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Performance
Performance
Monitoring
Monitoring
For Gas Turbines
For Gas Turbines




Introduction
Managing an asset requires numerous technologies designed to assess health. While
most gas turbines in the field are fitted with some type of mechanical condition mon-
itoring system (see companion article on page 48 in this issue of ORBIT), it is less
common to see the inclusion of thermodynamic performance monitoring systems.
However, performance monitoring is no less critical for those seeking to get the most
from their machinery and processes. As will be seen, the financial benefits for those
that employ performance monitoring are both consistent and compelling.
This article discusses the reasons for monitoring performance on both gas turbines
and the machines that they drive, the fundamentals of how a performance monitor-
ing system works, and the types of information the system can provide. It presents the
business case for monitoring performance along with several examples of how actual
customers are obtaining value from their performance monitoring systems. It also
describes the various performance monitoring solutions available from GE Energy,


Josef Petek                                 Patrick Hamilton, PE
Product Line Leader, Performance Software   Commercialization Manager, Performance Software
GE Energy                                   GE Energy
josef.petek@ge.com                          patrick.hamilton@ge.com
the applications that they target, and how they can be used individually or in
conjunction with one another as part of a larger System 1 implementation.
Gas Turbine Thermodynamics
Gas turbines convert fuel energy into mechanical power or – by connecting to
electric generators – electric power. The underlying thermodynamic cycle, known
as the Brayton Cycle, involves the compression of a gaseous medium (typically air),
the addition of fuel energy through combustion or heat exchange, and expansion
of the hot, compressed gas through a turbine to convert the thermal energy into
shaft power. In contrast to an ideal thermodynamic cycle, a real gas turbine cannot
perform these processes free of friction and losses. This results in the simplified
overall balance equation for a gas turbine as follows:

Shaft
Power    = Fuel –
           Energy
                         Power Required
                         for Compression          –   Exhaust
                                                      Energy     –    Mechanical
                                                                      Losses




                                                            [Vol.25   No.1   2005]   ORBIT   65
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MODERN GAS TURBINES                          MUST WORK AT PROCESS            CONDITIONS THAT PUSH                          THE

               MECHANICAL AND THERMAL            STRESS            OF GAS PATH COMPONENTS TO          THEIR LIMITS.


  The profitability of this process is directly related to the       pressure, the less mass flow that can be generated through
  difference between the cost of fuel and the value of the           the turbine. Humidity also plays a role. Higher specific
  machine’s output (e.g., electricity, if the turbine is driv-       humidity increases the specific volume of the inlet air
  ing an electric generator). However, operators have only           flow, so that the mass flow through the turbine is reduced
  limited (if any) control over their cost of fuel and the sell-     resulting in less power output and increased heat rate.
  ing price of the machine’s output. This leaves only the            At the turbine outlet, ambient conditions also play a
  efficiency of the machine’s conversion process (i.e., the          role. The higher the pressure (either exhausting into a
  consumption of fuel per unit of generated output) as               stack, or a heat recovery steam generator in combined
  something the operator can directly influence. The                 cycle plants) the less energy that can be converted to
  importance of maximizing efficiency is thus evident.               shaft power.
                                                                     Load is another consideration that affects performance.
  Factors Affecting Performance                                      Gas turbines are aerodynamically designed for optimal
  Gas turbines operate efficiently if the energy conversion          performance at base load levels. If the gas turbine is not
  process is operated at the following thermodynamically             operated at this load level, the flow triangles in the com-
  favorable conditions:                                              pressor and turbine expander stages will differ from
  1. high pressure and temperature at the turbine inlet;             design assumptions, and more energy will be dissipated.
  2. minimal losses during compression and expansion.                Other factors influencing gas turbine performance are
  While conversion losses can be minimized through opti-             the fuel heating value (the content of energy per mass
  mal aerodynamic design of the compressor and turbine               unit of fuel), and the injection of steam or water into the
  expander, the high pressures (ratios of 20:1 or greater)           combustors to boost power output and/or control NOx
  and turbine inlet temperatures (2500°F and above) desir-           emission levels.
  able for efficiency come at a price: reduced durability of
  the gas path components. Effectively, to achieve the ther-         Cause and Effect
  mal efficiencies delivered by modern gas turbines, they            So far, we have devoted quite a bit of this article to
  must work at process conditions that push the mechani-             explaining the complexity of gas turbine design and oper-
  cal and thermal stress of the materials used in the                ation. Why did we do this when our goal is to discuss gas
  machine’s gas path components to their limits. The tech-           turbine performance monitoring? The answer is that
  nologies developed to increase process efficiency while            assessing the efficiency of a gas turbine and its compo-
  mitigating the risk of parts failure include air or steam          nents requires a solid understanding of the factors that
  cooling, and the use of special materials such as high per-        can affect efficiency, and these are not always related to
  formance alloys, single-crystal materials, thermal barrier         equipment degradation. Indeed, changes in power out-
  coatings, and others. Adding to these complexities are             put and fuel consumption can have very ‘natural’ causes,
  the effects that ambient conditions and load have on the           and the effects can be as large – or larger – than those
  operating characteristics of gas turbines. This results in         arising from equipment degradation.
  considerable engineering challenges for those who design,          To illustrate this, Figure 1 shows the typical impact on
  manufacture, and refurbish today’s gas turbines.                   rated power and heat rate for a hypothetical 40 MW
  Ambient conditions affect a gas turbine at both the                industrial gas turbine that would be caused by changes
  compressor inlet and the turbine outlet. At the compres-           in inlet temperature, inlet pressure drop, part-load frac-
  sor inlet, the higher the temperature and the lower the            tion, and steam injection flow.




  66   ORBIT   [Vol.25     No.1   2005]
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                A                                 Inlet Temperature                                               B                         Inlet Pressure Drop

                      1.3                                                                                              1.02



                      1.2                                             Heat Rate Correction                             1.01

                                                                      Power Correction

                      1.1                                                                                                1
 Correction Factor




                                                                                                   Correction Factor
                                                                                                                                                                      Heat Rate Correction
                       1                                                                                               0.99
                                                                                                                                                                      Power Correction


                      0.9                                                                                              0.98



                      0.8                                                                                              0.97



                      0.7                                                                                              0.96



                      0.6                                                                                              0.95
                            0         20          40        60        80        100          120                              0     2         4        6          8            10            12

                                             Inlet Temperature (deg F)                                                            Excess Inlet Pressure Drop (inches of H2O)



                C                                Part Load Operation                                             D                            Steam Injection

                       1                                                                                                1.2


                     0.95
                                                                                                                       1.15

                     0.90
                                                                                                                        1.1
                     0.85
 Correction Factor




                                                                                                   Correction Factor




                                                                                                                                                                      Heat Rate Correction
                                                                                                                       1.05
                      0.8                                        Heat Rate Correction                                                                                 Power Correction

                     0.75                                                                                                1


                      0.7
                                                                                                                       0.95

                     0.65
                                                                                                                        0.9
                      0.6

                                                                                                                       0.85
                     0.55


                      0.5                                                                                               0.8
                            20   30         40         50   60   70        80       90       100                              0   10000     20000    30000      4000          5000           6000

                                           Load Fraction (% of Base Load)                                                                 Steam Injection Flow (lb/hr)




CHANGES IN POWER OUTPUT AND HEAT RATE FOR A 40 MW GAS TURBINE DUE TO A) INLET TEMPERATURE;
                                           B) INLET PRESSURE DROP; C) PARTIAL LOADING; AND, D) STEAM INJECTION FLOW. | FIG. 1




                                                                                                                                             [Vol.25       No.1       2005]         ORBIT           67
A P P L I C A T I O N S




IT IS   IMPORTANT             THAT THE SYSTEM BE ABLE TO         DIFFERENTIATE
BETWEEN “NATURAL” CAUSES                                  AND THOSE FROM ACTUAL

EQUIPMENT      PROBLEMS AND DEGRADATION.


Thus, changes can be due to both so-called “natural”            When combined with mechanical condition monitor-
causes (such as load and ambient temperature) as well as        ing, the ability to isolate the location of problems can
actual equipment degradation. Because the goal of a             be improved. For example, tip clearance and packing
performance monitoring system is to help operators and          leakage are clearly related to the rotor dynamics of the
performance engineers understand the cause/effect               turbomachinery, and can often show up as changes in
relationships when changes occur, it is important that          vibration. The combination of thermodynamic perform-
the system be able to differentiate between “natural”           ance monitoring and mechanical condition monitoring
causes and those from actual equipment problems and             (such as vibration) can thus allow better diagnostic capa-
degradation. This can only be determined by comparing           bilities for assessing the nature, severity, location, and
measured gas turbine performance against a model of             cause of machinery performance changes.
“expected” engine performance reflecting the impacts of
all “natural” causes. More details on how this is done are      Why Monitor Performance?
discussed later in this article.                                To answer this question, consider a simple, hypothetical
                                                                example:
Recoverable and
                                                                   # of machines: 1
Non-Recoverable Degradation
                                                                   Machine Type: 40 MW gas turbine
Another important distinction when monitoring                      Rated heat rate: 10,000 BTU/kWh
performance is the difference between recoverable and              Operating Mode: simple-cycle
non-recoverable degradation, which we define as follows:           Average load level: 80%
                                                                   Operating hours per year: 8,000
     Recoverable Degradation is the performance loss
     that can be recovered by operational procedures such       The correction factor for 80% part-load operation is
     as keeping the inlet and outlet pressures low, or          0.947 (see Figure 1-C). Corrected heat rate thus becomes
     online and offline water washing of the compressor.        approximately 10,600 BTU/kWh for the average load of
                                                                32 MW. Figure 2 shows the estimated potential savings
     Non-Recoverable Degradation is the perform-
                                                                in fuel costs for this hypothetical machine as a function
     ance loss that cannot be recovered without repair or       of relative improvement in efficiency for several different
     replacement of affected gas turbine components.            fuel price assumptions.
     Examples of non-recoverable degradation include:
                                                                Referring again to Figure 2, and assuming a fuel price of
     loss of surface finish on blades, increases in blade tip   $6 per MMBTU for the gas turbine in our example, a
     clearances, packing leakage of both the compressor         mere 0.5 % improvement in fuel efficiency can save as
     and turbine, and combustion system component               much as $ 70,000 per year.
     corrosion/erosion leading to flame instabilities or
     increased thermal stress on the subsequent turbine
                                                                       WHEN COMBINED WITH
     sections.
Limited instrumentation inside the engine generally                    MECHANICAL CONDITION
means that locating the actual stage where a significant
change in performance has occurred will be difficult or                MONITORING, THE ABILITY TO
impossible; however, the thermodynamic model will gen-                 ISOLATE THE LOCATION OF PROBLEMS
erally be able to flag a severe problem early enough to
prevent larger damage.                                                 CAN BE IMPROVED.


68   ORBIT   [Vol.25    No.1    2005]
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                                Projected Annual Fuel Cost Savings

  $250,000
                                                                                                         Projected
                           40 MW Rated Output                                                           Fuel Prices
                                                                                                      (USD/MMBTU)
                           10,000 BTU/kWh Rated Heat Rate
                           8,000 Operating Hours
  $200,000                                                                                                   $8.00
                           80% Average Load
                           32 MW Average Output
                           10,600 BTU/kWh Average Heat Rate                                                  $7.00

  $150,000
                                                                                                             $6.00



  $100,000                                                                                                   $5.00


   $70,000                                                                                                   $4.00

   $50,000




         $0
          0.1%      0.2%      0.3%     0.4%     0.5%     0.6%     0.7%    0.8%     0.9%     1.0%

                             Relative Improvement in Fuel Efficiency

        ANNUAL FUEL COST SAVINGS AS A FUNCTION OF EFFICIENCY IMPROVEMENTS AND FUEL PRICES FOR
                                                                   A 40 MW SIMPLE-CYCLE GAS TURBINE. | FIG. 2



Achieving the Savings
How are such savings actually accomplished in practice?         2. By improving plant output.
There are at least four ways, as summarized below:                 For production processes as well as capacity sales, a
1. By allowing optimal maintenance interval                        decline in power output due to degradation may
   planning for recoverable degradation.                           have even larger economic impacts than the costs of
    The rate at which a compressor fouls or an inlet               fuel, depending on the related product sales or power
    filter clogs is highly dependent on the site conditions        purchase agreements. This decrease in production
    as well as on current weather and climate. Moni-               may be worth as much or more than the additional
    toring the rate of degradation and scheduling/                 fuel. This means that performance improvements
    conducting maintenance procedures effectively, such            often have a compound effect, impacting not only
    as compressor washes or filter cleanings, will ensure          fuel costs favorably but by increasing plant output
    that the gas turbine operates most efficiently.                as well.



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                                                              Case History #1 –
                                                              Optimizing Fuel Costs
       THE   QUALITY           OF THE INCOMING

        MEASUREMENTS                     IS VERY              The operations team at a 1000 MW power plant
                                                              actively uses their EfficiencyMap ™ software to
                           IMPORTANT.
                                                              optimize daily plant operations. In addition to plant
                                                              optimization, the EfficiencyMap system is designed
                                                              to monitor the performance of the plant’s evapo-
                                                              rative coolers, gas turbines, heat recovery steam
3. By reducing unplanned outages.
                                                              generators (HRSG’s), steam turbines, condensers,
     In some cases, performance can degrade to the point
                                                              and cooling towers.
     that the engine trips or reaches operational limita-
     tions that prevent continued operation. A compre-        Equipment degradation must be accounted for in
     hensive performance monitoring system helps              order to effectively optimize the plant, which con-
     mitigate this risk, providing operators with the capa-   sists of two power blocks, each with two gas turbines.
     bility to detect engine problems in time, allowing       The software accounts for this degradation and
     an outage to be scheduled when economic and
                                                              advises the team on recommended changes to three
     production constraints have the smallest impact.
                                                              primary controllable parameters: gas turbine
4. By allowing more efficient outages.                        load, evaporative cooler operation, and duct burner
     Knowing in advance what needs to be maintained           fuel flow in the HRSG. In addition, the software
     or repaired during the next outage enables a mainte-     calculates the heat rate, heat consumption, and cost
     nance team to minimize the duration of the outage        savings associated with operational changes.
     by reducing the risk of “unpleasant surprises” when
     opening the machinery. Consider our earlier exam-        The EfficiencyMap system at this plant is configured
     ple of the single 40 MW gas turbine: one extra day       to provide Opportunity Cost which calculates the
     of outage will mean up to 24 hours x 32 MW = 768         potential cost savings at a given fuel price and current
     MWh of lost production. Assuming an electricity          operating conditions. In one recent scenario, the
     sales prices of 40 cents per kWh, this translates to     plant was generating approximately 900 MW with
     lost revenues exceeding $300,000 per day. If the         410 MW on Power Block 1 and 490 MW on Power
     gas turbine is used in a critical mechanical drive       Block 2. The online optimization results recom-
     application, such as with an unspared blower in a        mended that the HRSG duct burners in Power Block
     refinery, the downtime can even be even more costly
                                                              2 should be turned off while the gas turbine loads
     – sometimes, millions of dollars per day.
                                                              in Power Block 1 should be increased. The plant
The Importance of Good Data                                   engineer directed the operator to make the changes
                                                              recommended by the EfficiencyMap system. This
The performance monitoring system typically extracts
its required data from existing data sources in the plant,    allowed the plant to capture over 80% of the the-
such as the turbine control system, mechanical condi-         oretically possible savings at that particular combination
tion monitoring systems, and plant control systems.           of plant output and ambient conditions, which trans-
As described earlier, there are many “natural” causes for     lated to a nearly 1% fuel savings. These results were
performance changes that must be distinguished from           later validated by the plant engineer using the
actual mechanical degradation of the machinery.
                                                              measured and heat balance values for plant net
Deriving performance parameters from measurements
                                                              heat rate before and after the changes, further
in the turbine control system or plant control system
without correcting for ambient and load effects would         increasing the customer’s confidence in the system’s
produce practically useless information. Instead, a           value as an optimization tool suitable for making
performance monitoring system must be capable of not          real-time operating adjustments.



70   ORBIT   [Vol.25    No.1    2005]
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 Case History #2 –
 Optimizing When to Perform Maintenance

  The ethylene unit in a large refinery was known to have fouling problems on both the process compressor
  and its prime mover. This prompted the customer to purchase Bently PEFORMANCE™ software for the train.

  During a scheduled outage, the compressor was serviced and the performance was found to recover dramat-
  ically. The prime mover fouling, however, not only persisted, but continued to grow worse as detected by the
  software. Another outage was out of the question – the only practical remedy was an online wash. The software,
  along with our services organization, was drawn upon to help determine the optimal time to conduct a wash.

  Savings to the customer were three-fold. First, they were able to correct efficiency losses in the compressor,
  which translates directly to increased plant throughput and greater profits. Second, the customer would have
  reasonably assumed that maintenance conducted during the planned outage corrected the efficiency losses
  in both the prime mover and the compressor. But, because the software was able to conclusively demonstrate
  the prime mover was still experiencing problems, they were able to address this and avoid continued sub-
  stantial fuel waste. Third, our service personnel were able to recommend the ideal time to conduct an online
  wash, finding the time when fuel savings and increased plant throughput would optimally offset the costs of
  this maintenance.

  In the customer’s words, “dramatic improvements in production and efficiency” have been realized as a result
  of their investment in performance monitoring software.




only accepting the necessary data inputs, but of also           How is Performance Monitored?
containing the detailed thermodynamic models that               Basically, the procedure for performance monitoring
allow “correction” of the raw data for all relevant effects     consists of three steps:
of operation.
                                                                Step 1: Range and Reasonableness of Inputs
In some cases, the necessary data may not be available,
                                                                Incoming measured data that serve as inputs to the per-
or perhaps more commonly, the quality of the measure-
                                                                formance calculations are checked for validity, compared
ment may be insufficient for performance monitoring
                                                                to physical limits, and – if necessary – substituted with
purposes, necessitating the need for additional sensors.
                                                                reasonable default values in order to guarantee proper
The quality of the incoming measurements is very impor-
                                                                online operation of the systems.
tant. Because many performance calculations are derived
using mathematical relationships that involve exponents,        Step 2: Component Heat Balance
small inaccuracies in one measured variable can result in       A heat balance around the gas turbine produces addi-
very large inaccuracies or uncertainties in a derived result.   tional information on the conditions of the ingoing and
For this reason, a necessary part of any performance mon-       outgoing streams and also adds information on certain
itoring endeavor must be to review all data inputs for          parameters that cannot be measured directly. It is impor-
sufficiency during initial system installation and design,      tant to note that the heat balance calculation is not
and regularly thereafter to ensure that input quality is        designed to measure performance, but to create detailed
not degrading over time. Proper pre-processing and              information about the current operating point that is
range-checking of the data by the online system prior to        consistent with mass and energy balances around the
the performance analysis also helps to detect erroneous         equipment. If the monitoring system covers the entire
sensor readings. Failure to observe this will result in poor    plant, the redundancy of information between the indi-
accuracy and inconclusive information at best, or at            vidual equipment even allows reconciliation of plant
worst, false assumptions and forced outages due to per-         measurements and advisories regarding current sensor
formance problems that are not detected by the system.          conditions.


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IMPACT CALCULATIONS        HELP       THE OPERATOR OR PERFORMANCE ENGINEER

              TO   DECIDE       ON THE    URGENCY            OF MAINTENANCE      ACTIONS.

Step 3: Performance Analysis                                 Additional features that can be combined with the per-
Once a consistent set of data on the current operating       formance analysis include impact calculations which help
point has been generated, the performance analysis itself    personnel to decide on the urgency of maintenance
can be conducted, comparing current performance              actions. Impacts can be expressed in terms of additional
against expected performance calculated from detailed        cost per hour, or changes in overall plant heat rate or
equipment models based on design and test information.       power. If, for example, the gas turbine is exhausting into
In order to make performance data comparable over time,      a Heat Recovery Steam Generator (HRSG), the impact
the current performance degradation is corrected to ref-     of gas turbine degradation on the overall plant perform-
erence conditions, e.g. ISO or acceptance test conditions,   ance will differ from operation in simple-cycle mode,
so that it is easy for the operator or performance engi-     since part of the energy lost to the gas turbine exhaust
neer to evaluate trends of equipment performance.            can be recovered in the subsequent steam cycle.



Case History #3 –
Quantifying Maintenance Savings, Optimizing Load Sharing

  A 700MW combined cycle power plant in Asia uses EfficiencyMap™ software in conjunction with a contractual
  services agreement where our performance engineers regularly review data from the system and provide
  summary recommendations to the plant. The recommendations in these quarterly reports focus on operating
  and maintenance actions that the plant can take to optimize performance in light of current business condi-
  tions. They also quantify the results of operating and maintenance actions the plant took over the report’s
  time period.

  Two recent reports are particularly illustrative, highlighting the cost savings achieved through compressor
  offline washes and inlet filter replacements, allowing the plant to quantify the financial impact and make
  better decisions about optimal future maintenance intervals. In the first report, an offline water wash was
  performed on both GT1 and GT2. EfficiencyMap data showed a profit improvement of $1,100 per day on GT1
  and $1,700 per day on GT2 as a result of these washes. This was a combination of the additional revenue from
  increased power output and better fuel efficiency through reduced heat rate.

  In the second quarterly report, the inlet air filters were changed on both units and the EfficiencyMap data
  was able to quantify the financial impact, as with the offline water washes. In this case, GT1 saw a power output
  improvement of 1.6MW, translating to $1,200 in incremental revenue per day. GT2 saw an even better
  improvement of 1.9MW or $1,400 per day. The report also showed that the improvements resulting from
  filter replacement degraded more quickly in GT1 than in GT2, suggesting a more frequent maintenance interval
  for GT1 than GT2.

  Finally, the reports suggested that the plant begin using an integrated feature of the software: its online
  optimizer module, allowing them to perform more ideal load sharing. The reports showed that had the plant
  used this feature, they could have achieved an additional $16,000 per month in fuel savings over the previous
  six months – simply by more optimally distributing load between the two gas turbines. Based on these com-
  pelling numbers, the plant management emphasizes the use of this software module.




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Performance Monitoring
Solutions from GE Energy
GE Energy offers several complementary performance
                                                                                       THE   PERFORMANCE
monitoring products, able to deliver the functionality               MONITORING SYSTEMS                          IN THIS
discussed in this article. They can be used individually
or integrated with one another for both plant-wide                      ARTICLE HAVE BEEN        SPECIFICALLY
and machine-centric applications. They can also be
customized for specific application requirements. The
                                                                       DESIGNED             TO ADDRESS      ANY      GAS

following list is a brief summary of these offerings:                    TURBINE,    REGARDLESS               OF MAKE,
> EfficiencyMap™ is a comprehensive stand-alone
                                                                                        MODEL, OR MANUFACTURER.
online performance monitoring system that is designed
to cover the entire range of thermal power generation
equipment, whether gas turbine-based plants or coal-
fired steam plants. Designed for flexibility in end-to-end
monitoring of plant heat balance as well as the con-
stituent equipment in the plant’s thermodynamic cycle,
the system can be configured to address any type of power
generation process ranging from pure electricity genera-         their own calculation engine and performance data, but
tion to complex cogeneration such as district heat or            don’t need the added burden of developing their own
seawater desalination plants. EfficiencyMap uses the             display, database, communication interface, alarming,
System 1® platform for its embedded data historian func-         and other “shell” features of System 1 software. This
tions and is fully compatible with the Decision Support SM       approach works well for Original Equipment Manu-
module of System 1 software, allowing automated data             facturers, Engineering and Construction contractors,
analysis and “intelligent” alarm advisories that include         and others who want to offer a tailored performance
recommended corrective actions.                                  monitoring package to their customers while securely
                                                                 embedding the proprietary performance calculations and
> Bently PERFORMANCE™ focuses on individual
                                                                 algorithms unique to their designs.
machine performance, rather than end-to-end plant per-
formance, addressing gas and steam turbines, rotating            > GateCycle™ software is an offline modeling tool –
and reciprocating compressors, and pumps. It is designed         not an online monitoring system – and is used primarily
as a standard, fully integrated application package for the      by those who design new thermal power plants and
System 1 condition monitoring platform. Its wide vari-           modify existing plants. It provides heat balance model-
ety of equations of state and special calculation routines       ing and “what if” capabilities for studying the entire plant
for compressor modeling are particularly well-suited for         and the individual equipment components. However,
the mechanical drive applications found in the petro-            GateCycle software does play a role in our online sys-
chemical and chemical processing industries, including           tems – it is embedded as the calculation engine within
gas and oil pipeline booster stations. Capabilities for ana-     EfficiencyMap software.
lyzing Exhaust Gas Temperature (EGT) have recently               > Compressor Wash Advisor is an optional software
been added, allowing improved diagnostics on gas tur-            module that can be supplied with EfficiencyMap or
bine hot gas path components.                                    Bently PERFORMANCE software. The module utilizes
[Editor’s Note: For more information on EGT plot capabilities,   online performance information as well as manually
see the companion article on page 88.]                           entered user inputs on current prices and costs to esti-
> Machine Performance is a completely customiz-                  mate the optimal time to perform an offline compressor
able version of the Bently PERFORMANCE™ calcula-                 water wash. While an online water wash adds only minor
tion templates. It is intended for those who already have        costs to gas turbine operations, an offline water wash


                                                                                      [Vol.25     No.1   2005]   ORBIT     73
A P P L I C A T I O N S




(also called crank wash) requires a production interrup-       any gas turbine, regardless of make, model, or manu-
tion, and the cost of lost production incurred by this         facturer. Indeed, recent enhancements have extended
interruption must be added to the cost of detergent and        the applicability of the software as a platform upon which
labor required for the wash. However, these additional         any OEM can base a custom performance monitoring
costs are generally offset by the superior effectiveness of    solution, by securely embedding their own machine-
an offline wash compared with an online wash. The key          specific calculations and performance algorithms. These
is in determining the optimal time to conduct an offline       performance monitoring systems are today installed
wash. Utilizing the performance analysis results of the        on a wide variety of gas turbines, driven equipment, and
past operation period, the Compressor Wash Advisor             other prime movers from a broad range of machinery
extrapolates the current rate of fouling into the future       OEMs. This “OEM-neutral” posture remains at the core
and estimates the economically optimal time for the            of all condition monitoring software offered by
wash: the time at which the cost of fouled operation           GE Energy, whether used for mechanical or thermody-
exceeds the total cost of the water wash. With this infor-     namic assessment.
mation, the plant can effectively arrange for the most
practical time for the water wash (e.g., during low            Summary
demand periods). Other information provided by the             Performance monitoring constitutes a key practice to
performance monitoring system allows operators to opti-        ensure plant profitability, with considerable cost savings
mally combine the offline wash with additional mainte-         related to maintaining maximum fuel efficiency and
nance actions on inlet filters and other components.           availability. As shown in this article, gas turbine perform-
> Online Optimizer is an optional software module              ance is strongly affected by “natural” parameters such as
that calculates the optimal set points for gas turbine         ambient environmental and load conditions. As such,
load and other controllable parameters based on                only systems that use detailed thermodynamic models of
current performance of individual gas turbines. The            the gas turbine and its components are capable of cor-
module is compatible with both EfficiencyMap and               rectly separating these “natural” effects from actual equip-
Bently PERFORMANCE software. For example, plants               ment degradation.
with more than one gas turbine can use the Online              Correct performance information provides the plant with
Optimizer module to optimize load sharing between the          relevant, Actionable Information® on how to best man-
turbines, making the best out of differences in non-recov-     age recoverable and non-recoverable degradation. Such
erable degradation between multiple units. As every gas        information can help identify the cause and location of
turbine has its own specific rating and performance            overall performance degradation, quantify its impact on
degradation, it is clearly more profitable to distribute the   plant operating costs, and allow better optimization of
load between the equipment according to their current          plant equipment given the current level of degradation.
performance. Another application of the Online                 The performance monitoring solutions offered by
Optimizer module is in economically evaluating when            GE Energy enjoy widespread acceptance in both the
and how to use inlet chillers.                                 power generation and hydrocarbon processing indus-
                                                               tries, spanning many different machine types and
OEM Independence                                               manufacturers, and complementing GE’s mechanical
The performance monitoring systems and heat balance            condition monitoring solutions. For additional informa-
modeling software offered by GE Energy and described           tion, use the Reader Service Card in this issue of ORBIT,
in this article have been specifically designed to address     or send an e-mail to energy.optimization@ge.com.




74   ORBIT   [Vol.25    No.1   2005]

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Monitor gas turbine performance with real-time analytics

  • 1. Performance Performance Monitoring Monitoring For Gas Turbines For Gas Turbines Introduction Managing an asset requires numerous technologies designed to assess health. While most gas turbines in the field are fitted with some type of mechanical condition mon- itoring system (see companion article on page 48 in this issue of ORBIT), it is less common to see the inclusion of thermodynamic performance monitoring systems. However, performance monitoring is no less critical for those seeking to get the most from their machinery and processes. As will be seen, the financial benefits for those that employ performance monitoring are both consistent and compelling. This article discusses the reasons for monitoring performance on both gas turbines and the machines that they drive, the fundamentals of how a performance monitor- ing system works, and the types of information the system can provide. It presents the business case for monitoring performance along with several examples of how actual customers are obtaining value from their performance monitoring systems. It also describes the various performance monitoring solutions available from GE Energy, Josef Petek Patrick Hamilton, PE Product Line Leader, Performance Software Commercialization Manager, Performance Software GE Energy GE Energy josef.petek@ge.com patrick.hamilton@ge.com
  • 2. the applications that they target, and how they can be used individually or in conjunction with one another as part of a larger System 1 implementation. Gas Turbine Thermodynamics Gas turbines convert fuel energy into mechanical power or – by connecting to electric generators – electric power. The underlying thermodynamic cycle, known as the Brayton Cycle, involves the compression of a gaseous medium (typically air), the addition of fuel energy through combustion or heat exchange, and expansion of the hot, compressed gas through a turbine to convert the thermal energy into shaft power. In contrast to an ideal thermodynamic cycle, a real gas turbine cannot perform these processes free of friction and losses. This results in the simplified overall balance equation for a gas turbine as follows: Shaft Power = Fuel – Energy Power Required for Compression – Exhaust Energy – Mechanical Losses [Vol.25 No.1 2005] ORBIT 65
  • 3. A P P L I C A T I O N S MODERN GAS TURBINES MUST WORK AT PROCESS CONDITIONS THAT PUSH THE MECHANICAL AND THERMAL STRESS OF GAS PATH COMPONENTS TO THEIR LIMITS. The profitability of this process is directly related to the pressure, the less mass flow that can be generated through difference between the cost of fuel and the value of the the turbine. Humidity also plays a role. Higher specific machine’s output (e.g., electricity, if the turbine is driv- humidity increases the specific volume of the inlet air ing an electric generator). However, operators have only flow, so that the mass flow through the turbine is reduced limited (if any) control over their cost of fuel and the sell- resulting in less power output and increased heat rate. ing price of the machine’s output. This leaves only the At the turbine outlet, ambient conditions also play a efficiency of the machine’s conversion process (i.e., the role. The higher the pressure (either exhausting into a consumption of fuel per unit of generated output) as stack, or a heat recovery steam generator in combined something the operator can directly influence. The cycle plants) the less energy that can be converted to importance of maximizing efficiency is thus evident. shaft power. Load is another consideration that affects performance. Factors Affecting Performance Gas turbines are aerodynamically designed for optimal Gas turbines operate efficiently if the energy conversion performance at base load levels. If the gas turbine is not process is operated at the following thermodynamically operated at this load level, the flow triangles in the com- favorable conditions: pressor and turbine expander stages will differ from 1. high pressure and temperature at the turbine inlet; design assumptions, and more energy will be dissipated. 2. minimal losses during compression and expansion. Other factors influencing gas turbine performance are While conversion losses can be minimized through opti- the fuel heating value (the content of energy per mass mal aerodynamic design of the compressor and turbine unit of fuel), and the injection of steam or water into the expander, the high pressures (ratios of 20:1 or greater) combustors to boost power output and/or control NOx and turbine inlet temperatures (2500°F and above) desir- emission levels. able for efficiency come at a price: reduced durability of the gas path components. Effectively, to achieve the ther- Cause and Effect mal efficiencies delivered by modern gas turbines, they So far, we have devoted quite a bit of this article to must work at process conditions that push the mechani- explaining the complexity of gas turbine design and oper- cal and thermal stress of the materials used in the ation. Why did we do this when our goal is to discuss gas machine’s gas path components to their limits. The tech- turbine performance monitoring? The answer is that nologies developed to increase process efficiency while assessing the efficiency of a gas turbine and its compo- mitigating the risk of parts failure include air or steam nents requires a solid understanding of the factors that cooling, and the use of special materials such as high per- can affect efficiency, and these are not always related to formance alloys, single-crystal materials, thermal barrier equipment degradation. Indeed, changes in power out- coatings, and others. Adding to these complexities are put and fuel consumption can have very ‘natural’ causes, the effects that ambient conditions and load have on the and the effects can be as large – or larger – than those operating characteristics of gas turbines. This results in arising from equipment degradation. considerable engineering challenges for those who design, To illustrate this, Figure 1 shows the typical impact on manufacture, and refurbish today’s gas turbines. rated power and heat rate for a hypothetical 40 MW Ambient conditions affect a gas turbine at both the industrial gas turbine that would be caused by changes compressor inlet and the turbine outlet. At the compres- in inlet temperature, inlet pressure drop, part-load frac- sor inlet, the higher the temperature and the lower the tion, and steam injection flow. 66 ORBIT [Vol.25 No.1 2005]
  • 4. A P P L I C A T I O N S A Inlet Temperature B Inlet Pressure Drop 1.3 1.02 1.2 Heat Rate Correction 1.01 Power Correction 1.1 1 Correction Factor Correction Factor Heat Rate Correction 1 0.99 Power Correction 0.9 0.98 0.8 0.97 0.7 0.96 0.6 0.95 0 20 40 60 80 100 120 0 2 4 6 8 10 12 Inlet Temperature (deg F) Excess Inlet Pressure Drop (inches of H2O) C Part Load Operation D Steam Injection 1 1.2 0.95 1.15 0.90 1.1 0.85 Correction Factor Correction Factor Heat Rate Correction 1.05 0.8 Heat Rate Correction Power Correction 0.75 1 0.7 0.95 0.65 0.9 0.6 0.85 0.55 0.5 0.8 20 30 40 50 60 70 80 90 100 0 10000 20000 30000 4000 5000 6000 Load Fraction (% of Base Load) Steam Injection Flow (lb/hr) CHANGES IN POWER OUTPUT AND HEAT RATE FOR A 40 MW GAS TURBINE DUE TO A) INLET TEMPERATURE; B) INLET PRESSURE DROP; C) PARTIAL LOADING; AND, D) STEAM INJECTION FLOW. | FIG. 1 [Vol.25 No.1 2005] ORBIT 67
  • 5. A P P L I C A T I O N S IT IS IMPORTANT THAT THE SYSTEM BE ABLE TO DIFFERENTIATE BETWEEN “NATURAL” CAUSES AND THOSE FROM ACTUAL EQUIPMENT PROBLEMS AND DEGRADATION. Thus, changes can be due to both so-called “natural” When combined with mechanical condition monitor- causes (such as load and ambient temperature) as well as ing, the ability to isolate the location of problems can actual equipment degradation. Because the goal of a be improved. For example, tip clearance and packing performance monitoring system is to help operators and leakage are clearly related to the rotor dynamics of the performance engineers understand the cause/effect turbomachinery, and can often show up as changes in relationships when changes occur, it is important that vibration. The combination of thermodynamic perform- the system be able to differentiate between “natural” ance monitoring and mechanical condition monitoring causes and those from actual equipment problems and (such as vibration) can thus allow better diagnostic capa- degradation. This can only be determined by comparing bilities for assessing the nature, severity, location, and measured gas turbine performance against a model of cause of machinery performance changes. “expected” engine performance reflecting the impacts of all “natural” causes. More details on how this is done are Why Monitor Performance? discussed later in this article. To answer this question, consider a simple, hypothetical example: Recoverable and # of machines: 1 Non-Recoverable Degradation Machine Type: 40 MW gas turbine Another important distinction when monitoring Rated heat rate: 10,000 BTU/kWh performance is the difference between recoverable and Operating Mode: simple-cycle non-recoverable degradation, which we define as follows: Average load level: 80% Operating hours per year: 8,000 Recoverable Degradation is the performance loss that can be recovered by operational procedures such The correction factor for 80% part-load operation is as keeping the inlet and outlet pressures low, or 0.947 (see Figure 1-C). Corrected heat rate thus becomes online and offline water washing of the compressor. approximately 10,600 BTU/kWh for the average load of 32 MW. Figure 2 shows the estimated potential savings Non-Recoverable Degradation is the perform- in fuel costs for this hypothetical machine as a function ance loss that cannot be recovered without repair or of relative improvement in efficiency for several different replacement of affected gas turbine components. fuel price assumptions. Examples of non-recoverable degradation include: Referring again to Figure 2, and assuming a fuel price of loss of surface finish on blades, increases in blade tip $6 per MMBTU for the gas turbine in our example, a clearances, packing leakage of both the compressor mere 0.5 % improvement in fuel efficiency can save as and turbine, and combustion system component much as $ 70,000 per year. corrosion/erosion leading to flame instabilities or increased thermal stress on the subsequent turbine WHEN COMBINED WITH sections. Limited instrumentation inside the engine generally MECHANICAL CONDITION means that locating the actual stage where a significant change in performance has occurred will be difficult or MONITORING, THE ABILITY TO impossible; however, the thermodynamic model will gen- ISOLATE THE LOCATION OF PROBLEMS erally be able to flag a severe problem early enough to prevent larger damage. CAN BE IMPROVED. 68 ORBIT [Vol.25 No.1 2005]
  • 6. A P P L I C A T I O N S Projected Annual Fuel Cost Savings $250,000 Projected 40 MW Rated Output Fuel Prices (USD/MMBTU) 10,000 BTU/kWh Rated Heat Rate 8,000 Operating Hours $200,000 $8.00 80% Average Load 32 MW Average Output 10,600 BTU/kWh Average Heat Rate $7.00 $150,000 $6.00 $100,000 $5.00 $70,000 $4.00 $50,000 $0 0.1% 0.2% 0.3% 0.4% 0.5% 0.6% 0.7% 0.8% 0.9% 1.0% Relative Improvement in Fuel Efficiency ANNUAL FUEL COST SAVINGS AS A FUNCTION OF EFFICIENCY IMPROVEMENTS AND FUEL PRICES FOR A 40 MW SIMPLE-CYCLE GAS TURBINE. | FIG. 2 Achieving the Savings How are such savings actually accomplished in practice? 2. By improving plant output. There are at least four ways, as summarized below: For production processes as well as capacity sales, a 1. By allowing optimal maintenance interval decline in power output due to degradation may planning for recoverable degradation. have even larger economic impacts than the costs of The rate at which a compressor fouls or an inlet fuel, depending on the related product sales or power filter clogs is highly dependent on the site conditions purchase agreements. This decrease in production as well as on current weather and climate. Moni- may be worth as much or more than the additional toring the rate of degradation and scheduling/ fuel. This means that performance improvements conducting maintenance procedures effectively, such often have a compound effect, impacting not only as compressor washes or filter cleanings, will ensure fuel costs favorably but by increasing plant output that the gas turbine operates most efficiently. as well. [Vol.25 No.1 2005] ORBIT 69
  • 7. A P P L I C A T I O N S Case History #1 – Optimizing Fuel Costs THE QUALITY OF THE INCOMING MEASUREMENTS IS VERY The operations team at a 1000 MW power plant actively uses their EfficiencyMap ™ software to IMPORTANT. optimize daily plant operations. In addition to plant optimization, the EfficiencyMap system is designed to monitor the performance of the plant’s evapo- rative coolers, gas turbines, heat recovery steam 3. By reducing unplanned outages. generators (HRSG’s), steam turbines, condensers, In some cases, performance can degrade to the point and cooling towers. that the engine trips or reaches operational limita- tions that prevent continued operation. A compre- Equipment degradation must be accounted for in hensive performance monitoring system helps order to effectively optimize the plant, which con- mitigate this risk, providing operators with the capa- sists of two power blocks, each with two gas turbines. bility to detect engine problems in time, allowing The software accounts for this degradation and an outage to be scheduled when economic and advises the team on recommended changes to three production constraints have the smallest impact. primary controllable parameters: gas turbine 4. By allowing more efficient outages. load, evaporative cooler operation, and duct burner Knowing in advance what needs to be maintained fuel flow in the HRSG. In addition, the software or repaired during the next outage enables a mainte- calculates the heat rate, heat consumption, and cost nance team to minimize the duration of the outage savings associated with operational changes. by reducing the risk of “unpleasant surprises” when opening the machinery. Consider our earlier exam- The EfficiencyMap system at this plant is configured ple of the single 40 MW gas turbine: one extra day to provide Opportunity Cost which calculates the of outage will mean up to 24 hours x 32 MW = 768 potential cost savings at a given fuel price and current MWh of lost production. Assuming an electricity operating conditions. In one recent scenario, the sales prices of 40 cents per kWh, this translates to plant was generating approximately 900 MW with lost revenues exceeding $300,000 per day. If the 410 MW on Power Block 1 and 490 MW on Power gas turbine is used in a critical mechanical drive Block 2. The online optimization results recom- application, such as with an unspared blower in a mended that the HRSG duct burners in Power Block refinery, the downtime can even be even more costly 2 should be turned off while the gas turbine loads – sometimes, millions of dollars per day. in Power Block 1 should be increased. The plant The Importance of Good Data engineer directed the operator to make the changes recommended by the EfficiencyMap system. This The performance monitoring system typically extracts its required data from existing data sources in the plant, allowed the plant to capture over 80% of the the- such as the turbine control system, mechanical condi- oretically possible savings at that particular combination tion monitoring systems, and plant control systems. of plant output and ambient conditions, which trans- As described earlier, there are many “natural” causes for lated to a nearly 1% fuel savings. These results were performance changes that must be distinguished from later validated by the plant engineer using the actual mechanical degradation of the machinery. measured and heat balance values for plant net Deriving performance parameters from measurements heat rate before and after the changes, further in the turbine control system or plant control system without correcting for ambient and load effects would increasing the customer’s confidence in the system’s produce practically useless information. Instead, a value as an optimization tool suitable for making performance monitoring system must be capable of not real-time operating adjustments. 70 ORBIT [Vol.25 No.1 2005]
  • 8. A P P L I C A T I O N S Case History #2 – Optimizing When to Perform Maintenance The ethylene unit in a large refinery was known to have fouling problems on both the process compressor and its prime mover. This prompted the customer to purchase Bently PEFORMANCE™ software for the train. During a scheduled outage, the compressor was serviced and the performance was found to recover dramat- ically. The prime mover fouling, however, not only persisted, but continued to grow worse as detected by the software. Another outage was out of the question – the only practical remedy was an online wash. The software, along with our services organization, was drawn upon to help determine the optimal time to conduct a wash. Savings to the customer were three-fold. First, they were able to correct efficiency losses in the compressor, which translates directly to increased plant throughput and greater profits. Second, the customer would have reasonably assumed that maintenance conducted during the planned outage corrected the efficiency losses in both the prime mover and the compressor. But, because the software was able to conclusively demonstrate the prime mover was still experiencing problems, they were able to address this and avoid continued sub- stantial fuel waste. Third, our service personnel were able to recommend the ideal time to conduct an online wash, finding the time when fuel savings and increased plant throughput would optimally offset the costs of this maintenance. In the customer’s words, “dramatic improvements in production and efficiency” have been realized as a result of their investment in performance monitoring software. only accepting the necessary data inputs, but of also How is Performance Monitored? containing the detailed thermodynamic models that Basically, the procedure for performance monitoring allow “correction” of the raw data for all relevant effects consists of three steps: of operation. Step 1: Range and Reasonableness of Inputs In some cases, the necessary data may not be available, Incoming measured data that serve as inputs to the per- or perhaps more commonly, the quality of the measure- formance calculations are checked for validity, compared ment may be insufficient for performance monitoring to physical limits, and – if necessary – substituted with purposes, necessitating the need for additional sensors. reasonable default values in order to guarantee proper The quality of the incoming measurements is very impor- online operation of the systems. tant. Because many performance calculations are derived using mathematical relationships that involve exponents, Step 2: Component Heat Balance small inaccuracies in one measured variable can result in A heat balance around the gas turbine produces addi- very large inaccuracies or uncertainties in a derived result. tional information on the conditions of the ingoing and For this reason, a necessary part of any performance mon- outgoing streams and also adds information on certain itoring endeavor must be to review all data inputs for parameters that cannot be measured directly. It is impor- sufficiency during initial system installation and design, tant to note that the heat balance calculation is not and regularly thereafter to ensure that input quality is designed to measure performance, but to create detailed not degrading over time. Proper pre-processing and information about the current operating point that is range-checking of the data by the online system prior to consistent with mass and energy balances around the the performance analysis also helps to detect erroneous equipment. If the monitoring system covers the entire sensor readings. Failure to observe this will result in poor plant, the redundancy of information between the indi- accuracy and inconclusive information at best, or at vidual equipment even allows reconciliation of plant worst, false assumptions and forced outages due to per- measurements and advisories regarding current sensor formance problems that are not detected by the system. conditions. [Vol.25 No.1 2005] ORBIT 71
  • 9. A P P L I C A T I O N S IMPACT CALCULATIONS HELP THE OPERATOR OR PERFORMANCE ENGINEER TO DECIDE ON THE URGENCY OF MAINTENANCE ACTIONS. Step 3: Performance Analysis Additional features that can be combined with the per- Once a consistent set of data on the current operating formance analysis include impact calculations which help point has been generated, the performance analysis itself personnel to decide on the urgency of maintenance can be conducted, comparing current performance actions. Impacts can be expressed in terms of additional against expected performance calculated from detailed cost per hour, or changes in overall plant heat rate or equipment models based on design and test information. power. If, for example, the gas turbine is exhausting into In order to make performance data comparable over time, a Heat Recovery Steam Generator (HRSG), the impact the current performance degradation is corrected to ref- of gas turbine degradation on the overall plant perform- erence conditions, e.g. ISO or acceptance test conditions, ance will differ from operation in simple-cycle mode, so that it is easy for the operator or performance engi- since part of the energy lost to the gas turbine exhaust neer to evaluate trends of equipment performance. can be recovered in the subsequent steam cycle. Case History #3 – Quantifying Maintenance Savings, Optimizing Load Sharing A 700MW combined cycle power plant in Asia uses EfficiencyMap™ software in conjunction with a contractual services agreement where our performance engineers regularly review data from the system and provide summary recommendations to the plant. The recommendations in these quarterly reports focus on operating and maintenance actions that the plant can take to optimize performance in light of current business condi- tions. They also quantify the results of operating and maintenance actions the plant took over the report’s time period. Two recent reports are particularly illustrative, highlighting the cost savings achieved through compressor offline washes and inlet filter replacements, allowing the plant to quantify the financial impact and make better decisions about optimal future maintenance intervals. In the first report, an offline water wash was performed on both GT1 and GT2. EfficiencyMap data showed a profit improvement of $1,100 per day on GT1 and $1,700 per day on GT2 as a result of these washes. This was a combination of the additional revenue from increased power output and better fuel efficiency through reduced heat rate. In the second quarterly report, the inlet air filters were changed on both units and the EfficiencyMap data was able to quantify the financial impact, as with the offline water washes. In this case, GT1 saw a power output improvement of 1.6MW, translating to $1,200 in incremental revenue per day. GT2 saw an even better improvement of 1.9MW or $1,400 per day. The report also showed that the improvements resulting from filter replacement degraded more quickly in GT1 than in GT2, suggesting a more frequent maintenance interval for GT1 than GT2. Finally, the reports suggested that the plant begin using an integrated feature of the software: its online optimizer module, allowing them to perform more ideal load sharing. The reports showed that had the plant used this feature, they could have achieved an additional $16,000 per month in fuel savings over the previous six months – simply by more optimally distributing load between the two gas turbines. Based on these com- pelling numbers, the plant management emphasizes the use of this software module. 72 ORBIT [Vol.25 No.1 2005]
  • 10. A P P L I C A T I O N S Performance Monitoring Solutions from GE Energy GE Energy offers several complementary performance THE PERFORMANCE monitoring products, able to deliver the functionality MONITORING SYSTEMS IN THIS discussed in this article. They can be used individually or integrated with one another for both plant-wide ARTICLE HAVE BEEN SPECIFICALLY and machine-centric applications. They can also be customized for specific application requirements. The DESIGNED TO ADDRESS ANY GAS following list is a brief summary of these offerings: TURBINE, REGARDLESS OF MAKE, > EfficiencyMap™ is a comprehensive stand-alone MODEL, OR MANUFACTURER. online performance monitoring system that is designed to cover the entire range of thermal power generation equipment, whether gas turbine-based plants or coal- fired steam plants. Designed for flexibility in end-to-end monitoring of plant heat balance as well as the con- stituent equipment in the plant’s thermodynamic cycle, the system can be configured to address any type of power generation process ranging from pure electricity genera- their own calculation engine and performance data, but tion to complex cogeneration such as district heat or don’t need the added burden of developing their own seawater desalination plants. EfficiencyMap uses the display, database, communication interface, alarming, System 1® platform for its embedded data historian func- and other “shell” features of System 1 software. This tions and is fully compatible with the Decision Support SM approach works well for Original Equipment Manu- module of System 1 software, allowing automated data facturers, Engineering and Construction contractors, analysis and “intelligent” alarm advisories that include and others who want to offer a tailored performance recommended corrective actions. monitoring package to their customers while securely embedding the proprietary performance calculations and > Bently PERFORMANCE™ focuses on individual algorithms unique to their designs. machine performance, rather than end-to-end plant per- formance, addressing gas and steam turbines, rotating > GateCycle™ software is an offline modeling tool – and reciprocating compressors, and pumps. It is designed not an online monitoring system – and is used primarily as a standard, fully integrated application package for the by those who design new thermal power plants and System 1 condition monitoring platform. Its wide vari- modify existing plants. It provides heat balance model- ety of equations of state and special calculation routines ing and “what if” capabilities for studying the entire plant for compressor modeling are particularly well-suited for and the individual equipment components. However, the mechanical drive applications found in the petro- GateCycle software does play a role in our online sys- chemical and chemical processing industries, including tems – it is embedded as the calculation engine within gas and oil pipeline booster stations. Capabilities for ana- EfficiencyMap software. lyzing Exhaust Gas Temperature (EGT) have recently > Compressor Wash Advisor is an optional software been added, allowing improved diagnostics on gas tur- module that can be supplied with EfficiencyMap or bine hot gas path components. Bently PERFORMANCE software. The module utilizes [Editor’s Note: For more information on EGT plot capabilities, online performance information as well as manually see the companion article on page 88.] entered user inputs on current prices and costs to esti- > Machine Performance is a completely customiz- mate the optimal time to perform an offline compressor able version of the Bently PERFORMANCE™ calcula- water wash. While an online water wash adds only minor tion templates. It is intended for those who already have costs to gas turbine operations, an offline water wash [Vol.25 No.1 2005] ORBIT 73
  • 11. A P P L I C A T I O N S (also called crank wash) requires a production interrup- any gas turbine, regardless of make, model, or manu- tion, and the cost of lost production incurred by this facturer. Indeed, recent enhancements have extended interruption must be added to the cost of detergent and the applicability of the software as a platform upon which labor required for the wash. However, these additional any OEM can base a custom performance monitoring costs are generally offset by the superior effectiveness of solution, by securely embedding their own machine- an offline wash compared with an online wash. The key specific calculations and performance algorithms. These is in determining the optimal time to conduct an offline performance monitoring systems are today installed wash. Utilizing the performance analysis results of the on a wide variety of gas turbines, driven equipment, and past operation period, the Compressor Wash Advisor other prime movers from a broad range of machinery extrapolates the current rate of fouling into the future OEMs. This “OEM-neutral” posture remains at the core and estimates the economically optimal time for the of all condition monitoring software offered by wash: the time at which the cost of fouled operation GE Energy, whether used for mechanical or thermody- exceeds the total cost of the water wash. With this infor- namic assessment. mation, the plant can effectively arrange for the most practical time for the water wash (e.g., during low Summary demand periods). Other information provided by the Performance monitoring constitutes a key practice to performance monitoring system allows operators to opti- ensure plant profitability, with considerable cost savings mally combine the offline wash with additional mainte- related to maintaining maximum fuel efficiency and nance actions on inlet filters and other components. availability. As shown in this article, gas turbine perform- > Online Optimizer is an optional software module ance is strongly affected by “natural” parameters such as that calculates the optimal set points for gas turbine ambient environmental and load conditions. As such, load and other controllable parameters based on only systems that use detailed thermodynamic models of current performance of individual gas turbines. The the gas turbine and its components are capable of cor- module is compatible with both EfficiencyMap and rectly separating these “natural” effects from actual equip- Bently PERFORMANCE software. For example, plants ment degradation. with more than one gas turbine can use the Online Correct performance information provides the plant with Optimizer module to optimize load sharing between the relevant, Actionable Information® on how to best man- turbines, making the best out of differences in non-recov- age recoverable and non-recoverable degradation. Such erable degradation between multiple units. As every gas information can help identify the cause and location of turbine has its own specific rating and performance overall performance degradation, quantify its impact on degradation, it is clearly more profitable to distribute the plant operating costs, and allow better optimization of load between the equipment according to their current plant equipment given the current level of degradation. performance. Another application of the Online The performance monitoring solutions offered by Optimizer module is in economically evaluating when GE Energy enjoy widespread acceptance in both the and how to use inlet chillers. power generation and hydrocarbon processing indus- tries, spanning many different machine types and OEM Independence manufacturers, and complementing GE’s mechanical The performance monitoring systems and heat balance condition monitoring solutions. For additional informa- modeling software offered by GE Energy and described tion, use the Reader Service Card in this issue of ORBIT, in this article have been specifically designed to address or send an e-mail to energy.optimization@ge.com. 74 ORBIT [Vol.25 No.1 2005]