US2711071A - Arrangement for starting a prime mover by independently driven lubricating pump - Google Patents
Arrangement for starting a prime mover by independently driven lubricating pump Download PDFInfo
- Publication number
- US2711071A US2711071A US236665A US23666551A US2711071A US 2711071 A US2711071 A US 2711071A US 236665 A US236665 A US 236665A US 23666551 A US23666551 A US 23666551A US 2711071 A US2711071 A US 2711071A
- Authority
- US
- United States
- Prior art keywords
- prime mover
- hydraulic motor
- turbine
- starting
- arrangement
- 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 - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/34—Turning or inching gear
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/18—Lubricating arrangements
- F01D25/20—Lubricating arrangements using lubrication pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, 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
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
Definitions
- an arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes selfdriving comprises in combination: a prime mover, a hydraulic motor coupled to the said prime mover, a supply source of liquid, an independently driven auxiliary pump hydraulically connected between the said source and the said hydraulic motor, automatic pressure relief means connected between the said auxiliary pump and the said hydraulic motor, the discharge side of said hydraulic motor being hydraulically connected to the region of the prime mover using said liquid in operation, a nonreturn valve connected between said hydraulic motor and the said region, a by-pass line leading from the discharge side of the said auxiliary pump directly to the said region, and a stop valve connected into the said by-pass line.
- a low pressure compressor 27 is connected through an intercooler 28 and a pipe 31 in series fiow with a high pressure compressor 1 mechanically coupled to a high pressure turbine 2, and in fluid communication therewith through a combustion chamber 23.
- This low pressure compressor 27 is driven mechanically independent of turbine 2 by a turbine 29 which is in series flow connection with the said turbine 2 and with another mechanically independent turbine 30 through pipes 32, 33, respectively.
- turbine 2 is the high pressure turbine, driving the high pressure compressor 1 only;
- turbine 29 is the medium pressure turbine, driving the low pressure compressor 27 only, and turbine 30 is the low pressure turbine driving the useful load 3.
- This hydraulic starter motor 4 is coupled to the turbine 2 and compressor 1, for example by means of a freewheel or overdrive clutch 21 which automatically disengages itself when the turbine 1 reaches its self-driving speed.
- the pump 5 feeds oil from a sump 10 under pressure through a stop valve 22 into the lubrication system of all three turbine sets including the pipes 34, 34' to the bearings of the high pressure, compressor 1, pipes 35, 35' to the bearings of the low pressure compressor 27, pipes 36, 36 to the bearings of the medium pressure turbine 29, pipes 37, 37 to the bearings of the low pressure turbine 30, and pipes 38, 38 to the bearings of the high pressure turbine 2.
- There is a by-pass line 39 shunted over valve 22 which contains in series: the pressure relief valve 16, the hydraulic motor 4 and a nonreturn valve 12.
- the stop valve 22 is closed so that the oil pressure delivered by the pump 5 will then be as high as permitted by the pressure relief valve 16, and high enough to drive the hydraulic motor 4.
- the oil leaving this motor at reduced pressure is then fed through the non-return valve 12 into the lubricating system of the turbines, compressors and load.
- valve 22 is opened, and the pump 5 feeds lubricating oil through it directly into the lubricating system.
- the pressure will then be higher behind the non-return valve 12, and the latter will prevent oil from flowing back through the hydraulic motor 4, which is brought to a standstill and is uncoupled from the turbine 2 and compressor 1 by the automatic clutch 21.
- An arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes self-driving comprising in combination: a prime mover, an automatic overdrive clutch, a hydraulic motor coupled to the said prime mover by the said clutch, a supply source of liquid, an independently driven auxiliary pump hydraulically connected between the said source and the said hydraulic motor, automatic pressure relief means connected between the said auxiliary pump and the said hydraulic motor, the discharge side of said hydraulic motor being hydraulically connected to the region of the prime mover using said liquid in operation, a non-return valve connected between said hydraulic motor and the said region, a by-pass line leading from the discharge side of the said auxiliary pump directly self-driving, comprising in combination: a plurality of compressors in series flow connection with and mechanically independent of one another, a plurality of gas turbines in series flow connection with and mechanically independent of one another, the high pressure gas turbine being in driving connection with the high pressure compressor and forming with it the said prime mover, each of the other compressors being in driving connection with another one
- An arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes self-driving comprising in combination: a prime mover, a hydraulic motor coupled to the said prime mover, a supply source of liquid, an independently driven auxiliary pump hydraulically connected between the said source and the said hydraulic motor, automatic pressure relief means connected between the said auxiliary pump and the said hydraulic motor, the discharge side of said hydraulic motor being hydraulically connected to the region of the prime mover using said liquid in operation, a non-return valve connected between said hydraulic motor and the said region, a by-pass line leading from the discharge side of the said auxiliary pump directly to the said region, and a stop valve connected into the said by-pass line.
- An arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes self-driving comprising in combination: a plurality of compressors in series flow connection with and mechanically independent of one another, a plurality of gas turbines journalled mechanically independent of one another, a high pressure gas turbine being in driving connection with the high pressure compressor and forming with it the said prime mover, each of the other compressors being in driving connection with another one of the said turbines, and a low pressure turbine delivering the useful power output, a hydraulic motor connected to the said prime mover, an auxiliary pump, independent driving means in driving connection with the said auxiliary pump, a supply source of a liquid hydraulically connected to the inlet side of the said auxiliary pump, hydraulic connecting means connecting the delivery side of the said auxiliary pump to the inlet side of the said hydraulic motor, automatic pressure relief means arranged in the said hydraulic connecting means, hydraulic connecting means connecting the outlet side of the said hydraulic motor to the region of the said prime mover using in operation the said liquid, a non-return valve
Description
June 21, 1955 A ARRANGEMENT FOR STARTING A PRIME MOVER BY INDEPENDENTLY DRIVEN LUBRICATING PUMP Filed July 13, 1951 COM BUSTION CHAMBER wvavrok y i /W A T OPNE Y J A FRANKEL 2,711,071
United States Patent ARRANGEMENT FOR STARTING A PRIME MOVER BY INDEPENDENTLY DRIVEN LUBRICATING PUMP Adolf Frankel, Rugby, England, Electric Company Limited, company Application July 13, 1951, Serial No. 236,665 Claims priority, application Great Britain July 18, 1950 4 Claims. (Cl. 60-3914) assignor to The English London, England, a British during the starting period and to serve as a stand-by set which is automatically put into operation to take over the function of the first mentioned set in case of breakdown of he latter.
According to the main feature of the invention an arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes selfdriving comprises in combination: a prime mover, a hydraulic motor coupled to the said prime mover, a supply source of liquid, an independently driven auxiliary pump hydraulically connected between the said source and the said hydraulic motor, automatic pressure relief means connected between the said auxiliary pump and the said hydraulic motor, the discharge side of said hydraulic motor being hydraulically connected to the region of the prime mover using said liquid in operation, a nonreturn valve connected between said hydraulic motor and the said region, a by-pass line leading from the discharge side of the said auxiliary pump directly to the said region, and a stop valve connected into the said by-pass line.
In order that the invention may be better understood and readily carried into effect an embodiment thereof will now be described with reference to the accompanying diagrammatic drawing, which shows a compound gas turbine plant wherein the stand-by lubrication pump drives a hydraulic starter motor.
Referring now to this drawing, a low pressure compressor 27 is connected through an intercooler 28 and a pipe 31 in series fiow with a high pressure compressor 1 mechanically coupled to a high pressure turbine 2, and in fluid communication therewith through a combustion chamber 23. This low pressure compressor 27 is driven mechanically independent of turbine 2 by a turbine 29 which is in series flow connection with the said turbine 2 and with another mechanically independent turbine 30 through pipes 32, 33, respectively. Thus turbine 2 is the high pressure turbine, driving the high pressure compressor 1 only; turbine 29 is the medium pressure turbine, driving the low pressure compressor 27 only, and turbine 30 is the low pressure turbine driving the useful load 3.
For starting this compound gas turbine plant it suflices to drive the high pressure set consisting of the compressor 1 and turbine 2 up to self-driving speed, when the exhaust gases from this turbine 2 will automatically set the turbines 29 and 30 in rotation.
In this arrangement a pump 5, driven by an electric 2,711,071 Patented June 21, 1955 motor 6, serves as lubricating pump during the whole of the normal operation, a unit 4 serving as a hydraulic starter motor only. This hydraulic starter motor 4 is coupled to the turbine 2 and compressor 1, for example by means of a freewheel or overdrive clutch 21 which automatically disengages itself when the turbine 1 reaches its self-driving speed. 1
The pump 5 feeds oil from a sump 10 under pressure through a stop valve 22 into the lubrication system of all three turbine sets including the pipes 34, 34' to the bearings of the high pressure, compressor 1, pipes 35, 35' to the bearings of the low pressure compressor 27, pipes 36, 36 to the bearings of the medium pressure turbine 29, pipes 37, 37 to the bearings of the low pressure turbine 30, and pipes 38, 38 to the bearings of the high pressure turbine 2. There is a by-pass line 39 shunted over valve 22 which contains in series: the pressure relief valve 16, the hydraulic motor 4 and a nonreturn valve 12. For starting purposes the stop valve 22 is closed so that the oil pressure delivered by the pump 5 will then be as high as permitted by the pressure relief valve 16, and high enough to drive the hydraulic motor 4. The oil leaving this motor at reduced pressure is then fed through the non-return valve 12 into the lubricating system of the turbines, compressors and load.
As soon as self-driving speed is attained, valve 22 is opened, and the pump 5 feeds lubricating oil through it directly into the lubricating system. The pressure will then be higher behind the non-return valve 12, and the latter will prevent oil from flowing back through the hydraulic motor 4, which is brought to a standstill and is uncoupled from the turbine 2 and compressor 1 by the automatic clutch 21.
Where hereinabove single pumps or hydraulic motors are shown or described, two or more such pumps or hydraulic motors operating in series or in parallel can be used instead.
The arrangement of a hydraulic motor coupled to the prime mover by .means of a freewheel or overdrive clutch and supplied by an independently driven auxiliary pump, which during the ordinary operation continues supplying the prime mover with liquid such as lubricating oil or fuel, described hereinabove, could be simplified by omitting the said freewheel or overdrive clutch.
While I have described hereinabove what may be considered as particularly useful embodiments of my invention, I wish it to be understood that I do not limit myself to the particular arrangements shown and described, for obvious modifications will occur to a person skilled in the art according to the special requirements and circumstances under which my invention'may be used.
What I claim as my invention and desire to secure by Letters Patent is:
1. An arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes self-driving comprising in combination: a prime mover, an automatic overdrive clutch, a hydraulic motor coupled to the said prime mover by the said clutch, a supply source of liquid, an independently driven auxiliary pump hydraulically connected between the said source and the said hydraulic motor, automatic pressure relief means connected between the said auxiliary pump and the said hydraulic motor, the discharge side of said hydraulic motor being hydraulically connected to the region of the prime mover using said liquid in operation, a non-return valve connected between said hydraulic motor and the said region, a by-pass line leading from the discharge side of the said auxiliary pump directly self-driving, comprising in combination: a plurality of compressors in series flow connection with and mechanically independent of one another, a plurality of gas turbines in series flow connection with and mechanically independent of one another, the high pressure gas turbine being in driving connection with the high pressure compressor and forming with it the said prime mover, each of the other compressors being in driving connection with another one of the said turbines, and the low pressure turbine delivering the useful power output, a hydraulic motor, an automatic overdrive clutch mechanically connecting the said hydraulic motor to the said prime mover, an auxiliary pump, independent driving means in driving connection with the said auxiliary pump, a supply source of a liquid hydraulically connected to the inlet side of the said auxiliary pump, hydraulic connecting means connecting the delivery side of the said auxiliary pump to the inlet side of the said hydraulic motor, automatic pressure relief means arranged in the said hydraulic connecting means, hydraulic connecting means connecting the outlet side of the said hydraulic motor to the region of the said prime mover using in operation the said liquid, a non-return valve connected between the said hydraulic motor and the said region, a by-pass line leading from the delivery side of the said auxiliary pump directly to the said region, and stop valve means connected into the said by-pass line.
3. An arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes self-driving comprising in combination: a prime mover, a hydraulic motor coupled to the said prime mover, a supply source of liquid, an independently driven auxiliary pump hydraulically connected between the said source and the said hydraulic motor, automatic pressure relief means connected between the said auxiliary pump and the said hydraulic motor, the discharge side of said hydraulic motor being hydraulically connected to the region of the prime mover using said liquid in operation, a non-return valve connected between said hydraulic motor and the said region, a by-pass line leading from the discharge side of the said auxiliary pump directly to the said region, and a stop valve connected into the said by-pass line.
4. An arrangement for starting a prime mover which has to be driven up to a certain speed before it becomes self-driving, comprising in combination: a plurality of compressors in series flow connection with and mechanically independent of one another, a plurality of gas turbines journalled mechanically independent of one another, a high pressure gas turbine being in driving connection with the high pressure compressor and forming with it the said prime mover, each of the other compressors being in driving connection with another one of the said turbines, and a low pressure turbine delivering the useful power output, a hydraulic motor connected to the said prime mover, an auxiliary pump, independent driving means in driving connection with the said auxiliary pump, a supply source of a liquid hydraulically connected to the inlet side of the said auxiliary pump, hydraulic connecting means connecting the delivery side of the said auxiliary pump to the inlet side of the said hydraulic motor, automatic pressure relief means arranged in the said hydraulic connecting means, hydraulic connecting means connecting the outlet side of the said hydraulic motor to the region of the said prime mover using in operation the said liquid, a non-return valve connected between the said hydraulic motor and the said region, a by-pass line leading from the delivery side of the said auxiliary pump directly to, the said region, and stop valve means connected into the said by-pass line. 7
References Cited in the file of this patent UNITED STATES PATENTS 1,613,753 Hodgkinson Jan. 11, 1927 2,102,514 Clarkson Dec. 14, 1937 2,104,696 Hanson Jan. 4, 1938 2,155,218 Cain Apr. 18, 1939 2,318,905 Traupel May 11, 1943 2,339,185 Nettel Jan. 11,1944 2,347,744 Lehman May 2, 1944 2,390,959 Pfenninger Dec. 11, 1945 2,402,467 Thompson June 18, 1946 FOREIGN PATENTS 311,610 Great Britain c May 16, 1929
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB317251X | 1950-07-18 |
Publications (1)
Publication Number | Publication Date |
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US2711071A true US2711071A (en) | 1955-06-21 |
Family
ID=10327443
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US236665A Expired - Lifetime US2711071A (en) | 1950-07-18 | 1951-07-13 | Arrangement for starting a prime mover by independently driven lubricating pump |
Country Status (3)
Country | Link |
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US (1) | US2711071A (en) |
CH (1) | CH317251A (en) |
GB (1) | GB690120A (en) |
Cited By (28)
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 |
US3020716A (en) * | 1957-08-08 | 1962-02-13 | Napier & Son Ltd | Starting systems for gas turbine engines |
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 |
US3472024A (en) * | 1967-10-27 | 1969-10-14 | Sulzer Ag | Starting system for a gas turbine plant |
US3475907A (en) * | 1967-04-27 | 1969-11-04 | Cav Ltd | Gas turbine with lubricant and fuel supply systems therefor |
US3658153A (en) * | 1969-11-28 | 1972-04-25 | Westinghouse Electric Corp | Lubricating oil system for a prime mover |
US4171611A (en) * | 1975-08-07 | 1979-10-23 | Motoren- Und Turbinen-Union Munchen Gmbh | Vehicular gas turbine system |
US4211070A (en) * | 1977-06-24 | 1980-07-08 | Bbc Brown Boveri & Company Limited | Start-up motor assembly for rotational machines |
US4709785A (en) * | 1986-09-02 | 1987-12-01 | Westinghouse Electric Corp. | Retrofit friction-hydrostatic emergency lubrication system for a large rotating shaft |
US4899850A (en) * | 1987-11-04 | 1990-02-13 | Mannesmann Aktiengesellschaft | Lubricating device for a turbomachine |
US5184456A (en) * | 1991-04-08 | 1993-02-09 | Avco Corporation | Gas turbine motor drive |
US5735116A (en) * | 1995-12-20 | 1998-04-07 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | System for restarting an aircraft engine in flight after loss of engine power |
US6735952B2 (en) * | 2001-09-26 | 2004-05-18 | Ingersoll-Rand Energy Systems | Single pump lubrication and starter system |
US20060083633A1 (en) * | 2004-10-14 | 2006-04-20 | Hamilton Sundstrand Corporation | Pressure/flow sensing stall recovery for a ram air turbine |
US20100212281A1 (en) * | 2009-02-26 | 2010-08-26 | United Technologies Corporation | Auxiliary pump system for fan drive gear system |
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US20140245727A1 (en) * | 2013-03-01 | 2014-09-04 | Paccar Inc. | Turbine engine starting 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 |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US20160032773A1 (en) * | 2013-03-15 | 2016-02-04 | United Technologies Corporation | Circulating lubricant through a turbine engine component with parallel pumps |
CN106246247A (en) * | 2016-09-29 | 2016-12-21 | 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 on off control method thereof |
EP3124761A1 (en) * | 2015-07-28 | 2017-02-01 | Siemens Aktiengesellschaft | Turbine installation |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
US10634053B2 (en) | 2015-12-21 | 2020-04-28 | United Technologies Corporation | Electric windmill pump for gearbox durability |
CN111226574A (en) * | 2018-11-28 | 2020-06-05 | 迪尔公司 | System and method for reducing parasitic loads on an engine of a harvester |
Families Citing this family (5)
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 |
WO2015126500A1 (en) * | 2013-12-05 | 2015-08-27 | Mastro Jacob P | Fdgs auxiliary pump monitoring system |
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 |
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US2104696A (en) * | 1935-02-26 | 1938-01-04 | B F Sturtevant Company Inc | Refrigeration drive |
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US2318905A (en) * | 1939-05-10 | 1943-05-11 | Sulzer Ag | Gas turbine plant |
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US2347744A (en) * | 1943-01-11 | 1944-05-02 | Bendix Aviat Corp | Engine starting |
US2390959A (en) * | 1941-02-03 | 1945-12-11 | Bbc Brown Boveri & Cie | Gas turbine power plant |
US2402467A (en) * | 1944-01-31 | 1946-06-18 | Westinghouse Electric Corp | Lubrication control |
-
1950
- 1950-07-18 GB GB17930/50A patent/GB690120A/en not_active Expired
-
1951
- 1951-07-12 CH CH317251D patent/CH317251A/en unknown
- 1951-07-13 US US236665A patent/US2711071A/en not_active Expired - Lifetime
Patent Citations (10)
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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 |
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Cited By (33)
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 |
US3020716A (en) * | 1957-08-08 | 1962-02-13 | Napier & Son Ltd | Starting systems for gas turbine engines |
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 |
US3475907A (en) * | 1967-04-27 | 1969-11-04 | Cav Ltd | Gas turbine with lubricant and fuel supply systems therefor |
US3472024A (en) * | 1967-10-27 | 1969-10-14 | Sulzer Ag | Starting system for a gas turbine plant |
US3658153A (en) * | 1969-11-28 | 1972-04-25 | Westinghouse Electric Corp | Lubricating oil system for a prime mover |
US4171611A (en) * | 1975-08-07 | 1979-10-23 | Motoren- Und Turbinen-Union Munchen Gmbh | Vehicular gas turbine system |
US4211070A (en) * | 1977-06-24 | 1980-07-08 | Bbc Brown Boveri & Company Limited | Start-up motor assembly for rotational machines |
US4709785A (en) * | 1986-09-02 | 1987-12-01 | Westinghouse Electric Corp. | Retrofit friction-hydrostatic emergency lubrication system for a large rotating shaft |
US4899850A (en) * | 1987-11-04 | 1990-02-13 | Mannesmann Aktiengesellschaft | Lubricating device for a turbomachine |
US5184456A (en) * | 1991-04-08 | 1993-02-09 | Avco Corporation | Gas turbine motor drive |
US5735116A (en) * | 1995-12-20 | 1998-04-07 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | System for restarting an aircraft engine in flight after loss of engine power |
US6735952B2 (en) * | 2001-09-26 | 2004-05-18 | Ingersoll-Rand Energy Systems | Single pump lubrication and starter system |
US20060083633A1 (en) * | 2004-10-14 | 2006-04-20 | Hamilton Sundstrand Corporation | Pressure/flow sensing stall recovery for a ram air turbine |
US7197870B2 (en) | 2004-10-14 | 2007-04-03 | Hamilton Sundstrand Corporation | Pressure/flow sensing stall recovery for a ram air turbine |
US20100212281A1 (en) * | 2009-02-26 | 2010-08-26 | United Technologies Corporation | Auxiliary pump system for fan drive gear system |
US8307626B2 (en) * | 2009-02-26 | 2012-11-13 | United Technologies Corporation | Auxiliary pump system for fan drive gear system |
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8708083B2 (en) | 2009-05-12 | 2014-04-29 | Icr Turbine Engine Corporation | Gas turbine energy 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 |
US20140245727A1 (en) * | 2013-03-01 | 2014-09-04 | Paccar Inc. | Turbine engine starting system |
US9429070B2 (en) * | 2013-03-01 | 2016-08-30 | Paccar Inc | Turbine engine starting system |
US20160032773A1 (en) * | 2013-03-15 | 2016-02-04 | United Technologies Corporation | Circulating lubricant through a turbine engine component with parallel pumps |
US10494951B2 (en) * | 2013-03-15 | 2019-12-03 | United Technologies Corporation | Circulating lubricant through a turbine engine component with parallel pumps |
EP3124761A1 (en) * | 2015-07-28 | 2017-02-01 | Siemens Aktiengesellschaft | Turbine installation |
US10634053B2 (en) | 2015-12-21 | 2020-04-28 | United Technologies Corporation | Electric windmill pump for gearbox durability |
CN106246247A (en) * | 2016-09-29 | 2016-12-21 | 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 on off control method thereof |
CN111226574A (en) * | 2018-11-28 | 2020-06-05 | 迪尔公司 | System and method for reducing parasitic loads on an engine of a harvester |
Also Published As
Publication number | Publication date |
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CH317251A (en) | 1956-11-15 |
GB690120A (en) | 1953-04-15 |
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