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GB1374810A - Gas turbine electric power plant - Google Patents

Gas turbine electric power plant

Info

Publication number
GB1374810A
GB1374810A GB4879571A GB4879571A GB1374810A GB 1374810 A GB1374810 A GB 1374810A GB 4879571 A GB4879571 A GB 4879571A GB 4879571 A GB4879571 A GB 4879571A GB 1374810 A GB1374810 A GB 1374810A
Authority
GB
United Kingdom
Prior art keywords
program
turbine
power plant
gas turbine
inlet temperature
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.)
Expired
Application number
GB4879571A
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of GB1374810A publication Critical patent/GB1374810A/en
Expired legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
    • H02P9/08—Control of generator circuit during starting or stopping of driving means, e.g. for initiating excitation
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P2101/00—Special adaptation of control arrangements for generators
    • H02P2101/30—Special adaptation of control arrangements for generators for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Coating Of Shaped Articles Made Of Macromolecular Substances (AREA)
  • Treatments Of Macromolecular Shaped Articles (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

1374810 Automatic control of turbines WESTINGHOUSE ELECTRIC CORP 20 Oct 1971 [20 Oct 1970] 48795/71 Heading G3N [Also in Division F1] A gas turbine electric power plant is controlled so as to accelerate the turbine from a predetermined lower to an operating speed in a substantially fixed period of time, dependent on the selected gas turbine inlet temperature by controlling a fuel system in dependence on a selected representation of turbine speed for a constant turbine gas inlet temperature which is independent of the compressor air inlet temperature. A power plant 100 comprises a gas turbine 104 driving on A-C generator 102 through a reduction gear 106. The turbine is connected through ducting 112, 114 to inlet and exhaust silencers 108, 110. The plant is arranged in a sectional steel frame building not shown, and mounted on a bed-plate which is optionally extendable 116, to incorporate a master control station for up to three additional plant units. The power plant is controlled by a digital computer and system circuitry in a cabinet 118, having an operators panel 120 associated with a remote send/receive printer 122 and protective relay panel 124. An auxiliary bed-plate supports a starting diesel or induction motor 126 and a DC turning motor 154 for driving the turbine during non- operating periods to avoid thermally induced shaft bowing. Emergency power is provided from a battery 132 for the computer and emergency shut-down. The switchgear for the generator is provided on a pad 142. The programme system for the power plant comprises a sequencing program 600 and a control program 602 which determine computer inter facing and machine control. The program 600 also supervizes an automatic synchronization program 608 controlling generator voltage and turbine speed. Facilities are provided for operator control through a consol program 606, alarm printout through a program 610 co-ordinated with a thermocouple check program 616 and logging printout through program 618, 620.
GB4879571A 1970-10-20 1971-10-20 Gas turbine electric power plant Expired GB1374810A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8246970A 1970-10-20 1970-10-20

Publications (1)

Publication Number Publication Date
GB1374810A true GB1374810A (en) 1974-11-20

Family

ID=22171417

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4879571A Expired GB1374810A (en) 1970-10-20 1971-10-20 Gas turbine electric power plant

Country Status (4)

Country Link
JP (1) JPS5648685B1 (en)
BE (1) BE774180A (en)
CA (1) CA932397A (en)
GB (1) GB1374810A (en)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US10040577B2 (en) 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
US10358936B2 (en) 2016-07-05 2019-07-23 United Technologies Corporation Bowed rotor sensor system
US10384791B2 (en) 2016-07-21 2019-08-20 United Technologies Corporation Cross engine coordination during gas turbine engine motoring
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
US10508567B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10544717B2 (en) 2016-09-07 2020-01-28 Pratt & Whitney Canada Corp. Shared oil system arrangement for an engine component and a generator
US10598047B2 (en) 2016-02-29 2020-03-24 United Technologies Corporation Low-power bowed rotor prevention system
US10618666B2 (en) 2016-07-21 2020-04-14 United Technologies Corporation Pre-start motoring synchronization for multiple engines
US10633106B2 (en) 2016-07-21 2020-04-28 United Technologies Corporation Alternating starter use during multi-engine motoring
US10787933B2 (en) 2016-06-20 2020-09-29 Raytheon Technologies Corporation Low-power bowed rotor prevention and monitoring system
US10787968B2 (en) 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10823079B2 (en) 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine
US11047257B2 (en) 2016-07-21 2021-06-29 Raytheon Technologies Corporation Multi-engine coordination during gas turbine engine motoring

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5956085U (en) * 1982-10-08 1984-04-12 共栄レジン株式会社 Chuck ring for sharp pencil with chuck
CN114577267B (en) * 2022-03-07 2022-11-04 武汉新烽光电股份有限公司 Multi-parameter water quality hydrological monitor easy to install

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS456643Y1 (en) * 1966-07-06 1970-04-02

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US10040577B2 (en) 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US11274604B2 (en) 2016-02-12 2022-03-15 Raytheon Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10801371B2 (en) 2016-02-12 2020-10-13 Raytheon Technologies Coproration Bowed rotor prevention system
US10787277B2 (en) 2016-02-12 2020-09-29 Raytheon Technologies Corporation Modified start sequence of a gas turbine engine
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10625881B2 (en) 2016-02-12 2020-04-21 United Technologies Corporation Modified start sequence of a gas turbine engine
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
US10508567B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10598047B2 (en) 2016-02-29 2020-03-24 United Technologies Corporation Low-power bowed rotor prevention system
US10787933B2 (en) 2016-06-20 2020-09-29 Raytheon Technologies Corporation Low-power bowed rotor prevention and monitoring system
US10358936B2 (en) 2016-07-05 2019-07-23 United Technologies Corporation Bowed rotor sensor system
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
US11047257B2 (en) 2016-07-21 2021-06-29 Raytheon Technologies Corporation Multi-engine coordination during gas turbine engine motoring
US11840968B2 (en) 2016-07-21 2023-12-12 Rtx Corporation Motoring synchronization for multiple engines
US11807378B2 (en) 2016-07-21 2023-11-07 Rtx Corporation Alternating starter use during multi-engine motoring
US10384791B2 (en) 2016-07-21 2019-08-20 United Technologies Corporation Cross engine coordination during gas turbine engine motoring
US10618666B2 (en) 2016-07-21 2020-04-14 United Technologies Corporation Pre-start motoring synchronization for multiple engines
US11674411B2 (en) 2016-07-21 2023-06-13 Raytheon Technologies Corporation Multi-engine coordination during gas turbine engine motoring
US10633106B2 (en) 2016-07-21 2020-04-28 United Technologies Corporation Alternating starter use during multi-engine motoring
US11142329B2 (en) 2016-07-21 2021-10-12 Raytheon Technologies Corporation Pre-start motoring synchronization for multiple engines
US11225888B2 (en) 2016-09-07 2022-01-18 Pratt & Whitney Canada Corp. Shared oil system arrangement for an engine component and a generator
US10544717B2 (en) 2016-09-07 2020-01-28 Pratt & Whitney Canada Corp. Shared oil system arrangement for an engine component and a generator
US10787968B2 (en) 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
US10823079B2 (en) 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine

Also Published As

Publication number Publication date
CA932397A (en) 1973-08-21
JPS5648685B1 (en) 1981-11-17
BE774180A (en) 1972-04-20
JPS481718A (en) 1973-01-11

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee