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Research progress on cryogenic mixed-gases Joule-Thomson refrigeration in TIPC of CAS Maoqiong GONG Technical Institute of Physics and Chemistry (TIPC) Chinese Academy of Sciences (CAS) Email: [email protected] Tel/Fax: 86-10-82543728
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Research progress on cryogenic

mixed-gases Joule-Thomson refrigeration

in TIPC of CAS

Maoqiong GONG

Technical Institute of Physics and Chemistry (TIPC)

Chinese Academy of Sciences (CAS)

Email: [email protected]

Tel/Fax: 86-10-82543728

Contents

1. Introduction

2. Thermophysical properties and components

selection of mixed-refrigerants

3. Thermodynamic features of the recuperative heat

exchangers

4. Thermodynamic optimization of various cycle

configurations

5. Composition shift

6. Performance and application of cryogenic MJTR

1. Introduction

230

80

Refrigeration requirements in different temperature ranges

biomaterials Medicine Energy

Aerospace

Domestic refrigerators Air conditioners Heat pumps etc.

The mixed-gases Joule-Thomson refrigerator (MJTR) can satisfy such requirements

The MJTR play the dominant role in this deep cooling temperatures ranging from 80 to 230 K

Near ambient temperature range

Deep cooling temperature range

370

Advantages of MJTR

Off-the-shelf components

High reliability.

Low cost.

Easy to be built in large scale.

The mixed-gases Joule–Thomson refrigerator

230

80

Near ambient temperature range

Deep cooling temperature range

370

Technical challenges & Scientific problems

Mixture Components selection and optimal composition.

Cycle configurations with high efficiency and reliability.

Mixtures properties in large temperature span.

Working mechanism of low-temperature mixed-gases Joule-Thomson refrigeration.

Accurate component design and manufacture

The mixed-gases Joule–Thomson refrigeration

230

80

Near ambient temperature range

Deep cooling temperature range

370

2. Thermophysical properties and components selection of

mixed-refrigerants

2.1 Phase equilibria

Fluid equilibrium is the fundamental for other thermal physical properties.

Basic parameters for other properties prediction

Determining the lowest evaporation temperature of the MJTR ……

0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0140

150

160

170

180

190

T/K

x1, y

1

liquid-correlated

vapor-correlated

liquid-predicted

vapor-predicted

0.1 MPaInfluence of the presence of experimental data on the prediction results R14+R170 system

Experiments is most important and final method for phase equilibria study

Several facilities were built to study the mixtures VL(L)E behaviors used MJTRs

cryogenic apparatus T: 80~300 K

p: 0.1~10 MPa

Temperature uncertainty : ±10mK

Pressure uncertainty: ±2kPa

Composition uncertainty : ±0.003

2.1 Phase equilibria First apparatus for low-temperature

CH4+CF4 system C2H6+CF4 system

0.0 0.2 0.4 0.6 0.8 1.0

0.0

0.2

0.4

0.6

0.8

1.0 0.0

0.2

0.4

0.6

0.8

1.0

CH4

CF4

C2H

6

L+V

0.1 MPa

VLE of ternary system

(CH4+CF4+C2H6 system) 2.1 Phase equilibria

0.0 0.2 0.4 0.6 0.8 1.00.0

0.2

0.4

0.6

0.8

1.00.0

0.2

0.4

0.6

0.8

1.0

L+V

Bubble point

Dew point

R170 R23

R116

0.0 0.2 0.4 0.6 0.8 1.00.0

0.2

0.4

0.6

0.8

1.00.0

0.2

0.4

0.6

0.8

1.0

L+V

Bubble point

Dew point

R170 R23

R116

L+V

R170+R23 system(212.84 K) R170+R116 system(252.80 K)

(R170+R23+R116 system)

R170+R23+R116 Ternary system

2.1 Phase equilibria

The second VLLE apparatus T: 200~310 K

p: 0.1~5 MPa

Temperature uncertainty : ±4mK

Pressure uncertainty : ±0.2~0.5kPa

Composition uncertainty : ±0.002

2.1 Phase equilibria Second apparatus for VLLE

Journal Cover Journal of Chemical & Engineering Data,

2012, 57:541-544

Experimental data of the vapour-liquid-liquid

equilibria of {R134+R600a} system

(VLLE)

Clear single

liquid phase

Clear two

liquid phases

Vapor-liquid-liquid equilibria of R134+R600a system

Phase

separation

Critical

opalescence

0.20.3

0.40.5

0.60.7

0.80.9

0.070

0.075

0.080

0.085

0.090

235236

237238

239240

241242

p/M

Pa

T/Kx1

2.1 Phase equilibria

Institutes Experiment

method

Temperture

uncertainty

/mK

Pressure

uncertainty

/kPa

Mole

Composition

uncertainty

Seoul National University Vapor cycle 20 1 0.003

Ecole Nationale Supérieure des

Mines de Paris CENERG/TEP, France

Static method 10 0.3 0.02

Korea Institute of Science and

Technology (KIST), South Korea

Vapor and liquid

double cycle

10 1 0.002

Institute of Building Technologies, Italy Vapor cycle 20 1 0.003

Ajou University, Korea Vapor cycle 20 2 0.003

Instituto Politecnico Nacional, Mexico Static method 30 0.04% 0.01

National Metrology Institute of Japan,

National Institute of Advanced

Industrial Science and Technology,

Japan

Vapor and liquid

double cycle

3 0.62 0.001

TIPC,CAS

Three facilities,

temperature: 80~400 K

pressure: 0.1-10 MPa

Vapor cycle

quasi-static

Vapor cycle

4

4

10

0.3

0.26

2

0.003

0.002

0.002

Comparison of vapor liquid equilibria experimental facilities

Negative azeotropic

1 1 1 2

V L

1 1

( ) (d d )d0

d ( ) d

y xp

x v v x

2

2

1

d0

d

p

x

2

2

1

d0

d

p

x

Azeotropy prediction model of the

equilibria pressure extremum.

Positive azeotropic

(Theoretical prediction model)

Combined with experimental data, mixing principles for PR

thermodynamic model equations was improved, binary

interaction coefficients were also obtained.

Predictions of the binary azeotropic characteristics of several

systems were conducted.

0.0 0.2 0.4 0.6 0.8 1.0

0.2

0.3

0.4

0.5

0.6

p/M

Pa

x1,y

1

2.1 Phase equilibria

Summary on vapor-liquid equilibria work

Some VLE data of mixtures was were first measured:

HCs + R14/R23/R116 and other systems;

Some of the theoretical predictions and correlation models were

established and improved;

There are still many problems:

1) Gas-liquid, liquid-solid equilibria of oil with refrigerants

2) Vapor-liquid-liquid equilibria;

3) High-precision theoretical prediction model.

2.2 Throttling effect

0 10 20 30 40 50 600

100

200

300

400

500

600

700

T /

K

p /MPa

K

L

N

JT

>0

JT

<0

PN

Basic conceptions of throttling effects

Throttling device

High pressure, high

temperature gas Low pressure, low

temperature gas

Ts Tr

Some conceptions

50 100 150 200 250 300 350

Temperature (K)

-5

0

5

10

15

20

25

Isoth

erm

al th

rottle

effect (k

J/m

ol)

N2

CH4

C2H6

C3H8

iC4H10iC5H12

1 2 3 4 5

Pl=0.1MPa

1. PH=1.0MPa, 2. PH=2.0MPa, 3. PH=3.0MPa, 4. PH=4.0MPa, 5. PH=5.0MPa

The higher pressure

before throttling, the

wider temperature

range would be

covered with effective

throttling effect.

2.2 Throttling effect

Influence of pressures and temperatures on pure substance throttling effects

Isothermal J-T effect

50

100

150

200

250

T(K)

0

0.5

1

1.5

2

P(MPa)

0

1,000

2,000

3,000

4,000

5,000

6,000

7,000

0

1,000

2,000

3,000

4,000

5,000

6,000

7,000

50

100

150

200

250

T(K)

0

0.5

1

1.5

2

P(MPa)

0

10

20

30

40

50

60

70

0

10

20

30

40

50

60

70

50 100 150 200 250 300

T(K)

-10

0

10

20

30

40

50

60

70

80

inte

gra

ted

JT

eff

ec

t (K

)

mix.1

mix.2

mix.3

50 100 150 200 250 300

T(K)

-2,000

0

2,000

4,000

6,000

8,000

10,000

12,000

14,000

iso

the

rma

l J

T e

ffe

ct(

J/m

ol)

mix.1

mix.2

mix.3

A method for optimizing mixture composition

Throttling effect of mixed refrigerants under

various pressures and temperatures

2.2 Throttling effect

The minimum isothermal throttling effect of the

optimized mixture in the whole temperature range is

larger than that of any pure component, which is the

reason that mixed refrigerants could increase the

thermal efficiency of the MJTR cycle.

2.2 Throttling effect

90 120 150 180 210 240 270 3000

5

10

15

20

25 iC5H

12

iC4H

10

C3H

8

C2H

6

CF4

CH4

N2

pH=2.0 MPa

pL=0.1 MPa

h

T (

kJ/m

ol)

T (K)

mixture

A)

90 120 150 180 210 240 270 300 330 3600

10

20

30

40

50

60

70

80

90

100

N2

CH4

CF4

C2H

6

C3H

8

iC4H

10

iC5H

12

pH=2.0 MPa

pL=0.1 MPa

T

h (

K)

T (K)

mixture

B)

2.3 Components selection

Selecting component to make their effective throttle effect

temperature range cover each other (relaying) in

temperatures ranging from ambient to the target.

Physical and chemical stability, impact on the environment

(ODP, GWP), as well as economic factor, etc.

No. Components Boiling points(K) Temperature zone

1 He, Ne 4.2, 27.0 Low temperature zone

2 N2, Ar 77.4, 87.3 Normal temperature zone

3 CH4 111.7 Low-medium temperature zone

4 CF4 145.2 Low-medium temperature zone

5 C2H4, C2H6 169.4, 184.6 Medium temperature zone

6 C3H8, C3H6, iC4H10 231.04, 225.53, 261.4 Medium-high temperature zone

7 iC5H12 300.98 High temperature zone

Components selection for liquid nitrogen temperature refrigeration

3. Behaviors of the recuperative heat exchangers and two-phase

heat transfer study

Vapor Compression

Recuperator

Evaporator

After

cooler

Recuperative heat exchanger is a critical component of mixed-refrigerant J-T refrigerator.

Recuperative heat exchanger is the biggest difference between mixed-gases J-T refrigeration cycle and the vapor compression cycle in terms of hardware.

3.1 Experimental research on the operation features of tube-in-tube recuperative heat exchanger

3.1 Experimental research on the operation features of tube-in-tube recuperative heat exchanger

0 1 2 3 4 5150

175

200

225

250

275

300

A)

B)

TL

_A

TH

_A

TL

_B

TH

_B

T (

K)

lx (m)

1 2 3 4 5 6 7 8 9 100

300

600

900

1200

n

HT

C (

W/m

2K

) /

HE

AT

(W

)

HTC

HEAT

0

2

4

6

8

10

12

14

A)

AL

MT

D (

K)

ALMTD

1 2 3 4 5 6 7 8 9 100

300

600

900

1200

1500

B)

n

HT

C (

W/m

2K

) / H

EA

T(W

) HTC

HEAT

0

5

10

15

20

ALM

TD

(K

)

ALMTD

Built a special HX with 10

sections to measure:

temperature and

pressure distribution

Overall heat transfer

coefficients

The locations of pinch points. The distribution of heat load versus the temperature.

0 1 2 3 4 550

100

150

200

250

300

A3

pH

pL

T (

K)

lx (m)

0 1 2 3 4 5100

150

200

250

300

A4

pH

pL

T (

K)

lx (m)

1 2 3 4 5 6 7 8 9 100

60

120

180

240

300

A3

n

HT

C (

W/m

2K

) /

Q (

W) HTC

Q

0.0

3.2

6.4

9.6

12.8

16.0

AL

MT

D (

K)

ALMTD

1 2 3 4 5 6 7 8 9 100

140

280

420

560

700

A4

nH

TC

(W

/m2K

) /

Q (

W)

HTC

Q0

3

6

9

12

15

18

AL

MT

D (

K)

ALMTD

The mixture composition determines:

3.1 Experimental research on the operation features of tube-in-tube recuperative heat exchanger

Complicated heat and mass transfer process in the recuperator.

Flow-boiling

Flow-condensation

3.2 Researches on two-phase heat transfer of mixed-refrigerants

0 2 4 6 8 100

2

4

6

8

10

Palen&Small [22]

Jungnickel et. al [23]

Thomes&Shakir [24]

Fujita&Tsutsui [25]

Inoue et. al [26]

Calc

ula

ted r

esults (

kW

m-2

K-1)

Measured data(kW m-2K-1)

-25%

+25%

3.2 Researches on two-phase heat transfer Pool-boiling

Refrigerant tank

Keithley

2700

GC

1

2

5

4

3

Vacuum

pump

Cold lightHigh speed

camera

DC regulator

Compressor

DC regulator

scale

Computer

Pool-boiling experiments.

Covering 80~300 K.

Components of natural gas,

pure substances and mixtures.

Cooling

loop

Δp

DC Regulator 1

ΔppT

T

DC Regulator 2

Preheater

Vacume pump

T T T

pCharging port

Heat

exchanger

Liquid

reservoir

Throttling

valve

C

Maganetic

gear pump

Sight glass

Heat transfer test section

Adiabatic pressure drop test section

Vacume chamber

Sight glass

SENSORS

C:coriolis mass flow meter

T: resistances thermometer

p: absolute pressure sensor

Δp: differential pressure sensor

Throttling

valve

Researches on two-phase flow boiling heat transfer and flow characteristics.

Covering 100~300 K.

Components of natural gas,

pure substances and mixtures.

3.2 Researches on two-phase heat transfer Flow-boiling

0.875 0.714 0.230Re ( ) 0.92 0.45Ltp

kh BoK Co

D

New correlation of flow boiling

heat transfer coefficients:

0 3 6 9 120

3

6

9

12

R290

R152a

R170

Pre

dic

ted h (

kW

.m-2

.K-1)

Experimental h (kW.m-2.K

-1)

+20%

-20%

In the literature (Cryogenics

57,2013,18-25) on LNG heat

transfer, our correlation was proven

the best one with the smallest

deviation.

…the best correlation…

3.2 Researches on two-phase heat transfer Flow-boiling

Δp

ΔppT

T T T T

p

C

T T

p

TT

Vacume pump

Vacume chamber

Cooling

loop 2

Cooling

loop 1Heat

exchanger

Magnetic-

driven pump

Throttling

valve

Reservoir

DC Regulator

Preheater Sight glass Sight glass

Heat transfer test section

Adiabatic pressure drop section

SENSORS

C:Coriolis mass flow meter T: resistances thermometer

p: absolute pressure sensor Δp: differential pressure sensor

3.2 Researches on two-phase heat transfer Flow-condensation

Flow condensation heat transfer and flow characteristics.

Covering 100~300 K.

Components of natural gas,

pure substances and mixtures.

0.0 0.2 0.4 0.6 0.8 1.00

1000

2000

3000

4000

5000

6000

7000

8000

p=1.01 MPa G=202 kg (m2s)

-1 q

avg=64.4 kW m

-2

p=1.56 MPa G=201 kg (m2s)

-1 q

avg=76.4 kW m

-2

p=2.06 MPa G=201 kg (m2s)

-1 q

avg=81.9 kW m

-2

p=2.56 MPa G=201 kg (m2s)

-1 q

avg=85.1 kW m

-2

h (

W (

m2K

)-1)

x

0.0 0.2 0.4 0.6 0.8 1.050

100

150

200

250

300

350

Plug Transition

Slug Annular

G kg m

-2 s

-1

x

R170

4. Thermodynamic optimization of various cycle configurations

Optimization objective

function:

Maximize

thermodynamic

efficiency

Optimization parameters:

Mixture

components

Mixture

composition

High and low

pressures of cycle

The single-stage mixed-gases Joule-Thomson cycle

4.1 Thermodynamic optimization: single-stage cycle

0 5 10 15 20100

150

200

250

300

PL

PH

T (

K)

QHX

(kJ/mol)

4.1 Thermodynamic optimization: single-stage cycle

(1) Compression, throttling and evaporation processes Higher high-boiling component fraction leads to a smaller compressibility factor and a lower compressor inlet temperature, reducing the compression power consumption. Lower temperature before throttling results in smaller exergy loss

(2)Recuperative process

When the fraction of one component gets larger, the intrinsic temperature difference in the relevant temperature zone would increase, as well as the exergy loss.

0 5 10 15 20100

150

200

250

300

PL

PH

T (

K)

QHX

(kJ/mol)

0 5 10 15 20100

150

200

250

300

PL

PH

T (

K)

QHX

(kJ/mol)

More high-boiling components Optimized Composition More low-boiling and middle-

boiling components

0 3 6 9 12 15 18100

150

200

250

300

PL

PH

T (

K)

QHX

(kJ/mol)

Optimization results: The single-stage mixed-gases J-T cycle could achieve a theoretical cycle efficiency of 63% (relative Carnot efficient).

4.1 Thermodynamic optimization: single-stage cycle

0 5 10 15 20100

150

200

250

300

PL

PH

T (

K)

QHX

(kJ/mol)

iC4 iC5

Various configurations of mixed refrigerant J-T cycle

4.2 The influence of cycle configuration

DEACDEHX2DEJT1DBLEND

DEHX3DEJT2DEEVCEF

One phase separator Relative Carnot efficiency of 62.5%

DEAC

DEJT1

DEJT2

DEHX1

DEHX2

DEHX3

DBLEND1

DBLEND

DEJT3

DEEV

CEF

Two phase separators Relative Carnot efficiency of 61.5%

4.2 The influence of cycle configuration

DEAC

DEHX

DEJT

DEEV

CEF

63%

10%

9.5%

8.5%

9%

No phase separator Relative Carnot efficiency of 63%

Conclusions of thermodynamic analysis

Different cycle configurations could reach close performances under each optimal conditions, while the single-stage cycle with the most simple structure could achieve the best performance in the thermodynamic point of view .

Cycle configuration is the external factor while mixture is internal factor. Effective refrigeration could be achieved by matching the external and internal factors.

5. Composition shift

5.1 Composition shift characteristics of mixed refrigerants

0 10 20 30 40 50 60 70 80 90 100-100

-50

0

50

100

150

200

250

R

N2

CH4

C2H

6

C3H

8

iC4H

10

iC5H

12

T=300 K

p=101.3 kPa

Roil

, %

Rj,

%

0

25

50

75

100

R,

%

Composition shift characteristics of mixtures.

Circulation concentration changes from the original charged data in MJTRs

Two factors: liquid holdup and solution with oil

5.2 Composition shift caused by liquid holdup

1 2 3 4 5 6 7 8-100

-50

0

50

100

150

200

250

300

N2

CH4

C2H6

C3H8

iC4H10

Sampling Point

R /

%

120

150

180

210

240

270

300

T /

K

140 160 180 200 220-70

-60

-50

-40

-30

-20

-10

0

10

20

30

40

50

R /

%T /K

N2

CH4

C2H6

C3H8

iC4H10

Oil-free compressor liquid holdup

5.3 Composition shift caused by solubility in lubricants

21

11

nn

nx

PTv

v

PTv

VV

PTv

V

PTv

V

PTv

V

n

v

gasabs

v

cellcell

pump

v

pump

endend

v

begbeg

v

,1

,,,,

1

,

1

,2

11

bottle

1

bottle

1

Solubility:

Gas-liquid phase equilibria

Composition shift caused by the solubility in lubricants.

5.4 Composition shift characteristics

Problems caused by composition shift

Decreasing the concentration of high-boiling components

Reduce cycle performance.

Measures to reduce or eliminate the influences 1) The deep oil separation in compressor unit 2) Increasing volume ratio for warm to cold sections 3) Increasing charging quantity

6. Performance and application of cryogenic MJTR

6.1 Series cryo-freezers

Ambient

temperature

-40℃

-80℃

-150℃

-196℃ (LN2)

-120℃

Cryo-freezers for biomaterial long-term preservation Six temperature zone series:

-86℃ -105 ℃ -132 ℃ -154 ℃ -164 ℃ -186℃

Industrial production for almost 15 years!

6.1 Series cryo-freezers

Institutes Japan

SANYO

US FORMA、

REVCO This Project

Refrigeration cycle

two-stage cascade

two-stage cascade

Mixed-gases recuperative

cycle

Compressor lower back pressure

compressor

lower back pressure

compressor

Single-stage oil-lubricated

hermetic compressor

Refrigerant R407/

R508B+R290 R404a /

R508B+R290

Multivariate mixed

refrigerant Chamber volume/L

320 328 328

Compressor displacement/cc

47.1 (20.7+26.4)

51.2 (25.6+25.6)

34.8

Rated input power/kW

1.36 1.47 1.15

-80℃ energy consumption /kWh/Day/L

0.084 0.086 0.054

Ultimate temperature/℃

-85 -86 -92

Cooling time/hr > 5 > 5 <3.5

Performance comparison -86℃ cryogenic preservation chambers

Reducing energy consumption by ~36%.

Reducing cooling time by ~30%

Ultimate temperature lower more than 6K

25% smaller compressor displacement 16% smaller installed power (lower cost)

6.1 Series cryo-freezers

Requirements Recovery of remote and scatted natural gas resources, not suitable for pipeline and fixed LNG plant

Measures: 1) Efficient and compact cold box structure. 2) Compact air-cooled compressor unit. 3) Manufacture mini-liquefiers with high flexibility.

Results and effects: 5000 ~100,000Nm3/d moveable trailer-mounted liquefiers were developed.

The factory-assembled production mode of the liquefiers greatly reduced the construction period

6.2 Trailer-mounted natural gas / coalbed gas liquefier

No. Institutions Liquefaction technology

Capacity/Feed gas pressure

Efficiency

1

Gas Technology Institute (GTI), US

Mixed-refrigerant liquefaction process, skid-mounted, water-cooled

2000 Nm3/d 0.1~0.7MPa

25% consumed, 75% liquefied

2 Harbin Cryo, Jilin Songyuan

Mixed-refrigerant liquefaction process (centralized), water-cooled

70000 Nm3/d ≥0.3MPa

14.3% consumed, 85.7% liquefied, Calculated by the shaft power of all devices

3 Hamworthy, UK

Nitrogen expander process (peak load regulating)

100000 Nm3/d N/A

16% consumed, 84% liquefied

4 SINTEF, Norway

Mixed-refrigerant liquefaction process, seawater-cooled

30000 Nm3/d 1.82 MPa

16.7% consumed, 83.3% liquefied Estimated on literatures

5 TIPC, CAS

Mixed-refrigerant liquefaction process, trailer-mounted, full air-cooled

10000 Nm3/d 0.7~1.3MPa

15.3% consumed, 84.7% liquefied, Measured power consumption of all devices

The comparison of liquefaction performance with other devices

6.3 Trailer-mounted natural gas / coalbed gas liquefier

Summary of the researches on cryogenic mixed-gases Joule-Thomson refrigeration in TIPC

Root

Thermophysical properties

Heat transfer Two-phase flow

Trunk

Cycle configuration

Mixture Composition

Control and integrate technology

Tree crown and fruit

Natural gas liquefiers

Cryo-freezers High and low temperature experiment chamber

Technical Institute of Physics and Chemistry

Chinese Academy of Sciences

Email: [email protected]

Maoqiong Gong, Prof. Dr.

Thank you


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