1 Podstawowe wiadomości o wymianie ciepła i wymiennikach ang

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Theory of Heat Machines

2l.+1cl.

Theory of Heat Machines

2l.+1cl.

Paweł Skowroński Ph.D.,

P.Eng.

pskowr@itc.pw.edu.pl

Tel +22 243 52 13

p. 404

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Formalities

Formalities

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Scope of the Subject

• Processes in heat machines and

thermal devices

• Thermodynamical cycles – thermal

engines

• Heat machines and systems analysis

and synthesis

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Bibliography

Notes !!!
• Staniszewski B. – „Termodynamika”
• Other handbooks on thermodynamics,

technical thermodynamics, theory of
heat machines, …

• No textbook dedicated to this

lecture!!!!

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How to get credit? Three colloquies

• Conditions

– positive (≥ 3=) marks from at least two from

three colloquies

– sum of marks bigger than 8 (bigger – not

equal!) (+: +0,25; –: -0,25; =: -0,33)

– at least a partial answer on theoretical question

and a partial solution of the exercise is

necessary to get a positive mark of a colloquy

(it is necessary but not enough)

– the 1st and the 2nd colloquies can be repeated

during a „marathon”; mark obtained at the

„marathon” replaces the colloquy mark; the 3rd

colloquy will not be repeated

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How to get credit? The exam

– there is a written and oral part of the exam

– written examination consists with a complex

exercise and a theoretical topic

– oral examination covers knowledge of the theory

– to take an oral exam one must pass the written

part of the exam; passing the written part with a

mark 3- allows for single approach to the oral part;

– an average of colloquies marks equal or bigger

then 4 releases from the written examination

– an exam mark is given if a sum of colloquies marks

is higher then 8,

– if the sum of colloquies marks is less than 8, the

written part of the exam can be accepted with a

mark at least 4

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Energy Conversion

Energy Conversion

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energy conversion

Usable

(possible for use)

energy

carriers

-heat carrier

-mechanical energy

-electricity

use-ful energy

– delivered in
form of heat

–delivered in
form of work

–light
–information
processing

Primary Energy

-of wind
-geothermal
-solar
-water flows
-chemical
-nuclear

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energy conversion

Energy conversion is always accompanied with losses:

during conversion of heat to work (thermal engine cycles)

– results

from thermodynamic rules

resulted from irreversibility of thermodynamic processes
(irreversible entropy growth)

imperfectness of conversion of chemical energy into

internal

energy (not-full use of fuels)

mechanical fraction between machines elements, and

resistance

in fluid flow

electric and magnetic – „at cuprum and in iron”

others

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Chosen and basic

information on heat

transfer process and heat

exchangers

Chosen and basic

information on heat

transfer process and heat

exchangers

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heat transfer mechanisms

• conduction

• convection

– natural
– forced

• radiation

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δ

Q

S

t

1

t

2

λ

)

(

2

1

t

t

S

Q

λ

– heat conduction coefficient





K

m

W

t

1

, t

2

[K] – temperatures at surfaces of the heat conducting material

δ [m] – thickness of the wall

S [m

2

] – heat transfer area

heat conduction at a flat wall

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values of a heat conduction coefficient λ at 100°C

duralumin

181,4

increases with temperature

brass 70Cu/30Zn:

109,3

increases with temperature

carbon steel

52,3

decreases with temperature

chrome-nickel steel

ok. 11-13

change with temperature depends

on

the steel composition

brick

0,3÷1,2

mineral wool

0,035÷0,05





K

m

W





K

m

W





K

m

W





K

m

W





K

m

W





K

m

W

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)

(

2

1

t

t

S

Q

Q

S

t

1

t

2

α

heat infiltration coefficient α

fluid – wall surface or wall surface –

fluid depends on:

• velocity, density, viscosity, specific heat, heat conductivity of the fluid
• the fluid phase (gas, liquid, boiling liquid, condensing steam)
• the surface shape and roughness





K

m

W

2

heat infiltration

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heat transfer through a flat wall

)

(

)

(

)

(

2

2

2

2

1

1

1

1

f

w

w

w

w

f

t

t

dS

t

t

dS

t

t

dS

Q

d

Q

Q

Q

Q

Q

t

f1

t

w1

t

w2

t

f2

λ

δ

α

1

α

2

dS – elementary area

δ – partition thickness

t

w

– partition surface

temperature

t

f

– fluid temperature (far

away from a boundary
layer)

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heat transfer through a flat wall,

cont.

)

(

)

(

)

(

2

2

2

2

1

1

1

1

f

w

w

w

w

f

t

t

dS

t

t

dS

t

t

dS

Q

d

dS

Q

d

t

t

w

f

1

1

1

)

(

dS

Q

d

t

t

w

w

)

(

2

1

dS

Q

d

t

t

f

w

2

2

2

)

(

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



2

1

2

1

1

1

)

(

dS

Q

d

t

t

f

f

dS

Q

d

dS

Q

d

dS

Q

d

t

t

t

t

t

t

f

w

w

w

w

f

2

1

2

2

2

1

1

1

)

(

)

(

)

(

)

(

1

1

1

2

1

2

1

f

f

t

t

dS

Q

d





heat transfer through a flat wall,

cont.

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)

(

2

1

f

f

t

t

dS

k

Q

d





2

1

1

1

1

k

coefficient of a heat transfer through a flat wall :

heat transfer through a flat wall,

cont.

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heat transfer through a pipe wall

)

(

)

(

2

1

ext

w

ext

ext

w

in

in

in

t

t

dL

D

t

t

dL

d

Q

d

infiltration

of heat on both sides of the

partition:

a pipe of an elementary
length dL

Q

Q

t

i

n

t

w1

t

w2

t

ext

λ

α

ext

Q

Q

α

in

d

in

D

e

x

t

w

z

T

w 1

T

w 2

T

z

T

w

x

y

z

r

w

r

z

in

ext

ext

in

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dr

dt

dL

r

Q

d

2

Heat

conduction

through a pipe wall,

(an area of a heat conduction changes with a radius):

heat transfer through a pipe wall,

cont.

Q

Q

Q

t

in

t

w

1

t

w

2

t

ext

λ

α

ext

Q

Q

α

in

r

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dr

dt

dL

r

Q

d

2

r

dr

dL

Q

d

dt

2

in

ext

r

r

w

w

r

r

dL

Q

d

r

dr

dL

Q

d

t

t

ext

in

ln

2

2

2

1

2

1

ln

2

w

w

d

D

t

t

dL

Q

d

in

ext

heat transfer through a pipe wall,

cont.

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)

(

)

(

2

1

ext

w

ext

ext

w

in

in

in

t

t

dL

D

t

t

dL

d

Q

d

)

(

)

(

)

(

)

(

2

2

1

1

ext

w

w

w

w

in

ext

in

t

t

t

t

t

t

t

t

dL

D

Q

d

d

D

dL

Q

d

dL

d

Q

d

ext

ext

in

ext

in

in

ln

2

heat infiltration by the pipe surface:

temperature drops composition – infiltration and conduction





ext

ext

in

ext

in

in

D

d

D

d

dL

Q

d

1

ln

2

1

1

heat transfer through a pipe wall,

cont.

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)

(

1

ln

2

1

1

1

ext

in

ext

ext

in

ext

in

in

t

t

dL

D

d

D

d

Q

d













K

m

W

D

d

D

d

k

ext

ext

in

ext

in

in

L

1

ln

2

1

1

1

)

(

ext

in

L

t

t

dL

k

Q

d

a coefficient of heat transfer related to a pipe length:

heat transfer through a pipe wall,

cont.

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







K

m

W

D

d

d

D

d

k

ext

ext

in

in

ext

in

in

in

2

ln

2

1

1

)

(

)

(

)

(

out

in

in

in

out

in

in

in

L

out

in

L

t

t

dS

k

t

t

dL

d

d

k

t

t

dL

k

Q

d

heat transfer through a pipe wall

related to an

internal

surface of a pipe

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







K

m

W

d

D

D

d

D

k

ext

in

ext

ext

in

in

ext

ext

2

1

ln

2

1

)

(

)

(

ext

in

ext

ext

ext

in

ext

ext

t

t

dS

k

t

t

dL

D

k

Q

d

heat transfer through a pipe wall

related to an

external

surface of a pipe

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Assuming that value of the heat transfer coefficient k does not
change along the heat transfer partition (length, area)

or accepting an average value of the k for the whole heat
exchanger,

then taking into account that a difference of the both fluids
temperatures does change along the heat surface

for a flat wall

for a pipe, relating e.g. to the internal surface of the heat exchange:

where

Δt

av

- is an average temperature difference between fluids

in

the heat exchanger.

av

w

w

ext

in

in

in

t

S

k

dL

L

t

L

t

d

k

Q

d

Q

))

(

)

(

(

av

f

f

t

S

k

dS

S

t

S

t

k

Q

d

Q

))

(

)

(

(

2

1

background image

t

11

t

12

t

21

t

22

L

t

22

< t

12

t

t

11

t

21

t

12

)

(

)

(

ln

)

(

)

(

22

12

21

11

22

12

21

11

ln

t

t

t

t

t

t

t

t

t

common-flow heat exchanger

temperatures changes along the heat exchange

surface

background image

contrary-flow heat exchanger

temperatures changes along the heat exchange

surface

L

t

11

t

12

t

21

t

22

t

t

11

t

22

>

t

12

t

21

t

12

< t

22

)

(

)

(

ln

)

(

)

(

21

12

22

11

21

12

22

11

ln

t

t

t

t

t

t

t

t

t

background image

fluids temperature distribution in a heat

exchanger

volume

heat

C

c

m

C

p

After: - Wymiana ciepła, S. Wiśniewski, T.S.
Wiśniewski

fluids temperature distribution

in common-flow heat exchanger

fluids temperature distribution

in contrary-flow heat exchanger

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If a temperature difference between fluids along the
heat surface is a linear function of the both fluids
temperatures then an average difference between
fluids temperatures in a heat exchanger is an
logarithmic temperature difference

The condition for the linear dependence between the
fluids temperatures and the difference between these
temperatures is fulfilled if fluids do not change phases
and their heat volumes are constant (m·c = const.).

an average logarithmic difference of

temperatures in a heat exchanger

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)

(

2

2

2

1

1

1

t

dS

k

Q

d

dt

c

m

Q

d

dt

c

m

Q

d

f

f

L

t

t

11

t

21

t

22

< t

12

t

12

t

1

t

2

Δt=t

1

-

t

2

an average logarithmic difference of

temperatures in a heat exchanger

cont.

heat exchanged
(transferred)
through an
elementary area dS:

background image

t

dS

k

Q

d

av

t

k

S

Q

t

k

dt

c

m

t

k

Q

d

dS

f

1

1

1

outlet

inlet

f

t

k

dt

c

m

S

1

1

1

ale:

c

f1

, k, Δt change along the heat exchanger and so are a

functions of t

1

(and of t

2

)

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

outlet

inlet

f

av

av

t

k

dt

c

t

k

m

t

k

S

Q

)

(

)

(

)

(

1

1

1

outlet

inlet

f

dt

c

m

Q

1

1

1

and also:

so:

outlet

inlet

f

outlet

inlet

f

av

dt

c

t

k

dt

c

t

k

1

1

1

1

)

(

)

(

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

outlet

inlet

f

outlet

inlet

f

av

t

k

dt

c

dt

c

t

k

)

(

)

(

1

1

1

1

outlet

inlet

f

outlet

inlet

f

av

dt

c

t

k

dt

c

t

k

1

1

1

1

)

(

)

(

then:

if c

f

and k are const.:

if:

outlet

inlet

outlet

inlet

outlet

inlet

av

t

dt

t

t

t

dt

dt

t

1

11

12

1

1

an average logarithmic difference of

temperatures in a heat exchanger

cont.

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by analogy:

outlet

inlet

outlet

inlet

outlet

inlet

av

t

dt

t

t

t

dt

dt

t

2

21

22

2

2

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

)

(

)

(

21

2

2

2

1

11

1

1

t

t

c

m

t

t

c

m

f

f

2

2

2

1

1

1

dt

c

m

dt

c

m

f

f

)

(

1

11

2

2

1

1

21

2

t

t

c

m

c

m

t

t

f

f



11

2

2

1

1

21

1

2

2

1

1

2

t

c

m

c

m

t

t

c

m

c

m

t

f

f

f

f

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

b

t

a

t

t

c

m

c

m

t

c

m

c

m

t

f

f

f

f





1

21

11

2

2

1

1

1

2

2

1

1

1

2

1

t

t

t

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

1

2

1

2

11

12

11

12

11

12

11

12

11

12

11

12

1

1

11

12

1

11

12

ln

ln

)

(

)

(

ln

ln

1

t

t

t

t

b

t

a

b

t

a

b

t

a

b

t

a

b

t

a

b

t

a

t

a

t

a

b

t

a

b

t

a

a

t

t

b

at

dt

t

t

t

dt

t

t

t

outlet

inlet

outlet

inlet

av

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

outlet

inlet

outlet

inlet

śr

b

at

dt

t

t

t

dt

t

t

t

1

1

11

12

1

11

12

b

t

a

b

t

a

a

t

t

b

t

a

a

b

t

a

a

t

t

t

av

11

12

11

12

11

12

11

12

ln

1

)

ln(

1

)

ln(

1

1

2

1

2

11

12

11

12

11

12

11

12

ln

ln

)

(

)

(

ln

t

t

t

t

b

t

a

b

t

a

b

t

a

b

t

a

b

t

a

b

t

a

t

a

t

a

t

av

an average logarithmic difference of

temperatures in a heat exchanger

cont.

background image

t

22

t

11

t

12

t

21

)

(

)

(

ln

)

(

)

(

21

12

22

11

21

12

22

11

_

ln_

t

t

t

t

t

t

t

t

t

t

flow

contrary

for

av

ε<1 – a correction related to the heat exchanger
configuration, fluids temperatures drops, temperatures
at the heat exchangers inlet and outlet

cross-kind heat exchanger

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„Shell-tubular” heat exchanger of a

mixed flow structure

background image

isobaric condensing
p

1

= const.  t

1

= const.

t

L

t

2

2

t

21

Δt=t

1

-

t

2

Condenser

background image

As in the case of heat exchange between fluids without a change of
phase, also for an isobaric condensation:

outlet

inlet

outlet

inlet

outlet

inlett

av

t

dt

t

t

t

dt

dt

t

2

21

22

2

2

Δt is linearly related to t

2

(condensing temperature t

1

=

const.):

b

t

a

t

t

t

2

1

2

1

Condenser

background image

1

2

1

2

21

22

21

22

21

22

21

22

21

22

21

22

2

2

21

22

2

21

22

ln

ln

)

(

)

(

ln

ln

1

t

t

t

t

b

t

a

b

t

a

b

t

a

b

t

a

b

t

a

b

t

a

t

a

t

a

b

t

a

b

t

a

a

t

t

b

at

dt

t

t

t

dt

t

t

t

outlet

inlet

outlet

inlet

av

Condenser

background image

isobaric condensing
p = const.  t = const.

t

L

steam cooling

condensate
cooling

Δt

min

- „pinch

point”

steam cooling, steam condensing,

condensate cooling

background image

mass balances for a diaphragm-kind heat exchange:

0

22

22

21

21

12

12

11

11

22

22

21

21

12

12

11

11

i

m

i

m

i

m

i

m

Q

i

m

i

m

Q

i

m

i

m

energy balance for a diaphragm-kind heat exchange:

0

0

22

21

12

11

m

m

m

m

or:

balances for a diaphragm-kind heat exchanger

m

12

m

11

m

21

m

22

background image

)

(

)

(

21

22

2

21

12

11

1

11

t

t

c

m

t

t

c

m

Q

p

p

Energy balance for a diaphragm-kind heat exchange and one-
phase flows with c

p

=const.:

balances for a diaphragm-kind heat exchange

L

t

t

11

t

21

t

22

< t

12

t

12

t

1

t

2

Δt=t

1

-

t

2

)

(

2

2

2

1

1

1

t

dS

k

Q

d

dt

c

m

Q

d

dt

c

m

Q

d

w

w

background image

examples of a diaphragm-kind heat

exchangers

background image

examples of a diaphragm-kind heat

exchangers

background image

approximates values of the heat

infiltration coefficients at recuperates

heat inflitration coefficient [W/m

2

K]

heating or cooling

air

160

superheated steam

20120

oils

601800

liquid water

23012000

water boiling

60052000

film condensation of water

steam

46001800

0

drop-kind condensation of water

steam

46000140

000

condensation of organic

compounds steams

6002300

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marginal values of the heat transfer

coefficients k [W/m2K]

gas – gas

30

gas – liquid water

60

light oil – liquid water

350

liquid water – liquid water

1200

condensing water steam – liquid water 3000

condensing water steam – oils

350

condensing water steam – boiling oils

600

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liquid
(1)

heating steam
(2)

gases - vapors (4)

no-diaphragm kind
heat exchanger

thermal deairater

degasified
water (3)

no-diaphragm kind heat exchanger

– deairater (dearating heater)

background image

)

(

"

)

(

'

0

3

4

3

3

4

1

p

i

i

p

i

i

m

m

0

4

3

2

1

m

m

m

m

0

4

4

3

3

2

2

1

1

i

m

i

m

i

m

i

m

mass balance of a deairater

energy balance of a deairater

additional relations – approximated relation between mass of
vapors and supplying water

no-diaphragm kind heat exchanger

– deairater (dearating heater) cont.

background image

Exercise 1

• A fluid „2” is heated from T’

2

=293 K

to T”

2

=343 K. Heating agent „1”

cools down from T’

1

=453 K to

T”

1

=353 K. Compare heat exchange

area for common-flow and contrary-
flow heat exchangers of 1 MW
capacity, if heat transfer coefficient
is k=100 W/(m2K) in the both cases.

background image

Exercise 2

• Two fluids (1) & (2) of temperatures t

1

& t

2

(t

1

>t

2

) are

separated with a partition and exchange a heat. Heat

infiltration coefficient from the fluid (1) to a surface of

the partition α

1

is 300 W/m

2

K, and heat infiltration

coefficient from a surface of the partition to the fluid

(2) α

2

is 900 W/m

2

K. The partition is made of a

homogenous material of heat conduction factor λ

equal to 45 W/mK. Estimate a heat transfer coefficient

k if the partition is:

1. a flat plate 4 mm thick,
2. a pipe ø211x4,
3. a pipe ø32x4,

Formulate conclusions basing on the results.

background image

Exercise 3

• Estimate an area of heat exchanger

water – water, where one fluid is
cooled down form 80°C to 40°C. An
cooling agent is a water supplied
with temperature 30°C. Accept
additional assumptions, chose a
proper kind of a heat exchanger, and
estimate area of its surface.

background image

Exercise 4

• 100 kg/s of a wet steam of an enthalpy 2776

kJ/kg is condensing. Saturated condensate
outflows from the heat exchanger with an
enthalpy 763 kJ/kg. Saturation temperature is
180°C (saturation pressure 10 bar). An cooling
agent is a water supplied with temperature
90°C.

• Accept necessary additional assumptions (e.g.

heat exchanger configuration, k value, …) and
calculate area of heat exchange surface.


Document Outline


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