CN101595293A - Propellant transfer system - Google Patents

Propellant transfer system Download PDF

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Publication number
CN101595293A
CN101595293A CNA2007800407016A CN200780040701A CN101595293A CN 101595293 A CN101595293 A CN 101595293A CN A2007800407016 A CNA2007800407016 A CN A2007800407016A CN 200780040701 A CN200780040701 A CN 200780040701A CN 101595293 A CN101595293 A CN 101595293A
Authority
CN
China
Prior art keywords
sparger
chamber
liquid gas
liquid
steam
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CNA2007800407016A
Other languages
Chinese (zh)
Inventor
詹姆士·理查德·亨特
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
TURNER GEOFFREY RUSSELL HUNT JAMES RICHARD
TURNER GEOFFREY RUSSELL HUNT J
Original Assignee
TURNER GEOFFREY RUSSELL HUNT JAMES RICHARD
TURNER GEOFFREY RUSSELL HUNT J
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
Priority claimed from AU2006906054A external-priority patent/AU2006906054A0/en
Application filed by TURNER GEOFFREY RUSSELL HUNT JAMES RICHARD, TURNER GEOFFREY RUSSELL HUNT J filed Critical TURNER GEOFFREY RUSSELL HUNT JAMES RICHARD
Publication of CN101595293A publication Critical patent/CN101595293A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/023Valves; Pressure or flow regulators in the fuel supply or return system
    • F02M21/0239Pressure or flow regulators therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0203Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels characterised by the type of gaseous fuel
    • F02M21/0209Hydrocarbon fuels, e.g. methane or acetylene
    • F02M21/0212Hydrocarbon fuels, e.g. methane or acetylene comprising at least 3 C-Atoms, e.g. liquefied petroleum gas [LPG], propane or butane
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0248Injectors
    • F02M21/0278Port fuel injectors for single or multipoint injection into the air intake system
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0284Arrangement of multiple injectors or fuel-air mixers per combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/0287Details 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M31/00Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
    • F02M31/20Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for cooling
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

The present invention discloses a kind of propellant transfer system, and this system comprises have the chamber housing (3) of (310), and sparger (20) is arranged in chamber (310).Liquid gas inlet (301) is fed to liquid gas in the chamber (310), and this liquid gas can and then be supplied to described sparger (20) with in the cylinder that is ejected into motor like this.Dispatch tube (315) will be fed to steam jet ejector (313) by the liquid gas of described sparger (20) ejection in described chamber (310), and this steam jet ejector (313) is formed for regulating the pressure regulator of the pressure of described liquid gas in the described chamber (310) and any steam.Described sparger (313) has been overcome relevant problem of freezing as pressure regulator near described regulator, this problem can hinder the normal running of described regulator.

Description

Propellant transfer system
Technical field
The present invention relates to a kind of propellant transfer system, more specifically, relate to a kind of improvement disclosed fuel injector system among International Application PCT/AU2003/000971 (WO 2004/018862).
Background technique
Above-mentioned international application discloses a kind of being used for and will be transferred to the propellant transfer system of motor such as liquid gas fuels such as liquefied petroleum gas (LPG).Particularly, the system of above-mentioned international application discloses this fuel and has been transferred to motor with diesel fuel simultaneously.
The system of aforesaid international application comprises the piece with thorax hole, and described thorax hole is used to the liquid ejector of admitting the steam ejection liquefaction gaseous fuel to use.This piece comprises maze path, so that liquid gas fuel can cool off described by described path.Liquid gas fuel also is supplied to the chamber around liquid ejector, so that liquid ejector and liquid gas fuel keep cooling, thereby liquid gas fuel remains liquid state, with by described sparger ejection.Pressure regulator is arranged on described sparger downstream, be used for regulating the pressure in described chamber, thereby the pressure in the described chamber and supply pressure are about equally, described liquid gas to be provided and to make the pressure in regulator downstream keep relatively low than the pressure in the described chamber.This pressure regulator comprises tabula, spring, pin and Sealing, to be fixed on the bearing.
The system of aforesaid international application operates very good under most of situations.Yet, find recently, if there is very a large amount of water in the liquid gas fuel, can in regulator, form ice.This stops the normal running of regulator, thereby causes fuel that circulating phase-change between steam state and the liquid state takes place in sparger, and this prevention fuel normally sprays with liquid state.Like this, sparger possibly can't proper functioning so that fuel is provided to motor.
Summary of the invention
The objective of the invention is to overcome the problems referred to above.
The present invention can be considered to be devoted to provide a kind of propellant transfer system, is used for liquid gas fuel is transferred to the cylinder of motor, comprising:
Housing;
Being used in described housing admitted the chamber of sparger, and described sparger comprises that the permission liquid gas is fed to described sparger with the opening from this sparger ejection;
The liquid gas that is communicated with described chamber inlet is used for that liquid gas introduced described chamber and liquid gas is introduced described sparger when described sparger is arranged in described chamber;
The outlet in described chamber;
Pass the path of described housing, liquid gas can flow through this path; With
Be used to regulate the pressure regulator of the pressure of steam in the described chamber and/or liquid gas, this pressure regulator comprises the regulator injector that is arranged in downstream, described chamber.
Like this, by described sparger is used as pressure regulator,, when descending, pressure can not freeze even there is very a large amount of water in the liquid gas fuel yet, guarantee normally to keep the pressure in the described chamber thus, and guarantee that the liquid ejector normal running is to supply fuel to described motor.Reason to this is that by electrical signal is applied to sparger, regulator injector is operated with in good time opening and closing sparger, thereby reduces the pressure in the chamber.Because sparger opened and closed in good time, thereby this sparger can not stay the little opening that can be easy to freeze and trends towards staying open as the situation in traditional tabula formula regulator.Further, because the attribute of sparger and in good time opening and closing, thereby pressure descends to occurring in apart from sparger and exports some distances, has roughly very big force value thus in sparger, and this prevents to hinder the formation of the ice of sparger operation.
Preferably, described housing comprises maze path, is used to admit the liquid gas fuel of liquid state or steam state, further to help cooling off the fuel in described housing and described sparger and this sparger, thereby described fuel remains liquid state in described chamber, with by described liquid ejector ejection.
Preferably, described regulator injector is fed to described labyrinth with described steam and/or liquid gas fuel.
Preferably, described chamber, described regulator injector and described maze path form the flow path in the described housing, be used for cooling off the liquid gas and the described liquid ejector in described housing and described chamber, thereby make described liquid gas keep liquid, to spray by described liquid ejector.
Preferably, described housing adopts the form of piece.
Preferably, described path has inlet and fuel reservoir in upstream, described chamber, is used for liquid gas and/or steam is fed to the dispatch tube of described regulator injector from described chamber and at the outlet of described regulator injector and the expansion chamber between the described maze path.
Preferably, described maze path has outlet, and steam and/or liquid gas can be supplied to the steam piece from described outlet, so that described fuel is converted into steam condition fully, to be ejected into described motor as steam.
Preferably, described regulator injector comprises steam jet ejector.
Yet in other embodiments, described regulator injector can be the sparger of any other type.
Preferably, described system further comprises the diesel injection device that is used for diesel fuel is fed to simultaneously described motor.
Description of drawings
The preferred embodiments of the present invention will by example and reference will be made to the accompanying drawings, wherein:
Fig. 1 is the schematic representation of the preferred embodiment of the present invention;
Fig. 2 is the partial view of the preferred embodiment of the present invention;
Fig. 3 is a vertical view cutaway drawing according to the preferred embodiment of the invention, and it illustrates four injection apparatus correctly aiming at and be connected to inlet manifold with the ingress port of cylinder head; And
Fig. 4 is the embodiment's of Fig. 2 the partial view of a part, and it illustrates the complete structure details of this part of Fig. 2.
Embodiment
Referring to Fig. 1, liquefied petroleum gas container 12 is fed to operation circuit 16 with liquefied petroleum gas (LPG) via container lock 14 and is fed on the in-line filter 4.Then, the liquefied petroleum gas (LPG) after the filtration is sent to allocation block 38 by operation circuit 37.Petroleum gas liquid after the liquefaction flows through heat insulation transmission line 39 to case of sprayer 3 (being presented at Fig. 4 in more detail) from allocation block 38.
Referring to Fig. 2, enter housing 3 from the petroleum gas after the liquefaction of circuit 39, this describes in detail with reference to Fig. 4.Housing 3 has the liquid ejector 20 that is used for LPG supply is arrived motor E.
Use the liquid in the sparger 20 and be fed to the pulse width of sparger 20 from ECU 70, the liquefied petroleum gas (LPG) after the liquefaction is advanced by sparger 20 and is ejected to (see figure 3) in the manifold 32, and should spray directly towards ingress port 29 (see figure 3)s.The injection of the petroleum gas after the liquefaction is by ECU 70 set times, (see figure 3) before making pulsing (see figure 3) and inlet valve 132 being closed after escape cock 133 cuts out, thereby the downward action (see figure 3) of piston 131 can enter motor E, and the petroleum gas after all liquefaction is ejected, and does not leak by escape cock 133.
In the housing 3 do not enter sparger 20 and can be steam state or liquid liquefaction after gas, leave housing 3 by pipeline 240.Pipeline 240 passes bleed gas heater 250.Bleed gas heater 250 has inlet 251a and outlet 252a, inlet 251a and outlet 252a can be connected in the engine cooling waterpipe, so that temperature is about 70 ℃ engine cooling water by heater 250, thereby heat is fed to heater 250, particularly heat is fed to the part of pipeline 240 in heater 250 inside.Like this, any liquid gas by pipeline 240 all is heated also thereby is converted into steam state (if not the words that are in steam state).Pipeline 240 is connected to bleed injector 260, and sparger 260 is designed to spray gas rather than liquid, and sparger 260 sprays steam into inlet manifold 32, as shown in Figure 2.Bleed injector 260 is subjected to ECU 70 controls via the pulse that receives on the circuit 253.Be similar to the pulse on the circuit 86, the time set of the pulse on the circuit 253 makes sparger 260 open when closing with escape cock 133 at inlet valve 132 and activates, so that the liquefied petroleum gas (LPG) of steam state together is supplied to motor E with liquid from sparger 20 ejections.Like this, the identical mode of steam supply employing and liquid supply is controlled, thereby prevents or at least significantly reduce the spill and leakage (blow-through) of steam by motor.The length of the pulse of supply makes the gas flow of wishing be injected in the motor on the size of sparger 260 and the circuit 253, thereby injection can not affected adversely, simultaneously, the cooling effect that is provided by the path through inlet 11, housing 203 and pipeline 240 of liquid gas can not have a negative impact to the cooling of sparger 20.
Bleed gas heater 250 guarantees not have liquid liquid gas to arrive bleed injector 260, because this will change mixture because of the fuel density difference between the liquefied petroleum gas (LPG) of liquid and steam state.
By the heat of bleed gas heater 250 supply preferably the sufficient to guarantee temperature be higher than the steam point of liquefied petroleum gas (LPG) and relatively stable fully.
Fig. 2 and Fig. 3 also illustrate diesel injection device 171, are used for diesel fuel is arrived with the LPG supply via sparger 20 and sparger 260 supplies simultaneously the cylinder of motor E.Like this, by the fuel of supply from the form of liquid petroleum gas of sparger 20 and 260, required diesel fuel amount can be reduced, thereby situation about comparing when only supplying diesel fuels by diesel injection device 171 improves saving of fuel.Further, be transferred to motor by guaranteeing in housing 203 to become the liquid gas that is used for cooling injection device 20 that bubble overflows to close when opening once more with vapor form with inlet valve 132 at the escape cock 133 of engine cycles process, can guarantee that thereby fuel is effectively used increase power, this means does not need very big choke pressure, thereby further reduces firing rate.Fuel supplying also prevents spill and leakage by this way, and this spill and leakage is not only wasted fuel, and can make discharging significantly increase to undesirable level.
Fig. 4 illustrates the details of housing 3.As shown in Figure 4, housing 3 employings are by the form of the piece 300 that forms such as metals such as aluminium.Piece 300 has the lpg inlet 301 of reception from liquefied petroleum gas (LPG) (lpg) fuel of circuit 39.Inlet 301 links to each other with storage 380.
By passing the major diameter thorax hole that end face 309 forms, in piece 300, also form injector chambers 310.Storage 380 has the outlet 311 of the injector chambers of passing to 310 bottoms.Injector chambers 310 has from the chamber path 312 that 310 top extends to dispatch tube 315.Dispatch tube 315 links to each other with steam jet ejector 313, and steam jet ejector 313 is located in the thorax hole 320 that forms in the piece 300.Steam jet ejector 313 is formed for regulating the regulator of the pressure of liquefied petroleum gas (LPG) in the chamber 310 and/or steam, this regulator makes sparger 20 keep cooling, and make the liquefied petroleum gas (LPG) in the chamber 310 keep cooling then, thereby described liquid can not form bubble or evaporation and remain liquid state thus in sparger 20, to be ejected to motor E by liquid ejector 20.
Because the pressure in the chamber 310 is kept by the regulator injector 313 that adopts the steam jet ejector form, therefore,, when descending, pressure can not freeze even when in LP gas fuel, having too much water yet.Therefore, the LP gas fuel proper flow flow to outlet 317 to sparger 20 and from path 312, with desirable pressure in the holding chamber 310, and keeps the liquefied petroleum gas (LPG) in the sparger 20 to be in liquid phase, to spray from sparger.Sparger 313 has outlet 314, the first outlet thorax holes 315 that supply fuel to the first outlet thorax hole 315 and forms expansion chambers and combine with the labyrinth path 316 that passes piece 300.Labyrinth path 316 with combine referring to figs. 1 through the described outlet 317 that is connected to pipeline 240 of Fig. 3.
The various piece 380,315 of described path and 316 forms by boring the thorax hole and block this thorax hole with the pin (not shown) where necessary in piece, perhaps by formation thorax hole in the surface of piece 300, seal this surface with the cover plate (not shown) then and form.The cover plate (not shown) also can be used for Closed End 309 so that sparger 20 securely is positioned in the chamber 310.
Liquefied petroleum gas (LPG) 301 is transferred in the chamber 310 by entering the mouth.This liquefied petroleum gas (LPG) is in high pressure.Sparger 20 is arranged in chamber 310, and is the sparger of market circulation, and it comprises a plurality of inlet openings 330 around its periphery.Hole 330 is arranged to outlet 311 rough alignment that make itself and storage 380, makes liquid liquefied petroleum gas (LPG) can enter in the hole 330 of below, with from sparger 20 ejections.Signal is supplied to the terminal 20a of sparger 20 with operation sparger 20 from ECU 70.
Near outlet 311 and be converted into any liquefied petroleum gas (LPG) of steam state or bubble in the chamber 310 and will be roughly flow and flow to towards the top in chamber 310 and export in the thorax hole 312 around sparger 20.Sparger 20 is provided with around the hole 330 screen covering (not shown), and this also helps bubble and moves and do not enter in the hole 330 around the periphery of sparger 20.Like this, the fuel that enters sparger 20 is in liquid preparing against and sprays, rather than steam or bubble, if described steam that may form or bubble enter the operation that sparger 20 will hinder sparger 20.Outlet thorax hole 312 is communicated with regulator injector 313 with the pressure in the holding chamber 310.Yet, when the pressure in chamber 310 and the thorax hole 312 raises, by to terminal 391 regulator injector 313 being opened signal provision, make the liquefied petroleum gas (LPG) that is in steam or bubble state can pass through regulator injector 313, to be ejected to exit passageway 315 from regulator injector 313, to pass through labyrinth 316 to exit passageway 317, more then to heater 250 then, thereby be fed to motor with steam state, as preceding referring to figs. 1 through as described in Fig. 3.
Regulator 313 thereby be used for the high-pressure area of holding chamber 310, this high-pressure area connects back container 12 by inlet 301.Like this, the pressure in regulator 313 holding chambers 310 approaches supply container pressure as far as possible.This helps making liquefied petroleum gas (LPG) mainly to remain liquid state, to be sprayed by sparger 20.This with piece 300 by liquefied petroleum gas (LPG) from entering the mouth 301 to outlet 317 coolings, be used for minimizing the boiling of the liquefied petroleum gas (LPG) of piece 300, thereby can not hinder liquefied petroleum gas (LPG) to arrive flowing of sparger 20 and from the ejection of sparger 20.Yet, as previously mentioned, to flow to path 312 around sparger 20 by any bubble due to the boiling of liquefied petroleum gas (LPG) or steam, and by the increase of the pressure due to this vaporization regulator 313 will be opened to allow gentle bubble mixt of steam and excessive pressure to release by regulator 313, be closed up to pressure reduction and regulator 313.
At the pressure in regulator 313 downstream sides significantly less than the pressure in the chamber 310, and regulator 313 also keeps the environment under low pressure in downstream side, and making can the vaporization fully owing to the relatively low pressure environment of comparing at the pressure environment with in the chamber 310 in regulator 313 downstream sides by any liquefied petroleum gas (LPG) of regulator 313.Liquefied petroleum gas (LPG) helps cooling block 300 by exporting 317 path and vaporization thereof, thereby makes the liquefied petroleum gas (LPG) of regulator 313 upstream sides mainly remain liquid state as previously mentioned.
As described in referring to figs. 1 through Fig. 3, steam is fed to heater 250 by pipeline 240, and owing to the heat that is supplied to liquefied petroleum gas (LPG) by heater 250, any liquefied petroleum gas (LPG) that is not in steam state as yet will be vaporized.The liquefied petroleum gas (LPG) that is in steam state is supplied to bleed injector 260 then, in the inlet manifold that is introduced into motor E.
Regulator 313 is operated by signal being put on terminal 391, as previously mentioned.These signals can obtain from ECU 70 according to compiling the fuel mapping scheme (mapping plan) to the ECU 70, and described fuel mapping scheme also is used to start sparger 20 liquid gas fuel is transferred to motor E.
Yet, in other embodiments, regulator 313 can be opened and closed by electrical signal, described electric response is supplied by the pressure measuring value of the acquisition of the pressure transducer (not shown) in the chamber 310, make that when pressure reaches predeterminated level sparger 20 is opened, is closed then to allow fuel to leave regulator 313 and lead to piece 250.
Because those skilled in the art can be easy to be implemented in the various modifications in the spirit and scope of the invention, thereby it should be understood that the present invention is not limited only to the above specific embodiment of describing by example.
In in appended claims and more than of the present invention, describing, unless because language performance or necessary implication and in statement, need separately, otherwise, term " comprises " or its near synonym for example " comprise " or " having " is used for the Campatible statement, promptly, in various embodiments of the present invention, indicate the existence of described feature, but do not get rid of the possibility that exists or add further feature.

Claims (9)

1, a kind of propellant transfer system is used for liquid gas fuel is transferred to the cylinder of motor, comprising:
Housing;
Being used in described housing admitted the chamber of sparger, and described sparger comprises that the permission liquid gas is fed to described sparger with the opening from this sparger ejection;
The liquid gas that is communicated with described chamber inlet is used for that liquid gas introduced described chamber and liquid gas is introduced described sparger when described sparger is arranged in described chamber;
The outlet in described chamber;
Pass the path of described housing, liquid gas can flow through this path; With
Be used to regulate the pressure regulator of the pressure of steam in the described chamber and/or liquid gas, this pressure regulator comprises the regulator injector that is arranged in downstream, described chamber.
2, propellant transfer system according to claim 1, wherein said housing comprises maze path, be used to admit the liquid gas fuel of liquid state and/or steam state, further to help cooling off the fuel in described housing and described sparger and this sparger, thereby described fuel remains liquid state in described chamber, to be sprayed by described liquid ejector.
3, propellant transfer system according to claim 1, wherein said regulator injector is fed to described labyrinth with described steam and/or liquid gas fuel.
4, propellant transfer system according to claim 1, wherein said chamber, described regulator injector and described maze path form the flow path in the described housing, be used for cooling off the liquid gas and the described liquid ejector in described housing and described chamber, thereby make described liquid gas keep liquid, to spray by described liquid ejector.
5, propellant transfer system according to claim 1, wherein said housing adopts the form of piece.
6, propellant transfer system according to claim 2, wherein said path have at the inlet and the fuel reservoir of upstream, described chamber, are used for liquid gas and/or steam is fed to the dispatch tube of described regulator injector from described chamber and at the outlet of described regulator injector and the expansion chamber between the described maze path.
7, propellant transfer system according to claim 2, wherein said maze path has outlet, steam and/or liquid gas fuel can be supplied to the steam piece that is used for described fuel is converted into fully steam state from described outlet, to be ejected into described motor as steam.
8, propellant transfer system according to claim 1, wherein said regulator injector comprises steam jet ejector.
9, propellant transfer system according to claim 1, wherein said system further comprise the diesel injection device that is used for diesel fuel is fed to simultaneously described motor.
CNA2007800407016A 2006-10-31 2007-10-22 Propellant transfer system Pending CN101595293A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU2006906054 2006-10-31
AU2006906054A AU2006906054A0 (en) 2006-10-31 Fuel delivery system

Publications (1)

Publication Number Publication Date
CN101595293A true CN101595293A (en) 2009-12-02

Family

ID=39343677

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2007800407016A Pending CN101595293A (en) 2006-10-31 2007-10-22 Propellant transfer system

Country Status (4)

Country Link
EP (1) EP2158396A1 (en)
CN (1) CN101595293A (en)
AU (1) AU2007314133A1 (en)
WO (1) WO2008052248A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103502617A (en) * 2011-05-18 2014-01-08 艾莫股份公司 Injection rail

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8300441A (en) * 1983-02-04 1984-09-03 Vialle Bv EVAPORATIVE PRESSURE CONTROL DEVICE.
AU2087888A (en) * 1987-07-10 1989-02-13 Gaspower Limited Improvements in or relating to fuel injection
US5671711A (en) * 1995-12-07 1997-09-30 Ford Global Technologies, Inc. Low pressure LPG vapor fuel injection
AU2002950972A0 (en) * 2002-08-23 2002-09-12 Hunt, James Richard Fuel delivery system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103502617A (en) * 2011-05-18 2014-01-08 艾莫股份公司 Injection rail

Also Published As

Publication number Publication date
AU2007314133A1 (en) 2008-05-08
EP2158396A1 (en) 2010-03-03
WO2008052248A1 (en) 2008-05-08

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Open date: 20091202