Specification
No | Suction Pressure, kgf/сm2 | Discharge Pressure, kgf/сm2 | Flow Rate Capacity, MMCMD | Recommended compressor |
1 | 2,0 | 9,0 | 1,43 | 252GC1-540/2-9М126 |
2 | 2,4 | 10 | 2,48 | D203GC1-710/2.4-10М2 |
3 | 3,0 | 12 | 1,14 | 193GC1-260/3-12М56 |
4 | 3,0 | 7,5 | 2,28 | 252GC1-600/3-7.5М126 |
5 | 4,0 | 17 | 1,68 | 193GC1-330/4-17М126 |
6 | 4,6 | 21 | 2 | 193GC1-320/4.6-21 |
7 | 6,0 | 12 | 0,54 | 224GC2-72/6-12М1 |
8 | 6,0 | 19 | 1,58 | 193GC1-200/6-19М6 |
9 | 6,0 | 56 | 5,4 | S325GC2-650/6-56М12 |
10 | 6,0 | 14 | 3,33 | 224GC2-375/6-14А |
11 | 7,0 | 21 | 8,3 | 295GC2-800/7-21 |
12 | 7,0 | 17,5 | 2,28 | 223GC1-260/7-17.5М126 |
13 | 7,3 | 47,5 | 1,43 | D245GC2-148/7.3-47.5М1245 |
14 | 9.5 | 21 | 12,59 | 295GC2-880/9.5-21 |
15 | 10,0 | 20 | 6,1 | 294GC2-410/10-20М1235 |
16 | 11,5 | 82 | 1,14 | D223GC2-75/11.5-82М45 |
17 | 12,0 | 50 | 2,16 | 225GC2-135/12-50М1245 |
18 | 17,0 | 56 | 2,28 | 225GC2-105/17-56М124 |
19 | 17,0 | 62 | 1,68 | 185GC2-78/17-62М14 |
20 | 18,0 | 78 | 1,65;1,73 | 183GC2-64/18-78М45 |
21 | 18,0 | 46 | 1,58 | 185GC2-68/18-46М45 |
22 | 19,0 | 41 | 4,99 | 225GC2-200/19-41 |
23 | 20,0 | 76 | 2 | 223GC2-73/20.5-76 |
24 | 21,0 | 80 | 3,48 | 225GC2-125/21-80М124 |
25 | 33,0 | 56 | 7,92 | 8GC2-160/33-56 |
26 | 35,0 | 76 | 11,73 | 295GC2-215/35-76М1 |
27 | 35,0 | 75 | 12,7 | 295GC2-245/35-75М1 |
28 | 35,0 | 75 | 2,12 | 184GC2-41/35-75М124 |
29 | 37,0 | 76 | 3,13 | 224GC2-73/37-76М12 |
30 | 39,0 | 56 | 17,32 | 201GC2-290/39-56 |
31 | 39,0 | 56 | 17,32 | 222GC2-290/39-56 |
32 | 43,0 | 125 | 3,68 | S184GC2-60/43-125М1256 |
33 | 44,0 | 100 | 12,3 | 295GC2-190/44-100М |
34 | 44,5 | 76 | 4,5 | GC2-87/44.5-76 |
35 | 45,0 | 76 | 21,5 | 323GC2-310/45-76М |
36 | 47,0 | 80 | 17,4 | 295GC2-238/47-80М1 |
37 | 50,0 | 76 | 20 | 321GC2-292/50-76М1 |
38 | 53,0 | 76 | 32,3 | 291GC2-395/53-76S |
39 | 53,0 | 76 | 47,2 | 321GC2-560/53-76М |
40 | 56,0 | 76 | 11,88 | 224GC2-130/56-76М12 |
41 | 63,0 | 85 | 38,24 | 291GC2-385/63-85М1 |
42 | 65,0 | 155 | 6,23 | 154GC2-63/65-155М124 |
43 | 68,0 | 92 | 27,62 | 291GC2-286/68-92М1 |
44 | 70,0 | 100 | 45 | 352GC2-395/70-100М |
45 | 75,0 | 105 | 47,34 | 324GC2-420/75-105М1 |
46 | 75,0 | 100 | 60 | 352GC2-485/75-100М |
47 | 125,0 | 300 | 3,68 | S153GC2-21/125-300М125 |
Centrifugal compressor identification legend, example: S291GC2-395/53-76М13, where:
S – The letter shows the single-shell compressor packaging type.
The absence of a letter means the standard compressor design with one inlet and one outlet nozzle. Double-entry or multi-sectional shell design aredefined by the following letters:
D – double-entry compressor;
P – two-section compressor with consecutive impellers arrangement;
S – two-section compressor with “back-to-back” impeller arrangement;
Т – three-section compressor.
29 – Two digits show the basic diameter of the compressor’s shell inner bore, which is defined by a rounded value of ratio of bore diameters in millimeters to the number 50. Base 29 in the example refers to the diameter of 1450 mm.
The absence of a letter means the standard compressor design with one inlet and one outlet nozzle. Double-entry or multi-sectional shell design aredefined by the following letters:
D – double-entry compressor;
P – two-section compressor with consecutive impellers arrangement;
S – two-section compressor with “back-to-back” impeller arrangement;
Т – three-section compressor.
29 – Two digits show the basic diameter of the compressor’s shell inner bore, which is defined by a rounded value of ratio of bore diameters in millimeters to the number 50. Base 29 in the example refers to the diameter of 1450 mm.
1 – The digit shows the sequential number of basic shell design per the length.
The shell lengths increase from the sequential number 1 to 2, 3.
GC – Two letters show the compressor purpose and type:
GC- Gas Centrifugal; VC-Air Centrifugal.
2 – Compressor design :
Digit 1 – compressor design with horizontal shell joint.
Digit 2 – compressor design with vertical shell joint (“barrel” type).
395 – The number refers to a rounded value of volumetric production capacity, corrected for starting conditions, in m3/min.
53 – The number refers to the rounded value of nominal suction pressure (abs.), in kgf/cm2.
76 – The number refers to the rounded value of nominal discharge pressure (abs.), in kgf/cm2
М – Compressor modification stipulating various design versions of main assembly units.
13 – The digit (some digits) shows the compressor modification type:
0 – dopeless design (MS+DGS), when designating a dopeless compressor with no other modifications, “0” is not put down;
1 – end seals – DGS;
2 – rotor rotation direction – anti-clockwise (looking from the drive side);
3 – location of the inlet nozzle on the right (looking from the drive side);
4 – location of legs’ supporting surface along the longtitudal axis of the compressor (or a leg thickness lower than the axis);
5- location of driven rotor end on the outlet nozzle side;
6 – availability of driving and driven rotor ends in a multi-shell compressor design.
Learn more…
To order the equipment you are interested in, please complete the Questionnaire.
Details are specified in the Technical Catalog “Compressor equipment and GPU”.
The shell lengths increase from the sequential number 1 to 2, 3.
GC – Two letters show the compressor purpose and type:
GC- Gas Centrifugal; VC-Air Centrifugal.
2 – Compressor design :
Digit 1 – compressor design with horizontal shell joint.
Digit 2 – compressor design with vertical shell joint (“barrel” type).
395 – The number refers to a rounded value of volumetric production capacity, corrected for starting conditions, in m3/min.
53 – The number refers to the rounded value of nominal suction pressure (abs.), in kgf/cm2.
76 – The number refers to the rounded value of nominal discharge pressure (abs.), in kgf/cm2
М – Compressor modification stipulating various design versions of main assembly units.
13 – The digit (some digits) shows the compressor modification type:
0 – dopeless design (MS+DGS), when designating a dopeless compressor with no other modifications, “0” is not put down;
1 – end seals – DGS;
2 – rotor rotation direction – anti-clockwise (looking from the drive side);
3 – location of the inlet nozzle on the right (looking from the drive side);
4 – location of legs’ supporting surface along the longtitudal axis of the compressor (or a leg thickness lower than the axis);
5- location of driven rotor end on the outlet nozzle side;
6 – availability of driving and driven rotor ends in a multi-shell compressor design.
Learn more…
To order the equipment you are interested in, please complete the Questionnaire.
Details are specified in the Technical Catalog “Compressor equipment and GPU”.