final stage t2

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Page | 1 By: CangTo CHEAH (1 st June 2015), Senior Rotating Equipment Engineer (Technip) Project: SLIC HCL recycle project Equipment / type: Chlorine gas compressor / centrifugal Document title: Evaluation of compressor discharge temperatures when chilled water supply fails at inter-stage cooler, based on MDT’s proposal. Introduction The chlorine compressor proposed by MDT consists of two process stages; and inter-stage coolers will be supplied by MDT. The inter-stage cooling itself consists of two shell-and-tube coolers configured in series, note that coolant for 1 st cooler is cooling water (supply & return temperatures are 33 deg. C and 43 deg. C, respectively) and coolant for 2 nd cooler is chilled water (supply & return temperatures are 5 deg. C and 10 deg. C, respectively). 1 st cooler discharge temperature for process gas is 55 deg. C per MDT’s preliminary proposal. The LOPA (layer of protection analysis) performed in the earlier stage of SLIC HCL recycle project places an action item for EPC contractor to look at mitigation measures to limit compressor discharge temperature below 120 deg. C, during failure of chilled water supply. There are various ways to reduce discharge temperature for centrifugal compressor, namely: a) Improved efficiency b) Reduced head c) Reduced inlet temperature Noting that item a) can be realized in two ways. Efficiency can either be improved by varying suction volume flow rate along the x-axis of performance curve “efficiency vs. inlet volume flow rate”, or in case if inlet volume flow rates cannot be varied (due to process restrictions), then re-selection of impeller family may be considered. This study is based on the former (with combinations of b and c), as maintaining inlet volume flow rate at abnormal process conditions (e.g. failure of chilled water supply) is not a mandatory requirement. Basis of compressor performance calculation 1) Thermodynamic model Lee-Kesler-Plocker corresponding state is used, with binary interaction coefficients extracted from HYSYS. Polytropic temperature and polytropic volume exponents are used to calculate discharge temperature and discharge pressure, respectively. 2) Aerodynamic model MDT’s performance curves (polytropic head vs. actual inlet volume flow rate and polytropic efficiency vs. actual inlet volume flow rate) are modeled with 4 th order polynomial curve-fitting technique (i.e. least square method). Inputs are : Inlet volume flow rate & inlet pressure for LP stage, suction temperature for both LP and HP stages, inter-stage pressure loss (assumed 0.15 bar, per MDT’s data sheet), and project specific gas mixture. Calculated outputs are : Polytropic head, polytropic efficiency, discharge temperature, discharge pressure, compression power, polytropic exponents, compressibility factor, and mass flow rate. Conclusion : On page 8

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Page 1: Final stage T2

Page | 1

By: CangTo CHEAH (1st June 2015), Senior Rotating Equipment Engineer (Technip)

Project: SLIC HCL recycle project

Equipment / type: Chlorine gas compressor / centrifugal

Document title: Evaluation of compressor discharge temperatures when chilled water supply fails at inter-stage

cooler, based on MDT’s proposal.

Introduction

The chlorine compressor proposed by MDT consists of two process stages; and inter-stage coolers will be supplied

by MDT. The inter-stage cooling itself consists of two shell-and-tube coolers configured in series, note that coolant

for 1st cooler is cooling water (supply & return temperatures are 33 deg. C and 43 deg. C, respectively) and coolant

for 2nd cooler is chilled water (supply & return temperatures are 5 deg. C and 10 deg. C, respectively). 1st cooler

discharge temperature for process gas is 55 deg. C per MDT’s preliminary proposal. The LOPA (layer of protection

analysis) performed in the earlier stage of SLIC HCL recycle project places an action item for EPC contractor to look

at mitigation measures to limit compressor discharge temperature below 120 deg. C, during failure of chilled water

supply. There are various ways to reduce discharge temperature for centrifugal compressor, namely:

a) Improved efficiency b) Reduced head c) Reduced inlet temperature

Noting that item a) can be realized in two ways. Efficiency can either be improved by varying suction volume flow

rate along the x-axis of performance curve “efficiency vs. inlet volume flow rate”, or in case if inlet volume flow

rates cannot be varied (due to process restrictions), then re-selection of impeller family may be considered. This

study is based on the former (with combinations of b and c), as maintaining inlet volume flow rate at abnormal

process conditions (e.g. failure of chilled water supply) is not a mandatory requirement.

Basis of compressor performance calculation

1) Thermodynamic model

Lee-Kesler-Plocker corresponding state is used, with binary interaction coefficients extracted from HYSYS.

Polytropic temperature and polytropic volume exponents are used to calculate discharge temperature and

discharge pressure, respectively.

2) Aerodynamic model

MDT’s performance curves (polytropic head vs. actual inlet volume flow rate and polytropic efficiency vs. actual

inlet volume flow rate) are modeled with 4th order polynomial curve-fitting technique (i.e. least square method).

Inputs are: Inlet volume flow rate & inlet pressure for LP stage, suction temperature for both LP and HP stages,

inter-stage pressure loss (assumed 0.15 bar, per MDT’s data sheet), and project specific gas mixture.

Calculated outputs are: Polytropic head, polytropic efficiency, discharge temperature, discharge pressure,

compression power, polytropic exponents, compressibility factor, and mass flow rate.

Conclusion: On page 8

Page 2: Final stage T2

Page | 2

Normal: 55 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 116 deg. C. Okay

Page 3: Final stage T2

Page | 3

Maximum: 55 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 119 deg. C. Okay

Page 4: Final stage T2

Page | 4

Case A: 55 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 95 deg. C. Okay

Page 5: Final stage T2

Page | 5

Case B: 55 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 123 deg. C. Not okay.

Page 6: Final stage T2

Page | 6

Case B: 50 deg. C cooling water cooling discharge temperature

Remark: Final stage discharge temperature approx 120 deg. C. Okay

Page 7: Final stage T2

Page | 7

Case C: 55 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 129 deg. C. Not okay

Page 8: Final stage T2

Page | 8

Case C: 50 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 119 deg. C. Note that inlet volume flow rate 4191 m^3/hr (per

MDT’s Q_inlet) on LP stage would yield final stage discharge temperature 124.7 deg. C (based on 50 deg. C inter-

stage temperature); Therefore a larger Inlet volume flow rate, i.e. 4550 m^3/hr is used to estimate HP stage T2.

With Q_inlet 4550 m^3/hr, discharge temperatures on both LP and HP stages are reduced (LP stage T2 is reduced

with improved efficiency (from 82.58% to 83.60%) & reduced head; HP stage: even though efficiency is reduced

(from 82.65% to 81.60%), low T2 is however compensated by reduced head, as T2 is directly proportional to

compression ratio). See Appendix 1 for more details (page 10 to 15).

Conclusion: It is proposed to reduce 1st cooler discharge temperature (from 55 deg. C down to 50 deg. C), so that

HP stage discharge temperature can be controlled below 120 deg. C during a chilled water supply failure, and

chlorine compressor train can be coast-down in a safe manner.

Page 9: Final stage T2

Page | 9

Case D: 55 deg. C cooling water cooler discharge temperature

Remark: Final stage discharge temperature approx 115 deg. C

Page 10: Final stage T2

Page | 10

Appendix 1 (page 10 to 15)

Case C with Q_inlet 4191 m^3/hr and inter-stage temperature 50 deg. C

Performance curves: Refer to page 11 and 12 for LP and HP stages, respectively.

Page 11: Final stage T2

Page | 11

LP stage performance curves

Page 12: Final stage T2

Page | 12

HP stage performance curves

Page 13: Final stage T2

Page | 13

Case C with Q_inlet 4550 m^3/hr and inter-stage temperature 50 deg. C

Performance curves: Refer to page 14 and 15 for LP and HP stages, respectively.

Page 14: Final stage T2

Page | 14

LP stage performance curves

Page 15: Final stage T2

Page | 15

HP stage performance curves