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Integration of Oxygen Transport
Membranes in an IGCC power plant with
CO2 capture

Rahul Anantharaman1 and Olav Bolland2
1
    SINTEF Energy Research, Energy Processes
2
    Department of Energy and Process Engineering, NTNU


PRES 2011, Florence
May 9, 2011



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                                 SINTEF Energy Research   s   s   s   s   s   s   1
Overview of Presentation

Introduction
    Motivation
    Oxygen Transport Membranes
    Objective
    Project Framework

Integration of oxygen membranes in an IGCC
    Membrane operating methods
    Air integration

Summary



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                                 SINTEF Energy Research   s   s   s   s   s   s   2
concluded that the performance penalty associated with using E-class gas t
          technology would be a barrier to successful deployment of pre-combustion capture.
Integrated Gasification Combined Cycle
  These processing steps are shown in the outline flow scheme in Figure 3.1:
(IGCC)




 DYNAMIS D5.3.2:IGCC with pre-combustion CO2
  Figure 3.1: Recommendations for HYPOGEN Initiative   capture for co-production of electricity and hyd
                                                                                s   s   s   s   s   s

               from coal and lignite.                  SINTEF Energy Research   s   s   s   s   s   s   3
Air Separation Unit


  I ASU supplies O2 at 95% purity.
  I Theoretical minimum work consumption: 49 kWh/ton of O2
    produced.
  I State-of-the-art cryogenic ASU consumes: 175-200 kWh/ton of
    O2 produced.
  I Cryogenic ASU development prospects: 145-160 kWh/ton of O2
    produced.




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                                     SINTEF Energy Research   s   s   s   s   s   s   4
Oxygen Transport Membranes
 I Dense ceramic membranes (metal oxides).
 I Membrane operation based on mixed conduction of ions and
   electrons.
 I Separates O2 from air with 100% selectivity.
 I Operating temperature range: 800-1000°C.




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                                  SINTEF Energy Research   s   s   s   s   s   s   5
Integration of OTM in an IGCC

 I OTM are a promising technology that present a major source of
    efficiency improvement
 I Challenge lies in efficient integration of such membrane in an
    IGCC to realize this potential

Objectives

 I Develop efficient cycles integrating an Oxygen Transport
    Membranes as an ASU in an IGCC plant to reduce efficiency
    penalty.
 I Insight into considerations for such an integration.



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                                     SINTEF Energy Research   s   s   s   s   s   s   6
Framework
 I This work was done as part of the EU FP7 project DECARBit.
 I DECARBit investigates several advanced pre-combustion capture
   technologies, both at a fundamental and more applied level.

                         SP1 System integration and optimisation
                         including application
                         to other industries
                                                            SP2 Advanced Pre-
                                                            combustion CO2 separation              CO2 to
          Coal                                                                                     storage
                    Gasifier,             Shift                 CO2                CO2
                    Reformer            reactors   H2,       separation         compression
          Natural                                  CO2
          gas

                                O2                                   SP4 Enabling
                                                              H2
                                                                     technologies for
                                                             (fuel
                                                                     pre-combustion
                                                             gas)

                                        Air                                                        Electric
                       Air           Separation    N2           Gas                Steam           power
                                        Unit                  turbine              Cycle

                             SP3 Advanced oxygen
                             separation technologies


                                                        SP5 Pre-combustion pilots



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Reference cases

 I European Benchmarking Task Force (EBTF) established between
   3 EU FP7 projects - CESAR, CAESAR and DECARBit.
 I EBTF developed and published document on benchmarking
   reference cases with and without capture for
     1. Advanced Supercritical Pulverized Coal (post-combustion).
     2. Integrated Gasification Combined Cycle (pre-combustion).
     3. Natural Gas Combined Cycle (post-combustion).
 I Reference case for IGCC without capture: 46.88 %.
 I Reference case for IGCC with 90% CO2 capture: 36.66 %.
 I Relevant assumption: 50% air integration between GT and ASU.



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Membrane system design



 I The driving force is the partial pressure difference (pO2 = xO2 · P )
    between the oxygen rich feed side and the permeate side.
 I The oxygen flux across the membrane is given by modified
                                RT         ln pO ,perm    σel σion
    Wagner’s equation: JO2 = − 16F 2 L          2
                                          ln pO ,feed    σel +σion
                                                                   ∂   ln pO2
                                               2

 I Give a feed side oxygen partial pressure, to increase flux
      1. xO2 ,perm should decrease, and/or
      2. Pperm should should decrease.




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                                         SINTEF Energy Research        s   s   s   s   s   s   9
Membrane system design



 I The driving force is the partial pressure difference (pO2 = xO2 · P )
    between the oxygen rich feed side and the permeate side.
 I The oxygen flux across the membrane is given by modified
                                RT         ln pO ,perm    σel σion
    Wagner’s equation: JO2 = − 16F 2 L          2
                                          ln pO ,feed    σel +σion
                                                                   ∂   ln pO2
                                               2

 I Give a feed side oxygen partial pressure, to increase flux
      1. xO2 ,perm should decrease, and/or
      2. Pperm should should decrease.




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                                         SINTEF Energy Research        s   s   s   s   s   s   9
Membrane system design



 I The driving force is the partial pressure difference (pO2 = xO2 · P )
    between the oxygen rich feed side and the permeate side.
 I The oxygen flux across the membrane is given by modified
                                RT         ln pO ,perm    σel σion
    Wagner’s equation: JO2 = − 16F 2 L          2
                                          ln pO ,feed    σel +σion
                                                                   ∂   ln pO2
                                               2

 I Give a feed side oxygen partial pressure, to increase flux
      1. xO2 ,perm should decrease, and/or
      2. Pperm should should decrease.




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                                         SINTEF Energy Research        s   s   s   s   s   s   9
Membrane system design



 I The driving force is the partial pressure difference (pO2 = xO2 · P )
    between the oxygen rich feed side and the permeate side.
 I The oxygen flux across the membrane is given by modified
                                RT         ln pO ,perm    σel σion
    Wagner’s equation: JO2 = − 16F 2 L          2
                                          ln pO ,feed    σel +σion
                                                                   ∂   ln pO2
                                               2

 I Give a feed side oxygen partial pressure, to increase flux
      1. xO2 ,perm should decrease, and/or
      2. Pperm should should decrease.




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Membrane operating method
with sweep gas




 I Advantages:
     – Improved mechanical stability.
     – O2 is produced at higher pressure and hence compression work to
       gasifier condition is reduced.
 I Disadvantages:
     – Sweep gas temperature should be close to that of the feed side.
     – Sweep gas requirement.

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Sweep gas

 I Sweep gas will dilute the O2 .
 I Sweep gas can either be Steam or CO2 .
 I Large flow of sweep gas are required.

 I Steam
      – Extracted from bottoming cycle.
      – Leads to large efficiency penalty.
 I CO2
      – Recycled after separation from syn-gas and requires compression.
      – CO2 sweep increases CO2 captured, thus increasing energy
        penalty.
      – This is partly offset by the increased partial pressure of CO2 in the
        acid gas removal section.


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Sweep gas - efficiency penalty

                           120                                                                   37
                                      Steam flow (kg/s)
                           110
                                      Energy penalty (MW)                                        32




                                                                                                           nergy Penalty (MW)
                           100
       Steam flow (kg/s)




                            90                                                                   27

                            80                                                                   22
                            70




                                                                                                          En
                                                                                                 17
                            60

                            50                                                                   12
                                 10          12               14               16
                                               Sweep gas pressure (bar)




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Membrane operating method
without sweep gas




 I Advantages:
     – No efficiency penalty associated with sweep gas.
 I Disadvantages:
     – O2 produced at lower pressure leading to increased compression
       penalty.
     – Mechanical stability of membrane system.



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                                   SINTEF Energy Research   s   s   s   s   s   s   13
50% air integration - Scheme 1




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50% air integration - Scheme 1
  I Efficiency lower than reference case with cryogenic ASU

Reasons for low efficiency

  I Raising the OTM feed temperature to 900°C results in losses from
    the extra fuel conversion to H2 and eventual combustion in this
    process.
  I Transport limitation: The overall plant efficiency depends on the
    degree of O2 separation - mO2 ,perm /mO2 ,feed . The degree of
    separation for the process under consideration is 0.45.
  I A separate ASU required for N2 production. Nitrogen required for
    gas turbine fuel dilution and coal transport is supplied by a
    cryogenic ASU.
  I Improper integration!

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                                    SINTEF Energy Research   s   s   s   s   s   s   15
Reference case - Temperature profile




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50% Integration - Scheme 2




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50% air integration - Scheme 2


  I Efficiency lower than reference case with cryogenic ASU

Reasons for low efficiency

  I Turbine Inlet Temperature (TIT) is reduced compared to the
     reference case leading to increased efficiency penalty.
  I Transport limitation.
  I Need for seprate ASU for N2 production.
  I Improper integration!




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                                    SINTEF Energy Research   s   s   s   s   s   s   18
100% Integration




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                   SINTEF Energy Research   s   s   s   s   s   s   19
Figure 3: Process block diagram for OTM integrated IGCC plant with CO2 capture
100% Integration - Performance
             Table 1: Overall plant performance of OTM integrated IGCC plant with CO2 capture
                                      Coal flow rate      138.9 Tph
                       Thermal energy of fuel (LHV)       969.7 MWth
                      Thermal energy for coal drying       8.23 MWth
                                    Gas turbine output    280.5 MWe
                                  Steam turbine output    176.6 MWe
                          Gross electric power output     457.1 MWe
                   Total ancillary power consumption       92.1 MWe
                            Net electric power output     365.0 MWe
                                Net electric efficiency    37.3 %
                                      CO2 capture rate     90.9 %


             5. Conclusions
            System considerations for integration of an oxygen transport membrane based air
            separation unit are presented. Arguments for selection of membrane operating mode and
 I   Heat and mass GT is selected. detail. An integrated IGCC shows anand 100% airwith heating
            air integration are discussed in
            integration with
                               integration removewithout sweep gas efficiency gain of
                                              The OTM
                                                        OTM
                                                                 losses associated side
     fuel to0.7% points over the reference IGCC plant with cryogenic ASU. However, the trade-off
              900°C and transport limitation.
            is the tighter integration and reduced flexibility of the plant. Also, the number of plant
 I   This also required a separate to the OTM based ASU for O2 production a
            components is increased as in addition cryogenic ASU, but with smaller
            cryogenic ASU is required for N2 production.
     capacity.
 I Complete integration could lead to start-up/shut-down and
     availability issues.
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                                                          SINTEF Energy Research   s   s   s   s   s   s   20
Summary


 I An overview of the considerations when integrating an oxygen
    transport membrane as an ASU in an IGCC is presented.
 I An OTM with out sweep gas and 100% air integration is shown to
    have 0.7% points higher efficiency than the reference case cycle.
 I The trade-off is tighter integration - reduced flexibility.
 I Other cycles, e.g. combination of pre- and oxy-combustion
    concepts, are being evaluated.




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                                     SINTEF Energy Research   s   s   s   s   s   s   21
Acknowledgement




The research leading to these results has received funding from the
European Community’s Seventh Framework Programme
(FP7/2007-2013) under grant agreement nˇ 211971 (The DECARBit
                                           r
project).




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Integration of Oxygen Transport Membranes in an IGCC power plant with CO2 capture

  • 1. Integration of Oxygen Transport Membranes in an IGCC power plant with CO2 capture Rahul Anantharaman1 and Olav Bolland2 1 SINTEF Energy Research, Energy Processes 2 Department of Energy and Process Engineering, NTNU PRES 2011, Florence May 9, 2011 s s s s s s SINTEF Energy Research s s s s s s 1
  • 2. Overview of Presentation Introduction Motivation Oxygen Transport Membranes Objective Project Framework Integration of oxygen membranes in an IGCC Membrane operating methods Air integration Summary s s s s s s SINTEF Energy Research s s s s s s 2
  • 3. concluded that the performance penalty associated with using E-class gas t technology would be a barrier to successful deployment of pre-combustion capture. Integrated Gasification Combined Cycle These processing steps are shown in the outline flow scheme in Figure 3.1: (IGCC) DYNAMIS D5.3.2:IGCC with pre-combustion CO2 Figure 3.1: Recommendations for HYPOGEN Initiative capture for co-production of electricity and hyd s s s s s s from coal and lignite. SINTEF Energy Research s s s s s s 3
  • 4. Air Separation Unit I ASU supplies O2 at 95% purity. I Theoretical minimum work consumption: 49 kWh/ton of O2 produced. I State-of-the-art cryogenic ASU consumes: 175-200 kWh/ton of O2 produced. I Cryogenic ASU development prospects: 145-160 kWh/ton of O2 produced. s s s s s s SINTEF Energy Research s s s s s s 4
  • 5. Oxygen Transport Membranes I Dense ceramic membranes (metal oxides). I Membrane operation based on mixed conduction of ions and electrons. I Separates O2 from air with 100% selectivity. I Operating temperature range: 800-1000°C. s s s s s s SINTEF Energy Research s s s s s s 5
  • 6. Integration of OTM in an IGCC I OTM are a promising technology that present a major source of efficiency improvement I Challenge lies in efficient integration of such membrane in an IGCC to realize this potential Objectives I Develop efficient cycles integrating an Oxygen Transport Membranes as an ASU in an IGCC plant to reduce efficiency penalty. I Insight into considerations for such an integration. s s s s s s SINTEF Energy Research s s s s s s 6
  • 7. Framework I This work was done as part of the EU FP7 project DECARBit. I DECARBit investigates several advanced pre-combustion capture technologies, both at a fundamental and more applied level. SP1 System integration and optimisation including application to other industries SP2 Advanced Pre- combustion CO2 separation CO2 to Coal storage Gasifier, Shift CO2 CO2 Reformer reactors H2, separation compression Natural CO2 gas O2 SP4 Enabling H2 technologies for (fuel pre-combustion gas) Air Electric Air Separation N2 Gas Steam power Unit turbine Cycle SP3 Advanced oxygen separation technologies SP5 Pre-combustion pilots s s s s s s SINTEF Energy Research s s s s s s 7
  • 8. Reference cases I European Benchmarking Task Force (EBTF) established between 3 EU FP7 projects - CESAR, CAESAR and DECARBit. I EBTF developed and published document on benchmarking reference cases with and without capture for 1. Advanced Supercritical Pulverized Coal (post-combustion). 2. Integrated Gasification Combined Cycle (pre-combustion). 3. Natural Gas Combined Cycle (post-combustion). I Reference case for IGCC without capture: 46.88 %. I Reference case for IGCC with 90% CO2 capture: 36.66 %. I Relevant assumption: 50% air integration between GT and ASU. s s s s s s SINTEF Energy Research s s s s s s 8
  • 9. Membrane system design I The driving force is the partial pressure difference (pO2 = xO2 · P ) between the oxygen rich feed side and the permeate side. I The oxygen flux across the membrane is given by modified RT ln pO ,perm σel σion Wagner’s equation: JO2 = − 16F 2 L 2 ln pO ,feed σel +σion ∂ ln pO2 2 I Give a feed side oxygen partial pressure, to increase flux 1. xO2 ,perm should decrease, and/or 2. Pperm should should decrease. s s s s s s SINTEF Energy Research s s s s s s 9
  • 10. Membrane system design I The driving force is the partial pressure difference (pO2 = xO2 · P ) between the oxygen rich feed side and the permeate side. I The oxygen flux across the membrane is given by modified RT ln pO ,perm σel σion Wagner’s equation: JO2 = − 16F 2 L 2 ln pO ,feed σel +σion ∂ ln pO2 2 I Give a feed side oxygen partial pressure, to increase flux 1. xO2 ,perm should decrease, and/or 2. Pperm should should decrease. s s s s s s SINTEF Energy Research s s s s s s 9
  • 11. Membrane system design I The driving force is the partial pressure difference (pO2 = xO2 · P ) between the oxygen rich feed side and the permeate side. I The oxygen flux across the membrane is given by modified RT ln pO ,perm σel σion Wagner’s equation: JO2 = − 16F 2 L 2 ln pO ,feed σel +σion ∂ ln pO2 2 I Give a feed side oxygen partial pressure, to increase flux 1. xO2 ,perm should decrease, and/or 2. Pperm should should decrease. s s s s s s SINTEF Energy Research s s s s s s 9
  • 12. Membrane system design I The driving force is the partial pressure difference (pO2 = xO2 · P ) between the oxygen rich feed side and the permeate side. I The oxygen flux across the membrane is given by modified RT ln pO ,perm σel σion Wagner’s equation: JO2 = − 16F 2 L 2 ln pO ,feed σel +σion ∂ ln pO2 2 I Give a feed side oxygen partial pressure, to increase flux 1. xO2 ,perm should decrease, and/or 2. Pperm should should decrease. s s s s s s SINTEF Energy Research s s s s s s 9
  • 13. Membrane operating method with sweep gas I Advantages: – Improved mechanical stability. – O2 is produced at higher pressure and hence compression work to gasifier condition is reduced. I Disadvantages: – Sweep gas temperature should be close to that of the feed side. – Sweep gas requirement. s s s s s s SINTEF Energy Research s s s s s s 10
  • 14. Sweep gas I Sweep gas will dilute the O2 . I Sweep gas can either be Steam or CO2 . I Large flow of sweep gas are required. I Steam – Extracted from bottoming cycle. – Leads to large efficiency penalty. I CO2 – Recycled after separation from syn-gas and requires compression. – CO2 sweep increases CO2 captured, thus increasing energy penalty. – This is partly offset by the increased partial pressure of CO2 in the acid gas removal section. s s s s s s SINTEF Energy Research s s s s s s 11
  • 15. Sweep gas - efficiency penalty 120 37 Steam flow (kg/s) 110 Energy penalty (MW) 32 nergy Penalty (MW) 100 Steam flow (kg/s) 90 27 80 22 70 En 17 60 50 12 10 12 14 16 Sweep gas pressure (bar) s s s s s s SINTEF Energy Research s s s s s s 12
  • 16. Membrane operating method without sweep gas I Advantages: – No efficiency penalty associated with sweep gas. I Disadvantages: – O2 produced at lower pressure leading to increased compression penalty. – Mechanical stability of membrane system. s s s s s s SINTEF Energy Research s s s s s s 13
  • 17. 50% air integration - Scheme 1 s s s s s s SINTEF Energy Research s s s s s s 14
  • 18. 50% air integration - Scheme 1 I Efficiency lower than reference case with cryogenic ASU Reasons for low efficiency I Raising the OTM feed temperature to 900°C results in losses from the extra fuel conversion to H2 and eventual combustion in this process. I Transport limitation: The overall plant efficiency depends on the degree of O2 separation - mO2 ,perm /mO2 ,feed . The degree of separation for the process under consideration is 0.45. I A separate ASU required for N2 production. Nitrogen required for gas turbine fuel dilution and coal transport is supplied by a cryogenic ASU. I Improper integration! s s s s s s SINTEF Energy Research s s s s s s 15
  • 19. Reference case - Temperature profile s s s s s s SINTEF Energy Research s s s s s s 16
  • 20. 50% Integration - Scheme 2 s s s s s s SINTEF Energy Research s s s s s s 17
  • 21. 50% air integration - Scheme 2 I Efficiency lower than reference case with cryogenic ASU Reasons for low efficiency I Turbine Inlet Temperature (TIT) is reduced compared to the reference case leading to increased efficiency penalty. I Transport limitation. I Need for seprate ASU for N2 production. I Improper integration! s s s s s s SINTEF Energy Research s s s s s s 18
  • 22. 100% Integration s s s s s s SINTEF Energy Research s s s s s s 19
  • 23. Figure 3: Process block diagram for OTM integrated IGCC plant with CO2 capture 100% Integration - Performance Table 1: Overall plant performance of OTM integrated IGCC plant with CO2 capture Coal flow rate 138.9 Tph Thermal energy of fuel (LHV) 969.7 MWth Thermal energy for coal drying 8.23 MWth Gas turbine output 280.5 MWe Steam turbine output 176.6 MWe Gross electric power output 457.1 MWe Total ancillary power consumption 92.1 MWe Net electric power output 365.0 MWe Net electric efficiency 37.3 % CO2 capture rate 90.9 % 5. Conclusions System considerations for integration of an oxygen transport membrane based air separation unit are presented. Arguments for selection of membrane operating mode and I Heat and mass GT is selected. detail. An integrated IGCC shows anand 100% airwith heating air integration are discussed in integration with integration removewithout sweep gas efficiency gain of The OTM OTM losses associated side fuel to0.7% points over the reference IGCC plant with cryogenic ASU. However, the trade-off 900°C and transport limitation. is the tighter integration and reduced flexibility of the plant. Also, the number of plant I This also required a separate to the OTM based ASU for O2 production a components is increased as in addition cryogenic ASU, but with smaller cryogenic ASU is required for N2 production. capacity. I Complete integration could lead to start-up/shut-down and availability issues. s s s s s s SINTEF Energy Research s s s s s s 20
  • 24. Summary I An overview of the considerations when integrating an oxygen transport membrane as an ASU in an IGCC is presented. I An OTM with out sweep gas and 100% air integration is shown to have 0.7% points higher efficiency than the reference case cycle. I The trade-off is tighter integration - reduced flexibility. I Other cycles, e.g. combination of pre- and oxy-combustion concepts, are being evaluated. s s s s s s SINTEF Energy Research s s s s s s 21
  • 25. Acknowledgement The research leading to these results has received funding from the European Community’s Seventh Framework Programme (FP7/2007-2013) under grant agreement nˇ 211971 (The DECARBit r project). s s s s s s SINTEF Energy Research s s s s s s 22