WO2014078962A1 - Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine - Google Patents

Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine Download PDF

Info

Publication number
WO2014078962A1
WO2014078962A1 PCT/CA2013/050890 CA2013050890W WO2014078962A1 WO 2014078962 A1 WO2014078962 A1 WO 2014078962A1 CA 2013050890 W CA2013050890 W CA 2013050890W WO 2014078962 A1 WO2014078962 A1 WO 2014078962A1
Authority
WO
WIPO (PCT)
Prior art keywords
fuel
pressure
engine
vapor
pump
Prior art date
Application number
PCT/CA2013/050890
Other languages
French (fr)
Inventor
Gage D. GARNER
Stephen C. Anderson
Original Assignee
Westport Power Inc.
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 Westport Power Inc. filed Critical Westport Power Inc.
Priority to CN201380061316.5A priority Critical patent/CN104813016B/en
Priority to EP13857182.3A priority patent/EP2923062B1/en
Publication of WO2014078962A1 publication Critical patent/WO2014078962A1/en
Priority to US14/719,650 priority patent/US9771886B2/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/30—Controlling fuel injection
    • F02D41/3082—Control of electrical fuel pumps
    • 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
    • F17C5/00—Methods or apparatus for filling containers with liquefied, solidified, or compressed gases under pressures
    • F17C5/002—Automated filling apparatus
    • F17C5/007—Automated filling apparatus for individual gas tanks or containers, e.g. in vehicles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D19/00—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D19/02—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with gaseous fuels
    • F02D19/021—Control of components of the fuel supply system
    • F02D19/022—Control of components of the fuel supply system to adjust the fuel pressure, temperature or composition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D19/00—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D19/02—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with gaseous fuels
    • F02D19/026—Measuring or estimating parameters related to the fuel supply system
    • F02D19/027—Determining the fuel pressure, temperature or volume flow, the fuel tank fill level or a valve position
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D41/0027—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures the fuel being gaseous
    • 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
    • F02M21/0221—Fuel storage reservoirs, e.g. cryogenic tanks
    • F02M21/0224—Secondary gaseous fuel storages
    • 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
    • F02M21/0245—High pressure fuel supply systems; Rails; Pumps; Arrangement of 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
    • F02M21/0287—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers characterised by the transition from liquid to gaseous phase ; Injection in liquid phase; Cooling and low temperature storage
    • 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
    • F02M51/00—Fuel-injection apparatus characterised by being operated electrically
    • F02M51/04—Pumps peculiar thereto
    • 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
    • F02M57/00—Fuel-injectors combined or associated with other devices
    • F02M57/04—Fuel-injectors combined or associated with other devices the devices being combustion-air intake or exhaust valves
    • 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
    • F17C2205/0323—Valves
    • F17C2205/0326—Valves electrically actuated
    • 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
    • F17C2205/0323—Valves
    • F17C2205/0335—Check-valves or non-return valves
    • 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
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033—Small pressure, e.g. for liquefied gas
    • 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
    • F17C2223/04—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
    • F17C2223/042—Localisation of the removal point
    • F17C2223/043—Localisation of the removal point in the gas
    • 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
    • F17C2223/04—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
    • F17C2223/042—Localisation of the removal point
    • F17C2223/046—Localisation of the removal point in the liquid
    • 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
    • F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/01—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the phase
    • F17C2225/0107—Single phase
    • F17C2225/0123—Single phase gaseous, e.g. CNG, GNC
    • 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
    • F17C2225/00—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel
    • F17C2225/03—Handled fluid after transfer, i.e. state of fluid after transfer from the vessel characterised by the pressure level
    • F17C2225/035—High pressure, i.e. between 10 and 80 bars
    • 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
    • F17C2227/0128—Propulsion of the fluid with pumps or compressors
    • F17C2227/0135—Pumps
    • F17C2227/0142—Pumps with specified pump type, e.g. piston or impulsive type
    • 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
    • F17C2227/0128—Propulsion of the fluid with pumps or compressors
    • F17C2227/0171—Arrangement
    • F17C2227/0178—Arrangement in the vessel
    • 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
    • F17C2227/0128—Propulsion of the fluid with pumps or compressors
    • F17C2227/0171—Arrangement
    • F17C2227/0185—Arrangement comprising several pumps or compressors
    • 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
    • F17C2227/0302—Heat exchange with the fluid by heating
    • F17C2227/0309—Heat exchange with the fluid by heating using another fluid
    • 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
    • F17C2227/0302—Heat exchange with the fluid by heating
    • F17C2227/0309—Heat exchange with the fluid by heating using another fluid
    • F17C2227/0323—Heat exchange with the fluid by heating using another fluid in a closed loop
    • 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
    • F17C2227/0302—Heat exchange with the fluid by heating
    • F17C2227/0327—Heat exchange with the fluid by heating with recovery of heat
    • 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
    • F17C2227/0393—Localisation of heat exchange separate using a vaporiser
    • 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
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/03—Control means
    • F17C2250/032—Control means using computers
    • 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
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • 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
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/043—Pressure
    • 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
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/0439—Temperature
    • 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
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0486—Indicating or measuring characterised by the location
    • F17C2250/0491—Parameters measured at or inside the vessel
    • 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
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/04—Reducing risks and environmental impact
    • F17C2260/046—Enhancing energy recovery
    • 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
    • F17C2265/02—Mixing fluids
    • F17C2265/022—Mixing fluids identical fluid
    • 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
    • F17C2265/03—Treating the boil-off
    • F17C2265/032—Treating the boil-off by recovery
    • F17C2265/036—Treating the boil-off by recovery with heating
    • 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
    • F17C2270/0165—Applications for fluid transport or storage on the road
    • F17C2270/0168—Applications for fluid transport or storage on the road by vehicles
    • 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 disclosure relates to a method and a system for delivering a cryogenically stored fuel to the air intake system of gaseous fuelled internal combustion engine.
  • a fuel storage and delivery system for an internal combustion engine that is fuelled with a gaseous fuel such as natural gas is an example of an application that is particularly suited for the disclosed method and system.
  • Natural gas has been used to fuel vehicle engines for many years. The fuel supplied to a natural gas driven vehicle is stored either in a liquefied natural gas (LNG) tank or in a compressed natural gas (CNG) cylinder.
  • LNG liquefied natural gas
  • CNG compressed natural gas
  • CNG is normally stored at ambient temperatures at pressures up to 3600 pounds per square inch while LNG is normally stored in a cryogenic storage vessel at temperatures of between about -240° F and -175° F (about -150° C and -115° C) and at pressures of between 15 and 200 psig.
  • CNG has been the more broadly adopted form of fuel storage but it has a lower energy density compared to LNG. Now that natural gas is gaining greater acceptance as a fuel for transportation, the benefit of the higher energy density for LNG is attractive for vehicles that require a longer range between re-fuelling. LNG provides an energy density of about four times that of CNG with the aforementioned storage conditions.
  • Natural gas fuelled engines can operate by injecting the fuel in the engine's air intake manifold or by injecting the fuel directly into the engine's combustion chambers.
  • the required fuel supply pressure is relatively low, for example around 100 psig.
  • the fuel supply system has to deliver natural gas to the injector at higher pressures, for example at pressures of at least 3000 psig.
  • LNG low pressure fuelling systems described in the prior art generally comprise a liquid conduit which supplies liquid fuel from the storage vessel to the engine through a supply line comprising a vaporizer. Fuel is stored in the storage vessel at a pressure of around 150 psi which is higher than the fuel delivery pressure to the engine which can be between 70 to 100 psi.
  • One known method of increasing the pressure in the LNG storage vessel is to use pressure building coils interposed between the walls of a double-walled cryogenic tank which circulate low temperature fuel from the tank. Heat transferred from to the exterior through the wall of the LNG storage vessel to the pressure building coil vaporizes the liquid fuel and the created vapor can be supplied directly into the headspace of the storage vessel through a regulator when the pressure in the headspace becomes lower than a predetermined value.
  • a pressure building circuit is described in United States Patent Number 4,947,651.
  • the pressure building coil is external to the cryogenic tank.
  • cryogenic liquid from the tank is fed to a pressure builder heat exchanger where the liquid is vaporized and the produced gas is delivered to the tank to pressurize it.
  • a method for delivering a fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine comprises: determining a required fuel supply pressure according to an operating condition of the engine;
  • the step of determining the required fuel supply pressure comprises first determining a required engine intake pressure as a function of engine operating conditions and then adding to it a predetermined pressure threshold. Because the required fuel supply pressure is preferably higher than the engine intake pressure the dynamic engine demands can be easily met by the system pressure.
  • the predetermined pressure threshold which is added to the engine intake pressure to determine the required fuel supply pressure is also determined as a function of the engine operating condition.
  • the engine operating condition can be determined from a map stored in the controller's memory that correlates the engine speed with a parameter indicative of the engine condition, for example a parameter indicative of the fuel demand, such as the throttle position.
  • the step of activating the fuel pump comprises supplying hydraulic fluid from a hydraulic pump to a hydraulic drive unit that drives the fuel pump.
  • the hydraulic pump is preferably driven by an electric motor and the electric motor is driven independently from the operation of the internal combustion engine such that the fuel pump can be activated independently of the engine condition.
  • at least two hydraulic pumps can supply hydraulic fluid to the hydraulic drive unit that the drives the fuel pump and the present method further comprises electrically activating at least two hydraulic pumps at the same time for delivering hydraulic fluid to said hydraulic drive unit when a commanded hydraulic fluid flow rate is higher than that which can be supplied by only one hydraulic pump.
  • the temperature of the fuel is increased by flowing it through a heat exchanger.
  • the method can comprise increasing the heat exchange rate in the heat exchanger when the fuel is supplied from the liquid space of the fuel storage vessel, compared to when the fuel is supplied from the vapor space of the fuel storage vessel.
  • the heat exchange rate in the heat exchanger is not controlled by the system controller and is set to be constant.
  • the present method of delivering fuel to the engine further comprises: measuring pressure in the vapor space of each one of the plurality of storage vessels; comparing the measured pressure in the vapor space of each one of the plurality of storage vessels with the required fuel supply pressure; supplying fuel from the vapor space of any one of the plurality of storage vessels in which vapor pressure is higher than the required system fuel supply pressure; or activating the fuel pump and supplying fuel from one of the plurality of storage vessels when none of the plurality of storage vessels has a vapor pressure higher than the required system fuel supply pressure.
  • This method which involves supplying fuel from one of the plurality of storage vessels can further comprise measuring the amount of fuel in each of the plurality of storage vessels and, when activating the fuel pump, supplying fuel from one of the plurality of storage vessels that has the largest amount of fuel.
  • the present method further comprises: measuring pressure in the vapor space of each one of the plurality of storage vessels; comparing the measured pressure in the vapor space of each one of the plurality of storage vessels with the required fuel supply pressure; supplying fuel from the vapor space of any one of the plurality of storage vessels in which vapor pressure is higher than the required system fuel supply pressure; or selecting and activating one of the fuel pumps and supplying fuel from an associated one of the plurality of storage vessels when none of the plurality of storage vessels has a vapor pressure higher than the required system fuel supply pressure.
  • the step of selecting one of the fuel pumps that is to be activated is determined by operating each one of the fuel pumps in sequential order.
  • the step of selecting one of the fuel pumps that is to be activated is determined by measuring the amount of fuel in each one of the plurality of storage vessels and selecting the one of the plurality of fuel pumps that is associated with the storage vessel that has the largest amount of fuel.
  • the method further comprises increasing the temperature of the fuel by flowing it through a heat exchanger associated with a respective storage vessel from which fuel is supplied to the engine.
  • a system for delivering fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine.
  • the system comprises: a) a storage vessel for holding the fuel; b) a fuel pump fluidly connected to receive fuel from a liquid space of the storage vessel; c) a liquid supply line in fluid communication with a discharge outlet of the fuel pump for delivering fuel from the discharge outlet of the fuel pump to a delivery line which delivers fuel to the engine; d) a vapor supply line in fluid communication with a vapor space of the storage vessel for delivering fuel in a gaseous state from the vapor space to the delivery line; e) a pressure sensor for measuring vapor pressure in the vapor space of the storage vessel; and f) a controller which receives pressure measurements from the pressure sensor, determines a required fuel supply pressure according to an operating condition of the engine and compares the measured pressure to the required fuel supply pressure, wherein the controller commands the fuel pump to operate when the measured pressure is lower than the required fuel supply pressure.
  • the system preferably comprises a heat exchanger placed in the delivery line for increasing the temperature of the fuel being supplied to the engine.
  • the system also comprises a hydraulic pump which supplies hydraulic fluid to a hydraulic drive unit that drives the fuel pump.
  • the hydraulic pump is driven by an electric motor which operates independently from the operation of the engine such that the operation of the fuel pump can be controlled independently of the engine operation.
  • the system comprises at least two hydraulic pumps which can be electrically activated to deliver hydraulic fluid to the hydraulic drive unit that drives the fuel pump.
  • the fuel pump is disposed within a cryogenic space of the storage vessel.
  • the system comprises more than one storage vessel.
  • Each storage vessel in the system has a respective vapor space and a liquid space, and is fluidly connected to the fuel pump.
  • the controller is programmed to activate the fuel pump to supply fuel from the liquid space of one of the plurality of storage vessels when none of the plurality of storage vessels has a vapor pressure higher than the required fuel supply pressure.
  • the system comprises more than one storage vessel, each storage vessel having a respective vapor space and liquid space, and each being fluidly connected to a respective fuel pump.
  • the controller is programmed to select and activate one of the fuel pumps and supply fuel from a storage vessel associated with the selected fuel pump when none of the plurality of storage vessels has a vapor pressure higher than the required fuel supply pressure.
  • the system comprises an engine that is the prime mover for a vehicle.
  • Figure 1 is schematic diagram of a system for delivering fuel in gaseous state into the air intake system of an internal combustion engine according to the present disclosure
  • Figure 2 is a schematic diagram illustrating the basic steps of a method for delivering fuel from a cryogenic storage vessel to the air intake system of a gaseous fuelled internal combustion engine according to the present disclosure
  • Figure 3 is a representation of a map correlating the engine speed with the throttle position which is used by the system's controller to determine the engine operating condition
  • Figure 4 is schematic diagram of another embodiment of a fuel delivery system comprising two hydraulic pumps for supplying hydraulic fluid to the hydraulic drive unit of the system's fuel pump;
  • Figure 5 is a schematic diagram of another embodiment of a fuel delivery system comprising two fuel storage vessels, each storage vessel being associated with a fuel pump, and a controller which activates each of the fuel pumps according to the method described in the present disclosure
  • Figure 6 is a schematic diagram of another embodiment of a fuel delivery system comprising two fuel storage vessels which are both fluidly connected to one external fuel pump and a controller which activates the fuel pump according to the method described in the present disclosure.
  • FIG. 1 schematically illustrates a fuel delivery system 100 which is employed to supply a fuel in gaseous state into the air intake system of an internal combustion engine.
  • Engine 110 is an internal combustion engine which is operated by injecting fuel into the engine's air intake manifold or into the air intake port, which is a different method than injecting fuel directly into the engine's combustion chamber.
  • Gaseous fuel is injected into the engine's air intake manifold 111 or into the air intake ports 113 at pressures that are generally around 70 to 100 psig (pounds per square inch gauge) and can reach around 500 psig. Such pressures are much lower than the operating pressure of a direct injection internal combustion engine where gaseous fuel is injected directly into the combustion chamber at around 4000 psig.
  • Fuel delivery system 100 comprises fuel storage vessel 112 which stores gaseous fuel in liquefied form at cryogenic temperatures in liquid space 114 within the cryogenic space of the storage vessel. Since heat is transmitted from the surrounding environment to the walls of the storage vessel, liquid fuel stored in the vessel can vaporize and the generated vapor occupies the headspace of the storage vessel, creating a vapor space 116.
  • Liquid space 114 is fluidly connected to fuel pump 118 which can be placed inside the cryogenic space of the storage vessel, as illustrated in the embodiment shown in Figure 1, or can be an external pump that communicates through a supply line with the liquid space in the storage vessel.
  • Fuel pump 118 can be activated by starting hydraulic pump 120 which supplies hydraulic fluid from storage vessel 121 through flow switching device 124 to the hydraulic drive unit of fuel pump 118.
  • Hydraulic pump 120 is driven by an electric motor and therefore can operate independently of the operating condition of the engine.
  • the hydraulic pump that activates the fuel pump is mechanically actuated by the engine accessory drive and therefore depends on the engine rotation (rpm).
  • Liquid fuel from liquid space 114 of fuel storage vessel 112 can be pumped by fuel pump 118 through liquid fuel supply line 123 to delivery line 122 which supplies fuel to engine 110.
  • Liquid fuel supply line 123 comprises a check valve 125 which prevents fuel backflow to the storage vessel.
  • Fuel in vapor form can be supplied from vapor space 116 to delivery line 122 through vapor supply line 126 whose one end fluidly communicates with vapor space 116 of storage vessel 112. Vapor supply line 126 is provided with a check valve 128 to prevent fuel backflow to the storage vessel.
  • Liquid fuel line 123 and vapor supply line 126 are each connected to delivery line 122 downstream of their respective check valve.
  • Delivery line 122 further comprises heat exchanger 130 which transmits heat from a heat exchange fluid to the fuel as further explained below.
  • the heat exchange fluid in heat exchanger 130 can be for example the engine coolant.
  • Delivery line 122 further comprises module 132 for dampening the pressure fluctuations in the stream of fuel being supplied to the engine and pressure regulator 134 for adjusting the pressure of the fuel supplied to the engine to the required engine intake pressure.
  • Automatic fuel shut-off valve 136 is provided on delivery line 122 between pressure regulator 134 and engine 110. Fuel shut-off valve 136 is used as a safety measure for stopping any fuel flow to the engine when the engine is not operating.
  • the system further comprises controller 140 which commands the operation of fuel pump 118 and hydraulic pump 120 and receives measurement signals from pressure sensors 150 and 152 and from temperature sensor 154.
  • Pressure sensor 150 measures the pressure in vapor space 116 of fuel storage vessel 112 and pressure sensor 152 measures the fuel supply pressure which is the pressure in fuel delivery line 122 downstream of module 132 and upstream of pressure regulator 134.
  • Temperature sensor 154 measures the temperature of the fuel flowing through delivery line 122 downstream of heat exchanger 130 and controller 140 can command the operation of heat exchanger 130 to ensure that the temperature of the fuel supplied to engine 110 is higher than a predetermined limit.
  • Controller 140 also receives input from the engine regarding the engine speed and another parameter indicative of the engine operating condition, for example one of the parameters indicative of the fuel demand, for example the throttle position.
  • the controller can determine the required fuel supply pressure based on the information from a map, which correlates the engine speed data with the other parameter indicative of the engine operating condition as further detailed below.
  • controller 140 determines the required fuel supply pressure which is the pressure of the fuel flowing through delivery line 122 upstream of pressure regulator 134.
  • controller 140 receives information from the engine regarding its operating condition and uses the map illustrated in Figure 3 to determine a point on the map which indicates the current engine operating condition.
  • Map 300 stored in the controller's memory is divided into two regions a low flow region 310 and a high flow region 320.
  • Low flow region 310 is delimited by boundary line 330 set by a low speed S L and by boundary line 340 set by a low throttle position T L and high flow region 320 is delimited by boundary line 350 set by a high engine speed S H and a high throttle position 3 ⁇ 4.
  • controller 140 can determine based on predetermined algorithms, the engine intake pressure P eng ine A required for operating the engine efficiently.
  • the fuel supply pressure which is the pressure in fuel delivery line 122 upstream of pressure regulator 134 is higher than the engine intake pressure which is the pressure in fuel delivery line 122 downstream of pressure regulator 134 such that dynamic engine demands can be easily met.
  • the controller determines that a different engine intake pressure P en gine B is required for operating the engine efficiently.
  • the value of the pressure threshold that is added to the required engine intake pressure when the engine operates in the low flow region 310 is different than the pressure threshold that is added to the required engine intake pressure when the engine operates in the high flow region 320.
  • the measured pressure P v in vapor space 116 is compared to the required fuel supply pressure P SU ppiy , which was determined in previous step 210. If the measured pressure in the vapor space is equal to or higher than the predetermined required fuel supply pressure, fuel is supplied in gaseous state from vapor space 116 in storage vessel 112 through vapor supply line 126 to fuel delivery line 122, which is step 240 of the present method. If the measured pressure in the vapor space is lower than the predetermined required fuel supply pressure, the controller executes step 250 of the present method and activates fuel pump 118 whereby fuel is supplied from liquid space 114 through liquid fuel supply line 123 to fuel delivery line 122.
  • the temperature of the fuel supplied to fuel delivery line 122 is increased by flowing the fuel through heat exchanger 130. If fuel is supplied from liquid space 114 the heat exchange rate in heat exchanger 130 is increased compared to when the fuel is supplied from vapor space 116 because the temperature of the fuel supplied from the liquid space is slightly lower than the temperature of the fuel supplied in vapor state from the vapor space.
  • the advantage of the present method over the known methods for delivering fuel in gaseous state to the air intake system of a gaseous fuelled engine is that fuel can be delivered to the engine without relying on the fuel saturation pressure to push the fuel out of the storage vessel.
  • FIG. 4 illustrates another embodiment of the present fuel delivery system.
  • Fuel delivery system 400 is delivering fuel in gaseous state from cryogenic storage vessel 412 to air intake manifold 411 or to air intake ports 413 of gaseous fuelled internal combustion engine 410.
  • Fuel can be delivered to fuel delivery line 422 either from vapor space 416 through vapor supply line 426 or it is supplied by fuel pump 418 from liquid space 414 through liquid fuel supply line 423.
  • Liquid supply line 423 and vapor supply line 426 are each provided with a check valve 425 and respectively 428 for preventing fuel backflow.
  • Fuel passing through fuel delivery line 422 is heated in heat exchanger 430 and the pressure fluctuations in the fuel stream are dampened in module 432.
  • Pressure regulator 434 regulates the fuel pressure to the engine intake pressure.
  • Automatic shut-off valve 436 is provided as a safety measure during the times when the engine is not operating.
  • the pressure in fuel delivery line 422 is measured by pressure sensor 452.
  • System 400 illustrated in Figure 4 is different than the system illustrated in Figure 1 in that it uses two hydraulic pumps 420 and 460 for activating fuel pump 418. Hydraulic pumps 420 and 460 supply hydraulic fluid from storage vessel 421 through flow switching unit 424 to the hydraulic drive unit that drives fuel pump 418. In this arrangement, both hydraulic fluid pumps can be used at the same time when the hydraulic fluid flow rate commanded by controller 440 is higher than that which can be supplied by only one hydraulic pump.
  • heat exchanger 430 is not commanded by controller 440 and provides the same amount of heat to the fuel flowing through delivery line 422 independently of where the fuel is supplied from.
  • the temperature of the fuel flowing through fuel delivery line 422 is measured by temperature sensor 454 and communicated to controller 440.
  • the method of delivering fuel from storage vessel 412 to engine 410 is the same as the method described in relation to Figure 2 and therefore it will not be described here in great detail.
  • the pressure in vapor space 416 is measured by pressure sensor 450 and it is compared to the required fuel supply pressure. If the pressure measured in vapor space 416 is equal to or higher than the required fuel supply pressure fuel is supplied in gaseous state from vapor space 416 to the engine, and if the pressure measured in vapor space 416 is lower than the required fuel supply pressure, fuel pump 418 is activated and fuel is delivered by the pump from liquid space 414 to the engine.
  • the required fuel supply pressure is determined following the same algorithm as the one applied for the system illustrated in Figure 1.
  • FIG. 5 illustrates another embodiment of the present fuel delivery system.
  • Fuel delivery system 500 is delivering fuel in gaseous state to air intake manifold 511 or to air intake ports 513 of gaseous fuelled internal combustion engine 510.
  • Fuel system 500 is different than the previous embodiments because it comprises two cryogenic storage vessels 512A and 512B, each storage vessel having a respective vapor space 516A and 516B, and a respective liquid space 514A and 514B, and being fluidly connected to a respective fuel pump 518A and 518B.
  • Each of the two fuel pumps 518A or 518B is activated by supplying hydraulic fluid from hydraulic storage vessel 521 through one of the two hydraulic pumps 520 or 560 or through both of them, through flow switching units 562, and further through one of the flow switching units 524A or 524B, to the hydraulic drive unit of the respective fuel pump to be activated.
  • Hydraulic fluid pumps 520 and 560 are driven by an electric motor and therefore can be operated independently from the operation of the internal combustion engine.
  • pressure in fuel delivery line 522 is measured by pressure sensor 552 upstream of pressure regulator 534 and downstream of module 532. Pressure fluctuations in fuel delivery line 522 are dampened in module 532. Temperature in fuel delivery line 522 is measured by temperature sensor 554.
  • Automatic shut-off valve 536 is provided as a safety measure on fuel delivery line 522 during the times when the engine is not operating.
  • a similar method of delivering fuel to the engine as described in relation to Figures 1 and 4 is applied here.
  • the pressure in the vapor space of each tank 512A and 512B is measured by a respective pressure sensor 550A and 550B and communicated to controller 540.
  • Controller 540 compares the pressure measured in each vapor space with the required fuel supply pressure which is determined in a similar way as in the methods described in relation to Figures 1 and 4 and fuel is supplied from a vapor space of one of storage vessels 512A or 512B in which vapor pressure is higher than the required fuel supply pressure.
  • Fuel is supplied from the respective vapor space through vapor liquid line 526A or 526B and through heat exchanger 530A or 530B to delivery line 522.
  • controller 540 selects and activates one of the two fuel pumps 518A and 518B to supply fuel from the liquid space of the storage vessel associated with the activated pump.
  • Liquid fuel is supplied through a respective liquid supply line 523A or 523B and through heat exchanger 530A or respectively 530B to delivery line 522.
  • Liquid fuel supply lines 523A and 523B and vapor supply lines 526A and 526B are each provided with a check valve 525 A, 525B and respectively 528A, 528B to prevent backflow.
  • controller 540 selects which one of the two fuel pumps should be activated such that the two fuel pumps are operated in sequential order. Alternatively, the amount of fuel remaining in each storage vessel 512A and 512B is measured and controller 540 selects one of fuel pumps 518A or 518B based on which storage vessel has the most fuel.
  • FIG. 6 illustrates another fuel delivery system 600 for delivering fuel in gaseous state to air intake manifold 611 or to air intake ports 613 of gaseous fuelled internal combustion engine 610.
  • Fuel system 600 is different than the previous embodiments because it comprises one external fuel pump 618 and two cryogenic storage vessels 612A and 612B whereby fuel pump 618 can supply fuel from liquid space 614A or 614B of the respective storage vessels 612A and 612B.
  • Fuel pump 618 is activated when hydraulic pump 620 supplies hydraulic fluid from storage vessel 621 to the hydraulic drive unit of the fuel pump 618 through flow switching unit 624.
  • pressure in fuel delivery line 622 is measured by pressure sensor 652 upstream of pressure regulator 634 and downstream of module 632. Pressure fluctuations in fuel delivery line 622 are dampened in module 632. Automatic shut-off valve 636 is provided as a safety measure on fuel delivery line 622 during the times when the engine is not operating. Vapor supply lines 626A and 626B are each provided with a check valve 628A and respectively 628B and check valve 625 is provided on delivery line 622 downstream of fuel pump 618 to prevent fluid backflow.
  • a similar method of delivering fuel to the engine as described in relation to Figures 1, 4 and 5 is applied here.
  • Pressure in vapor spaces 616A and 616B of each storage vessel 612A and respectively 612B is measured by a respective pressure sensor 650A and 650B and communicated to controller 640.
  • Controller 640 compares the pressure measured in each vapor space with the required fuel supply pressure which is calculated in a similar way as in the methods described in relation to Figures 1, 4 and 5 and fuel is supplied from a vapor space of one of storage vessels 612A or 612B in which vapor pressure is higher than the required fuel supply pressure.
  • Fuel is supplied from the respective vapor space through vapor liquid line 626A or 626B and through heat exchanger 630 to delivery line 622.
  • controller 640 activates fuel pump 618 to supply fuel from the liquid space of one of the two storage vessels 612A or 612B. Fuel is supplied from liquid space 614A or 614B through respective liquid supply line 623A or 623B to delivery line 622.
  • each liquid supply line 623A and 623B is provided with a shut-off valve 670A and respectively 670B which can be commanded by controller 640.
  • controller 640 commands shut-off valve 670B to close and fuel pump 618 supplies fuel from liquid space 614A to delivery line 622.
  • controller 640 commands shut-off valve 670A to close and fuel pump 618 supplies fuel from liquid space 614B to delivery line 622.
  • the pressure measurements in this embodiment are communicated by pressure sensors 652, 650A and 650B to controller 640 and the temperature of the fuel flowing through delivery line 622 is measured by temperature sensor 654.
  • the required fuel supply pressure is determined following the same logic as the one applied for the systems illustrated in Figures 1, 4 and 5.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

A method and system is disclosed for delivering a cryogenically stored fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine. The method comprises measuring the pressure in the vapor space of the cryogenic storage vessel, comparing the measured pressure to a required fuel supply pressure and supplying fuel in gaseous state directly from the vapor space of the cryogenic storage vessel to the fuel delivery line that supplies fuel to the engine, when the pressure measured in the vapor space of the cryogenic storage vessel is equal to or higher than the required fuel supply pressure. The method further comprises activating a cryogenic pump to deliver fuel to the internal combustion engine from the liquid space of the cryogenic storage vessel when the measured pressure in the vapor space is lower than the required fuel supply pressure.

Description

METHOD AND SYSTEM FOR DELIVERING A GASEOUS FUEL INTO THE AIR INTAKE SYSTEM OF AN INTERNAL COMBUSTION ENGINE
Technical Field
[0001 ] The present disclosure relates to a method and a system for delivering a cryogenically stored fuel to the air intake system of gaseous fuelled internal combustion engine.
Background
[0002] A fuel storage and delivery system for an internal combustion engine that is fuelled with a gaseous fuel such as natural gas, is an example of an application that is particularly suited for the disclosed method and system. Natural gas has been used to fuel vehicle engines for many years. The fuel supplied to a natural gas driven vehicle is stored either in a liquefied natural gas (LNG) tank or in a compressed natural gas (CNG) cylinder.
[0003] CNG is normally stored at ambient temperatures at pressures up to 3600 pounds per square inch while LNG is normally stored in a cryogenic storage vessel at temperatures of between about -240° F and -175° F (about -150° C and -115° C) and at pressures of between 15 and 200 psig. CNG has been the more broadly adopted form of fuel storage but it has a lower energy density compared to LNG. Now that natural gas is gaining greater acceptance as a fuel for transportation, the benefit of the higher energy density for LNG is attractive for vehicles that require a longer range between re-fuelling. LNG provides an energy density of about four times that of CNG with the aforementioned storage conditions. Increased demand for natural gas engines has increased the need to develop improved on-board fuel supply systems with natural gas stored as LNG instead of CNG. [0004] Natural gas fuelled engines can operate by injecting the fuel in the engine's air intake manifold or by injecting the fuel directly into the engine's combustion chambers. In systems where fuel is injected into the engine's air intake system the required fuel supply pressure is relatively low, for example around 100 psig. In systems where the fuel is injected directly into the engine's combustion chamber and where the fuel injection pressure needs to be higher than the in-cy Under pressure the fuel supply system has to deliver natural gas to the injector at higher pressures, for example at pressures of at least 3000 psig.
[0005] LNG low pressure fuelling systems described in the prior art generally comprise a liquid conduit which supplies liquid fuel from the storage vessel to the engine through a supply line comprising a vaporizer. Fuel is stored in the storage vessel at a pressure of around 150 psi which is higher than the fuel delivery pressure to the engine which can be between 70 to 100 psi.
[0006] In these systems, heat is transferred to the LNG fuel storage vessel and a portion of the stored liquid fuel can vaporize thereby increasing the pressure inside the vessel. One method of relieving the pressure inside an LNG storage vessel is to vent the gas into the atmosphere. However this method is wasteful and can be represent a hazard. As an alternative, the existing delivery systems for low pressure engines are provided with an economizer circuit which comprises a vapor conduit through which vapor can be withdrawn from the vapor headspace in the storage vessel and can be supplied to the engine. In engine supply systems provided with an economizer circuit, most of the time, the engine operates with LNG fuel supplied from the liquid space in the storage vessel and vapor is pulled from the vapor headspace only when the pressure in the storage vessel rises above a predetermined limit set by a regulator placed in the vapour conduit. An example of such a system is described in United States Patent Number 5,421,161 which illustrates an economizer circuit including means for providing a fixed back pressure in the liquid withdrawal conduit such that when the pressure in the storage vessel increases over a predetermined amount, the path of least resistance is through the vapor conduit and vapor is preferentially withdrawn from the vapor headspace of the storage vessel to thereby lower the pressure within the LNG storage tank faster.
[0007] The known systems using LNG storage vessels to supply fuel to a low pressure internal combustion engine fuelled with natural gas rely on a high saturation pressure in the storage vessel to push fuel out of the liquid space of the storage vessel and to the engine. When heat is transferred from the surrounding environment to the storage vessel, the saturation pressure of the LNG increases and can be sufficient for pushing fuel out of the vessel. When the engine operates at high load the saturation pressure of the LNG in the storage vessel can drop below a level that is required for pushing fuel out of the tank. In these situations, the engine becomes starved of fuel and can run in underperforming conditions. In these situations, the driver has to stop the vehicle and wait for the pressure in the storage vessel to increase until he can restart the vehicle. [0008] One known method of increasing the pressure in the LNG storage vessel is to use pressure building coils interposed between the walls of a double-walled cryogenic tank which circulate low temperature fuel from the tank. Heat transferred from to the exterior through the wall of the LNG storage vessel to the pressure building coil vaporizes the liquid fuel and the created vapor can be supplied directly into the headspace of the storage vessel through a regulator when the pressure in the headspace becomes lower than a predetermined value. Such a pressure building circuit is described in United States Patent Number 4,947,651. In other pressure building circuits used for cryogenic tanks in general, such as the one described in United States Patent Number 5,937,655, the pressure building coil is external to the cryogenic tank. In such systems cryogenic liquid from the tank is fed to a pressure builder heat exchanger where the liquid is vaporized and the produced gas is delivered to the tank to pressurize it.
[0009] The disadvantage of the methods using pressure building circuits to pressurize a cryogenic fluid storage vessel is that the heat used for generating the vapor that is supplied to the headspace of the storage vessel to pressurize it, is also transferred to the liquid contained in the vessel reducing the vessel's fluid holding time and requiring more frequent venting.
[0010] One other disadvantage of the existing low pressure fuel supply systems which rely on the fuel saturation pressure in the storage vessel to supply fuel to the engine is that they cannot adequately supply engines with fuel under transient conditions, when the required fuel supply pressure can vary dynamically between a lower pressure that is required for low load operation and a higher pressure that is required for high load operation. This issue becomes more important if such natural gas fuel systems are installed on larger vehicles, such as heavy duty trucks, which have larger engines that consume fuel at a higher rate. [001 1 ] Accordingly, there is a need for a method of reliably delivering fuel from a cryogenic storage vessel into the air intake system of a gaseous fuelled internal combustion engine at low pressures, to ensure that fuel is delivered to the engine at the required fuel injection pressure at all times and during different engine operating modes including during transients.
Summary
[0012] A method is disclosed for delivering a fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine. The method comprises: determining a required fuel supply pressure according to an operating condition of the engine;
measuring pressure in a vapor space of a storage vessel which stores the fuel; comparing the measured pressure to the required fuel supply pressure, and supplying fuel in gaseous state to the engine from the vapor space in the storage vessel when the measured pressure is equal to or higher than the required fuel supply pressure, or
activating a fuel pump and delivering fuel to the engine from a liquid space in the storage vessel when the measured pressure in the vapor space is lower than the required fuel supply pressure.
[0013] In this method the step of determining the required fuel supply pressure comprises first determining a required engine intake pressure as a function of engine operating conditions and then adding to it a predetermined pressure threshold. Because the required fuel supply pressure is preferably higher than the engine intake pressure the dynamic engine demands can be easily met by the system pressure. In preferred embodiments, the predetermined pressure threshold which is added to the engine intake pressure to determine the required fuel supply pressure is also determined as a function of the engine operating condition. The engine operating condition can be determined from a map stored in the controller's memory that correlates the engine speed with a parameter indicative of the engine condition, for example a parameter indicative of the fuel demand, such as the throttle position. [0014] In the present method, the step of activating the fuel pump comprises supplying hydraulic fluid from a hydraulic pump to a hydraulic drive unit that drives the fuel pump. The hydraulic pump is preferably driven by an electric motor and the electric motor is driven independently from the operation of the internal combustion engine such that the fuel pump can be activated independently of the engine condition. [0015] In some embodiments, at least two hydraulic pumps can supply hydraulic fluid to the hydraulic drive unit that the drives the fuel pump and the present method further comprises electrically activating at least two hydraulic pumps at the same time for delivering hydraulic fluid to said hydraulic drive unit when a commanded hydraulic fluid flow rate is higher than that which can be supplied by only one hydraulic pump.
[0016] In preferred embodiments the temperature of the fuel is increased by flowing it through a heat exchanger. The method can comprise increasing the heat exchange rate in the heat exchanger when the fuel is supplied from the liquid space of the fuel storage vessel, compared to when the fuel is supplied from the vapor space of the fuel storage vessel. In other embodiments the heat exchange rate in the heat exchanger is not controlled by the system controller and is set to be constant.
[0017] If the fuel delivery system comprises a plurality of storage vessels each having a respective vapor space and a liquid space, and the present method of delivering fuel to the engine further comprises: measuring pressure in the vapor space of each one of the plurality of storage vessels; comparing the measured pressure in the vapor space of each one of the plurality of storage vessels with the required fuel supply pressure; supplying fuel from the vapor space of any one of the plurality of storage vessels in which vapor pressure is higher than the required system fuel supply pressure; or activating the fuel pump and supplying fuel from one of the plurality of storage vessels when none of the plurality of storage vessels has a vapor pressure higher than the required system fuel supply pressure. [0018] This method which involves supplying fuel from one of the plurality of storage vessels can further comprise measuring the amount of fuel in each of the plurality of storage vessels and, when activating the fuel pump, supplying fuel from one of the plurality of storage vessels that has the largest amount of fuel. [0019] If the fuel delivery system comprises a plurality of storage vessels, each having a respective vapor space and liquid space, and each having a respective fuel pump, the present method further comprises: measuring pressure in the vapor space of each one of the plurality of storage vessels; comparing the measured pressure in the vapor space of each one of the plurality of storage vessels with the required fuel supply pressure; supplying fuel from the vapor space of any one of the plurality of storage vessels in which vapor pressure is higher than the required system fuel supply pressure; or selecting and activating one of the fuel pumps and supplying fuel from an associated one of the plurality of storage vessels when none of the plurality of storage vessels has a vapor pressure higher than the required system fuel supply pressure.
[0020] In this method the step of selecting one of the fuel pumps that is to be activated is determined by operating each one of the fuel pumps in sequential order. Alternatively, the step of selecting one of the fuel pumps that is to be activated is determined by measuring the amount of fuel in each one of the plurality of storage vessels and selecting the one of the plurality of fuel pumps that is associated with the storage vessel that has the largest amount of fuel.
[0021 ] In preferred embodiments of the method where fuel is supplied from one of a plurality of fuel storage vessels, the method further comprises increasing the temperature of the fuel by flowing it through a heat exchanger associated with a respective storage vessel from which fuel is supplied to the engine.
[0022] A system is also disclosed for delivering fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine. The system comprises: a) a storage vessel for holding the fuel; b) a fuel pump fluidly connected to receive fuel from a liquid space of the storage vessel; c) a liquid supply line in fluid communication with a discharge outlet of the fuel pump for delivering fuel from the discharge outlet of the fuel pump to a delivery line which delivers fuel to the engine; d) a vapor supply line in fluid communication with a vapor space of the storage vessel for delivering fuel in a gaseous state from the vapor space to the delivery line; e) a pressure sensor for measuring vapor pressure in the vapor space of the storage vessel; and f) a controller which receives pressure measurements from the pressure sensor, determines a required fuel supply pressure according to an operating condition of the engine and compares the measured pressure to the required fuel supply pressure, wherein the controller commands the fuel pump to operate when the measured pressure is lower than the required fuel supply pressure.
[0023] The system preferably comprises a heat exchanger placed in the delivery line for increasing the temperature of the fuel being supplied to the engine. The system also comprises a hydraulic pump which supplies hydraulic fluid to a hydraulic drive unit that drives the fuel pump. Preferably, the hydraulic pump is driven by an electric motor which operates independently from the operation of the engine such that the operation of the fuel pump can be controlled independently of the engine operation.
[0024] In some embodiments, the system comprises at least two hydraulic pumps which can be electrically activated to deliver hydraulic fluid to the hydraulic drive unit that drives the fuel pump. In some embodiments the fuel pump is disposed within a cryogenic space of the storage vessel.
[0025] In some embodiments the system comprises more than one storage vessel. Each storage vessel in the system has a respective vapor space and a liquid space, and is fluidly connected to the fuel pump. In these systems the controller is programmed to activate the fuel pump to supply fuel from the liquid space of one of the plurality of storage vessels when none of the plurality of storage vessels has a vapor pressure higher than the required fuel supply pressure.
[0026] In other embodiments, the system comprises more than one storage vessel, each storage vessel having a respective vapor space and liquid space, and each being fluidly connected to a respective fuel pump. In these systems the controller is programmed to select and activate one of the fuel pumps and supply fuel from a storage vessel associated with the selected fuel pump when none of the plurality of storage vessels has a vapor pressure higher than the required fuel supply pressure.
[0027] In preferred embodiments the system comprises an engine that is the prime mover for a vehicle.
Brief Description of the Drawings
[0028] Figure 1 is schematic diagram of a system for delivering fuel in gaseous state into the air intake system of an internal combustion engine according to the present disclosure; [0029] Figure 2 is a schematic diagram illustrating the basic steps of a method for delivering fuel from a cryogenic storage vessel to the air intake system of a gaseous fuelled internal combustion engine according to the present disclosure;
[0030] Figure 3 is a representation of a map correlating the engine speed with the throttle position which is used by the system's controller to determine the engine operating condition;
[0031 ] Figure 4 is schematic diagram of another embodiment of a fuel delivery system comprising two hydraulic pumps for supplying hydraulic fluid to the hydraulic drive unit of the system's fuel pump;
[0032] Figure 5 is a schematic diagram of another embodiment of a fuel delivery system comprising two fuel storage vessels, each storage vessel being associated with a fuel pump, and a controller which activates each of the fuel pumps according to the method described in the present disclosure; [0033] Figure 6 is a schematic diagram of another embodiment of a fuel delivery system comprising two fuel storage vessels which are both fluidly connected to one external fuel pump and a controller which activates the fuel pump according to the method described in the present disclosure. Detailed Description
[0034] Figure 1, schematically illustrates a fuel delivery system 100 which is employed to supply a fuel in gaseous state into the air intake system of an internal combustion engine. Engine 110 is an internal combustion engine which is operated by injecting fuel into the engine's air intake manifold or into the air intake port, which is a different method than injecting fuel directly into the engine's combustion chamber. Gaseous fuel is injected into the engine's air intake manifold 111 or into the air intake ports 113 at pressures that are generally around 70 to 100 psig (pounds per square inch gauge) and can reach around 500 psig. Such pressures are much lower than the operating pressure of a direct injection internal combustion engine where gaseous fuel is injected directly into the combustion chamber at around 4000 psig.
[0035] Fuel delivery system 100 comprises fuel storage vessel 112 which stores gaseous fuel in liquefied form at cryogenic temperatures in liquid space 114 within the cryogenic space of the storage vessel. Since heat is transmitted from the surrounding environment to the walls of the storage vessel, liquid fuel stored in the vessel can vaporize and the generated vapor occupies the headspace of the storage vessel, creating a vapor space 116.
[0036] Liquid space 114 is fluidly connected to fuel pump 118 which can be placed inside the cryogenic space of the storage vessel, as illustrated in the embodiment shown in Figure 1, or can be an external pump that communicates through a supply line with the liquid space in the storage vessel. Fuel pump 118 can be activated by starting hydraulic pump 120 which supplies hydraulic fluid from storage vessel 121 through flow switching device 124 to the hydraulic drive unit of fuel pump 118. Hydraulic pump 120 is driven by an electric motor and therefore can operate independently of the operating condition of the engine. In the existent prior art fuel delivery systems, the hydraulic pump that activates the fuel pump is mechanically actuated by the engine accessory drive and therefore depends on the engine rotation (rpm).
[0037] Liquid fuel from liquid space 114 of fuel storage vessel 112 can be pumped by fuel pump 118 through liquid fuel supply line 123 to delivery line 122 which supplies fuel to engine 110. Liquid fuel supply line 123 comprises a check valve 125 which prevents fuel backflow to the storage vessel.
[0038] Fuel in vapor form can be supplied from vapor space 116 to delivery line 122 through vapor supply line 126 whose one end fluidly communicates with vapor space 116 of storage vessel 112. Vapor supply line 126 is provided with a check valve 128 to prevent fuel backflow to the storage vessel.
[0039] Liquid fuel line 123 and vapor supply line 126 are each connected to delivery line 122 downstream of their respective check valve. Delivery line 122 further comprises heat exchanger 130 which transmits heat from a heat exchange fluid to the fuel as further explained below. The heat exchange fluid in heat exchanger 130 can be for example the engine coolant. Delivery line 122 further comprises module 132 for dampening the pressure fluctuations in the stream of fuel being supplied to the engine and pressure regulator 134 for adjusting the pressure of the fuel supplied to the engine to the required engine intake pressure. Automatic fuel shut-off valve 136 is provided on delivery line 122 between pressure regulator 134 and engine 110. Fuel shut-off valve 136 is used as a safety measure for stopping any fuel flow to the engine when the engine is not operating.
[0040] The system further comprises controller 140 which commands the operation of fuel pump 118 and hydraulic pump 120 and receives measurement signals from pressure sensors 150 and 152 and from temperature sensor 154. Pressure sensor 150 measures the pressure in vapor space 116 of fuel storage vessel 112 and pressure sensor 152 measures the fuel supply pressure which is the pressure in fuel delivery line 122 downstream of module 132 and upstream of pressure regulator 134. Temperature sensor 154 measures the temperature of the fuel flowing through delivery line 122 downstream of heat exchanger 130 and controller 140 can command the operation of heat exchanger 130 to ensure that the temperature of the fuel supplied to engine 110 is higher than a predetermined limit. [0041 ] Controller 140 also receives input from the engine regarding the engine speed and another parameter indicative of the engine operating condition, for example one of the parameters indicative of the fuel demand, for example the throttle position. The controller can determine the required fuel supply pressure based on the information from a map, which correlates the engine speed data with the other parameter indicative of the engine operating condition as further detailed below.
[0042] The method of delivering fuel in gaseous state into the air intake system of a gaseous fuelled internal combustion engine will now be described in relation to the embodiment of the fuel delivery system illustrated in Figure 1. The steps of the method are illustrated in Figure 2. In first step 210 of method 200, controller 140 determines the required fuel supply pressure which is the pressure of the fuel flowing through delivery line 122 upstream of pressure regulator 134. At this step, controller 140 receives information from the engine regarding its operating condition and uses the map illustrated in Figure 3 to determine a point on the map which indicates the current engine operating condition. Map 300 stored in the controller's memory is divided into two regions a low flow region 310 and a high flow region 320. Low flow region 310 is delimited by boundary line 330 set by a low speed SL and by boundary line 340 set by a low throttle position TL and high flow region 320 is delimited by boundary line 350 set by a high engine speed SH and a high throttle position ¾. If the engine operates for example at a point A, which is characterized by coordinates (Si, Ti) corresponding to a value Si for the engine speed and a value Ti for the throttle position, it is determined that the engine operates in a low flow region 310. Once the point on the map where the engine operates is identified, controller 140 can determine based on predetermined algorithms, the engine intake pressure Pengine A required for operating the engine efficiently. The required fuel supply pressure PSUppiy A is then determined by the formula PSUppiy A = Pengine A + PthreshoidA, where PthreshoidA is the pressure value that needs to be added to the engine intake pressure to obtain the fuel supply pressure. The fuel supply pressure, which is the pressure in fuel delivery line 122 upstream of pressure regulator 134 is higher than the engine intake pressure which is the pressure in fuel delivery line 122 downstream of pressure regulator 134 such that dynamic engine demands can be easily met. Similarly, if the engine operates at point B characterized by coordinates (S2, T2), corresponding to a different engine speed S2 and a different throttle position T2, located in the high flow region 320 on map 300, the controller determines that a different engine intake pressure Pengine B is required for operating the engine efficiently. The required fuel supply pressure is then determined by the same formula: Psuppiy B = Pengine B + Pthreshoid B- The value of the pressure threshold that is added to the required engine intake pressure when the engine operates in the low flow region 310 is different than the pressure threshold that is added to the required engine intake pressure when the engine operates in the high flow region 320. Both the engine intake pressure Pengine and the threshold pressure Pthreshoid are determined by the controller through control algorithms based on the region on map 300 where the engine operates. [0043] In next step 220 of the present method, pressure Pv within vapor space 116 of fuel storage vessel 112 is measured by pressure sensor 150 and the measured value is communicated to controller 140.
[0044] In the next step 230, the measured pressure Pv in vapor space 116 is compared to the required fuel supply pressure PSUppiy , which was determined in previous step 210. If the measured pressure in the vapor space is equal to or higher than the predetermined required fuel supply pressure, fuel is supplied in gaseous state from vapor space 116 in storage vessel 112 through vapor supply line 126 to fuel delivery line 122, which is step 240 of the present method. If the measured pressure in the vapor space is lower than the predetermined required fuel supply pressure, the controller executes step 250 of the present method and activates fuel pump 118 whereby fuel is supplied from liquid space 114 through liquid fuel supply line 123 to fuel delivery line 122.
[0045] The temperature of the fuel supplied to fuel delivery line 122 is increased by flowing the fuel through heat exchanger 130. If fuel is supplied from liquid space 114 the heat exchange rate in heat exchanger 130 is increased compared to when the fuel is supplied from vapor space 116 because the temperature of the fuel supplied from the liquid space is slightly lower than the temperature of the fuel supplied in vapor state from the vapor space.
[0046] The advantage of the present method over the known methods for delivering fuel in gaseous state to the air intake system of a gaseous fuelled engine is that fuel can be delivered to the engine without relying on the fuel saturation pressure to push the fuel out of the storage vessel.
[0047] Other embodiments of fuel delivery system are illustrated in Figures 4 to 6. These embodiments have many components that are equivalent to like components of the embodiment presented in Figure 1 and like components are identified by like reference numbers. Persons skilled in the technology will understand that in this disclosure like-numbered components function in substantially the same way in each embodiment. Accordingly, if like components have already been described with respect to one embodiment, while identified in the figures for other embodiments, the purpose and function of like components may not be repeated for each of the illustrated embodiments.
[0048] Figure 4 illustrates another embodiment of the present fuel delivery system. Fuel delivery system 400 is delivering fuel in gaseous state from cryogenic storage vessel 412 to air intake manifold 411 or to air intake ports 413 of gaseous fuelled internal combustion engine 410. Fuel can be delivered to fuel delivery line 422 either from vapor space 416 through vapor supply line 426 or it is supplied by fuel pump 418 from liquid space 414 through liquid fuel supply line 423. Liquid supply line 423 and vapor supply line 426 are each provided with a check valve 425 and respectively 428 for preventing fuel backflow. Fuel passing through fuel delivery line 422 is heated in heat exchanger 430 and the pressure fluctuations in the fuel stream are dampened in module 432. Pressure regulator 434 regulates the fuel pressure to the engine intake pressure. Automatic shut-off valve 436 is provided as a safety measure during the times when the engine is not operating. The pressure in fuel delivery line 422 is measured by pressure sensor 452. [0049] System 400 illustrated in Figure 4 is different than the system illustrated in Figure 1 in that it uses two hydraulic pumps 420 and 460 for activating fuel pump 418. Hydraulic pumps 420 and 460 supply hydraulic fluid from storage vessel 421 through flow switching unit 424 to the hydraulic drive unit that drives fuel pump 418. In this arrangement, both hydraulic fluid pumps can be used at the same time when the hydraulic fluid flow rate commanded by controller 440 is higher than that which can be supplied by only one hydraulic pump. [0050] In this embodiment heat exchanger 430 is not commanded by controller 440 and provides the same amount of heat to the fuel flowing through delivery line 422 independently of where the fuel is supplied from. The temperature of the fuel flowing through fuel delivery line 422 is measured by temperature sensor 454 and communicated to controller 440.
[0051 ] The method of delivering fuel from storage vessel 412 to engine 410 is the same as the method described in relation to Figure 2 and therefore it will not be described here in great detail. The pressure in vapor space 416 is measured by pressure sensor 450 and it is compared to the required fuel supply pressure. If the pressure measured in vapor space 416 is equal to or higher than the required fuel supply pressure fuel is supplied in gaseous state from vapor space 416 to the engine, and if the pressure measured in vapor space 416 is lower than the required fuel supply pressure, fuel pump 418 is activated and fuel is delivered by the pump from liquid space 414 to the engine. The required fuel supply pressure is determined following the same algorithm as the one applied for the system illustrated in Figure 1.
[0052] Figure 5 illustrates another embodiment of the present fuel delivery system. Fuel delivery system 500 is delivering fuel in gaseous state to air intake manifold 511 or to air intake ports 513 of gaseous fuelled internal combustion engine 510. Fuel system 500 is different than the previous embodiments because it comprises two cryogenic storage vessels 512A and 512B, each storage vessel having a respective vapor space 516A and 516B, and a respective liquid space 514A and 514B, and being fluidly connected to a respective fuel pump 518A and 518B.
[0053] Each of the two fuel pumps 518A or 518B is activated by supplying hydraulic fluid from hydraulic storage vessel 521 through one of the two hydraulic pumps 520 or 560 or through both of them, through flow switching units 562, and further through one of the flow switching units 524A or 524B, to the hydraulic drive unit of the respective fuel pump to be activated. Hydraulic fluid pumps 520 and 560 are driven by an electric motor and therefore can be operated independently from the operation of the internal combustion engine. [0054] Similar to the other embodiments described here, pressure in fuel delivery line 522 is measured by pressure sensor 552 upstream of pressure regulator 534 and downstream of module 532. Pressure fluctuations in fuel delivery line 522 are dampened in module 532. Temperature in fuel delivery line 522 is measured by temperature sensor 554. Automatic shut-off valve 536 is provided as a safety measure on fuel delivery line 522 during the times when the engine is not operating. [0055] A similar method of delivering fuel to the engine as described in relation to Figures 1 and 4 is applied here. The pressure in the vapor space of each tank 512A and 512B is measured by a respective pressure sensor 550A and 550B and communicated to controller 540. Controller 540 compares the pressure measured in each vapor space with the required fuel supply pressure which is determined in a similar way as in the methods described in relation to Figures 1 and 4 and fuel is supplied from a vapor space of one of storage vessels 512A or 512B in which vapor pressure is higher than the required fuel supply pressure. Fuel is supplied from the respective vapor space through vapor liquid line 526A or 526B and through heat exchanger 530A or 530B to delivery line 522. When none of two storage vessels has a vapor pressure higher than the required fuel supply pressure, controller 540 selects and activates one of the two fuel pumps 518A and 518B to supply fuel from the liquid space of the storage vessel associated with the activated pump. Liquid fuel is supplied through a respective liquid supply line 523A or 523B and through heat exchanger 530A or respectively 530B to delivery line 522. Liquid fuel supply lines 523A and 523B and vapor supply lines 526A and 526B are each provided with a check valve 525 A, 525B and respectively 528A, 528B to prevent backflow.
[0056] In the embodiment illustrated in Figure 5 controller 540 selects which one of the two fuel pumps should be activated such that the two fuel pumps are operated in sequential order. Alternatively, the amount of fuel remaining in each storage vessel 512A and 512B is measured and controller 540 selects one of fuel pumps 518A or 518B based on which storage vessel has the most fuel.
[0057] Even if only two storage vessels are shown in the embodiment illustrated in Figure 5, a person skilled in this technology would easily recognize that the system can comprise more than two cryogenic storage vessels and that the method of selecting and activating one fuel pump for supplying fuel from a liquid space of one storage vessel will be similar to the method described above. [0058] Figure 6 illustrates another fuel delivery system 600 for delivering fuel in gaseous state to air intake manifold 611 or to air intake ports 613 of gaseous fuelled internal combustion engine 610. Fuel system 600 is different than the previous embodiments because it comprises one external fuel pump 618 and two cryogenic storage vessels 612A and 612B whereby fuel pump 618 can supply fuel from liquid space 614A or 614B of the respective storage vessels 612A and 612B. Fuel pump 618 is activated when hydraulic pump 620 supplies hydraulic fluid from storage vessel 621 to the hydraulic drive unit of the fuel pump 618 through flow switching unit 624.
[0059] Similar to the other embodiments described here, pressure in fuel delivery line 622 is measured by pressure sensor 652 upstream of pressure regulator 634 and downstream of module 632. Pressure fluctuations in fuel delivery line 622 are dampened in module 632. Automatic shut-off valve 636 is provided as a safety measure on fuel delivery line 622 during the times when the engine is not operating. Vapor supply lines 626A and 626B are each provided with a check valve 628A and respectively 628B and check valve 625 is provided on delivery line 622 downstream of fuel pump 618 to prevent fluid backflow.
[0060] A similar method of delivering fuel to the engine as described in relation to Figures 1, 4 and 5 is applied here. Pressure in vapor spaces 616A and 616B of each storage vessel 612A and respectively 612B is measured by a respective pressure sensor 650A and 650B and communicated to controller 640. Controller 640 compares the pressure measured in each vapor space with the required fuel supply pressure which is calculated in a similar way as in the methods described in relation to Figures 1, 4 and 5 and fuel is supplied from a vapor space of one of storage vessels 612A or 612B in which vapor pressure is higher than the required fuel supply pressure. Fuel is supplied from the respective vapor space through vapor liquid line 626A or 626B and through heat exchanger 630 to delivery line 622. When none of two storage vessels has a vapor pressure higher than the required fuel supply pressure, controller 640 activates fuel pump 618 to supply fuel from the liquid space of one of the two storage vessels 612A or 612B. Fuel is supplied from liquid space 614A or 614B through respective liquid supply line 623A or 623B to delivery line 622.
[0061 ] In this embodiment each liquid supply line 623A and 623B is provided with a shut-off valve 670A and respectively 670B which can be commanded by controller 640. When none of the two storage vessels has a vapor pressure higher than the required fuel supply pressure, the amount of fuel in each storage vessel is measured and fuel is supplied from the storage vessel which has the most fuel. For example, when it is determined that storage vessel 612A has the most fuel, controller 640 commands shut-off valve 670B to close and fuel pump 618 supplies fuel from liquid space 614A to delivery line 622. Alternatively if it is determined that storage vessel 612B has the most fuel controller 640 commands shut-off valve 670A to close and fuel pump 618 supplies fuel from liquid space 614B to delivery line 622.
[0062] The pressure measurements in this embodiment are communicated by pressure sensors 652, 650A and 650B to controller 640 and the temperature of the fuel flowing through delivery line 622 is measured by temperature sensor 654.
[0063] In this embodiment, the required fuel supply pressure is determined following the same logic as the one applied for the systems illustrated in Figures 1, 4 and 5.
[0064] Even if only two storage vessels are shown in the embodiment illustrated in Figure 6, a person skilled in this technology would easily recognize that the system can comprise more than two cryogenic storage vessels and that the method of selecting the liquid space from which fuel is supplied when none of the storage vessels has a vapor space higher than the required fuel supply system is similar to the one described above. [0065] The present invention has been described with regard to a plurality of illustrative embodiments. However, it will be apparent to persons skilled in the art that a number of variations and modifications can be made without departing from the scope of the invention as defined in the claims.

Claims

A method for delivering a fuel in a gaseous state into an air intake system of a gaseous fuelled internal combustion engine, said method comprising: determining a required fuel supply pressure according to an operating condition of said engine; measuring pressure in a vapor space of a storage vessel which stores said fuel; comparing said measured pressure to said required fuel supply pressure, and supplying said fuel in said gaseous state from said vapor space in said storage vessel when said measured pressure is equal to or higher than said required fuel supply pressure, or activating a fuel pump and delivering fuel from a liquid space in said storage vessel when said measured pressure is lower than said required fuel supply pressure.
The method of claim 1 wherein determining said required fuel supply pressure comprises first determining a required engine intake pressure as a function of engine operating conditions and then adding to it a predetermined pressure threshold.
The method of claim 2 further comprising determining said predetermined pressure threshold as a function of said engine operating condition.
The method of claim 1 wherein the step of activating said fuel pump comprises supplying hydraulic fluid from a hydraulic pump to a hydraulic drive unit that drives said fuel pump.
5. The method of claim 4 wherein said hydraulic pump is driven by an electric motor.
6. The method of claim 5 further comprising operating said electric motor independently from operation of said internal combustion engine.
7. The method of claim 4 wherein said hydraulic pump is a first one of at least two hydraulic pumps, the method further comprising electrically activating at least one additional hydraulic pump to deliver hydraulic fluid to said hydraulic drive unit when a commanded hydraulic fluid flow rate is higher than that which can be supplied by said first one of at least two hydraulic pumps.
8. The method of claim 1 further comprising increasing the temperature of said fuel by flowing it through a heat exchanger.
9. The method of claim 8 further comprising increasing heat exchange rate in said heat exchanger when said fuel is supplied from said liquid space, compared to when said fuel is supplied from said vapor space.
10. The method of claim 1 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and a liquid space, said method further comprising: measuring pressure in said vapor space of each one of said plurality of storage vessels; comparing measured pressure in said vapor space of each one of said plurality of storage vessels with said required fuel supply pressure; supplying said fuel from said vapor space of any one of said plurality of storage vessels in which vapor pressure is higher than said required system fuel supply pressure; or activating said fuel pump and supplying said fuel from one of said plurality of storage vessels when none of said plurality of storage vessels has a vapor pressure higher than said required system fuel supply pressure.
11. The method of claim 10, said method further comprising measuring the amount of fuel in each of said plurality of storage vessels and, when activating said fuel pump, supplying said fuel from one of said plurality of storage vessels that has the most of said fuel.
12. The method of claim 1 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and liquid space, and each having a respective fuel pump, said method further comprising: measuring pressure in said vapor space of each one of said plurality of storage vessels; comparing measured pressure in said vapor space of each one of said plurality of storage vessels with said required fuel supply pressure; supplying said fuel from said vapor space of any one of said plurality of storage vessels in which vapor pressure is higher than said required system fuel supply pressure; or selecting and activating one of said fuel pumps and supplying said fuel from an associated one of said plurality of storage vessels when none of said plurality of storage vessels has a vapor pressure higher than said required system fuel supply pressure.
13. The method of claim 12 wherein selecting one of said fuel pumps that is to be activated is determined by operating each one of said fuel pumps in sequential order.
14. The method of claim 12 wherein selecting one of said fuel pumps that is to be activated is determined by measuring the amount of fuel in each one of said plurality of storage vessels and selecting the one of said plurality of fuel pumps that is associated with the storage vessel that has the most of said fuel.
15. The method of claim 12 further comprising increasing the temperature of said fuel by flowing it through a heat exchanger associated with a respective storage vessel from which fuel is supplied to said engine.
16. A system for delivering a fuel in a gaseous state into an air intake system of a gaseous fuelled internal combustion engine, said system comprising: a. a storage vessel for holding said fuel; b. a fuel pump fluidly connected to receive fuel from a liquid space of said storage vessel; c. a liquid supply line in fluid communication with a discharge outlet of said fuel pump for delivering fuel from said discharge outlet of said fuel pump to a delivery line which delivers fuel to said engine; d. a vapor supply line in fluid communication with a vapor space of said storage vessel for delivering fuel in a gaseous state from said vapor space to said delivery line; e. a pressure sensor for measuring vapor pressure in said vapor space of said storage vessel; and f. a controller which receives pressure measurements from said pressure sensor, determines a required fuel supply pressure according to an operating condition of said engine and compares said measured pressure to said required fuel supply pressure , wherein said controller commands said fuel pump to operate when said measured pressure is lower than said required fuel supply pressure.
17. The system of claim 16 further comprising a heat exchanger placed in said delivery line for increasing the temperature of said fuel being supplied to said engine.
18. The system of claim 16 further comprising a hydraulic pump which supplies hydraulic fluid to a hydraulic drive unit that drives said fuel pump.
19. The system of claim 18 wherein said hydraulic pump is driven by an electric motor.
20. The system of claim 19 wherein said electric motor operates independently from operation of said engine.
21. The system of claim 18 wherein said hydraulic pump is a first one of at least two hydraulic pumps which can be electrically activated to deliver hydraulic fluid to said hydraulic drive unit that drives said fuel pump.
22. The system of claim 18 wherein said fuel pump is disposed within a cryogenic space of said storage vessel.
23. .The system of claim 18 wherein said engine is the prime mover for a vehicle.
24. The system of claim 18 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and a liquid space, and being fluidly connected to said fuel pump, and wherein said controller is programmed to activate said fuel pump to supply fuel from said liquid space of one of said plurality of storage vessels when none of said plurality of storage vessels has a vapor pressure higher than said required fuel supply pressure.
25. The system of claim 18 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and a liquid space, and each being fluidly connected to a respective fuel pump, and wherein said controller is programmed to select and activate one of said fuel pumps and supply fuel from one of said plurality of storage vessels which is associated with said activated fuel pump when none of said plurality of storage vessels has a vapor pressure higher than said required fuel supply pressure.
PCT/CA2013/050890 2012-11-23 2013-11-22 Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine WO2014078962A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201380061316.5A CN104813016B (en) 2012-11-23 2013-11-22 Gaseous fuel is delivered to the method and system in the gas handling system of explosive motor
EP13857182.3A EP2923062B1 (en) 2012-11-23 2013-11-22 Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine
US14/719,650 US9771886B2 (en) 2012-11-23 2015-05-22 Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CA2796794A CA2796794C (en) 2012-11-23 2012-11-23 Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine
CA2,796,794 2012-11-23

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US14/719,650 Continuation US9771886B2 (en) 2012-11-23 2015-05-22 Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine

Publications (1)

Publication Number Publication Date
WO2014078962A1 true WO2014078962A1 (en) 2014-05-30

Family

ID=50771678

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CA2013/050890 WO2014078962A1 (en) 2012-11-23 2013-11-22 Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine

Country Status (5)

Country Link
US (1) US9771886B2 (en)
EP (1) EP2923062B1 (en)
CN (1) CN104813016B (en)
CA (1) CA2796794C (en)
WO (1) WO2014078962A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017003569A1 (en) * 2015-06-29 2017-01-05 Caterpillar Inc. Hydraulic drive multi-element cryogenic pump
US20170016434A1 (en) * 2015-07-13 2017-01-19 Caterpillar Inc. Hydraulic Distributor for Pump
CN107614962A (en) * 2015-04-30 2018-01-19 西港能源有限公司 Intelligent pressure management system for cryogen system
US20180313496A1 (en) * 2015-06-29 2018-11-01 Westport Power Inc. Multi-Vessel Fluid Storage and Delivery System

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2833619C (en) * 2013-11-21 2020-06-30 Westport Power Inc. Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine
US9233679B2 (en) * 2014-04-24 2016-01-12 Ford Global Technologies, Llc Systems and methods for supplying gaseous fuel to an engine
US9915250B2 (en) * 2015-08-24 2018-03-13 Caterpillar Inc. Hydraulic drive system for cryogenic pump
KR101734701B1 (en) * 2015-11-02 2017-05-11 현대자동차주식회사 Apparatus and method for filling lpg of lpg vehicle
CN106762167B (en) * 2015-11-23 2019-12-17 陕西汽车集团有限责任公司 Intelligent gas supply control system of LNG vehicle
CN105757449B (en) * 2016-04-26 2018-11-02 杭州西港低温技术有限公司 A kind of automobile-used LNG active boosts system and its air supply method
DE102016208166A1 (en) * 2016-05-12 2017-11-16 Robert Bosch Gmbh A fuel supply system for a gas powered internal combustion engine and method for operating a fuel supply system
DK179056B1 (en) * 2016-05-26 2017-09-25 Man Diesel & Turbo Filial Af Man Diesel & Turbo Se Tyskland Fuel supply system for a large two-stroke compression-ignited high-pressure gas injection internal combustion engine
SE542897C2 (en) * 2018-06-04 2020-08-18 Scania Cv Ab Method and system for controlling a state of fuel provided to an engine
DE102018211173A1 (en) 2018-07-06 2020-01-09 Robert Bosch Gmbh Method for operating a fuel delivery device for cryogenic fuels, fuel delivery device for cryogenic fuels
WO2020249681A1 (en) * 2019-06-14 2020-12-17 Volkswagen Ag Fuel supply system for primary supply of an energy conversion device from a gas cushion of a fuel tank in which gaseous fuel is stored in liquefied form
WO2021132513A1 (en) * 2019-12-25 2021-07-01 株式会社クボタ Work machine
DE102020001257A1 (en) * 2020-02-26 2021-08-26 Man Truck & Bus Se Device for fuel supply and vehicle with such a device
JP2021167795A (en) * 2020-04-13 2021-10-21 国立大学法人大阪大学 Blood analyzer
US11649156B2 (en) * 2020-12-28 2023-05-16 China Energy Investment Corporation Limited System and method for pre-cooling fuel dispenser
SE545674C2 (en) * 2021-06-15 2023-11-28 Scania Cv Ab A method and a control arrangement for determining the status of a fluid tank
KR102521520B1 (en) * 2021-07-09 2023-04-12 변혜숙 Cryogenic fuel tank with a pump

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4932214A (en) * 1987-10-04 1990-06-12 Deutsche Forsehungs- und Versuchsanslalt fuer Luft- und Raumfahrt e.v. Processing system for liquid hydrogen
WO1994023201A2 (en) * 1993-03-30 1994-10-13 Process Systems International, Inc. Cryogenic fluid pump and tank apparatus and method
US5566712A (en) * 1993-11-26 1996-10-22 White; George W. Fueling systems
EP1990272A1 (en) * 2007-05-08 2008-11-12 Daewoo Shipbuilding & Marine Engineering Co., Ltd Fuel gas supply system and method of an LNG carrier
US8113006B2 (en) * 2006-06-01 2012-02-14 Bayerische Motoren Werke Aktiengesellschaft System for the fuel storage and fuel delivery of cryogenic fuel
WO2012040835A1 (en) * 2010-10-01 2012-04-05 Westport Power Inc. Two engine system with a gaseous fuel stored in liquefied form

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0220453Y2 (en) * 1984-09-27 1990-06-04
US4947651A (en) 1989-04-07 1990-08-14 Minnesota Valley Engineering, Inc. Pressure building circuit for a container for low temperature fluids
US5228295A (en) 1991-12-05 1993-07-20 Minnesota Valley Engineering No loss fueling station for liquid natural gas vehicles
JP3165214B2 (en) * 1992-01-31 2001-05-14 マツダ株式会社 Fuel supply system for gaseous fuel engine
US5163409A (en) 1992-02-18 1992-11-17 Minnesota Valley Engineering, Inc. Vehicle mounted LNG delivery system
DE4212626C2 (en) * 1992-04-15 2001-04-19 Linde Ag Liquid hydrogen storage container and method for operating a drive unit with liquid or gaseous hydrogen from a storage container
US5329908A (en) * 1993-06-08 1994-07-19 Cummins Engine Company, Inc. Compressed natural gas injection system for gaseous fueled engines
US5421161A (en) 1993-09-27 1995-06-06 Minnesota Valley Engineering, Inc. Storage system for cryogenic fluids
US5673673A (en) * 1996-04-30 1997-10-07 Servojet Products International Method and apparatus for the high Mach injection of a gaseous fuel into an internal combustion engine
US5884488A (en) 1997-11-07 1999-03-23 Westport Research Inc. High pressure fuel supply system for natural gas vehicles
US6659730B2 (en) 1997-11-07 2003-12-09 Westport Research Inc. High pressure pump system for supplying a cryogenic fluid from a storage tank
US5937655A (en) 1997-12-04 1999-08-17 Mve, Inc. Pressure building device for a cryogenic tank
US6494191B2 (en) 1997-12-16 2002-12-17 Bechtel Bwxt Idaho, Llc Systems and method for delivering liquified gas to an engine
JP2002303211A (en) * 2001-04-04 2002-10-18 Yamaha Motor Co Ltd Gas fuel supply system for internal combustion engine
DE10230958A1 (en) * 2001-09-18 2004-01-22 Winkelmann, Karlheinrich, Dipl.-Ing. (TH) Fuel injection system, for an IC motor using LPG fuel, has an additional fuel pump in the fuel line to the injection pump to increase the fuel pressure in the flow from the tank
US6505469B1 (en) 2001-10-15 2003-01-14 Chart Inc. Gas dispensing system for cryogenic liquid vessels
US6799429B2 (en) 2001-11-29 2004-10-05 Chart Inc. High flow pressurized cryogenic fluid dispensing system
US6698211B2 (en) 2002-06-04 2004-03-02 Chart Inc. Natural gas fuel storage and supply system for vehicles
US7114342B2 (en) 2003-09-26 2006-10-03 Harsco Technologies Corporation Pressure management system for liquefied natural gas vehicle fuel tanks
KR100949692B1 (en) * 2005-09-15 2010-03-29 도요타 지도샤（주） Internal combustion engine using hydrogen
CA2527122C (en) 2005-12-20 2007-05-01 Westport Research Inc. Apparatus and method for pumping a fluid from a storage vessel and detecting when the storage vessel is empty
CA2653643C (en) 2009-02-26 2010-08-31 Westport Power Inc. Pressure control system and method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4932214A (en) * 1987-10-04 1990-06-12 Deutsche Forsehungs- und Versuchsanslalt fuer Luft- und Raumfahrt e.v. Processing system for liquid hydrogen
WO1994023201A2 (en) * 1993-03-30 1994-10-13 Process Systems International, Inc. Cryogenic fluid pump and tank apparatus and method
US5566712A (en) * 1993-11-26 1996-10-22 White; George W. Fueling systems
US8113006B2 (en) * 2006-06-01 2012-02-14 Bayerische Motoren Werke Aktiengesellschaft System for the fuel storage and fuel delivery of cryogenic fuel
EP1990272A1 (en) * 2007-05-08 2008-11-12 Daewoo Shipbuilding & Marine Engineering Co., Ltd Fuel gas supply system and method of an LNG carrier
WO2012040835A1 (en) * 2010-10-01 2012-04-05 Westport Power Inc. Two engine system with a gaseous fuel stored in liquefied form

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP2923062A4 *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112066246A (en) * 2015-04-30 2020-12-11 西港能源有限公司 Intelligent pressure management system for cryogenic fluid systems
CN107614962A (en) * 2015-04-30 2018-01-19 西港能源有限公司 Intelligent pressure management system for cryogen system
EP3289278A4 (en) * 2015-04-30 2018-11-07 Westport Power Inc. Intelligent pressure management system for cryogenic fluid systems
US10400712B2 (en) 2015-04-30 2019-09-03 Westport Power Inc. Intelligent pressure management system for cryogenic fluid systems
CN107614962B (en) * 2015-04-30 2020-09-11 西港能源有限公司 Intelligent pressure management system for cryogenic fluid systems
US10982626B2 (en) 2015-04-30 2021-04-20 Westport Power Inc. Intelligent pressure management system for cryogenic fluid systems
CN112066246B (en) * 2015-04-30 2022-04-19 西港燃料系统加拿大公司 Intelligent pressure management system for cryogenic fluid systems
US10060421B2 (en) 2015-06-29 2018-08-28 Caterpillar Inc. Hydraulic drive multi-element cryogenic pump
US20180313496A1 (en) * 2015-06-29 2018-11-01 Westport Power Inc. Multi-Vessel Fluid Storage and Delivery System
WO2017003569A1 (en) * 2015-06-29 2017-01-05 Caterpillar Inc. Hydraulic drive multi-element cryogenic pump
US11441736B2 (en) 2015-06-29 2022-09-13 Westport Fuel Systems Canada Inc. Multi-vessel fluid storage and delivery system
US20170016434A1 (en) * 2015-07-13 2017-01-19 Caterpillar Inc. Hydraulic Distributor for Pump
US9945364B2 (en) * 2015-07-13 2018-04-17 Caterpillar Inc. Hydraulic distributor for pump

Also Published As

Publication number Publication date
EP2923062B1 (en) 2018-02-28
CA2796794C (en) 2015-06-16
EP2923062A1 (en) 2015-09-30
CN104813016B (en) 2017-07-28
CN104813016A (en) 2015-07-29
EP2923062A4 (en) 2016-08-31
US20160017835A1 (en) 2016-01-21
US9771886B2 (en) 2017-09-26
CA2796794A1 (en) 2014-05-23

Similar Documents

Publication Publication Date Title
EP2923062B1 (en) Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine
EP3071826B1 (en) Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine
US11441736B2 (en) Multi-vessel fluid storage and delivery system
US10982626B2 (en) Intelligent pressure management system for cryogenic fluid systems
EP2622190B1 (en) Two engine system with a gaseous fuel stored in liquefied form
US9212643B2 (en) Dual fuel system for an internal combustion engine
CA2860682C (en) Gaseous fluid supply system with subsystem for isolating a storage vessel from an end user
JP6102152B2 (en) Liquefied gas fuel supply system and liquefied gas fuel supply method
AU2007270173B2 (en) System for injecting liquid vapour
EP3168445A1 (en) Dual fuel system for powering combustion engines

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 13857182

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2013857182

Country of ref document: EP