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    Last Stage Performance Considerations in Low-Pressure Turbines of Power Plants: A Case Study

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 002::page 23004
    Author:
    Komandur S. Sunder Raj
    DOI: 10.1115/1.2795781
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The last stage blades (LSBs) of low-pressure (LP) turbine power plants have been historically specified and designed on the basis of optimization studies by matching the turbine to the condenser/cooling system for a specified unit rating. LSB sizes for U.S. nuclear applications currently range from 38 in. to 52 in. for unit ratings of 600 MWe to 1200 MWe. LP turbine arrangements usually consist of two or three double-flow sections in parallel. Last stage end loadings (last stage mass flow divided by the last stage annulus area) vary from approximately 8000lb∕hsqftto14,000lb∕hsqft, with corresponding unit loadings (electrical output in megawatts divided by last stage annulus area) of 1.1 MWe∕sqftto2.1MWe∕sqft. Several power plants have been upgrading/replacing their LP turbines. Considerations include efficiency, reliability, power uprates, operating license renewals (nuclear), aging, inspection, and maintenance. In some cases, LP turbine rotors are being replaced with new rotors, blading, and steam path. Others are replacing LP turbines with new and advanced designs incorporating improved technology, better materials, optimized steam paths, more efficient blading, longer LSB sizes, redesigned exhaust hoods, etc. Unlike the other stages in the LP turbine, the last stage performance is affected by both the upstream (load) and downstream (condenser) conditions. While the LP turbines are being upgraded or replaced, no major modifications or upgrades are being made to the condensers. To address vibration effects due to increased flows and velocities from power uprates, the condenser tubes may be staked. Circulating water pumps may or may not be upgraded depending upon the particular application. Consequently, while improvements in LP turbines lead to more efficient utilization of the available energy and higher output, the last stage performance may be out of synchronization with the existing condenser/cooling system. Undersized or oversized LSB sizes in relation to the unit rating and end loading may result in less than optimum performance depending upon the design and operating range of the condenser/cooling system. This paper examines the various factors that affect last stage performance of LP turbines. Using a case study, it discusses the relationships between the last stage, the unit rating, the end loading, and the operating range of the condenser/cooling system. It examines different last stage exhaust loss curves and provides recommendations for selection of LSB sizes for optimum performance.
    keyword(s): Pressure , Flow (Dynamics) , Power stations , Turbines , Annulus , Blades , Condensers (steam plant) , Exhaust systems , Power uprate , Steam , Stress , Design AND Cooling systems ,
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      Last Stage Performance Considerations in Low-Pressure Turbines of Power Plants: A Case Study

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    https://yetl.yabesh.ir/yetl1/handle/yetl/137994
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorKomandur S. Sunder Raj
    date accessioned2017-05-09T00:28:03Z
    date available2017-05-09T00:28:03Z
    date copyrightMarch, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-27001#023004_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137994
    description abstractThe last stage blades (LSBs) of low-pressure (LP) turbine power plants have been historically specified and designed on the basis of optimization studies by matching the turbine to the condenser/cooling system for a specified unit rating. LSB sizes for U.S. nuclear applications currently range from 38 in. to 52 in. for unit ratings of 600 MWe to 1200 MWe. LP turbine arrangements usually consist of two or three double-flow sections in parallel. Last stage end loadings (last stage mass flow divided by the last stage annulus area) vary from approximately 8000lb∕hsqftto14,000lb∕hsqft, with corresponding unit loadings (electrical output in megawatts divided by last stage annulus area) of 1.1 MWe∕sqftto2.1MWe∕sqft. Several power plants have been upgrading/replacing their LP turbines. Considerations include efficiency, reliability, power uprates, operating license renewals (nuclear), aging, inspection, and maintenance. In some cases, LP turbine rotors are being replaced with new rotors, blading, and steam path. Others are replacing LP turbines with new and advanced designs incorporating improved technology, better materials, optimized steam paths, more efficient blading, longer LSB sizes, redesigned exhaust hoods, etc. Unlike the other stages in the LP turbine, the last stage performance is affected by both the upstream (load) and downstream (condenser) conditions. While the LP turbines are being upgraded or replaced, no major modifications or upgrades are being made to the condensers. To address vibration effects due to increased flows and velocities from power uprates, the condenser tubes may be staked. Circulating water pumps may or may not be upgraded depending upon the particular application. Consequently, while improvements in LP turbines lead to more efficient utilization of the available energy and higher output, the last stage performance may be out of synchronization with the existing condenser/cooling system. Undersized or oversized LSB sizes in relation to the unit rating and end loading may result in less than optimum performance depending upon the design and operating range of the condenser/cooling system. This paper examines the various factors that affect last stage performance of LP turbines. Using a case study, it discusses the relationships between the last stage, the unit rating, the end loading, and the operating range of the condenser/cooling system. It examines different last stage exhaust loss curves and provides recommendations for selection of LSB sizes for optimum performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLast Stage Performance Considerations in Low-Pressure Turbines of Power Plants: A Case Study
    typeJournal Paper
    journal volume130
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2795781
    journal fristpage23004
    identifier eissn0742-4795
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsPower stations
    keywordsTurbines
    keywordsAnnulus
    keywordsBlades
    keywordsCondensers (steam plant)
    keywordsExhaust systems
    keywordsPower uprate
    keywordsSteam
    keywordsStress
    keywordsDesign AND Cooling systems
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 002
    contenttypeFulltext
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