CA2205008A1 - Fuel control - Google Patents

Fuel control

Info

Publication number
CA2205008A1
CA2205008A1 CA002205008A CA2205008A CA2205008A1 CA 2205008 A1 CA2205008 A1 CA 2205008A1 CA 002205008 A CA002205008 A CA 002205008A CA 2205008 A CA2205008 A CA 2205008A CA 2205008 A1 CA2205008 A1 CA 2205008A1
Authority
CA
Canada
Prior art keywords
check valve
chamber
valve chamber
regulator
diaphragm
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.)
Abandoned
Application number
CA002205008A
Other languages
French (fr)
Inventor
Walter J. Diederich
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.)
ThermoLyte Corp
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of CA2205008A1 publication Critical patent/CA2205008A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D16/00Control of fluid pressure
    • G05D16/04Control of fluid pressure without auxiliary power
    • G05D16/0402Control of fluid pressure without auxiliary power with two or more controllers mounted in series
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D16/00Control of fluid pressure
    • G05D16/04Control of fluid pressure without auxiliary power
    • G05D16/06Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule
    • G05D16/063Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule the sensing element being a membrane
    • G05D16/0644Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule the sensing element being a membrane the membrane acting directly on the obturator
    • G05D16/0655Control of fluid pressure without auxiliary power the sensing element being a flexible membrane, yielding to pressure, e.g. diaphragm, bellows, capsule the sensing element being a membrane the membrane acting directly on the obturator using one spring-loaded membrane
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/465Details, e.g. noise reduction means for torches
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23KFEEDING FUEL TO COMBUSTION APPARATUS
    • F23K2400/00Pretreatment and supply of gaseous fuel
    • F23K2400/20Supply line arrangements
    • F23K2400/201Control devices
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/87917Flow path with serial valves and/or closures
    • Y10T137/88054Direct response normally closed valve limits direction of flow

Abstract

A fuel control system for use with a source of pressurized fuel includes housing structure (10, 12, 14) defining an inlet (51), an outlet, a check valve chamber (66) and a regulating valve (78) chamber disposed between the inlet and outlet structures. Check valve structure (62) is disposed in the check valve chamber (66) for preventing liquid fuel from reaching the outlet structure, and control valve structure is disposed in the regulating valve chamber (78). The control valve structure includes diaphragm structure (22) dividing the regulating valve chamber into a downstream chamber (80) open to atmospheric pressure and an upstream chamber on the opposite side of the diaphragm structure that is in communication with the check valve chamber (66). Regulator valve structure is coupled to the diaphragm structure (22) for movement between a first position in which the valve passage is open to permit flow of fuel from the check valve chamber (66) to the outlet structure and a second position in which the valve passage is closed.

Description

CA 0220~008 1997-0~-09 WO96115405 PCT~S95/14706 FUE~ ~0~
This invention relates to fuel ~On~LO1 systems and 5 more particularly to regulators of the type useful for co~necting a portable gas appliance such as a flashlight or gas torch to a fuel supply reservoir and controlling fuel vapor flow rate to the gas appliance.
In such appliances, a controller desirably lO controls the rate of flow of fuel from the fuel supply and shuts off the fuel supply when desired. It is also neceCc~ry to substantially reduce the pressure of liquified fuel as it passes out of the supply to the gas appliance and to aid in vaporization of liquified fuel.
15 In many such appli~ncec, the operating characteristics of the appl;An~ may change widely ~epenA; ng on the operating temperature and the orientation of the fuel supply. If liquid fuel is passed to the appliance without complete vaporization, a markedly increased burn 20 rate may result. Also, if the liquid fuel with a small amount of entrained impurity such as paraffin in solution p~s~c through the control system, a downstream orifice may be clogged or permanently disabled.
In accordance with one aspect of the invention, 25 there is provided a fuel control system for use with a source of pressurized fuel includes housing structure defining an inlet, an outlet, a check valve chamber and a regulating valve chamber disposed between the inlet and outlet structures. First (check) valve structure ~s 30 disposed in the check valve chamber for preventing liquid fuel from reaching the outlet structure, and ~eco~
(control) valve structure is disposed in the regulating valve chamber. The second valve structure includes regulator ~i~phragm structure dividing the regulating 35 valve chamber into a downstream chamber open to CA 0220~008 1997-05-09 W O 96/15405 PCTrUS95/14706 atmospheric pressure and an uy~L~eam chamber on the opposite side of the ~;Arh~agm structure that is in communication with the check valve c-h~hsr. Regulator r valve structure is coupled to the regulator diaphragm S structure for movement between a first position in which the valve r~CcAge is open to permit flow of fuel from the check valve chamber to the outlet structure and a s~con~
position in which the valve passage is closed; and includes adjustment structure for shifting the regulator 10 valve structure relative to the regulator diaphragm structure for changing the pressure across the regulator ~i~rhragm structure that will cause the regulator valve structure to move between the first and second positions.
Preferably, the first valve structure includes a 15 check valve diaphragm member disposed in the check valve chamber that divides that check valve chamber into upstream and downstream chambers. Check valve structure is carried by the check valve diaphragm and valve seat structure is disposed in the upstream check valve 20 chamber, the check valve structure being adapted to close when the pressure differential between the upstream and downstream check valve chambers is less than a predetermined value such that fuel does not flow from the upstream check valve chamber to the do~nstream check 25 valve chamber. In a particular embodiment the check valve pressure differential that causes the check valve structure to close is in the range of 35-80 kilopascals (5-12 psi).
In a particular embodiment, the regulator valve 30 structure adjustment structure includes a threaded member carried by the regulator ~;~phragm and coupling structure threadedly connected to the threaded member. The regulator valve structure is carried by the coupling structure and rotation of the coupling structure relative 35 to the regulator diaphragm structure axially shifts the CA 0220~008 1997-0~-09 WO96/15405 PCT~S95114706 position of the regulator valve structure relative to the ~;~phragm structure.
Preferably, the check valve diaphragm and the regulator valve ~;~phragm are of metallic material, a 5 particularly preferred material being stainless steel, although other materials, including polymeric material may be used in particular embodiments. In a particular emhoAiment, restricted flow structure connects the inlet structure and the check valve chamber, the restricted lO flow structure in a particular embodiment being a passage of about 0.3 millimeter diameter and a length of about two millimeters.
In accordance with another aspect, there is provided a control system for use with a source of 15 pressurized fuel that includes housing structure defining inlet structure for receiving fuel from a source of pressurized fuel, outlet structure, check valve chamber structure, and regulator valve chamber structure between the inlet and outlet structures. First (check) valve 20 structure is disposed in the check valve chamber for preventing liquid fuel from reaching the outlet structure, the first valve structure including metallic check valve diaphragm structure that divides the check valve chamber into upstream and downstream chambers, a 25 check valve member carried by the check valve diaphragm, and valve seat structure disposed in the upstream check valve chamber. The check valve is adapted to close when the pressure differential between the upstream check valve chamber and the downstream check valve chamber is 30 less than a predetermined value so that fuel does not flow from the upstream check valve chamber to the downstream check valve chamber. Second valve structure is disposed in the regulator valve chamber and includes metallic regulator valve diaphragm structure that is 35 disposed generally parallel to the check valve diaphragm CA 0220~008 1997-0~-09 WO 96115405 }'CT/US95/14706 structure and divides the regulator valve chamber into a downstream regulator valve chamber open to atmospheric pressure and an upstream regulator valve ch~h~ on the opposite side of the regulator valve ~;~phragm structure 5 from the downstream regulator valve chamber and in communication with the downstream check valve chamber through first passage structure. Second passage structure connects the regulator valve upstream chamber and the outlet structure, and regulator valve structure 10 is coupled to the regulator valve diaphragm structure for movement between a first position in which the first passage structure is open to permit flow of vaporized fuel from the check valve ch~h~r through the first passage structure to the outlet structure and a seco~
15 position in which the first passage structure is closed.
Preferably, each of the upstream and downstream check valve chambers has a depth that is less than one tenth the width of the check valve chamber; and-in a particular embodiment, each of the u~ ~L eam and downstream check 20 valve chambers has a depth of less than one millimeter.
Other features and advantages of the invention will be seen as the following description of a particular embodiment progresses, in conjunction with the drawings, in which:
Fig. 1 is a sectional view of gas flow control apparatus in accordance with the invention; and Fig. 2 is an exploded perspective view of components of the gas flow control apparatus shown in Figure 1.
De~cription of Particular Embodime~t The flow control apparatus shown in Figure 1 includes housing structure with base member 10, intermediate member 12, and cap member 14 that are secured together with bolts 16. Secured between members 35 10 and 12 is stainless steel diaphrag~ 18 that carries a CA 0220~008 1997-0~-09 WO 96/15405 PCI'IUS95/14706 first (check valve) assembly 20; and secured between housing members 12 and 14 is stainless steel ~;Aphragm 22 that carries coupling assembly 24 to which regulator valve member 26 of a seco,nd valve,assembly is threadedly 5 attached.
Cap member 14 includes tubular extension portion 30 with internal thread 31 (Fig. 2) and shoulder 33 on which is disposed sleeve 32. Sleeve 32 is seated against shoulder 33 and is secured in angular position with set 10 screw 34. Apertures 35 (Fig. 2) in extension portion 30 allow insertion of a regulator valve adjustment tool for axially adjusting the position of regulator valve member 26 relative to valve seat 74 in valve-open position.
Ports 36 in extension portion 30 cooperate with ports 38 15 in sleeve 32 for adjusting aspirated air inlet port area.
Thr~ ly disposed within extension 30 is Venturi 40 and seated on leading edge 41 of Venturi 40 is internal flange 42 of elastomeric coupling member 44. Mullite tube 46 has trailing end 47 received within coupling 44 20 and seated on flange 42. Received on the remote end of mullite tube 46 is refractory metal oxide fabric gas mantle 48 of the type disclosed in Nelson U.S. Patent No.
4,976,606 for use in a thermophotovoltaic system, whose disclosure is incorporated herein by reference. This 25 fuel control system is adapted for use in a portable light source of the general type shown in Diederich U.S.
Patent Nos. 4,975,044 and 5,240,407, the disclosures of which are incorporated herein by reference.
Base member 10 includes tubular structure 50 that 30 defines an inlet fuel passage 51 of about one centimeter diameter and that includes screw threads 52 for co~n~ction to a suitable cont~;n~r (diagrammatically indicated at 54) of liquified fuel such as propane that has a pressure of about 700 kilopascals at room 35 temperature. Formed at the inner end of the inlet CA 0220~008 1997-0~-09 WO96/1~05 PCT~S95/14706 passage 51 iS restricted flow passage 56 of about 0.3 millimeter diameter and a length of about two millimeters. In an alternate embodiment, a porous metal filter having flow characteristics similar to pA~C~e 56 5 may be utilized to provide a restricted flow passage from the inlet pACc~e 51 to the u~ LLeam side of check valve ~;~phragm 18. Formed in base member 10 adjacent the outlet of pA.Cc~qe 56 iS recess 58 that receives resilient check valve seat member 60 that cooperates with check 10 valve disc member 62 carried by diaphragm 18.
Diaphragm 18 is a stainless steel disk that is about 0.1 millimeter thick and has a diameter of about two centimeters and is seated between base member 10 and intermediate member 12 with its peripheral portion 15 disposed between circumferential ridges 63 and sealed by O-rings 64. Secured to the center of diaphragm 18 by press fit metal ring 67 iS check valve member 62 that has through passage 70 of about one-half millimeter diameter and about two millimeters length. Upstream check valve 20 chamber 66 has a depth of about one-tenth millimeter and a diameter of about 1. 8 centimeters and downstream check valve chamber 68 has a diameter dimension similar to that of upstream chamber 66 and a depth of about one-half millimeter. The small depth dimension of chamber 66 25 prevents damage to ~iAphragm 18 when fuel container 54 iS
removed.
With reference to Figs. 1 and 2, formed in downstream check valve chamber 68 iS recess 72 at the base of which is formed valve seat 74 and through passage 30 76 of about 1.5 millimeter diameter in which is disposed the stem portion 84 of valve member 26 with a diametrical clearance of about o. 05 millimeter. Secured between intermediate member 12 and cap member 14 iS stainless steel ~;~phragm 22 which cooperates with intermediate 35 member 12 to define regulating valve chamber 78 of about CA 0220~008 1997-0~-09 WO96/15405 PCT~S95114706 1/2 millimeter depth and about 1.7 centimeters diameter, and cooperates with cap member 14 to define chamber 80 which is open to atmosphere through apertures 35. The peripheral edge 73 of diaphragm 22 is secured between 5 An~ r ridge 75 of cap member 14 and sealing O-ring 77 carried by intermediate member 12.
Carried by diaphragm 22 is coupling assembly 24 to which regulator valve member 26 is threadedly attached.
Valve member 26 has head portion 82 and a shank portion 10 that has slot 130 at its end, cylindrical stem portion 84 and threaded section 86 with flat 88 that extends beyond the length of threaded section 86. Received in yLoo~e 87 at the base of head portion 82 is 0-ring 90 that is adapted to seat against valve seat 74 when the regulator 15 valve 26 is closed to block flow of fuel from check valve chamber 68. When valve 26 is closed, regulating valve chamber 78 remains open through valve flat 88 and slot 130 so that pressure in chamber 78 bleeds off through orifice holder 116 and orifice 120.
Coupling assembly 24 (as shown in Figure 2) includes coupling ring member 92 with portion 94 that is received in aperture 96 of ~i~phragm 22 and secured with press fit ring 98. Coupling ring 92 has internal thread 100 and internal annular recess 101 which receives seal 25 ring 102 carried in yLoo~e 103 of cooperating coupling member 104 that has external thread 106 that engages internal thread 100. Member 106 also has internal thread 108 which thre~ y receives threaded shank 86 of valve member 26, head portion 110 with crenelated portion 112 30 and a socket portion which receives head portion 114 of brass orifice holder 116 that carries jewel (sapphire) 118 that defines a metering orifice 120 about 0.05 millimeter diameter. Ring 122 centers orifice holder 116 within recess 123 in tubular extension 30 of cap member 35 14.

CA 0220~008 1997-0~-09 Thr~A~e~ly received in extension 30 is Venturi member 40 that delivers an air-fuel ratio of up to about 25:1 (as a function of angular adjustment of sleeve 32);
and seated on the leading edge 41 of Venturi 40 is flange 5 42 of resilient coupling sleeve 44 . ~7h~ r mullite member 46 of six millimeters diameter and twenty-five millimeters length has its trailing end 47 inserted in resilient coupling 42 and refractory metal oxide fabric gas mantle 48 is mounted on the remote end of mullite 10 tube 46.
The forked end 125 of control lever 124 is received between head 114 and flange 115 for coupling to orifice holder 116 and is pivoted on pin 126 and engaged by the ~ollL~ol bolt 128 for axially shifting the 15 regulator valve assembly 24 between a closed position in which 0-ring 90 is seated on valve seat 74 and an open position in which 0-ring 9o is spaced from seat 74. The fuel vapor flow rate is adjustable over a range of about ten - twenty cubic centimeters per minute.
In operation, a tank 54 of liquified propane fuel (at a pressure of about 100 psi at room temperature) is attached to tubular inlet 50. The liquified propane fuel fills inlet fuel passage 51, flows through restricted passage 56 and is vaporized in upstream check valve 25 chamber 66. When the fuel is in vaporized form in downstream check valve chamber 68, the check valve is open in response to a pressure differential in the range of 35-80 kilopascals across diaphragm 18. Should liquified fuel begin to flow through check valve passage 30 70 into chamber 68, the pressure in ch~rhpr 68 will immediately reduce the pressure differential across diaphragm 18 and cause check valve 20 to close instantly.
Valve 20 will remain closed until the fuel in chamber 68 is fully vaporized and the pressure in downstream chamber CA 0220~008 1997-0~-09 WO96/15405 PCT~S95/14706 68 is sufficiently reduced so that the bias force of ~iArhragm 18 is overcome.
Regulator valve 26 is normally biased to an open position by diaphragm 22 and is manually closed by action J
5 of coupling lever 124 against flange 115 of orifice holder 116 to move valve member 26 axially and seat O-ring 90 on valve seat 74 to close valve 26. On release of control lever 124, diaphragm 22 moves coupling assembly 24 to open the regulator valve 26.
The pressure in valve chamber 78 (which establishes the pressure which will close valve 26 and thus the flow rate through orifice 120) is adjusted by rotating coupling member 104 through engagement of crenelated head portion 112 with an adjustment tool 15 inserted through an aperture 35 in tubular extension 30.
Rotation of coupling member 104 (which carries valve member 26) shifts the valve subassembly 26 relative to support ring 92 and diaphragm 22 to adjust the spacing of O-ring so from valve seat 74 when the diaphragm 22 is in 20 neutral (valve open) position, thus providing adjustment of the flow rate (over a range of about ten - twenty cubic centimeters per minute) through orifice 120. Slot 129 in head portion 86 of valve member 26 allows firm seating of member 26 in coupling member 104 during system 25 assembly.
Fuel vapor flows from the regulating valve chamber 78, and through the passage defined by shank side wall flat 88 and end slot 130 into the central passage of orifice holder 116 for flow through metering orifice 120.
30 That fuel flow entrains air introduced through ports 36 S for flow through Venturi 40 and the fuel/air mixture flows through mullite tube 46 to gas mantle 48 for ignition. Should the fuel pressure in chamber 78 increase sufficiently to flex ~;Aphragm 22, valve 26 will 35 close and remain closed until the continuing fuel flow CA 0220~008 l997-0~-09 through flat 88, slot 130 and orifice 120 r~Allç~s that pressure in chamber 78 such that the valve 26 will reo~en and allow fuel flow through valve passage 76 to resume.
Should liquid propane pass through check valve 5 pA~~e 70 into downstream check valve chamber 68, the pressure in chamber 68 immediately rises and slams check valve 20 closed. Valve 20 remains closed until the li~uid fuel in check valve chamber 68 is vaporized and then reopens automatically to allow continued fuel flow 10 through the check valve to mantle 48.
While a particular embodiment of the invention has been shown and described, various modifications will be apparent to those skilled in the art, and therefore it is not int~n~ that the invention be limited to the 15 disclosed embodiment, or to details thereof, and departures may be made therefrom within the spirit and scope of the invention.
What is claimed is:

Claims (16)

1. A control system for use with a source of pressurized fuel comprising housing structure defining inlet structure for receiving fuel from a source of pressurized fuel, outlet structure, check valve chamber structure, regulator valve chamber structure disposed between said inlet and outlet structures, first passage structure connecting said check valve chamber and said regulator valve chamber, first valve structure disposed in said check valve chamber for preventing liquid fuel from reaching said outlet structure, second valve structure disposed in said regulator valve chamber, said second valve structure including regulator diaphragm structure dividing said regulator valve chamber into a downstream chamber open to atmospheric pressure and an upstream chamber on the opposite side of said diaphragm structure from said downstream chamber and in communication with said check valve chamber through said first passage structure, second passage structure connecting said upstream chamber and said outlet structure, regulator valve structure coupled to said regulator diaphragm structure for axial movement between a first position in which said first passage structure is open to permit flow of vaporized fuel from said check valve chamber through said first passage structure to said outlet structure and a second position in which said first passage structure is closed, characterized by the provision of adjustment structure for shifting said regulator valve structure relative to said regulator diaphragm structure for changing the pressure on said regulator diaphragm structure that will cause said regulator valve structure to move between said first and second positions.
2. The system of claim 1 characterized in that said first valve structure includes a check valve diaphragm disposed in said check valve chamber that divides said check valve chamber into upstream and downstream chambers, check valve structure carried by said check valve diaphragm, and valve eat structure disposed in said upstream check valve chamber, said check valve structure being adapted to close when the pressure differential between said upstream check valve chamber and said downstream check valve chamber is less than a predetermined value so that fuel does not flow from said upstream check valve chamber to said downstream check valve chamber.
3. The system of claim 2 characterized in that each of said diaphragm members is of metallic material.
4. A control system for use with a source of pressurized fuel comprising housing structure defining inlet structure for receiving fuel from a source of pressurized fuel, outlet structure, check valve chamber structure, regulator valve chamber structure between said inlet and outlet structures, first valve structure disposed in said check valve chamber for preventing liquid fuel from reaching said outlet structure, said first valve structure including check valve diaphragm structure disposed in said check valve chamber that divides said check valve chamber into upstream and downstream chambers, check valve structure carried by said check valve diaphragm structure, and valve seat structure disposed in said upstream check valve chamber, said check valve structure being adapted to close when the pressure differential between said upstream check valve chamber and said downstream check valve chamber is less than a predetermined value so that fuel does not flow from said upstream check valve chamber to said downstream check valve chamber, second valve structure disposed in said regulator valve chamber, said second valve structure including regulator valve diaphragm structure disposed generally parallel to said check valve diaphragm structure and dividing said regulator valve chamber into a downstream regulator valve chamber open to atmospheric pressure and an upstream regulator valve chamber on the opposite side of said regulator valve diaphragm structure from said downstream regulator valve chamber and in communication with said downstream check valve chamber through first passage structure, second passage structure connecting said regulator valve upstream chamber and said outlet structure, and regulator valve structure coupled to said regulator valve diaphragm structure for axial movement between a first position in which said first passage structure is open to permit flow of vaporized fuel from said check valve chamber through said first passage structure to said outlet structure and a second position in which said first passage structure is closed, characterized in that each of said diaphragm members is of metallic material.
5. The system of claim 4 further characterized by the provision of adjustment structure for shifting said regulator valve structure relative to said regulator valve diaphragm structure for changing the pressure on said regulator valve diaphragm structure that will cause said regulator valve structure to move between said first and second positions.
6. The system of any one of claims 2-5 further characterized in that said housing structure includes a base member that defines said inlet structure, a cap member that defines said outlet structure, and intermediate structure connected between said base and cap, said check valve diaphragm member is disposed between said base member and said intermediate structure, and said regulator diaphragm structure is supported by said intermediate structure in generally parallel relation to said check valve diaphragm.
7. The system of any one of claims 2-6 further characterized in that each of said upstream and downstream check valve chambers has a depth that is less than one tenth the width of said check valve chamber.
8. The system of any one of claims 2-7 further characterized in that each of said upstream and downstream check valve chambers has a depth of less than one millimeter.
9. The system of any one of claims 2-8 further characterized in that said check valve pressure differential that causes said check valve structure to close is in the range of thirty to eighty kilopascals.
10. The system of any one of claims 1-3 and 5-9 further characterized in that said adjustment structure includes coupling structure, said regulator valve structure being carried by said coupling structure such that movement of said coupling structure relative to said regulator valve diaphragm structure axially shifts the position of said regulator valve structure relative to said regulator valve diaphragm structure.
11. The system of claim 10 further characterized in that said coupling structure includes an actuating portion for moving said regulator valve structure to said second position.
12. The system of any preceding claim further characterized by the provision of Venturi structure in said outlet structure for delivering an air fuel mixture.
13. The system of any preceding claim further characterized by the provision of metal oxide fabric mantle structure mounted on said outlet structure.
14. The system of any preceding claim further characterized by the provision of restricted flow structure connecting said inlet structure and said check valve chamber.
15. The system of claim 14 further characterized in that said restricted flow structure is a passage of about 0.3 millimeter diameter and a length of about 2 millimeters.
16. The system of any preceding claim furhter characterized by the provision of manually operable control structure for moving said regulator valve structure between said first and second positions.
CA002205008A 1994-11-10 1995-11-08 Fuel control Abandoned CA2205008A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/338,000 1994-11-10
US08/338,000 US5522722A (en) 1994-11-10 1994-11-10 Fuel control

Publications (1)

Publication Number Publication Date
CA2205008A1 true CA2205008A1 (en) 1996-05-23

Family

ID=23322970

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002205008A Abandoned CA2205008A1 (en) 1994-11-10 1995-11-08 Fuel control

Country Status (4)

Country Link
US (1) US5522722A (en)
EP (1) EP0792432A4 (en)
CA (1) CA2205008A1 (en)
WO (1) WO1996015405A1 (en)

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WO1996015405A1 (en) 1996-05-23
EP0792432A1 (en) 1997-09-03
US5522722A (en) 1996-06-04
EP0792432A4 (en) 1998-11-11

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