WO2014026696A1 - Locomotive à turbine à gaz à deux sections - Google Patents

Locomotive à turbine à gaz à deux sections Download PDF

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Publication number
WO2014026696A1
WO2014026696A1 PCT/EA2012/000010 EA2012000010W WO2014026696A1 WO 2014026696 A1 WO2014026696 A1 WO 2014026696A1 EA 2012000010 W EA2012000010 W EA 2012000010W WO 2014026696 A1 WO2014026696 A1 WO 2014026696A1
Authority
WO
WIPO (PCT)
Prior art keywords
gas
cryogenic
section
gas turbine
equipment
Prior art date
Application number
PCT/EA2012/000010
Other languages
English (en)
Russian (ru)
Inventor
Владимир Федорович РУДЕНКО
Валерий Семенович КОССОВ
Давид Львович КИРЖНЕР
Валентин Александрович ГАПАНОВИЧ
Александр Дмитриевич КОРЧАГИН
Андрей Геннадиевич ВОРОНКОВ
Евгений Юрьевич СТАЛЬНОВ
Original Assignee
Открытое Акционерное Общество "Российские Железные Дороги"
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 Открытое Акционерное Общество "Российские Железные Дороги" filed Critical Открытое Акционерное Общество "Российские Железные Дороги"
Priority to CN201280022461.8A priority Critical patent/CN103889808B/zh
Priority to CA2833117A priority patent/CA2833117C/fr
Priority to EP12876586.4A priority patent/EP2719600B1/fr
Publication of WO2014026696A1 publication Critical patent/WO2014026696A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61C—LOCOMOTIVES; MOTOR RAILCARS
    • B61C5/00—Locomotives or motor railcars with IC engines or gas turbines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61C—LOCOMOTIVES; MOTOR RAILCARS
    • B61C17/00—Arrangement or disposition of parts; Details or accessories not otherwise provided for; Use of control gear and control systems
    • B61C17/04—Arrangement or disposition of driving cabins, footplates or engine rooms; Ventilation thereof
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T30/00—Transportation of goods or passengers via railways, e.g. energy recovery or reducing air resistance

Definitions

  • the invention relates to railway transport and for the design of locomotives, in particular gas turbines.
  • each of the two sections is supported by two triaxial trolleys with wheel sets equipped with traction motors.
  • a power unit with a gas turbine engine leading through a traction reducer. and auxiliary generators, a fuel system comprising a pump supplying fuel from a tender tank to a gas turbine combustion chamber.
  • a control cabin and auxiliary equipment including an auxiliary diesel generator, a tank with diesel fuel, a diesel cooling system, brake compressors, and control equipment.
  • the sections are connected by power cables, control cables, two cooling water supply hoses, a diesel fuel supply pipeline to start the gas turbine engine, and brake hoses.
  • a jet gas turbine locomotive (gas turbo locomotive) is known, which contains a turbojet gas turbine engine with a dual-fuel combustion chamber, a heat exchanger, a gasifier for liquefied natural gas, heated by the heat of hot gas from a gas turbine engine, cryogenic containers for storing liquefied gas inside the body or on the roof of a locomotive (patent RU5. , Cl. 61 C 1 1/06, 2005).
  • Known two-section gas turbine locomotive containing two traction sections, which are equipped with bodies with a frame and a control cabin, carts with wrapped wheel pairs.
  • a power unit including a gas turbine engine, which drives the traction and auxiliary turbogenerators and auxiliary equipment.
  • a cryogenic tank for storing liquefied cryogenic gas fuel, an auxiliary diesel generator. The tank is located, so that the center of gravity coincides (along the vertical axis) with the center of gravity of the section, which does not allow the occurrence of different loads on the bogies during fuel production.
  • the capacity and the power unit are separated by partitions from the control cabins (patent RU M> 2352484 C2, B61C5 / 00, 2007).
  • the technical result of the invention is:
  • the specified technical result is achieved in that in a two sectional gas turbine locomotive containing two traction sections, which are equipped with bodies with a frame and a control cabin, trolleys with wrapped wheel pairs.
  • a power unit including a gas turbine engine, which drives a traction turbogenerator, auxiliary equipment, a gas equipment unit, which includes a gas receiver and control automatics, an electrical compartment and other equipment necessary to ensure locomotive movement.
  • a removable container for liquefied natural gas (or other cryogenic fuel), a block of cryogenic equipment with a piston cryogenic pump, a compartment for high-voltage electrical equipment and a compartment with auxiliary equipment are located.
  • the cryogenic tank with thermal insulation for LNG storage is removable in the size of a standard container and is located in an open area with fastening in the form of standard supports for containers.
  • the supports are equipped with special weighing devices that allow you to control the amount of fuel in the tank, both in the parking lot and in motion.
  • Fuel is supplied to the block of cryogenic equipment through a quick disconnect connection that allows you to quickly undock the container and also quickly dock it.
  • Fuel from the cryogenic equipment unit is supplied to the gas equipment unit of the first section through a flexible intersectional connection.
  • the figure 1 schematically shows a General view of the first section of a gas turbine locomotive side view
  • the figure 2 schematically shows a General view of the first section of a gas turbine locomotive top view
  • Figure 3 schematically shows a General view of the second section of a gas turbine locomotive side view
  • Figure 4 schematically shows a General view of the second section of a gas turbine locomotive from above;
  • a two-section gas turbine locomotive contains two traction sections 1 and 2 (Figs. 1, 2), which are equipped with bodies 3 and 4 with frames 5, 6 and control cabins 7 located at opposite ends of the gas turbine locomotive.
  • Frames 5, 6 of sections 1 and 2 are mounted on carts 8 with wheel pairs wrapped by traction electric motors 9.
  • a power unit 10 including a gas turbine engine (GTE) 11, a traction turbogenerator 12, a compartment of electrical equipment 13 with traction rectifiers 14, a high-voltage chamber 15 and an axial fan, a gas equipment block 16.
  • GTE gas turbine engine
  • traction turbogenerator 12 a compartment of electrical equipment 13 with traction rectifiers 14, a high-voltage chamber 15 and an axial fan
  • gas equipment block 16 Under the frame 4 of section 1 between the carts 8 there is a compartment with rechargeable batteries 17.
  • the body 4 of section 2 is divided into two compartments front 18 and rear 19, between the compartments in an open area there is a removable tank 20.
  • the capacity is attached to the frame 6 of section 2 with standard supports for containers 21 that do not allow its movement and provide reliable fixation. Supports 21 are equipped with special weighing devices 22.
  • Quick disconnect cryogenic joints 23 are connected to the rear end of the tank 20, access to which is carried out through the doorway 24 on the wall of the rear compartment 19 of the body 4.
  • the sections are connected by two cryogenic intersection pipelines 30.
  • flexible metal buses 31 are installed located on roofs of bodies 3 and 4.
  • transition platforms 32 with door blocks 33 are located.
  • Gas turbine carrier works as follows:
  • the tank 20 filled with cryogenic fuel is mounted on the supports 21 of the frame 6 of section 2.
  • Quick-disconnect cryogenic connections 22 are connected to the tank 20.
  • cryogenic fuel is supplied to the cryogenic piston pump 26 through quick-disconnect connections 23 and is supplied through the piping system 27 through intersection pipelines 30 to the block gas equipment 16.
  • cryogenic fuel is gasified and supplied through pipelines to the gas turbine engine 11 of the power unit 10.
  • the gas turbine engine 1 1 is started by means of an electric starter 34 laid on it.
  • Launched gas turbine engine drives the rotor of the traction turbogenerator 12.
  • the electric current generated by the turbogenerator 12 is supplied to the traction rectifiers 14 of the compartment 13.
  • the rectified current from the traction rectifiers 14 enters the high-voltage chamber 15 of section 1 and through intersection metal buses 30 to the high-voltage chamber 28 of section 2. From high-voltage chambers 15 and 28, the current flows to the traction motors 9.

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Control Of Eletrric Generators (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

L'invention se rapporte à la construction de locomotives qui utilise comme carburant un carburant cryogénique, notamment du gaz naturel liquéfié. Cette locomotive à turbine à gaz comprend deux sections possédant chacune un châssis avec une carrosserie, une cabine de commande, des bogies avec des moteurs électriques d'entraînement, et une unité d'équipement électrique avec des chambres à haute tension alimentant les moteurs électriques d'entraînement. La première section comprend un moteur à turbine à gaz, un turbogénérateur d'entraînement, une unité d'équipement pour gaz, tandis que la seconde comprend un récipient cryogénique pour le gaz naturel liquéfié et un équipement cryogénique relié à l'unité d'équipement pour gaz de la première section. La carrosserie de la seconde section de la locomotive à turbine à gaz comprend des compartiments avant et arrière entre lesquels est disposée une plateforme ouverte du châssis. Le récipient cryogénique pour le gaz naturel liquéfié est amovible et est disposé sur la plateforme ouverte du châssis. La cabine de commande est disposée dans le compartiment avant, tandis que l'équipement cryogénique et les chambres à haute tension sont disposés dans le compartiment arrière.
PCT/EA2012/000010 2012-08-17 2012-09-27 Locomotive à turbine à gaz à deux sections WO2014026696A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201280022461.8A CN103889808B (zh) 2012-08-17 2012-09-27 双单元燃气轮机机车
CA2833117A CA2833117C (fr) 2012-08-17 2012-09-27 Locomotive a turbine a gaz a deux unites
EP12876586.4A EP2719600B1 (fr) 2012-08-17 2012-09-27 Locomotive à turbine à gaz à deux sections

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EA201201026 2012-08-17
EA201201026A EA018298B1 (ru) 2012-08-17 2012-08-17 Двухсекционный газотурбовоз

Publications (1)

Publication Number Publication Date
WO2014026696A1 true WO2014026696A1 (fr) 2014-02-20

Family

ID=48699390

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EA2012/000010 WO2014026696A1 (fr) 2012-08-17 2012-09-27 Locomotive à turbine à gaz à deux sections

Country Status (4)

Country Link
CN (1) CN103889808B (fr)
CA (1) CA2833117C (fr)
EA (1) EA018298B1 (fr)
WO (1) WO2014026696A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3551493A4 (fr) * 2016-12-06 2020-07-29 CNGMotive Inc. Systèmes et procédés de production de puissance de véhicule

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU179975U1 (ru) * 2017-07-26 2018-05-29 Открытое Акционерное Общество "Российские Железные Дороги" Узел подачи криогенного топлива для питания двигателя

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5129328A (en) 1988-04-06 1992-07-14 Donnelly Frank W Gas turbine locomotive fueled by compressed natural Gas
RU2251505C1 (ru) 2003-11-17 2005-05-10 Самарская государственная академия путей сообщения (СамГАПС) Реактивный газотурбинный локомотив
RU2295467C1 (ru) * 2005-12-29 2007-03-20 Федеральное государственное унитарное предприятие Всероссийский научно-исследовательский и конструкторско-технологический институт подвижного состава Министерства путей сообщения Российской Федерации (ФГУП ВНИКТИ МПС России) Газотурбовоз
RU2352484C2 (ru) 2007-06-08 2009-04-20 Открытое акционерное общество "Российские железные дороги" (ОАО "РЖД") Двухсекционный газотурбовоз
RU2427724C1 (ru) * 2010-05-12 2011-08-27 Открытое Акционерное Общество "Российские Железные Дороги" Система подачи криогенного топлива для питания двигателя

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5566712A (en) * 1993-11-26 1996-10-22 White; George W. Fueling systems
US6308639B1 (en) * 2000-04-26 2001-10-30 Railpower Technologies Corp. Hybrid battery/gas turbine locomotive

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5129328A (en) 1988-04-06 1992-07-14 Donnelly Frank W Gas turbine locomotive fueled by compressed natural Gas
RU2251505C1 (ru) 2003-11-17 2005-05-10 Самарская государственная академия путей сообщения (СамГАПС) Реактивный газотурбинный локомотив
RU2295467C1 (ru) * 2005-12-29 2007-03-20 Федеральное государственное унитарное предприятие Всероссийский научно-исследовательский и конструкторско-технологический институт подвижного состава Министерства путей сообщения Российской Федерации (ФГУП ВНИКТИ МПС России) Газотурбовоз
RU2352484C2 (ru) 2007-06-08 2009-04-20 Открытое акционерное общество "Российские железные дороги" (ОАО "РЖД") Двухсекционный газотурбовоз
EP2154044A2 (fr) * 2007-06-08 2010-02-17 Open Joint Stock Company "Russian Railways" Locomotive à turbine à gaz
RU2427724C1 (ru) * 2010-05-12 2011-08-27 Открытое Акционерное Общество "Российские Железные Дороги" Система подачи криогенного топлива для питания двигателя

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
"Gas-Turbine Traction: History and Outlook", LOCOMOTIVE MAGAZINE, 2005, pages 41

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3551493A4 (fr) * 2016-12-06 2020-07-29 CNGMotive Inc. Systèmes et procédés de production de puissance de véhicule
US11371445B2 (en) 2016-12-06 2022-06-28 Cngmotive, Inc. Systems and methods for vehicular power generation

Also Published As

Publication number Publication date
EA201201026A1 (ru) 2013-06-28
EA018298B1 (ru) 2013-06-28
CN103889808B (zh) 2016-03-02
CA2833117A1 (fr) 2014-02-17
CN103889808A (zh) 2014-06-25
CA2833117C (fr) 2015-06-09

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