produced is air.
  • 104. Major Problems Encountered in HRU  Fouling/choking of Cold Box Exchangers. – Low regeneration of adsorbers – High temperature of inlet gas. – Upsets in NH3 recovery unit. – Bellow leakages at V-4581A/B. – Passing of inlet valve TV-45083.  Inlet Strainer Choking.  Failure of PV-45022 (Letdown Valve).
  • 105. Major Problems in HRU Contd..  Insulation Shell Pressure Monitoring and Sampling.  Condensation and Icing on External Surfaces.  No specialty for maintenance of fin exchangers on site.
  • 106. Deriming Operation Problems • Deriming process is very slow. – Drain valve #45112 line occasionally chokes. – Warming rate control is sometimes problematic. – Temperature gradients limits were not followed (occasionally). – Procedure revised to improve the understanding.
  • 107. Areas of Concern  There is no procedure available to carryout following activities: – Removal and refilling of perlite. – Leak test of HRU cold box. – Inspection of E-4552A/B and V-4583 etc. – Repair of any damaged part including brazing procedure and alignment of exchangers.
  • 108. Areas of Concern Contd..  Flow / Pressure Variations During Adsorber Changeover.  Sampling Points Sensing Tubing Blockage
  • 109. N2 Plant Problems Encountered  Turbine Flow Control nozzles sticking during startup; resolved by repacking of valve.  Nitrogen Plant Evaporation Pit Y-3919: – Icing and condensate formation around the pit. – Seepage of water inside the pit and solidfication. – LS tracing around the pit was provided.
  • 110. Nitrogen Plant Problems Contd..  After T/A-2000 liquid N2 inventory dropped to 25.4% & level rise rate was slow. Probable reason is low insulation level.  Plant Tripping at Low Lube Oil Temperature.  Refrigeration Unit Performance Deterioration.  Leakage From Storage Liquid Inlet Line during commissioning.
  • 111.
  • 112. Compounds Critical Temperature Tc (K) to Critical Pressure Pc (Atm) Ammonia 405.5 111.3 Carbon dioxide 304.2 72.9 Hydrogen 33.3 12.8 Hydrogen Sulfied 373.6 88.9 Nitrogen 126.2 33.5 Oxygen 154.4 49.7 Sulfur dioxide 430.7 77.8 Water 647.3 218.2 Methane 190.7 45.8 Ethane 305.43 48.2 Propane 369.9 42.01
  • 113.
  • 114.
  • 115.
  • 116.
  • 117.
  • 118.
  • 119.
  • 120.
  • 121.
  • 122.
  • 123.
  • 124.
  • 125.
  • 126.
  • 127.
  • 128.
  • 129.
  • 130.
  • 131.
  • 132.
  • 133.
  • 135.
  • 136.
  • 137.
  • 138.
  • 139.
  • 140.
  • 141.
  • 143.
  • 144.
  • 145.
  • 146.
  • 147.
  • 148.
  • 150.
  • 152.