Monday, 10 June 2013

Design Procedure for U – tube type Horizontal Heat Exchanger

Design Procedure for U – tube type Horizontal Heat Exchanger

SHELL SIDE :-
Note :- For Shell Side J = 0.85
   1)Shell Diameter :-

a)Area occupied by each tube (a) = (ST )2  (for square pitch)
                                                      = 0.866 (ST )2  (for triangular pitch)
Here ST  is the pitch of tube.

b) Area occupied by ‘n’ tubes (an) =  2 x n x (ST )2  (for square pitch)
                                                      = 2 x n x 0.866 (ST )2  (for triangular pitch)
    
     c) Area of shell (As) = an
            Here β is the proportionality factor whose value is,
0.8 - For single pass
0.7 - For double pass
0.6 - For multiple pass
      
      d) Also, Area of shell (As) = π/4 Di 2  
              Here Di  is the Shell inside diameter.
        
Therefore from c) and d) we can say that,
                                 an /β = π/4 Di 2  
From the above equation we can calculate Di ,Which should be a multiple of 50.

2)Shell Thickness :-

t = (PDi / 2fJ – P) = (PDo / 2fJ + P) = (PD / 2fJ)

P   = Design Pressure
Di   = Inner diameter of shell as calculated above
Do  = Outer diameter of shell
D    = Mean diameter of shell = Do + Di /2
f    = Allowable stress of shell material
The calculated value of ‘t’ must be greater than 8mm,if it is less than 8mm than take t = 8mm.
   
    3)Nozzle (Inlet & Outlet) :-

Nozzle Thickness (tn) = (PDi / 2fJ – P)

Here, Di = Nozzle Inlet & Outlet Diameter
After adding corrosion allowance to the above calculated value of tn it must be greater than 4mm,if it is less than 4mm than take tn = 4mm.
   
   4)Head Thickness :- For a U – tube type Horizontal Heat Exchanger the head used is always a Torispherical Head.
Therefore,

Head thickness(th) = (PRcW/2fJ) + c

Here,
Rc = Crown Radius
Rk = Knuckle Radius
W = 1/4 ( 3+ (Rc /Rk)1/2 )
If Rc is not given then take shell Inside Diameter as Rc .
Also Rk = 6% of Rc
OR
If it is mentioned in question that, U- tube type horizontal heat exchanger head is joined to the shell with the help of flanges which are cold, then, For cold forming calculate
5 x t(shell thickness) and take it as Rk .

    5) Baffles :- 
        The baffles used will be of the Transverse type with spacing = Di / 5
Thickness of baffles will be = 6mm
The baffles are 25% cut
Therefore, Baffle length = 0.75 x Di
   
    6) Tie Rods :-
 No. of Tie rods = 6
Dia. Of tie rod = 10mm
       
    7) Flange Joint Between Shell & Tubesheet :-

Note:- Some times G is taken same as calculated for Tube Side.

a)  Design of Gasket :-

i)Gasket inside diameter (Gi)= Do + 10
ii)Go / Gi = ( y – pm / y – p(m+1) )1/2
Now, After calculating the ratio Go / Gi substitute the value of Gi and calculate
iii) Go i.e Gasket outside diameter .
Then calculate,

iv) Mean Gasket Diameter(G)  = Go + Gi / 2

v) Width of Gasket ( N ) = Go - Gi / 2
       
       vi) Basic Gasket seating width bo = N/2
Now,
If bo < 6.3 then b = bo    &
If bo > 6.3 then b = 2.5(bo)1/2
Here, b is Effective gasket seating width

b) Design of Bolt :-

i) Wm1 = π b G Yb
         
         ii) Wm2 = π (2b) G m p + π/4 G2 P

Consider the greater value from Wm1 and Wm2 for all the further calculations.

iii) Bolt Area (A) = Wm(max) / f

iv) No. of Bolts(n) = G / 25 (should be a factor of 4)


  v)   Bolt Diameter ( db ) = ( 4 x A / π x n ) 

 vi) Bolt circle Diameter (B) = Go + 2 db

c)   Design of Flange :-
      
            Flange thickness( tf ) = G ( P/ kf )1/2

 k = 1 / ( 0.3 +( 1.5 Wm(max) hG/H x G ))

 H = π/4 G2 P

 hG = B – G / 2

TUBE SIDE :-
Note :- For Tube Side J = 1
   
   1)Tube Thickness :-
 
        t = (PDi / 2fJ – P) = (PDo / 2fJ + P)

If t is less than 2mm then take t = 2mm.
   
   2)Tubesheet Thickness :-

     t = FG ( 0.25P/f )

For U – tube type Horizontal Heat Exchanger  F = 1.25 & take G = 380 if not given.

   3)Channel & Channel Cover :-

It is proposed to make the channel & channel cover out of a single plate.
Therefore,

Thickness of Channel Plate( t ) = Gc ( kp/f )1/2

For Ring type gasket or gasket bolted with narrow faced k = 0.3
For cover bolted with full faced gasket k = 0.25

     4) Flange joint between Tubesheet and Channel :-

a)  Design of Gasket :-

If G is assumed 380 then take Ring Gasket width(w) = 22mm  & bo = w/8
Ya = 126.6 N/mm2
m = Gasket Factor = 5.5
And if G is to calculated then calculate G by the method as given below.

i)Gasket inside diameter (Gi)= Do + 10

ii)Go / Gi = ( y – pm / y – p(m+1) )1/2
Now, After calculating the ratio Go / Gi substitute the value of Gi and calculate

iii) Go i.e Gasket outside diameter .
Then calculate,

iv) Mean Gasket Diameter(G)  = Go + Gi / 2

v) Width of Gasket ( N ) = Go - Gi / 2

       vi) Basic Gasket seating width bo = N/2
Now,
If bo < 6.3 then b = bo    &
If bo > 6.3 then b = 2.5(bo)1/2
Here, b is Effective gasket seating width

Design of Bolt & Flange is same whether G is calculated or assumed.

b) Design of Bolt :-

i) Wm1 = π b G Yb
        
         ii) Wm2 = π (2b) G m p + π/4 G2 P

Consider the greater value from Wm1 and Wm2 for all the further calculations.

iii) Bolt Area (A) = Wm(max) / f

iv) No. of Bolts(n) = G / 25 (should be a factor of 4)

v) Bolt circle Diameter (B) = Go + 2 db

b)Design of Flange :-

Flange thickness( tf ) = G ( P/ kf )1/2

k = 1 / ( 0.3 +( 1.5 Wm(max) hG/H x G ))

H = π/4 G2 P

hG = B – G / 2

      5)Nozzle (Inlet & Outlet) :-

Nozzle Thickness (tn) = (PDi / 2fJ – P)

Here, Di = Nozzle Inlet & Outlet Diameter

After adding corrosion allowance to the above calculated value of tn it must be greater than 4mm,if it is less than 4mm than take tn = 4mm.

Also,
Area compensated for each nozzle is (A) =
Nozzle inlet & outlet diameter x cover plate thickness


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