GB690120A - Improvements in and relating to the starting of gas turbines - Google Patents

Improvements in and relating to the starting of gas turbines

Info

Publication number
GB690120A
GB690120A GB17930/50A GB1793050A GB690120A GB 690120 A GB690120 A GB 690120A GB 17930/50 A GB17930/50 A GB 17930/50A GB 1793050 A GB1793050 A GB 1793050A GB 690120 A GB690120 A GB 690120A
Authority
GB
United Kingdom
Prior art keywords
pump
valve
pressure
oil
closed
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
GB17930/50A
Inventor
Adolf Frankel
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.)
English Electric Co Ltd
Original Assignee
English Electric Co Ltd
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 English Electric Co Ltd filed Critical English Electric Co Ltd
Publication of GB690120A publication Critical patent/GB690120A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/34Turning or inching gear
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18Lubricating arrangements
    • F01D25/20Lubricating arrangements using lubrication pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started

Abstract

690,120. Gas turbine plant; rotary pumps. ENGLISH ELECTRIC CO.. Ltd. July 13, 1951 [July 18. 1950]. No. 17930/50. Classes 110(ii) and 110(iii) [Also in Group XXVII] A gas turbine plant is driven up to its self starting speed by a hydraulic motor which is supplied with liquid under pressure by an independently driven auxiliary pump of the plant such as a lubricating oil or fuel pump. In the plant shown, Fig. 1, a gas turbine 2 drives a compressor 1, a load 3 and a lubricating oil pump 4. An auxiliary lubricating oil pump 5 driven by an electric motor 6 is provided to supply oil during the starting period and in the event of failure of the pump 4. Both pumps draw oil from a sump 10. A stop or non-return valve 11 is arranged between the sump 10 and the pump 4 which discharges through a non-return valve 12 to the bearings. A stop valve 15 is arranged between the delivery of the pump 5 and the inlet to the pump 4. A pressure relief valve 16, stop valve 17 and non- return valve 18 are arranged between the delivery of the pump 5 and the bearings. In normal operation. the valves 11 and 17 are open and the stop valve 15 closed and the pump 4 draws oil from the sump 10 and delivers it to the bearings. The non-return valve 18 is closed by the oil pressure and the pressure responsive capsule 13 keeps the switch 14 open. Should the pump 4 fail, switch 14 is closed by the capsule 13 and the relay 31 energised to close the switch 31<SP>1</SP> and start the motor 6. The pump 5 then delivers oil from the sump 10 to the bearings through the non-return valve 18. A latch 31<SP>11</SP> keeps the switch 31<SP>1</SP> closed when the oil pressure regains its normal value. For starting, the valves 11 and 17 are closed and the valve 15 opened. The pump 5 is then started and delivers oil under pressure to the pump 4 which acts as a hydraulic motor and drives the machines 1, 2, 3. As soon as the machines 1, 2, 3 are self-running, the valves 11, 17 are opened and the valve 15 closed. The relative sizes and speeds of the pumps 4, 5 are chosen that. at the self-running speed of the machines 1, 2. 3. the requirements of the pump 4 are 2 per cent to 25 per cent less than that of the pump 5. Above this speed, the requirements of the pump 4 should exceed the delivery of the pump 5 so that it commences to suck oil from the sump 10. In a modification, the valve 15 is replaced by a spring loaded valve in a cylinder which controls two sets of ports. One set is connected to the suction of the pump 4 and the other set to a return to the sump 10. The arrangement is such that when the valve 17 is closed, the pressure in the conduit 26 rises and the spring loaded valve opens the ports connected to the pump 4. Any further increase in pressure causes the valve to open the second set of ports and allows the excess oil to return to the sump. In this arrangement the relief valve 16 is placed in the conduit between the discharge of the pump 4 and the bearings. In another modification, the valve 15 is replaced by a two way cock which may connect the discharge of the pump 5 either to the suction conduit 8 of the pump 4 or to the conduit 26. In this arrangement, a pressure relief valve which can be set to two different loadings is placed between the discharge of the pump 5 and the two way cock. In normal operation, the two way cock is set to connect the discharge of the pump 5 with the conduit 26 and the relief valve set to the lower loading. For starting, the cock is set to connect the discharge of the pump to the conduit 8 and the relief valve set to the higher loading. The two way cock and the means for varying the loading of the relief valve may be coupled to one another but it is preferred to retain independent operation of these members so that the relief valve may be set to the lower loading and the pump 5 connected to the conduit 8 when it is desired to drive the machines 1, 2. 3 for a prolonged period below the self driving speed. In another plant, Fig. 4, comprising a low pressure compressor 27 driven by an intermediate pressure turbine 29, a high pressure compressor 1 driven by a high pressure turbine 2 and a useful output low pressure turbine 30, only the set consisting of the high pressure compressor 1 and turbine 2 is driven up to the self-driving speed. In this arrangement, the pump 5 driven by the electric motor 6 acts as the lubricating pump during normal operation and the unit 4 serves only as a hydraulic starter motor which is connected to the turbine-compressor unit 1. 2 by a free wheel or overdrive clutch 21 which automatically disengages itself when the turbine 1 reaches its self-driving speed. The pump 5 normally discharges through a valve 22 to the bearings. When it is desired to start the unit 1, 2, the valve 22 is closed, the pump discharge pressure rises and the motor 4 operated. A modification in which the pump 5 is the fuel pump is also described. The starting arrangements described with reference to Fig. 4 can be applied to the plant shown in Fig. 1.
GB17930/50A 1950-07-18 1950-07-18 Improvements in and relating to the starting of gas turbines Expired GB690120A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB317251X 1950-07-18

Publications (1)

Publication Number Publication Date
GB690120A true GB690120A (en) 1953-04-15

Family

ID=10327443

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17930/50A Expired GB690120A (en) 1950-07-18 1950-07-18 Improvements in and relating to the starting of gas turbines

Country Status (3)

Country Link
US (1) US2711071A (en)
CH (1) CH317251A (en)
GB (1) GB690120A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2838908A (en) * 1953-06-18 1958-06-17 Daimler Benz Ag Starting and control system for a power plant
US3090199A (en) * 1960-09-22 1963-05-21 Lucas Industries Ltd Machines incorporating a plurality of engines
US3170292A (en) * 1960-04-04 1965-02-23 Ford Motor Co Lubricating system for a gas turbine engine
WO2015126500A1 (en) * 2013-12-05 2015-08-27 Mastro Jacob P Fdgs auxiliary pump monitoring system
CN113153460A (en) * 2021-01-26 2021-07-23 东方电气集团东方汽轮机有限公司 High-level oil tank system for turbine lubricating oil

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2821927A (en) * 1952-07-15 1958-02-04 Belton A Copp Control mechanism for power fluid supply
BE570177A (en) * 1957-08-08 1958-08-30
US3063242A (en) * 1959-11-02 1962-11-13 Plissey Company Ltd Liquid-fuel operated engine starters
US3451214A (en) * 1967-03-15 1969-06-24 Garrett Corp Cold engine start facilitating apparatus
GB1222085A (en) * 1967-04-27 1971-02-10 Cav Ltd Hot gas generators
US3472024A (en) * 1967-10-27 1969-10-14 Sulzer Ag Starting system for a gas turbine plant
BE759344A (en) * 1969-11-28 1971-05-24 Westinghouse Electric Corp TURBINE LUBRICATION SYSTEM
US4171611A (en) * 1975-08-07 1979-10-23 Motoren- Und Turbinen-Union Munchen Gmbh Vehicular gas turbine system
CH622061A5 (en) * 1977-06-24 1981-03-13 Bbc Brown Boveri & Cie
US4709785A (en) * 1986-09-02 1987-12-01 Westinghouse Electric Corp. Retrofit friction-hydrostatic emergency lubrication system for a large rotating shaft
DE3737844C1 (en) * 1987-11-04 1989-02-16 Mannesmann Ag Lubrication device for a turbomachine
US5184456A (en) * 1991-04-08 1993-02-09 Avco Corporation Gas turbine motor drive
FR2742805B1 (en) * 1995-12-20 1998-01-16 Snecma ENGINE RESTART ASSISTANCE SYSTEM AFTER TOTAL LOSS OF MOTORIZATION
US6735952B2 (en) * 2001-09-26 2004-05-18 Ingersoll-Rand Energy Systems Single pump lubrication and starter system
US7197870B2 (en) * 2004-10-14 2007-04-03 Hamilton Sundstrand Corporation Pressure/flow sensing stall recovery for a ram air turbine
US8307626B2 (en) * 2009-02-26 2012-11-13 United Technologies Corporation Auxiliary pump system for fan drive gear system
BRPI1007723A2 (en) 2009-05-12 2018-03-06 Icr Turbine Engine Corp gas turbine storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US8669670B2 (en) 2010-09-03 2014-03-11 Icr Turbine Engine Corporation Gas turbine engine configurations
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
US9429070B2 (en) * 2013-03-01 2016-08-30 Paccar Inc Turbine engine starting system
EP2971662B1 (en) * 2013-03-15 2020-10-28 United Technologies Corporation Circulating lubricant through a turbine engine component with parallel pumps
DE102015214270A1 (en) * 2015-07-28 2017-02-02 Siemens Aktiengesellschaft turbine plant
US10634053B2 (en) 2015-12-21 2020-04-28 United Technologies Corporation Electric windmill pump for gearbox durability
CN106246247B (en) * 2016-09-29 2017-10-13 华北电力科学研究院有限责任公司 A kind of thermal power plant's Turbo-generator Set lubricating oil system and its start-up and shut-down control method
US11248680B2 (en) * 2018-11-28 2022-02-15 Deere & Company System and method to reduce parasitic loads on an engine of a harvesting machine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1613753A (en) * 1924-12-27 1927-01-11 Westinghouse Electric & Mfg Co Hydraulic regulating device
GB311610A (en) * 1928-08-09 1929-05-16 Anciens Ets Hotchkiss & Cie Lubrication system for fluid pressure engines
US2104696A (en) * 1935-02-26 1938-01-04 B F Sturtevant Company Inc Refrigeration drive
US2102514A (en) * 1936-11-21 1937-12-14 Marion C Clarkson Auxiliary oiling device
US2155218A (en) * 1938-05-21 1939-04-18 Gen Electric Bearing lubricating system
US2318905A (en) * 1939-05-10 1943-05-11 Sulzer Ag Gas turbine plant
US2390959A (en) * 1941-02-03 1945-12-11 Bbc Brown Boveri & Cie Gas turbine power plant
US2339185A (en) * 1941-06-13 1944-01-11 Nettel Friedrich Combustion turbine
US2347744A (en) * 1943-01-11 1944-05-02 Bendix Aviat Corp Engine starting
US2402467A (en) * 1944-01-31 1946-06-18 Westinghouse Electric Corp Lubrication control

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2838908A (en) * 1953-06-18 1958-06-17 Daimler Benz Ag Starting and control system for a power plant
US3170292A (en) * 1960-04-04 1965-02-23 Ford Motor Co Lubricating system for a gas turbine engine
US3090199A (en) * 1960-09-22 1963-05-21 Lucas Industries Ltd Machines incorporating a plurality of engines
DE1235662B (en) * 1960-09-22 1967-03-02 Lucas Industries Ltd Fuel feed system for engines
WO2015126500A1 (en) * 2013-12-05 2015-08-27 Mastro Jacob P Fdgs auxiliary pump monitoring system
US10072521B2 (en) 2013-12-05 2018-09-11 United Technologies Corporation FDGS auxiliary pump monitoring system
CN113153460A (en) * 2021-01-26 2021-07-23 东方电气集团东方汽轮机有限公司 High-level oil tank system for turbine lubricating oil
CN113153460B (en) * 2021-01-26 2022-03-25 东方电气集团东方汽轮机有限公司 High-level oil tank system for turbine lubricating oil

Also Published As

Publication number Publication date
CH317251A (en) 1956-11-15
US2711071A (en) 1955-06-21

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