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US20110146276A1 - Method of starting a steam turbine - Google Patents

Method of starting a steam turbine
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Publication number
US20110146276A1
US20110146276A1US12/646,201US64620109AUS2011146276A1US 20110146276 A1US20110146276 A1US 20110146276A1US 64620109 AUS64620109 AUS 64620109AUS 2011146276 A1US2011146276 A1US 2011146276A1
Authority
US
United States
Prior art keywords
steam
section
pressure
steam turbine
upstream
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/646,201
Inventor
Dileep Sathyanarayana
Steven Dipalma
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric CofiledCriticalGeneral Electric Co
Priority to US12/646,201priorityCriticalpatent/US20110146276A1/en
Assigned to GENERAL ELECTRIC COMPANYreassignmentGENERAL ELECTRIC COMPANYASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS).Assignors: DIPALMA, STEVEN, SATHYANARAYANA, DILEEP
Priority to GB1020966Aprioritypatent/GB2476553A/en
Priority to JP2010278690Aprioritypatent/JP2011132951A/en
Priority to RU2010152280/06Aprioritypatent/RU2010152280A/en
Priority to DE102010061449Aprioritypatent/DE102010061449A1/en
Publication of US20110146276A1publicationCriticalpatent/US20110146276A1/en
Abandonedlegal-statusCriticalCurrent

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Abstract

The present invention has the technical effect of reducing the start-up time associated with starting a steam turbine. Embodiments of the present invention provide a new methodology for reducing the steam-to-metal temperature mismatch present during the start-up of a steam turbine. Essentially, embodiments of the invention may raise the pressure of the steam upstream of an admission valve associated with a High Pressure (HP) section of a steam turbine. The initial high pressure of the steam may reduce the enthalpy of steam, reducing temperature of the steam admitted to the HP section.

Description

Claims (20)

10. A method of starting a powerplant comprising a steam turbine, the method comprising:
providing a steam turbine configured for converting steam to a mechanical torque; wherein the steam turbine comprises an HP section and a bypass system;
determining whether a cold start of the steam turbine is requested;
increasing a pressure the steam upstream of an admission valve to a pressure matching range, wherein the admission valve is located upstream of the HP section;
determining whether the steam upstream of the admission valve is within the pressure matching range;
initiating a start-up of the steam turbine if a start-up permissive is satisfied; and
modulating the admission valve such that allow the steam flows into the HP section;
wherein the step of increasing the pressure of the steam decreases a temperature of the steam before steams flows into the HP section.
18. A system configured for starting a steam turbine, the system comprising:
a steam turbine configured for converting steam to a mechanical torque;
wherein the steam turbine comprises an HP section; and
a control system configured for starting the steam turbine, wherein the control system performs the steps of:
determining whether a cold start of the steam turbine is requested;
increasing a pressure the steam upstream of an admission valve to a pressure matching range, before the steam flows into the HP section, wherein an admission valve is located upstream of the HP section;
determining whether the steam upstream of the admission valve is within the pressure matching range;
initiating a start-up of the steam turbine if a start-up permissive is satisfied; and
opening the admission valve to allow the steam to flow into the HP section;
wherein the step of increasing the pressure of the steam decreases a temperature of the steam prior to admission into the HP section.
US12/646,2012009-12-232009-12-23Method of starting a steam turbineAbandonedUS20110146276A1 (en)

Priority Applications (5)

Application NumberPriority DateFiling DateTitle
US12/646,201US20110146276A1 (en)2009-12-232009-12-23Method of starting a steam turbine
GB1020966AGB2476553A (en)2009-12-232010-12-10Steam turbine starting method
JP2010278690AJP2011132951A (en)2009-12-232010-12-15Method of starting steam turbine
RU2010152280/06ARU2010152280A (en)2009-12-232010-12-21 STEAM TURBINE STARTING METHOD
DE102010061449ADE102010061449A1 (en)2009-12-232010-12-21 Method for starting up a steam turbine

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
US12/646,201US20110146276A1 (en)2009-12-232009-12-23Method of starting a steam turbine

Publications (1)

Publication NumberPublication Date
US20110146276A1true US20110146276A1 (en)2011-06-23

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ID=43566990

Family Applications (1)

Application NumberTitlePriority DateFiling Date
US12/646,201AbandonedUS20110146276A1 (en)2009-12-232009-12-23Method of starting a steam turbine

Country Status (5)

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US (1)US20110146276A1 (en)
JP (1)JP2011132951A (en)
DE (1)DE102010061449A1 (en)
GB (1)GB2476553A (en)
RU (1)RU2010152280A (en)

Cited By (27)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US20120131917A1 (en)*2010-11-302012-05-31General Electric CompanyMethods and Systems for Loading a Steam Turbine
US20140047840A1 (en)*2012-08-172014-02-20General Electric CompanySteam flow control system
CN104169531A (en)*2012-03-292014-11-26阿尔斯通技术有限公司Method of operating turbine engine after flame off
US9664070B1 (en)2016-02-122017-05-30United Technologies CorporationBowed rotor prevention system
US10040577B2 (en)2016-02-122018-08-07United Technologies CorporationModified start sequence of a gas turbine engine
US10100679B2 (en)2015-08-282018-10-16General Electric CompanyControl system for managing steam turbine rotor stress and method of use
US10125691B2 (en)2016-02-122018-11-13United Technologies CorporationBowed rotor start using a variable position starter valve
US10125636B2 (en)2016-02-122018-11-13United Technologies CorporationBowed rotor prevention system using waste heat
US10174678B2 (en)2016-02-122019-01-08United Technologies CorporationBowed rotor start using direct temperature measurement
US10221774B2 (en)2016-07-212019-03-05United Technologies CorporationSpeed control during motoring of a gas turbine engine
US10358936B2 (en)2016-07-052019-07-23United Technologies CorporationBowed rotor sensor system
US10384791B2 (en)2016-07-212019-08-20United Technologies CorporationCross engine coordination during gas turbine engine motoring
US10436064B2 (en)2016-02-122019-10-08United Technologies CorporationBowed rotor start response damping system
US10443505B2 (en)2016-02-122019-10-15United Technologies CorporationBowed rotor start mitigation in a gas turbine engine
US10443507B2 (en)2016-02-122019-10-15United Technologies CorporationGas turbine engine bowed rotor avoidance system
US10443543B2 (en)2016-11-042019-10-15United Technologies CorporationHigh compressor build clearance reduction
US10508567B2 (en)2016-02-122019-12-17United Technologies CorporationAuxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10508601B2 (en)2016-02-122019-12-17United Technologies CorporationAuxiliary drive bowed rotor prevention system for a gas turbine engine
US10539079B2 (en)2016-02-122020-01-21United Technologies CorporationBowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10598047B2 (en)2016-02-292020-03-24United Technologies CorporationLow-power bowed rotor prevention system
US10618666B2 (en)2016-07-212020-04-14United Technologies CorporationPre-start motoring synchronization for multiple engines
US10633106B2 (en)2016-07-212020-04-28United Technologies CorporationAlternating starter use during multi-engine motoring
US10787933B2 (en)2016-06-202020-09-29Raytheon Technologies CorporationLow-power bowed rotor prevention and monitoring system
US10787968B2 (en)2016-09-302020-09-29Raytheon Technologies CorporationGas turbine engine motoring with starter air valve manual override
US10823079B2 (en)2016-11-292020-11-03Raytheon Technologies CorporationMetered orifice for motoring of a gas turbine engine
US11047257B2 (en)2016-07-212021-06-29Raytheon Technologies CorporationMulti-engine coordination during gas turbine engine motoring
US11428115B2 (en)*2020-09-252022-08-30General Electric CompanyControl of rotor stress within turbomachine during startup operation

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US9157406B2 (en)*2014-02-052015-10-13General Electric CompanySystems and methods for initializing a generator
US9988928B2 (en)*2016-05-172018-06-05Siemens Energy, Inc.Systems and methods for determining turbomachine engine safe start clearances following a shutdown of the turbomachine engine

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US4267458A (en)*1972-04-261981-05-12Westinghouse Electric Corp.System and method for starting, synchronizing and operating a steam turbine with digital computer control
US4448026A (en)*1981-09-251984-05-15Westinghouse Electric Corp.Turbine high pressure bypass pressure control system
US4589255A (en)*1984-10-251986-05-20Westinghouse Electric Corp.Adaptive temperature control system for the supply of steam to a steam turbine
US4598551A (en)*1985-10-251986-07-08General Electric CompanyApparatus and method for controlling steam turbine operating conditions during starting and loading
US5203160A (en)*1990-10-181993-04-20Kabushiki Kaisha ToshibaCombined generating plant and its start-up control device and start-up control method
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US20070113562A1 (en)*2005-11-182007-05-24General Electric CompanyMethods and apparatus for starting up combined cycle power systems

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US4267458A (en)*1972-04-261981-05-12Westinghouse Electric Corp.System and method for starting, synchronizing and operating a steam turbine with digital computer control
US4228359A (en)*1977-07-291980-10-14Hitachi, Ltd.Rotor-stress preestimating turbine control system
US4204258A (en)*1978-10-031980-05-20Westinghouse Electric Corp.Turbine acceleration governing system
US4448026A (en)*1981-09-251984-05-15Westinghouse Electric Corp.Turbine high pressure bypass pressure control system
US4589255A (en)*1984-10-251986-05-20Westinghouse Electric Corp.Adaptive temperature control system for the supply of steam to a steam turbine
US4598551A (en)*1985-10-251986-07-08General Electric CompanyApparatus and method for controlling steam turbine operating conditions during starting and loading
US5203160A (en)*1990-10-181993-04-20Kabushiki Kaisha ToshibaCombined generating plant and its start-up control device and start-up control method
US5435138A (en)*1994-02-141995-07-25Westinghouse Electric Corp.Reduction in turbine/boiler thermal stress during bypass operation
US20070113562A1 (en)*2005-11-182007-05-24General Electric CompanyMethods and apparatus for starting up combined cycle power systems

Cited By (38)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US8843240B2 (en)*2010-11-302014-09-23General Electric CompanyLoading a steam turbine based on flow and temperature ramping rates
US20120131917A1 (en)*2010-11-302012-05-31General Electric CompanyMethods and Systems for Loading a Steam Turbine
CN104169531A (en)*2012-03-292014-11-26阿尔斯通技术有限公司Method of operating turbine engine after flame off
US9963995B2 (en)2012-03-292018-05-08Ansaldo Energia Ip Uk LimitedMethod of operating a turbine engine after flame off
US20140047840A1 (en)*2012-08-172014-02-20General Electric CompanySteam flow control system
US8925319B2 (en)*2012-08-172015-01-06General Electric CompanySteam flow control system
US10100679B2 (en)2015-08-282018-10-16General Electric CompanyControl system for managing steam turbine rotor stress and method of use
US10443505B2 (en)2016-02-122019-10-15United Technologies CorporationBowed rotor start mitigation in a gas turbine engine
US10787277B2 (en)2016-02-122020-09-29Raytheon Technologies CorporationModified start sequence of a gas turbine engine
US10125691B2 (en)2016-02-122018-11-13United Technologies CorporationBowed rotor start using a variable position starter valve
US10125636B2 (en)2016-02-122018-11-13United Technologies CorporationBowed rotor prevention system using waste heat
US10174678B2 (en)2016-02-122019-01-08United Technologies CorporationBowed rotor start using direct temperature measurement
US11274604B2 (en)2016-02-122022-03-15Raytheon Technologies CorporationBowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10801371B2 (en)2016-02-122020-10-13Raytheon Technologies CoprorationBowed rotor prevention system
US10625881B2 (en)2016-02-122020-04-21United Technologies CorporationModified start sequence of a gas turbine engine
US10436064B2 (en)2016-02-122019-10-08United Technologies CorporationBowed rotor start response damping system
US9664070B1 (en)2016-02-122017-05-30United Technologies CorporationBowed rotor prevention system
US10443507B2 (en)2016-02-122019-10-15United Technologies CorporationGas turbine engine bowed rotor avoidance system
US10040577B2 (en)2016-02-122018-08-07United Technologies CorporationModified start sequence of a gas turbine engine
US10508567B2 (en)2016-02-122019-12-17United Technologies CorporationAuxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10508601B2 (en)2016-02-122019-12-17United Technologies CorporationAuxiliary drive bowed rotor prevention system for a gas turbine engine
US10539079B2 (en)2016-02-122020-01-21United Technologies CorporationBowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10598047B2 (en)2016-02-292020-03-24United Technologies CorporationLow-power bowed rotor prevention system
US10787933B2 (en)2016-06-202020-09-29Raytheon Technologies CorporationLow-power bowed rotor prevention and monitoring system
US10358936B2 (en)2016-07-052019-07-23United Technologies CorporationBowed rotor sensor system
US10618666B2 (en)2016-07-212020-04-14United Technologies CorporationPre-start motoring synchronization for multiple engines
US10633106B2 (en)2016-07-212020-04-28United Technologies CorporationAlternating starter use during multi-engine motoring
US11840968B2 (en)2016-07-212023-12-12Rtx CorporationMotoring synchronization for multiple engines
US11674411B2 (en)2016-07-212023-06-13Raytheon Technologies CorporationMulti-engine coordination during gas turbine engine motoring
US10384791B2 (en)2016-07-212019-08-20United Technologies CorporationCross engine coordination during gas turbine engine motoring
US11807378B2 (en)2016-07-212023-11-07Rtx CorporationAlternating starter use during multi-engine motoring
US11047257B2 (en)2016-07-212021-06-29Raytheon Technologies CorporationMulti-engine coordination during gas turbine engine motoring
US11142329B2 (en)2016-07-212021-10-12Raytheon Technologies CorporationPre-start motoring synchronization for multiple engines
US10221774B2 (en)2016-07-212019-03-05United Technologies CorporationSpeed control during motoring of a gas turbine engine
US10787968B2 (en)2016-09-302020-09-29Raytheon Technologies CorporationGas turbine engine motoring with starter air valve manual override
US10443543B2 (en)2016-11-042019-10-15United Technologies CorporationHigh compressor build clearance reduction
US10823079B2 (en)2016-11-292020-11-03Raytheon Technologies CorporationMetered orifice for motoring of a gas turbine engine
US11428115B2 (en)*2020-09-252022-08-30General Electric CompanyControl of rotor stress within turbomachine during startup operation

Also Published As

Publication numberPublication date
DE102010061449A1 (en)2011-06-30
GB201020966D0 (en)2011-01-26
GB2476553A (en)2011-06-29
RU2010152280A (en)2012-06-27
JP2011132951A (en)2011-07-07

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Legal Events

DateCodeTitleDescription
ASAssignment

Owner name:GENERAL ELECTRIC COMPANY, NEW YORK

Free format text:ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SATHYANARAYANA, DILEEP;DIPALMA, STEVEN;SIGNING DATES FROM 20091211 TO 20091215;REEL/FRAME:023695/0795

STCBInformation on status: application discontinuation

Free format text:ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION


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