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WO2020169191A1 - Système d'alimentation en carburant gazeux - Google Patents

Système d'alimentation en carburant gazeux Download PDF

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Publication number
WO2020169191A1
WO2020169191A1 PCT/EP2019/054191 EP2019054191W WO2020169191A1 WO 2020169191 A1 WO2020169191 A1 WO 2020169191A1 EP 2019054191 W EP2019054191 W EP 2019054191W WO 2020169191 A1 WO2020169191 A1 WO 2020169191A1
Authority
WO
WIPO (PCT)
Prior art keywords
flow passage
filter unit
supply line
fuel supply
feeding system
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.)
Ceased
Application number
PCT/EP2019/054191
Other languages
English (en)
Inventor
Klaus Widjeskog
Tomas HÖGNABBA
Marko KUUSISAARI
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.)
Wartsila Finland Oy
Original Assignee
Wartsila Finland Oy
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 Wartsila Finland Oy filed Critical Wartsila Finland Oy
Priority to PCT/EP2019/054191 priority Critical patent/WO2020169191A1/fr
Publication of WO2020169191A1 publication Critical patent/WO2020169191A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0221—Fuel storage reservoirs, e.g. cryogenic tanks
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0227—Means to treat or clean gaseous fuels or fuel systems, e.g. removal of tar, cracking, reforming or enriching
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/023—Valves; Pressure or flow regulators in the fuel supply or return system
    • F02M21/0242—Shut-off valves; Check valves; Safety valves; Pressure relief valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0293—Safety devices; Fail-safe measures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00—Flanged joints
    • F16L23/02—Flanged joints the flanges being connected by members tensioned axially
    • F16L23/032—Flanged joints the flanges being connected by members tensioned axially characterised by the shape or composition of the flanges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L39/00—Joints or fittings for double-walled or multi-channel pipes or pipe assemblies
    • F16L39/005—Joints or fittings for double-walled or multi-channel pipes or pipe assemblies for concentric pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C7/00—Methods or apparatus for discharging liquefied, solidified, or compressed gases from pressure vessels, not covered by another subclass
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D2273/00—Operation of filters specially adapted for separating dispersed particles from gases or vapours
    • B01D2273/10—Allowing a continuous bypass of at least part of the flow, e.g. of secondary air, vents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/0002—Casings; Housings; Frame constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/24—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
    • B01D46/2403—Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00—Flanged joints
    • F16L23/006—Attachments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L41/00—Branching pipes; Joining pipes to walls
    • F16L41/008—Branching pipes; Joining pipes to walls for connecting a measuring instrument
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0104—Shape cylindrical
    • F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/03—Orientation
    • F17C2201/035—Orientation with substantially horizontal main axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05—Size
    • F17C2201/054—Size medium (>1 m3)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/03—Thermal insulations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01—Mounting arrangements
    • F17C2205/0153—Details of mounting arrangements
    • F17C2205/018—Supporting feet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/03—Fluid connections, filters, valves, closure means or other attachments
    • F17C2205/0302—Fittings, valves, filters, or components in connection with the gas storage device
    • F17C2205/0341—Filters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/03—Mixtures
    • F17C2221/032—Hydrocarbons
    • F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146—Two-phase
    • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/01—Propulsion of the fluid
    • F17C2227/0107—Propulsion of the fluid by pressurising the ullage
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
    • F17C2227/03—Heat exchange with the fluid
    • F17C2227/0367—Localisation of heat exchange
    • F17C2227/0388—Localisation of heat exchange separate
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2265/00—Effects achieved by gas storage or gas handling
    • F17C2265/06—Fluid distribution
    • F17C2265/066—Fluid distribution for feeding engines for propulsion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0102—Applications for fluid transport or storage on or in the water
    • F17C2270/0105—Ships
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/30—Use of alternative fuels, e.g. biofuels

Definitions

  • the present invention relates to a gaseous fuel feeding system compris- ing a fuel supply line enclosed by a barrier wall system such that the fuel supply line comprises a primary flow passage for the gaseous fuel and a secondary flow passage around the primary flow passage inside the barrier wall system, accord ing to the preamble of claim 1.
  • Natural gas or in general mixtures of hydrocarbons that are volatile enough to make the mixture appear in gaseous form in room temperature, con stitutes an advantageous alternative to fuel oil as the fuel of internal combustion engines and will also enable more rapid transformation towards CO2 neutral fuels.
  • the natural gas In marine vessels that use natural gas as fuel, the natural gas is typically stored onboard in liquefied form, giving rise to the commonly used acronym LNG (Liquefied Natural Gas). Natural gas can be kept in liquid form by maintaining its temperature below a boiling point, which is approximately -162 degrees centi grade (-260 degrees Fahrenheit).
  • LNG Liquefied Natural Gas
  • Natural gas can be kept in liquid form by maintaining its temperature below a boiling point, which is approximately -162 degrees centi grade (-260 degrees Fahrenheit).
  • the output of the engines In internal combustion piston engines, for instance in the marine vessels, the output of the engines has constantly increased.
  • Fuel systems for feeding gaseous fuel to an internal combustion engine in a marine vessel are commonly constructed such that a fuel supply line runs inside, i.e. is enclosed by a barrier wall system, in order to prevent direct leakage to surrounding should the fuel supply line leak.
  • WO2015040267 A1 is referred to as an example of using gaseous fuel in one or more engines of a sea-going vessel. In particular it discloses an architec ture of the system that is used to store the gaseous fuel in liquefied form and to deliver it to the engine or engines as gaseous gas comprising an LNG bunkering station located on the deck of the vessel which is used to fill up the system with LNG.
  • an LNG fuel storage system comprising one or more thermally insulated tanks for storing the LNG in liquid form, and the so-called tank room where the LNG is controllably evaporated and its distribution to the en gine ⁇ ) is arranged.
  • the engine or engines of the vessel are located in an engine room.
  • Each engine has its respective engine-specific Gas Valve Unit (GVU).
  • the GVU includes for example a manual shut-off valve, a pressure control valve, a gas filter, and a block and bleed valve arrangement.
  • the GVU comprises a barrier wall system to controllably handle possible gas leak.
  • the bar rier wall system of the GVU comprises a vent line connecting the internal space of the GVU and the surroundings so that gas leakage can be vented out of the GVU in case of failure of the fuel supply line, such as a pipe rupture.
  • the gas pressure inside barrier wall system can increase too much due the fact that vent line cannot purge the pressure caused by the leaking gas, and will even tually break the fuel system.
  • An object of the invention is to provide a gaseous fuel feeding system in which the performance is considerably improved compared to the prior art solu tions by enhancing the pressure control during possible leakage situations im proving the system safety and reliability. Disclosure of the Invention
  • a gaseous fuel feeding sys tem comprises a fuel supply line which is enclosed by a barrier wall system such that the fuel supply line comprises a primary flow passage for the gaseous fuel and a secondary flow passage around the primary flow passage inside the barrier wall system.
  • the secondary flow passage among other things secures primary flow passage from direct leak into the surroundings.
  • the fuel supply line com prises a first fuel supply line section, and a second fuel supply line section and a filter unit between them.
  • the filter unit comprises a body and at least two coupling adapters arranged to the body of the filter, a filter element disposed in the body of the filter, wherein the primary flow passage in the filter body is arranged to extend through the coupling adapters and the filter element of the filter unit.
  • the filter unit comprises a primary flow passage and a secondary flow passage, wherein the secondary flow passage of the filter unit is arranged to extend through the coupling adapters and the body.
  • the secondary flow passage is sep arate and parallel to the primary flow passage in the filter unit, and the filter unit is coupled between the first and the second fuel supply line sections such that the primary flow passage in the first fuel supply line section is in flow connection with the primary flow passage in the second fuel supply line section via the pri mary flow passage and the filter element in the filter unit, and the secondary flow passage in the first fuel supply line section is in continuous flow connection with the secondary flow passage in the second fuel supply line section via the sec ondary flow passage in the filter unit.
  • the filter element may be of any suitable type and structure being known for those skilled in the art.
  • the fuel feeding system comprises a gas fuel tank configured to store the fuel in liquefied form, and a liquefied gas evaporation system, in which fuel feeding system the fuel supply line is arranged to extend from the tank to a gas valve unit arranged in the sys tem, and wherein the filter unit is arranged to the fuel supply line between the tank and the gas valve unit.
  • the secondary flow passage in the filter unit is provided with a flow throttling section. The flow throttling section is advantageously arranged in connection with the secondary flow passage in the coupling adapter of the filter unit.
  • the secondary flow passage in the filter unit is arranged to provide a continuous flow connection through the coupling adapters and the body of the filter unit.
  • the coupling adapters of the filter unit comprise a circular flange arranged perpendicularly to a center axis of the primary flow passage, and the primary flow passage is an opening arranged to the center of the flange, and the secondary flow passage comprises at least one opening in the flange at a radial distance from the primary flow passage.
  • the gaseous fuel feeding system can be fur ther developed by providing at least one one-way valve, such as a reed valve, into the secondary flow passage for preventing, or at least minimizing, possible back flow of the leaked gas in the secondary flow passage.
  • the filter unit is provided with at least one one-way valve in the secondary flow pas sage.
  • gaseous fuel feeding sys- tern configured to feed gaseous fuel to more than one gas consumer
  • the second fuel supply line section downstream the filter unit comprises several par allel branch sections, each one of which being provided with a gas valve unit, wherein the primary flow passage in the first fuel supply line section is in flow connection with the primary flow passage of each branch section of the second fuel supply line section via the primary flow passage of the filter unit and the filter element of the filter unit, and the secondary flow passage in the first fuel supply line section is in continuous flow connection with the secondary flow passage of each branch of the second fuel supply line section via the secondary flow pas sage of the filter unit.
  • the gaseous fuel feeding system can be further developed by providing at least one one-way valve, such as a reed valve, into at least one, advantageously in each one, of the secondary flow passage of each branch of the second fuel supply line section preventing, or at least minimizing, possible back flow of the leaked gas from the second fuel supply section to the first fuel supply section in the secondary flow passage.
  • At least one one-way valve such as a reed valve
  • Invention is also applicable to power plant which are directly connected to a source of gas without a need of a gas fuel tank.
  • the filter unit comprises a first flow connection path which opens into the first fluid passage at its first end and into an outer side of the filter unit at its second end for monitoring purposes.
  • the first flow connection path is provided with a pressure transmitter.
  • the first flow connection path is arranged to the at least one of the coupling adapters of the filter unit.
  • the filter unit comprises a second flow connection path which opens into the second fluid passage at its first end and into an outer side of the filter unit at its second end for monitoring purposes.
  • the second flow connec tion path is provided with a gas detector.
  • the second flow connec tion path is arranged to the at least one of the coupling adapters of the filter unit.
  • FIG. 1 illustrates a gaseous fuel feeding system according to an embodiment of the invention
  • Figure 2 illustrates a sectional view of a filter unit according to another embodi ment of the invention
  • Figure 3 illustrates a face view of a coupling flange of the filter unit according to still another embodiment of the invention
  • Figure 4 illustrates a gaseous fuel feeding system according to another embodi ment of the invention
  • FIG. 5 illustrates a gaseous fuel feeding system according to another embodi ment of the invention.
  • Figure 6 illustrates a filter unit according to another embodiment of the invention.
  • FIG. 1 depicts schematically a gaseous fuel feeding system 10 config ured to feed gaseous fuel to a gas consumer 1 such as a gas engine according to an embodiment of invention.
  • the gaseous fuel feeding system 10 comprises a gas fuel tank 14 configured to store the fuel mainly in liquefied form, the fuel being e.g. liquefied natural gas.
  • the tank has an inner shell 12 and an outer shell 14 between which an insulation is arranged.
  • the tank connection space is housing auxiliaries such as various valves and cryogenic pump (if needed) by means of which the emptying of the tank and fuel introduction to the engine is controlled.
  • the tank connection space is arranged gas tight but also accessible e.g. for maintenance.
  • the tank connection space is usually provided at one end of the tank 14 attached to the tank, but can also located within a distance of the tank 14.
  • the tank fuel feeding system 10 may comprise also a pressure build up system 18 in which an evaporator is arranged to evaporate the liquefied gas in the tank 14 and lead the evaporated gas back to the tank 14.
  • the fuel feeding system 10 may comprise a pump or alike in the primary flow passage 30.
  • the pressure build-up system 18 is housed by the tank connection space 16.
  • the tank fuel feeding system 10 may comprise also a main gas evaporator system 20 in which a main evaporator is arranged to evaporate the liquefied gas in the tank 14 and lead the evaporated gas to one or more gas consumers 1.
  • the main evaporator is housed by the tank connection space 16.
  • the fuel feeding system 10 comprises a fuel supply line 22 arranged to extend from the tank 14 or the tank connection space 16, as is the case in the figure 1 , to the gas consumer 1 , which may be for example an internal combus tion piston engine 1 such that the gas may be delivered to the engine 1 for use as its fuel.
  • the gas evaporator system 20 is configured to evaporate the liquefied gas into gaseous form and optionally to heat the evaporated gas to a desired temperature suitable for the engine 1.
  • the fuel feeding system 10 comprises a gas valve unit (GVU) 24 for each engine 1.
  • the gas valve unit 24 is arranged, in connection with or before, in other words upstream to the engine 1 in the normal flow direction of the gas.
  • the GVU 24 may comprise several control devices, such as gas feed pressure regulation device 26, a valve member and/or a num ber of desired optional instruments generally and collectively depicted by a box 28.
  • the instruments may comprise necessary equipment for measuring, analys ing, filtering or otherwise handling the gas and arranged in the gas valve unit 24.
  • the fuel supply line 22 is provided a primary flow passage 30 for the gas eous fuel, which may be in a form of an inner pipe.
  • the fuel supply line 22 is also provided with a barrier wall system 32, or an outer pipe, which forms a double wall surrounding the primary flow passage 30.
  • the primary flow passage 30 is an inner pipe and the barrier is an outer pipe arranged substantially coaxially to each other.
  • the GVU 24 also comprises a barrier wall system 32’ enclosing the gas handling de vices inside the gas valve unit 24.
  • the space between the primary flow passage 30 and the barrier wall 32, 32’ forms a secondary flow passage 34 for the gas. So, the possibly leaked gas is gathered into the secondary flow passage making it possible to safely handle the leaked gas, which may be highly toxic e.g. to environment and humans.
  • the fuel supply line 22 comprises, starting from the tank connection space 16, successively a first line section 22.1 and a second line section 22.2 and a filter unit 100 coupled between the first and the second fuel supply line sections 22.1 , 22.2.
  • the primary flow passage 30 in the first fuel supply line section 22.1 is in flow connection with the primary flow passage 30 in the second fuel supply line section 22.2 via a primary flow passage 30’ of the filter unit 100.
  • the primary flow passage 30’ of the filter unit 100 comprises at least one filter element 102.
  • the secondary flow passage 34 in the first fuel sup ply line section 22.1 is in continuous flow connection with the secondary flow passage 34 in the second fuel supply line section 22.2 via a secondary flow pas sage 34’ of the filter unit 100.
  • the secondary flow passage 34’ and the primary flow passage 34 in the filter unit 100 are separate passages parallel with each other. The structure and operation of the filter unit 100 and the flow passages will be described later in more detailed manner.
  • FIG. 2 there is schematically shown a sectional view of the filter unit 100 according to an embodiment of the invention in more detail.
  • the filter unit 100 comprises a body 110 and coupling adapters 112 at its opposite ends for coupling the filter unit 100 to the fuel supply line 20 between the first and the second fuel supply line sections 22.1 , 22.2.
  • the filter unit 100 comprises a primary flow passage 30’ and a secondary flow passage 34’ fluidly separated from each other and arranged parallel to each other.
  • the primary flow passage 30’ of the filter unit 100 is arranged to extend through the coupling adapters 112 and through a filter element 1 14 provided in the body 110 of the filter unit 100. Instead of one filter element 1 14 there may be several filter elements arranged parallel to each other.
  • the secondary flow pas sage 34’ is arranged to extend through the coupling adapters 112 and the body 1 10 of the filter unit 100 so as to form a second flow connection through the filter unit 100.
  • the secondary flow passage 34’ is fluidly separated from the primary flow passage 30’.
  • Each one of the coupling adapters 112 comprise a circular flange ar ranged perpendicularly to a center axis A of the primary flow passage 30’.
  • the flange 112 is arranged to the body of the filter unit such that the primary flow passage 30’ is symmetrical to the center of the flange 112.
  • the body 110 comprises a first enclosure 116 and a second enclosure 118 arranged between the coupling adapters 1 12 in length wise. Both of the enclosures are generally of cylindrical shape having their axial ends attached to the flanges 112 in a gas tight manner.
  • the filter unit 100 comprises a first flow connection path 61 , which opens into the first fluid passage 30’ at its first end and into an outer side of the of the valve unit 100 at its second end.
  • the first flow connection path 61 is advantageously arranged to the at least one of the coupling flanges 112 of the valve unit 100.
  • the first flow connection path may be advantageously a radial bore in the coupling flange. If needed or otherwise desired, such can be arranged in more than one of the coupling flanges 112.
  • the first flow connection path 61 is arranged for e.g. measuring or detection pur poses.
  • the first flow connection path 61 may be provided with a pressure trans mitter 60.
  • Pressure measurements of the gas in the first fluid passage may be carried out via the first flow path 61. This allows the operation of filter unit 100 and the entire fuel feeding system to be controlled in more accurate manner. If a flow connection path 61 is provided at the coupling flanges at both ends of the filter unit 100 for pressure measurements, a differential pressure can be deter mined, and then monitor the function of filter unit 100, for example.
  • a second flow connection path 62 The filter unit is provided alternatively, or in addition to the first flow connection path 61 the second flow connection path 62, which opens into the second fluid passage 34’ of the filter unit 100 at its first end and into an outer side of the filter unit 100 at its second end.
  • the second flow connection path 62 is arranged to the at least one of the coupling flanges 112.
  • the second flow connection path may be advantageously a radial bore in the coupling flange. If needed, such can be arranged in more than one of for coupling flanges 1 12 as well.
  • the second flow connection path 62 is advantageously provided with a gas detector and/or a pressure transmitter 64.
  • the second enclosure 118 is arranged to enclose the first enclosure 116.
  • the first enclosure 116 and the second enclosure 118 are ar ranged parallel to the center axis A of the primary flow passage.
  • the primary flow passage 30’ is inside the first enclosure 116 and the secondary flow passage 34’ is arranged radially between the first enclosure 116 and the second enclosure 118.
  • the filter element 114 is arranged inside the first enclosure 114.
  • the filter element 1 14 is coupled to the first enclosure 116 in gas tight manner so that the gas flow cannot bypass the filter element 1 14 in the primary flow passage 30’.
  • the first enclosure 116 and the second enclosure 118 are arranged coaxially with respect to each other. That is not absolutely essential to the inven- tion although it makes is easier to manufacture the filter unit 100 this way.
  • the first and the second enclosures 1 16, 118 are arranged to extend between the coupling flanges 112.
  • the filter element is of cylindrical form.
  • the filter element provided with an inlet opening 120 at its first axial end and with an end wall 122 at its second axial end.
  • the filter element divides the primary flow passage 30’ into inlet side 30. T and into outlet side channel 30.2’. Outlet 123 of the primary flow passage 30’ opens into the outlet side channel 30.2’ in the filter unit 100.
  • the filter unit 100 shown in the figure 2 can be coupled to the fuel feeding system 10 shown in the figure 1 such that the coupling flanges 112 of the filter unit 100 are attached to the fuel supply line 22 with a counter-flanges welded into the piping structure of the fuel supply line 22.
  • Figure 3 shows a face view of the coupling flanges 112 of the filter unit 100 according to the figure 2. As can be seen in the figure 3 the coupling flange
  • first opening 1 12 is provided with a first center opening 112.1 and plurality of second openings 1 12.2 arranged at a radial distance from the first opening 112.1 angularly distrib uted around the first opening 1 12.1.
  • the first opening 1 12.1 forms as its part the primary flow passage 30’ and the second openings 112.2 form the secondary flow passage 34’ of the coupling flange 112.
  • first flow connection path 61 and the second flow connection path 62 in the coupling flange 112. Both the flow connection paths are formed by radial borings.
  • the number of second openings 1 12.2 and the distribution of the open ings may vary depending on the case.
  • the second openings 1 12.2 act as a throt tling section providing suitable local pressure loss coefficient to potential gas flow in the secondary flow passage 34’.
  • the secondary flow passage 34’ forms a continuous flow connection through the coupling adapters 112 and the body 110 of the filter unit 100 surrounding the primary flow passage 30’.
  • the primary flow passage 30 in the first fuel supply line section 22.1 is in flow connection with the primary flow passage 30 in the second fuel supply line section 22.2 via the primary flow passage 30’ of the filter unit 100.
  • the primary flow passage 30’ is arranged to provide a flow connection through the coupling adapters, i.e. coupling flanges 112, the body 110 and the filter element 114.
  • the secondary flow passage 34 in the first fuel supply line section 22.1 is in continuous flow connection with the sec ondary flow passage 34 in the second fuel supply line section 22.2 via the sec ondary flow passage 34’ of the filter unit 100.
  • the secondary flow passage 34’ is arranged to provide a continuous flow connection through the coupling adapters, i.e. extending through the coupling flanges 112 and the body 110. Thus it forms a passage parallel to the primary flow passage between the flanges 112.
  • the second openings 1 12.2 in the flange 112 are advantageously arranged to restrict the flow from the first fuel supply line section 22.1 to second fuel supply line section 22.2 through the filter unit 100.
  • the second openings 1 12.2 therefore act as a flow throttling section.
  • the size, form and number of openings 112.2 is defined and calculated on a case-specific basis.
  • the openings 1 12.2 i.e. the flow throttling section provides a local reduction to the face area of the secondary flow passage 34’ of the filter unit 100.
  • the reduction to the face area is 10-70%.
  • equipment fail e.g.
  • the second openings 112.2 in the flange 112 may be advanta geously provided with one-way valves 124 such that an allowed flow direction of the gas of the valve is towards the gas valve unit 24.
  • the one-way valve may be for example a reed valve comprising a flexible flap covering the second opening 1 12.2 providing an automatic flow control for the gas.
  • the flap is fastened to the flange with suitable means, such as a screws of alike (not shown).
  • the second openings 1 12.2 for the secondary flow passage 34’ are arranged at a radial distance from the first opening 112.2.
  • the second openings 112.2 are also preferably angularly evenly distributed around the primary flow passage 30’ in the flange 112. It is also an operable, if not preferred in all cases, that the second openings 112.2 are unevenly distrib uted.
  • the second openings 112.2 can be in the form of various shapes, prefera- bly elongated or circular shapes.
  • the filter unit 100 is arranged on the fuel supply line 22 between the tank 14 and the gas valve unit 24.
  • the location is preferably selected so that the location is closer to the gas valve unit 24 than to the tank, although the loca- tion can be arranged in anywhere on the fuel supply line 22 depending on the need, i.e., where the system requires protection against a pressure increase.
  • Ad vantageously the filter unit 100 is right next to the gas valve unit 24.
  • the filter unit 100 is advanta geously utilized in a gaseous fuel feeding system in a following manner. Firstly, during normal operation of the system the filter unit 100 removes impurities from the gas flowing through the filter element 144. Should there emerge a rupture in the primary flow passage 30 of the first fuel supply line section 22.1 , the flow communication of the primary flow passage 30 between the first and the second fuel supply line sections 22.1 , 22.2 is also advantageously closed by a valve not shown in the figure 1. If the leak is in the first fuel supply line section 22.1 i.e.
  • the leaked gas continues to flow into the sec- ondary flow passage 34 of the gas valve unit 24 through the secondary flow pas sage 34’ of the filter unit 100.
  • the flow rate through the secondary flow passage 34’ is kept restricted by the flow throttling section i.e. the second opening 112.2 in secondary flow passage 34’ of the filter unit 100.
  • the gas valve unit 24 com prises a vent channel 27 which opens into the secondary flow passage 34.
  • the tank connection space may be provided with a vent channel 27. Only a certain flow rate of gas can be obtained through the vent channel and the flow rate into the gas valve unit 24 is restricted by the flow throttling section 112.2.
  • the pres sure rise in the gas valve unit is thus kept moderate and the construction of the gas valve unit 24 can be dimensioned to endure lower pressure level. Additionally the risk of damages caused to any instruments assembled in the gas valve unit is minimized.
  • the flow rate of the leaking gas in the secondary flow passage 34 is considerably lower so that it will not cause damages to the gas valve unit 24 and the barrier wall system 32’ of the gas valve unit 24. This way, if the first fuel supply line 30 is ruptured, rapid flow of the gas via the secondary flow pas- sage 32 to inside the barrier wall system 32’ of the gas valve unit 24 can be prevented.
  • the secondary flow pas sage 34’ in the filter element 100 is provided with a separate flow throttling ele ment removably assembled to the second opening 112.2. Throttling effect can also be accomplished by dimensioning the secondary flow passage 34’ of the filter unit 100 such that it provides desired local pressure loss which limits the pressure raise rate in the gas valve unit 24.
  • Figure 4 depicts a further developed advantageous embodiment of that shown in the figure 1.
  • the gaseous fuel feeding system 10 is configured to feed gaseous fuel to more than one gas consumer 1.
  • the fuel feeding system 10 com prises a fuel supply line 22 arranged to extend from the tank 14 or the tank con- nection space 16 to more than one gas consumers 1 , which may be for example internal combustion piston engines 1.
  • the fuel supply line 22 comprises parallel branch sections which are branching downstream the filter unit 100. This way one filter unit 100 of the gaseous fuel feeding system is configured to serve more than one gas consumers.
  • Figure 5 depicts a further developed advantageous embodiment of that shown in the figure 4.
  • the gaseous fuel feeding system 10 is configured to feed gaseous fuel to more than one gas consumer 1.
  • the fuel feeding system 10 com prises a fuel supply line 22 arranged to extend from the tank 14 or the tank con nection space 16 to more than one gas consumers 1 , which may be for example internal combustion piston engines 1.
  • the fuel supply line 22 comprises parallel branch sections which are branching in the filter unit 100. This way one filter unit 100 of the gaseous fuel feeding system is configured to serve more than one gas consumers.
  • the fuel feeding system 10 com- prises a gas valve unit 24 for each engine 1.
  • the gas valve unit 24 is arranged before, or upstream to each one of the engines 1 , in the normal flow direction of the gas.
  • the fuel supply line 22 is provided a primary flow passage 30 for the gas eous fuel, which may be in a form of an inner pipe.
  • the fuel supply line 22 is also provided with a barrier wall system 32, or an outer pipe, which forms a double wall surrounding the primary flow passage 30.
  • the primary flow passage 30 in the first fuel supply line section 22.1 is in flow connection with the primary flow passage 30 in each parallel branch section of the second fuel supply line section 22.2 via the primary flow passage 30’ and the filter element 114 of the filter unit 100
  • the secondary flow passage 34 in the first fuel supply line section 22.1 is in continuous flow connection with the sec ondary flow passage 34 in each parallel the second fuel supply line section 22.2 via the secondary flow passage 34’ of the filter unit 22.
  • the second fuel supply section 22.2 branches at one common branch point which in advan tageous in the filter unit 100. It is also conceivable to arrange the branch point outside the filter unit 100, as is shown in the figure 4, even if in that case the fuel feeding system is more complex.
  • the branch point outside the filter unit 100, as is shown in the figure 4, even if in that case the fuel feeding system is more complex.
  • the leaked gas continues to flow into the secondary flow passage 34 of the gas valve unit 24 through the secondary flow passage 34’ of the filter unit 100.
  • the flow rate through the secondary flow passage 34’ is kept restricted by the flow throttling section i.e. the second opening 1 12.2 in secondary flow passage 34’ of the filter unit 100.
  • each of the branch sections of the fuel supply line 22 is provided with at least one one-way valve 128 in connection with its secondary flow pas sage 34.
  • the one-way valve may be for example a reed valve.
  • the one-way valve is arranged in connection with the filter unit 100, advantageously integrated thereto.
  • the one-way valve is arranged so as to prevent or at least minimize possible back flow of the leaked gas from a branch section to the upstream side of the filter unit 100 and to other branch sections.
  • Figure 6 discloses a filter unit 100 which has a provision of branching the second fuel supply line section 22.2 in connection with the filter unit 100.
  • the filter unit is provided with a common inlet 121 comprising the primary flow pas sage 30 and the secondary flow passage 34.
  • the filter unit 100 according to figure 5 has several outlets 123 in which the primary flow passages are opening into common outlet side channel 30.2’ inside the filter unit 100, which may be referred to as a primary manifold section.
  • the secondary flow passages are opening into a common outlet side channel 34’ inside the filter unit 100, which may be referred to as a secondary manifold section.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Combustion & Propulsion (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

L'Invention concerne un système d'alimentation en carburant gazeux (10), comprenant une conduite d'alimentation en carburant (22) entourée par un système de paroi barrière (32,32') de telle sorte que la conduite d'alimentation en carburant (22) comprend un passage d'écoulement primaire (30,30') pour le combustible gazeux et un passage d'écoulement secondaire (34,34') autour du passage d'écoulement primaire (30,30') à l'intérieur du système de paroi de barrière (32,32'.). La conduite d'alimentation en carburant (22) comprend une première section de conduite d'alimentation en carburant (22.1), et une seconde section de conduite d'alimentation en carburant (22.2), et il y a une unité de filtre (100) dans le système comprenant un corps (110) et au moins deux adaptateurs de couplage (112) disposés sur le corps (110), et l'élément de filtre (102) disposé dans le corps (110), dans lequel l'unité de filtre (100) comprend un passage d'écoulement primaire (30') et un passage d'écoulement secondaire (34') et le passage d'écoulement primaire (30') est conçu pour s'étendre à travers les adaptateurs de couplage (1 12) et l'élément de filtre (102) de l'unité de filtre (100), et le passage d'écoulement secondaire (34') de l'unité de filtre (100) est agencé pour s'étendre à travers les adaptateurs de couplage (1 12) et le corps (1 10), et lequel passage d'écoulement secondaire (34') est séparé et parallèle au passage d'écoulement principal (30') dans l'unité de filtre (100), et l'unité de filtre (100) étant couplée entre les première et seconde sections de ligne d'alimentation en carburant (22.1, 22.2) de telle sorte que le passage d'écoulement primaire (30) dans la première section de ligne d'alimentation en carburant (22.1, 22.2) est en connexion d'écoulement avec le passage d'écoulement primaire (30) dans la seconde section de ligne d'alimentation en carburant (22.2) par l'intermédiaire du passage d'écoulement primaire (30') et de l'élément de filtre (102) dans l'unité de filtre (100), et le passage d'écoulement secondaire (34) dans la première section de conduite d'alimentation en carburant est en liaison d'écoulement continu avec le passage d'écoulement secondaire (34) dans la seconde section de conduite d'alimentation en carburant (16.2) par l'intermédiaire du passage d'écoulement secondaire (34') dans l'unité de filtre (100).
PCT/EP2019/054191 2019-02-20 2019-02-20 Système d'alimentation en carburant gazeux Ceased WO2020169191A1 (fr)

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PCT/EP2019/054191 WO2020169191A1 (fr) 2019-02-20 2019-02-20 Système d'alimentation en carburant gazeux

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20240125429A1 (en) * 2022-10-13 2024-04-18 L'air Liquide, Societe Anonyme Pour L'etude Et L’Exploitation Des Procedes Georges Claude Cryogenic unit

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2589791A1 (fr) * 2011-11-04 2013-05-08 Caterpillar Motoren GmbH & Co. KG Soupape d'admission de carburant et culasse pour accueillir la soupape d'admission de carburant
WO2015040267A1 (fr) 2013-09-20 2015-03-26 Wärtsilä Finland Oy Système de stockage de carburant et unité de vanne de gaz intégrée
EP3098430A1 (fr) * 2015-05-28 2016-11-30 Caterpillar Motoren GmbH & Co. KG Unité de vannes de gaz a double paroi
WO2018087417A1 (fr) * 2016-11-11 2018-05-17 Wärtsilä Finland Oy Agencement de tuyaux de gaz
WO2018134437A1 (fr) * 2017-01-23 2018-07-26 Eltronic A/S Unité de traitement pour matériau dangereux

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2589791A1 (fr) * 2011-11-04 2013-05-08 Caterpillar Motoren GmbH & Co. KG Soupape d'admission de carburant et culasse pour accueillir la soupape d'admission de carburant
WO2015040267A1 (fr) 2013-09-20 2015-03-26 Wärtsilä Finland Oy Système de stockage de carburant et unité de vanne de gaz intégrée
EP3098430A1 (fr) * 2015-05-28 2016-11-30 Caterpillar Motoren GmbH & Co. KG Unité de vannes de gaz a double paroi
WO2018087417A1 (fr) * 2016-11-11 2018-05-17 Wärtsilä Finland Oy Agencement de tuyaux de gaz
WO2018134437A1 (fr) * 2017-01-23 2018-07-26 Eltronic A/S Unité de traitement pour matériau dangereux

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20240125429A1 (en) * 2022-10-13 2024-04-18 L'air Liquide, Societe Anonyme Pour L'etude Et L’Exploitation Des Procedes Georges Claude Cryogenic unit

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