TINKER’S FLOW MODEL FOR SHELL & TUBE HEAT EXCHANGER DESIGN
All the latest
methods (Bell’s method) and many computer programs (HTRI, BJEC, Aspen EDR) for
the process design of the heat exchangers without phase change are based on
Tinker’s flow model.
If there is no
phase change of shell side fluid then shell side heat transfer coefficient and
the shell side pressure drop in all latest methods are calculated based on
Tinker’s flow model. In conventional method for heat exchanger design like
those developed by the Kern, it is assumed that entire shell side fluid is
flowing across the tube bundle and between the baffles. But in really shell
side fluid is flowing in various ways. In Tinker’s flow model the sell side
flow is divided in total five different streams.
1.
Stream A
2.
Stream B
3.
Stream C
4.
Stream E
5.
Stream F
Fig 1: Tinker’s
Flow Model
·
Stream A
Stream A is
the tube-to-baffle leakage stream or it is the fraction of shell side fluid flowing
through the clearance between tube hole in baffle and tube outside diameter.
This stream does not bypass the heat transfer area (outside area of tubes) and hence,
it does not create any adverse effect on the value of heat transfer
coefficient. However, it makes the significant difference in pressure drop
(loss). When stream A leaves this clearance, it forms free flowing jet. Hence,
boundary layer separation occurs and considerable friction loss or pressure
drop takes place. Effect of stream A must be considered in the calculation of
pressure drop.
·
Stream B
Stream B is
the actual cross flow stream or it is the fraction of shell side fluid which is
flowing across the tube bundle and between the baffles. In Kern’s method and
other old methods, it is assumed that entire shell side fluid is flowing like
stream B.
·
Stream C
Stream C is
bundle to shell bypass stream or it is the fraction of shell side fluid flowing
through the clearance area between shell inside diameter and tube bundle.
Stream C is the main bypass stream. (bypassing the heat transfer area). This
clearance area provides low pressure drop path for the shell side fluid. Hence,
% of shell side fluid bypassed through this clearance area is quite
significant. It is maximum with pull through floating head heat exchanger and
minimum with fixed tube sheet heat exchanger. Amount of stream C can be reduced
considerably by using sealing strips which are attached on inside surface of
shell. They provide the partial blockage or the additional resistance in the
path of stream C.
·
Stream E
Stream E is the baffle to shell leakage
stream. It is a part of shell side fluid flowing through the clearance between
the edge of baffle and shell wall. Like stream C, this stream is also bypassing
the heat transfer area and hence, reduces shell side heat transfer coefficient.
But amount of stream E is lesser than amount of stream C. Normally, the
clearance between baffle outside diameter and shell inside diameter is in the
range of 1.6 to 4.8 mm while clearance between tube bundle and shell inside
diameter is in the range of 10 to 100 mm.
·
Stream F
Stream F is the pass-partition bypass stream.
In tube sheets where pass partition plates are attached (for forming tube side
passes), in that portion tubes cannot be provided. In multipass heat
exchangers, one can find more number of gaps in tube bundle. Stream F is the
fraction of shell side fluid flowing through these gaps. If the gap is vertical
it provides low pressure drop path for fluid flow. Just like stream C and
stream E, this stream is also bypassing the heat transfer area and reduces
shell side heat transfer coefficient. Amount of stream F and its adverse
effects are significant in multipass heat exchanger. To reduce the amount of
this stream sometimes dummy tubes are used.
NOTE: There is no stream designated as stream “D”.
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