experimental comparison of single and multistage air

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RAMBABU. 1Associate professor-Mechanical Engineering Department ... Compressors are widely used for many engineering ..... J.K Gupta and R.S.Khurmi. 80.
AIJRRLJSM VOLUME 1, ISSUE 6 (2016, JUNE) (ISSN-2455-6300) ONLINE ANVESHANA’S INTERNATIONAL JOURNAL OF RESEARCH IN ENGINEERING AND APPLIED SCIENCES

EXPERIMENTAL COMPARISON OF SINGLE AND MULTISTAGE AIR COMPRESSOR EFFICIENCIES UNDER THE SAME RECEIVER TANK PRESSURE 1

P.V.RAMANA & 2D.RAMBABU

1

Associate professor-Mechanical Engineering Department 2 Asst. professor-Mechanical Engineering Department CVR College of Engineering - Hyderabad (T.S)-India

ABSTRACT Compressors are widely used for many engineering applications in day to day life. Compressors are classified based on design as reciprocating and rotary compressors, Reciprocating compressors are single acting ,double acting ,air cooled ,water cooled and single stage ,multistage ,depends on application of usage. It is clear by theory as given by author’s multistage compressors having advantage over single stage compressors but practically not aware to what extent the variations in efficiencies are taking place and exact experimental figures in that area not focused with clarity. So here focus is given to conduct experiment on both single stage and multi stage compressors at the different receiver tank pressure. Obtained readings are calculated for the same receiver tank pressure and then comparing the results for both the compressors. To know the variations in efficiencies of both compressors results are tabulated and compared to find out the efficiencies for better understanding the subject. Keywords: single stage compressor, multistage compressor, LP cylinder, HP cylinder, volumetric efficiency, isothermal efficiency.

cylinder say L.P cylinder and allow this pressurized air to another cylinder say Intermediate cylinder (IP) and develop Higher pressure higher than the LP cylinder and allow this pressurized air in another cylinder say HP cylinder and develop more pressure then intermediate cylinder finally highly developed pressurized air is delivered to the end user applications. This is possible by going for multi stage cylinder compressor. This paper focused on conducting the experiment on compressors to find what differences made when using single and multistage compressor in efficiencies and comparing its experimental results for giving the conclusions for the usage. 2.0 EXPERIMENTAL SET UP SINGLE STAGE COMPRESSOR

OF

The details of the experimental setup of single stage reciprocating Air compressor is as follows

1.0 INTRODUCTION Reciprocating air compressors are widely used to get high discharge pressure. To get high discharge pressure single stage compressor has to work against high compression ratio in terms of pressure so to withstand high compression ratio body of compressor also be made robust in construction . It will add more weight to compressor and also leads many mechanical problems because it is working for the development of high pressure in single cylinder and also it is not suitable because of this reasons when to go for developing high delivery pressure for industrial applications. So alternative is increasing the delivery pressure in number of cylinders step by step and reducing the weight of the compressor. first developing pressure in one cylinder of

Fig1: single compressor

stage

reciprocating

Air

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Specifications of the compressor: Make Type Stage Cylinder Bore Stroke length Motor rating Motor speed Compressor speed Electric supply HZ Type of starter Belt size Type of lubrication Type of cooling Type of fan

: ELGI : Reciprocating Type : single stage : single cylinder : 60 mm : 60 mm : 2 HP : 1420 RPM : 930 RPM : 415V/380V, 3ph, 50

Rec eiv er Tan k Pre ssur e (bar s)

Suc tio n Pre ssu re P1( bar s)

Disc harg e pres sure P2(b

Suctio n Temp eratur e T1 0 C

ars)

3.1 Sample calculations for Reading -1 at 2 bar pressure Sample calculations for Reading -1 Volume of air sucked in to the cylinder Va =Cd x Ao x

: DOl : B40 : splash : Air cooled : forced draught

Where H =

Disc harge Tem perat ure T2 0 C

S pe ed R P M

Man omet er Read ing(h )mm

x 3600 x

= 16.825 meters

Ti me per 10 Re vol uti on ssec

2

3

2

4

6

1

1

1

3.8

6.4

8.4

24

24

24

109

125

136

8 7 6. 0 8 7 2. 2 8 6 9. 3

20

6.7 8

x

Theoretical volume of air Vth = d2xLxNx60

M3/hr

Vth = x0.062 x0.06 x876x60= 8.9165 M3/hr Volumetric efficiency

ηvol

=

ηvol

=

x 100 x 100 = 80.3%

Compression ratio Rp = 1

M3/hr

Va =0.62 x 1.767 x10-4 x 3600 = 7.1656 M3/hr

3.0 SINGLE STAGE COMPRESSOR Table1: table of Readings of single stage compressor as follows S . N O

Ta = Ambient Temperature of air P1 = suction pressure of air P2 = discharge (cylinder outlet) pressure

=

= 3.8

Piso = max RaxT1 x ln(Rp) Where ma = Va x

15

6.5

=density of air ma = 7.1656 x 1.1887 =8.5117 M3/hr

14

6.0

Piso = max RaxT1 x ln(Rp) Piso =

x 0.287xT1 (273+24)x ln(3.8)

=0.269 KW T1 = suction Temperature of air entering in to the cylinder T2 = discharge Temperature of air leaving the compressor

As per the relation (temperature, pressure and volume) for polytrophic process

=

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ln(

) = =

Theoretical volume of air

x ln(3.8)

Vth = d2xLxNx60

= 0.1885

M3/hr

Vth = 8.877 M3/hr I.P = I.P

x

max RaxT1

=

1]

x

x

Volumetric efficiency ηvol = x 100

0.287x297

ηvol

1] =0.302 KW

= 70.46%

Power input to Motor (Pm )

Compression ratio Rp =

Pm =

Piso = max RaxT1 x ln(Rp)

Where 3200 = Energy meter constant Pm =

Where ma = Va x

= 1.659 KW

=density of air

Power input to compressor Pc = Pm x 0.8 Pc = 1.659 x 0.8 = 1.327 Kw

Mechanical efficiency

= =

x 100 x 100 =

ma = 7.4365

M3/hr

Piso = max RaxT1 x ln(Rp) Piso =0.326 KW As per the relation (temperature, pressure and

22.75 %

Overall efficiency

= 6.4

=

x 100 =

x 100 =

volume) for polytrophic process ln(

) =

=

x ln(6.4)

20.27 % = 0.15768 Isothermal efficiency

= =

x 100 x 100 = 89

%

I.P =

x

max RaxT1

1]

I.P =0.3796 KW

3.2 Similarly Sample calculations for Reading -2 at 4 bar pressure Volume of air sucked in to the cylinder Va =Cd x Ao x

x 3600

M3/hr

Power input to Motor (Pm ) Pm = Where 3200 = Energy meter constant

Where H = 12.618 meters

Pm = 1.7307 KW

Va = 6.256 M3/hr

Power input to compressor Pc = Pm x 0.8

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Pc = 1.7307 x 0.8 = 1.384 Kw

Piso =0.359 KW As per the relation (temperature, pressure and

Mechanical efficiency Overall efficiency

=

= x 100 = 27.41 % x 100 = 23.5 %

=

Isothermal efficiency

volume) for polytrophic process ln(

) =

x ln(8.4)

= 0.1503

x 100

I.P =

= 85.8%

=

x

max RaxT1

1]

I.P =0.423 KW

3.3 Similarly Sample calculations for Reading -3 at 6 bar pressure

Power input to Motor (Pm )

Volume of air sucked in to the cylinder

Pm =

Va =Cd x Ao x

x 3600

M3/hr

Where 3200 = Energy meter constant

Where H = 11.77 meters

Pm = 1.875 KW

Va = 5.995 M3/hr

Power input to compressor Pc = Pm x 0.8

Theoretical volume of air Vth = d2xLxNx60

Pc = 1.875 x 0.8 = 1.5 Kw

M3/hr

Mechanical efficiency

Vth = 8.877 M3/hr

=

= 28.2 %

Volumetric efficiency

ηvol

=

ηvol

= 67.52 %

Overall efficiency

x 100

Compression ratio Rp =

x 100

=

x 100 = 23.9 %

= 8.4

Isothermal efficiency

=

x 100

= 84.8%

Piso = max RaxT1 x ln(Rp) Where ma = Va x =density of air

Ma = 7.126 M3/hr Piso = max RaxT1 x ln(Rp) ANVESHANA’S INTERNATIONAL JOURNAL OF RESEARCH IN ENGINEERING AND APPLIED SCIENCES

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3.4 Comparisons table of values for single stage compressor Table2: table of results B ηv a ol r 2 80 .3 4

6

70 .4 6 67 .5 2

Pis

IP

Pc

o

ηm

ηo

ηi

ech

vera

so

T 2

8 9. 0 8 5. 8 8 4. 8

1 0 9 1 2 5 1 3 6

ll

0. 26 9 0. 32 6 0. 35 9

0.3 02 0.3 79 6 0.4 23

1. 32 7 1. 38 4 1. 5

22 .7 5 27 .4 1 28 .2

20 .2 7 23 .5 23 .9

R P M 87 6 87 2. 2 86 9. 3

Comparison shows as pressure is increasing volumetric efficiency and isothermal efficiency is decreasing but isothermal power increases and also other efficiencies like mechanical, overall efficiencies are increases with increase of the pressure 4.0 EXPERIMENTAL SET UP MULTISTAGE COMPRESSOR

Stroke length Motor rating Motor speed Compressor speed Electric supply HZ Type of starter Belt size Type of lubrication Type of cooling Type of fan

Table3: Table of Readings of multistage compressor as follows Ta P P P nk 1 2 3 Pr ess ur e 2

4

6

Specifications of the compressor: Make Model Type Stage Cylinder LP cylinder bore HP cylinder bore

: ELGI : TS 03120 : Reciprocating Type : two stages : two cylinders : 70 mm : 50 mm

: DOl : A68 : splash : Air cooled : forced draught

5.0 MULTISTAGE COMPRESSOR

OF

Fig2: multistage compressor test rig.

: 85mm : 3 HP : 1420 RPM : 930 RPM : 415V/380V, 3ph, 50

1 0 . 9 5 1 1 . 0 5 1 1 . 1

1 . 9 4 . 4 5 6 . 4

M a n o m et er 2 0 0

Time RPM per 5 revol ution s

T T 1 2

T T 3 4

42.75 928

2 1 8 0 0

8 8 6 8

1 9 3

36.97 923

2 1 9 1 4

9 1 6 3 1

1 8 9

34.59 917

2 1 9 1 4

9 1 8 5 7

T1 =Temperature of air entering L.P cylinder T2 =Temperature of air leaving L.P cylinder T3 =Temperature of air after intercooler and entering H.P cylinder T4 = temperature air leaving HP cylinder Ta = ambient temperature/ P1 = atmosphere pressure 1 bar P2 = L.P cylinder outlet pressure P3 = H.P cylinder outlet pressure

5.1 Sample calculations for Reading -1 at 2 bar pressure Sample calculations for Reading -1 Volume of air sucked in to the cylinder Va =Cd x Ao x x 3600 M3/hr

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Where H =

x

I.P =

= 170.517 meters

Va =0.62 x 1.767 x10-4 x 3600 = 22.812 M3/hr

x

I.P

x

max RaxT1

=

1]

x

x

0.287x301

1] =0.430 KW Theoretical volume of air Vth = LxNc (A1 + A2) x60 M3/hr

Power input to Motor (Pm )

Area of first cylinder-A1=

Pm =

Area of first cylinder-A1= Where 3200 = Energy meter constant -3

-3

Vth = 0.085x928 (1.9634 x 10 + 3.848 x 10 ) x60 M3/hr Vth = 27.506 M3/hr

= 2.105 KW

Power input to compressor Pc = Pm x 0.8 Pc = 2.105 x 0.8 = 1.684 Kw

Volumetric efficiency ηvol = x 100

ηvol

Pm =

Mechanical efficiency =

=

x 100

x 100 = 82.9%

= Compression ratio Rp =

=

= 1.9

x 100 =

25.53%

Piso = max RaxT1 x ln(Rp) Overall efficiency Where ma = Va x =density of air

=density

of air

=

x 100 =

=

=1.1729

x 100

= 24.47 % Isothermal efficiency

ma = 22.812 x 1.729 =26.756 M3/hr

= =

x 100 x 100 =

Piso = max RaxT1 x ln(Rp)

95.9 %

Piso =

5.2 Sample calculations for Reading -2 at 4 bar pressure

x 0.287x (273+28)x ln(1.9)

=0.4121 KW Sample calculations for Reading -2 As per the relation (temperature, pressure and volume) for polytrophic process ln(

) = =

=

x ln(1.9) = 0.28317 and n=1.396

Volume of air sucked in to the cylinder Va =Cd x Ao x x 3600 M3/hr Where H =164.549 meters Va =0.62 x 1.767 x10-4 x 3600 = 22.812 M3/hr

x

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Theoretical volume of air Vth = LxNc (A1 + A2) x60 M3/hr

Pm = Where 3200 = Energy meter constant

Area of first cylinder-A1= Area of first cylinder-A1=

Pm = 2.434 KW

Vth = 0.085x923 (1.9634 x 10-3 + 3.848 x 10-3) x60 M3/hr

Power input to compressor Pc = Pm x 0.8 Pc = 2.434 x 0.8 = 1.947 Kw

Vth = 27.354 M3/hr

Mechanical efficiency

Volumetric efficiency ηvol = x 100

ηvol

=

=4.45

Overall efficiency

=

x 100 =

x 100

= 48.3 %

Where ma = Va x =density of air of air

x 100

= 52.09%

Piso = ma x RaxT1 x ln(Rp)

=density

x 100

=

x 100 = 81.9%

Compression ratio Rp =

=

Isothermal efficiency

=

x 100

= =

=1.1729

x 100 =

92.8 % 3

ma = 22.409 x 1.729 =26.283 M /hr Piso = max RaxT1 x ln(Rp)

5.3 Sample calculations for Reading -3 at 6 bar pressure

Piso =

Sample calculations for Reading -1

x 0.287x (273+28)x ln(4.45)

=0.9415 KW As per the relation (temperature, pressure and

Volume of air sucked in to the cylinder Va =Cd x Ao x x 3600 M3/hr

volume) for polytrophic process

Where H = 161.139 meters

ln(

) = =

I.P =

=

Va = 22.175 M3/hr

x ln(4.45)

Theoretical volume of air Vth = LxNc (A1 + A2) x60 M3/hr

= 0.1971 and n=1.2454

x

max RaxT1

I.P = 1.0143 KW Power input to Motor (Pm)

Area of first cylinder-A1= 1]

Area of first cylinder-A1= Vth = 0.085x917 (1.9634 x 10-3 + 3.848 x 10-3) x60 M3/hr Vth = 27.178 M3/hr

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Mechanical efficiency

Volumetric efficiency ηvol = x 100

ηvol

Overall efficiency

Isothermal efficiency

of air

Table 4: table of results for multistage compressor

Piso = max RaxT1 x ln(Rp) x 0.287x (273+28)x ln(6.4)

pre ssu re 2

ηv

Pis

ol

o

8 2. 9

0. 41 21

0. 45 19

1. 68 4

2 6. 8

4

8 1. 9 2 8 1. 5 9

0. 94 15

1. 09 4

1. 94 7

5 6. 1

1. 15 85

1. 33 7

2. 08 15

6 4. 2 3

=1.1585 KW As per the relation (temperature, pressure and

) =

=

x ln(6.4) 6

= 0.1921 and n=1.2377

I.P =

x

x 100

5.4 Comparisons of values for multi stage compressor

=

ma = 22.175 x 1.729 =26.009 M3/hr

volume) for polytrophic process

= = 93.5%

=1.1729

ln(

x 100 = 55.6 %

Where ma = Va x =density of air

Piso =

=

=

Piso = max RaxT1 x ln(Rp)

=density

x 100

= 59.6%

=81.59%

Compression ratio Rp =

=

max RaxT1

1]

I.P =1.2377 KW Power input to Motor (Pm) Pm = Where 3200 = Energy meter constant Pm = 2.6019 KW

IP

Pc

η

ηo

ηi

me

vr

so

2 4. 4 7 4 8. 3

9 1. 1

ch

5 5. 6

8 6. 0 6 8 6. 6

T R 4 P M 8 9 9 2 8 1 3 1

9 2 3

1 5 7

9 1 7

Comparison shows as pressure is increasing volumetric efficiency and isothermal efficiency is decreasing but isothermal power and indicated power increases and also other efficiencies like mechanical, overall efficiencies increases with increase of the pressure. It was observed this is same in both cases of single and multi stage compressor

5.5 Comparisons tables for single stage and multi stage compressors

Power input to compressor Pc = Pm x 0.8 Pc = 2.6019 x 0.8 = 2.0815 Kw

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Table: 5 -Comparisons table for single and

Table: 6 -Comparisons table for single and

multi stage compressor

multistage compressor

Tank Press ure

Volumetric Efficiency

Piso

2

Sin gle stag e 80.3

Sin gle stag e 0.20 9 0.32 6 0.35 9

4 6

IP

70.4 6 67.5 2

Mul ti stag e 82.9 81.9 2 81.5 9

Mult i stage

Singl e stage

Multi stage

0.41 21 0.94 15 1.15 85

0.30 2 0.37 96 0.42 3

0.451

Tank Pressure

ηmech

Pc

ηover

Single Multi stage stage

Single Multi Single Multi stage stage stage stage

2

1.327

1.684

22.75

26.8

20.27

24.47

4

1.384

1.947

27.41

56.1

23.5

48.3

6

1.5

2.0815 28.2

64.23 23.9

55.6

1.094 1.337

power to compressor 3

volumetric efficiency

2

100 Single stage

50

Multi stage

0 2

4 Tank pressure

1

Single stage

0

Multi stage 2

6

4

6

Tank pressure

Isothermal power

mechanical efficiency

1.5 1 0.5 0

100 50

Single stage 2

4

6

Single stage

0

Multi stage

2

4

Multi stage

6

Tank pressure

Tank pressure

Indicated power

overal efficiency 60

1.5 1 0.5 0

40 Single stage 2

4

6

Multi stage

20

Single stage

0

Multi stage 2

tankpressure

4

6

Tank pressure

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Table: 7 -Comparisons table for single and

multi stage compressor Tank Pressu re

Delivery temperatur e

ηiso Singl e stage

Mul ti stae

Singl e stage

2

89.0

91.1

109

4

85.8

125

6

84.8

86.0 6 86.6

136

RPM

Mu lti sta ge 88

Single stage

876

Mul ti stag e 928

13 1 15 7

872.2

923

869.3

917

multistage compressor having higher efficiency then the single stage compressor. REFERENCES [1] Internal combustion engines and Air pollution by professor (Dr.) R.Yadav Third revised edition –central publishing house 18C, Sarojini Naidu Marge-Allahabad-211001 [2]A Text book of internal combustion Engines (Including Air compressor, Gas turbines and Jet propulsions) Unit second Edition By R.K.Rajput published by Laxmi Publications Pvt Ltd 113, Golden house,Daryaganj,New Delhi-110002 [3] A Text book of Thermal Engineering by J.K Gupta and R.S.Khurmi

iso thermal efficiency 92 90 88 86 84 82 80

Single stage Multi stae 2

4

6

Tankpressure

6.0 CONCLUSIONS It was observed with increase of tank pressure isothermal power, indicated power mechanical efficiencies are increasing for both single and multistage compressors and also observed with increase of delivery pressure volumetric efficiency is reducing in both cases. As temperature of incoming air increasing, the density of air decreasing and volume of air sucked in to cylinder increases, it may be the reason because of less dense of air which may be entering in to the engine cylinder. On comparison of volumetric efficiency, isothermal power indicated power, mechanical efficiency; isothermal efficiencies are higher for multistage compressor then the single stage compressor with marginal rise of power input to the compressor. We may conclude for almost same equal power consumption ANVESHANA’S INTERNATIONAL JOURNAL OF RESEARCH IN ENGINEERING AND APPLIED SCIENCES

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