GB1582585A - Vapour recovery in a liquid dispensing unit - Google Patents

Vapour recovery in a liquid dispensing unit Download PDF

Info

Publication number
GB1582585A
GB1582585A GB3120578A GB3120578A GB1582585A GB 1582585 A GB1582585 A GB 1582585A GB 3120578 A GB3120578 A GB 3120578A GB 3120578 A GB3120578 A GB 3120578A GB 1582585 A GB1582585 A GB 1582585A
Authority
GB
United Kingdom
Prior art keywords
vapor
diaphragm
conduit
valve
liquid
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.)
Expired
Application number
GB3120578A
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.)
Individual
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
Priority to GB3120578A priority Critical patent/GB1582585A/en
Publication of GB1582585A publication Critical patent/GB1582585A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B67OPENING, CLOSING OR CLEANING BOTTLES, JARS OR SIMILAR CONTAINERS; LIQUID HANDLING
    • B67DDISPENSING, DELIVERING OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR
    • B67D7/00Apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or into portable containers, e.g. for retail sale purposes
    • B67D7/04Apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or into portable containers, e.g. for retail sale purposes for transferring fuels, lubricants or mixed fuels and lubricants
    • B67D7/0476Vapour recovery systems
    • B67D7/0478Vapour recovery systems constructional features or components
    • B67D7/048Vapour flow control means, e.g. valves, pumps
    • B67D7/0482Vapour flow control means, e.g. valves, pumps using pumps driven at different flow rates
    • B67D7/0484Liquid jet pumps, e.g. venturis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B67OPENING, CLOSING OR CLEANING BOTTLES, JARS OR SIMILAR CONTAINERS; LIQUID HANDLING
    • B67DDISPENSING, DELIVERING OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR
    • B67D7/00Apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or into portable containers, e.g. for retail sale purposes
    • B67D7/06Details or accessories
    • B67D7/42Filling nozzles
    • B67D7/54Filling nozzles with means for preventing escape of liquid or vapour or for recovering escaped liquid or vapour

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)

Description

(54) VAPOR RECOVERY IN A LIQUID DISPENSING UNIT (71) I, JAMES WILLIAM HEALY, a Citizen of the United States of America, of 54 Plymouth Road, Wakefield, Massachusetts, United States of America, do hereby declare the invention for which I pray that a patent may be granted to me, and the method by which it is to be performed, to be particularly described in and by the following statement: This invention relates to vapor recovery systems for preventing the escape of vapors to the atmosphere during the refilling of a volatile liquid container from a dispensing apparatus. In particular, this invention deals with a vapor recovering system for preventing the escape of hydrocarbon vapors from a vehicle's fuel tank during refueling from a service station's fuel dispensing unit.
A number of systems have been proposed for dealing with the vapors displaced from a volatile liquid container while it is being refilled, such as the hydrocarbon vapors displaced from a vehicle's fuel tank during a refueling operation.
Previous vapor recovery systems for recovering hydrocarbon vapors from a vehicle's fuel tank have included passages in the dispensing nozzle for collecting vapors from the fuel tank, as well as a vapor return line for delivery of the collected vapors to the reservoir. Each of these prior systems, however, has suffered from one or more of various drawbacks.
Some of these systems have relied solely upon vapor pressure within the fuel tank to push the vapor through the vapor return line.
Such systems required a large and cumbersome vapor return line to minimize resistance to vapor flow. Additionally, when that return line became blocked by liquid (e.g., from fuel splashback or condensation), the vapor pressure developed in the vehicle fuel tank was usually insufficient to overcome the blockage.
The result was vapor leakage to the atmosphere at the nozzle-fuel tank interface.
Other systems used for fuel dispensing have employed a vacuum-assist for drawing vapor through a vapor return line. To avoid the expense of a separate vacuum pump at each dispensing station, such systems have typically resorted to a powerful, continuouslyoperating blow-type vacuum pump and a complicated arrangement of electrically actuated valves for connecting the various vapor return lines to the vacuum pump when the various pumps were actuated for dispensing.
Acceptance of these systems has been minimal because of the expense and difficulty of both installation and maintenance. Additionally such systems typically draw such a large volume of ambient air, relative to the volume of fuel vapor, that there is a danger of an explosive mixture being formed.
It has also been suggested that each dispensing unit include a vacuum pump driven by the dispensing unit's conventional meter and connected to a vapor return line. However, the well-known fragility of such meters renders suspect the practicality of this suggestion.
Finally, some systems utilize a venturi injector as a vacuum source. Such injectors make inefficient use of the liquid power source.
The present invention is divided from my copending Application No. 41484/77 (Serial No. 1582584) in which there is claimed a system for dispensing volatile liquids, such as liquid fuels, from a reservoir, the system comprising a hose having a vapor recovery dispensing nozzle at its outlet end, means for pumping the liquid under pressure through the hose for discharge through the nozzle into the inlet of a container such as a fuel tank, a liquid jet gas pump having its liquid inlet in communication with the pump for receipt of a portion of the liquid dispensed by said pump in use of the system; and a vapor conduit having one end in said nozzle and adapted to be placed in communication with the interior of the container when said nozzle is inserted into said container inlet and the other end in communication with the vapor inlet of the jet pump, the outlet of said jet pump discharging into said reservoir whereby vapor displaced from the container as it is filled in use of the system will be drawn off through said conduit by suction created by the passage of the liquid through the jet pump.
According to the present invention there is provided a liquid dispensing nozzle apparatus comprising a body having a liquid conduit leading to a spout insertable into a volatile liquid container in use of the nozzle; a manually operable dispensing valve in the liquid conduit; a vapor conduit for transporting vapor displaced from said container to a remote vapor handling system in use of the nozzle; a vapor shut-off valve in the vapor conduit, said vapor shut-off valve comprising a first diaphragm having a first surface facing the vapor conduit and a second surface facing a chamber within the nozzle, said first diaphragm causing the vapor conduit to be blocked when the diaphragm is in a first position and not to be blocked when the diaphragm is in a second position, and biasing means urging said first diaphragm to said first position; valve opening means for urging the first diaphragm toward the second position only when liquid is flow ing past the dispensing valve; and a vapor regulator valve in said vapor conduit operable in response to a predetermined vapor pressure condition in the container, said vapor pressure regulator valve comprising a second diaphragm mounted in the nozzle with a first surface facing the first said diaphragm and a second surface facing the vapor conduit, said second diaphragm blocking said vapor conduit in a first position and not blocking said vapor conduit in a second position, and biasing means urging said second diaphragm to said second position.
In another aspect, the invention provides a valve apparatus for use in a liquid dispensing nozzle comprising a body including a liquid conduit and a dispensing valve and a vapor conduit, the valve apparatus comprising a rigid body member for abutting engagement with the nozzle body and having internal vapor passage means defining a portion of the vapor conduit, the body member also defining a peripheral surface around a portion of the passage means; a hollow cap member overlying said body member, a first flexible diaphragm clamped around its periphery between said cap and body members, said hollow cap member defining a chamber adjacent a first surface of said first diaphragm and said vapor passage means of said body member being adjacent the second surface of said first diaphragm, said first diaphragm being movable between a first position in which it causes blockage of the vapor passage means at said peripheral surface and a second position; biasing means urging said diaphragm toward the first position: valve opening means for urging the first diaphragm toward the second position only when liquid is flowing past the dispensing valve; and a vapor regulator valve in said vapor passage means operable in response to a predetermined vapor pressure condition in the container, said vapor pressure regulator valve comprising a second diaphragm mounted between the first diaphragm and the peripheral surface, said second diaphragm engaging said peripheral surface in a first position and being spaced apart therefrom in a second position, biasing means urging the second diaphragm to said second position.
Other advantages and features of the invention will be apparent from the following description and accompanying drawings of a preferred embodiment thereof.
In the drawings: Figure 1 is a schematic illustration of a fuel dispensing system, such as may be used at a filling station, incorporating features of the present invention Figure 2 is a sectional view of a liquid jet gas pump as used in the fuel dispensing system; Figure 3 is a partially sectioned side elevation of a vapor recovery dispensing nozzle as used in the dispensing system and embodying features of the present invention; and Figure 4 is a sectional view taken along line 4-4 of Figure 3.
Turning now to the drawings, there is shown in Figure 1 a generally conventional gasoline dispensing system having an underground reservoir 10 containing a supply of gasoline 12 and a dispensing station comprising a pump housing 14 and a flexible fuel hose 16 extending between housing 14 and a vapor recovery dispensing nozzle 18. A conduit 20 supplies gasoline 12 from reservoir 10 to a fuel pump 22 disposed within housing 14. The fuel pump output is delivered, via conduit 24, to a conventional meter or computer 26 for measuring the amount of gasoline dispensed. Another conduit 28 delivers gasoline from meter 26 to a fitting 30 connected to flexible fuel hose 16.
A portion of the liquid fuel delivered by fuel pump 22 is fed by a conduit 32 to liquid jet gas pump 34, the output of which is returned, by pipe 37, to reservoir 10. The suction side of liquid jet gas pump 34 communicates via conduit 38 and fitting 40 to a suction line in the form of a flexible vapor hose 42 disposed within the fuel hose 16. The hose 42 is connected to a vapor recovery dispensing nozzle 18 to receive vapors collected from a vehicle fuel tank being refueled through the nozzle.
For use in a conventional one inch (2.54 cm.) diameter fuel hose 16, hose 42 has a 5/, 6 inch (0.79 cm.) inner diameter and inch (1.27 cm.) outer diameter. Hose 42 is formed from a material which will not be degraded by continuous immersion in gasoline over a wide range of temperature. Additionally, it must be sufficiently strong to withstand 20 to 30 psig (1406 to 2109 grams per sq. cm.) external pressure, which is typically developed within conventional hose 16, while conveying vapors internally at vacuum levels of approximately 16 to 20 inches of water. One suitable material which achieves all the above requirements for the hose 42 is polyurethane tubing having dimensions as stated above.
Vapor hose 42, with the characteristics described above, will transmit one and one-half standard cubic feet of vapor per minute a distance of sixteen feet at a velocity of approximately 2800 feet (853 meters) per minute with a pressure differential of approximately 16 to 20 inches (40.64 to 50.80 cm.) of water. This volume of vapor is substantially equivalent to the volume of gasoline delivered to the vehicle fuel tank at a rate of about 11 U.S. gallons (41.6 liters) per minute. Thus, a suction line as described, along with a liquid jet gas pump 34 capable of developing a vacuum of 16 to 20 inches of water, can handle the vapor displaced in the vehicle fuel tank by the liquid gasoline entering at rates up to 11 gallons per minute.
Further, the vapor velocities developed within vapor hose 42 (e.g., in the range of 1500 to 2800 feet per minute) are sufficient to break up and remove any liquid blocking the vapor hose, thus eliminating that problem.
Conventional gasoline pumps 22 have a pressure setting of approximately 20 psig and an internal liquid bypass system to accommodate variations in fueling rates from the extremes of no flow up to about 11 U.S.
gallons per minute when the conventional fuel control valve within dispensing nozzle 18 is at a full open position. The conduit sizes and fluid resistance in the liquid channel defined by conduits 32 and 37 and jet pump 34 are chosen such that approximately 11/2 to 2 U.S. gallons (5.7 to 7.6 liters) per minute of gasoline are consumed from the pump discharge. The jet pump is designed to generate the desired pressure differential of 16 to 20 inches of water using a liquid flow rate in the range of approximately 2 gallons per minute of liquid when pumping 11/2 cubic feet (0.042 cubic meters) per minute of a saturated air and hydrocarbon vapor mixture.
Referring to Figure 2, the vertically mounted liquid jet gas pump, indicated generally at 34, includes a housing 50 which comprises cover 51, upper body portion 52, and lower body portion 53 - all secured by bolts 54. 0ring 56 provides a seal between the upper and lower body portions.
The housing has an interior passage 60 which communicates at its upper end with conduit 32 through liquid inlet 61, and at its lower end with surge chamber 64 through jet orifice 66 in pilot valve seat 62. Pilot valve seat 62 is sealingly positioned in passage 60 by o-rings 65.
Jet orifice 66 is coaxial with mixing tube 36 along central axis c and communicates therewith through surge chamber 64 adjacent the lower end of housing 50.
Surge chamber 64 communicates at its upper end with vapor conduit 38 through vapor inlet 72.
A vapor pressure regulator diaphragm 74 is clamped around its periphery between cover 51 and upper body portion 52 to define on its opposite sides, together with cover 51 and upper body portion 52, upper and lower chambers 76 and 78 respectively. Lower chamber 78 communicates with surge chamber 64 through bore 80. Upper chamber 76 is vented to the atmosphere through vent 81.
Needle rod 82 is connected at its upper end to disc 84 which is biased upwardly against diaphragm 74 by spring 86. The lower end of needle rod 82 passes through a central bore 83 in pilot valve 88, u-cup 98 providing a seal therebetween. The lower end of needle rod 82 is positioned above jet orifice 66 -- the needle rod 82, jet orifice 66, and mixing tube 36 being coaxially aligned along central axis c.
Pilot valve 88 is positioned within passage 60 and is biased downwardly against valve seat 62 by spring 90, o-ring 92 providing a seal therebetween. U-cup 94 positioned adjacent the upper end of valve 88 provides a seal between the valve, lower chamber 78, and passage 60.
Referring to Figure 3, the dispensing nozzle includes a body 110, a spout assembly 112, and a spout shroud 114. Body 110 comprises casting 116 having a liquid conduit 118 extending from fuel hose 16 to the spout. A conventional biased-closed fuel valve 122 is operated by a conventional manual fuel valve operator 124.
The spout assembly 112 includes spout 136, and a fitting 140 which secures the spout to the body casting 116. The shroud 114 includes a flexible bellows 142 surrounding the upper portion of the spout, an attachment portion 144 secured to the fitting 140, and an end plate 146 which includes an opening 148 communicating with the space between the bellows and the spout. End plate 146, which seals against the mouth of fuel tank fill pipe 150 when the spout is inserted into the fill pipe, also includes a disc magnet 152 (preferably a ceramic-rare earth magnet having eight poles per face). The nozzle can be held in place in the fill pipe by a ring 154 which catches under the lip of the fill pipe mouth.
(Alternatively, a conventional spring wrapped around the lower spout segment could be used.) A series of relatively inextensible filaments 1 55 can be provided extending between the end plate and the attachment portion. When under tension, the filaments would serve to support part of the nozzle's weight by the magnetic attraction to the fill pipe. Naturally, a variety of other structures could perform the same function.
The shroud 114 also includes a resilient receptacle 156 which is integral with a shroud portion 158 adjacent the attachment portion 144 and which has an opening 160 for receiving a tube 162 in a leak-proof friction fit. In the preferred embodiment illustrated, the shroud 114 is molded as an integral unit from a resilient flexible material that is substantially unaffected by hydrocarbon liquid or vapors.
One suitable material is urethane rubber. The shroud portions 144 and 158, as well as the receptacle 156 and the end plate 146, preferably have a greater wall thickness than the bellows portion 142. The thicker portions, of course, have functions which require somewhat greater rigidity, and somewhat less flexibility, than the bellows. It is also preferred that the magnet 1 52 be completely encased in the material of which the shroud is formed in order to protect the magnet from damage and to eliminate the possibility of sparks which could develop if the magnet were to directly strike the fuel tank fill pipe 150. A shroud formed in this fashion is easily installed on existing conventional fuel dispensing nozzles.
The space between the shroud 114 and the spout 1 36 forms a channel for receiving vapors displaced from the fuel tank. Such vapors enter that space through the opening 148 and exit through a tube 162 which extends from the receptacle 1 56 through an opening in a cap assembly 164 of the nozzle to convey the vapors to a chamber 166 in the cap assembly.
The chamber 166, in turn, communicates with a passageway 168, also provided in the cap assembly. The passageway 168 leads to vapor hose 42. Preferably, tube 162, passageway 168, and vapor hose 42 have the same inner diameter (e.g., 5116 inch) in order to provide a relatively uniform vapor flow conduit.
The cap assembly 164 comprises a stacked arrangement of parts which can be secured to the conventional nozzle body 116 by a series of screws (not shown) passing through all parts of the stack. The main structural elements of the cap assembly 164 are a body 172, spacer 174, and cap 176. The body 172 includes an opening 1 78 which receives the tube 162 and which communicates with the chamber 166 provided in the body 172. The passageway 168 in the body 172 terminates in an upwardly facing annular surface 180 which, as described below, forms a valve seat.
A vapor pressure regulator diaphragm 182 and a vapor shut-off diaphragm 184 are clamped around their peripheries between, respectively, the body 172 and spacer 174 and the spacer 174 and cap 176. In the rest configuration illustrated, the diaphragms 182, 184 are substantially parallel and are separated by a spacer disc 186, preferably formed from a closed cell foam rubber and having a thickness substantially equal to the thickness of spacer 174. A small opening 188 in the spacer 1 74 maintains the volume between the diaphragms 182 and 184 at atmospheric pressure.The cap 176 defines a chamber 190 above the shut-off diaphragm 1 84. A shut-off diaphragm biasing spring 192 is disposed in that chamber and biases the diaphragm 184 toward the diaphragm 182 and the valve scat 180. The regulator diaphragm 182 is biased upwardly by a spring 194 disposed around the valve seat 180 in the chamber 166. The biasing forces of springs 192 and 194 are chosen such that the force of spring 192 can overcome the force of spring 194. Aligned openings 196 and 198 in the spacer 174 and the cap 176 connect the chamber 190 with the conduit 138.
Referring to Figure 4, the shroud portion 158 is provided with a pair of integral pressure relief valves 200, 202. Each valve comprises a pair of adjacent flexible flaps 204, each integral with a biasing panel 206 that is, in turn, integral with the wall 158 at an opening 208 therein.
As will be evident to those skilled in the art, valve 200 will permit air to enter the shroud to relieve an excessive vacuum and valve 202 will permit vapor to escape from the shroud to relieve excessive pressure. With tight seal of end plate 146 to the fill pipe 150, the valves serve as an additional protection against pressure extremes which could damage the vehicle fuel tank.
In operation vapor recovery dispensing nozzle 18 is placed in the fuel tank of the vehicle to be refueled and fuel pump 22 is activated. A portion of the gasoline output of fuel pump 22 is delivered by conduit 32 to interior passage 60 of liquid jet gas pump 34. Pilot valve 88 is initially biased downwardly by spring 90 against seat 62, o-ring 92 and u-cup 94 providing seals which prevent further flow of the gasoline and, therefore, cause the pressure of the gasoline within passage 60 to rise. Due to the differential sealing areas of u-cup 94 and o-ring 92 (u-cup 94 providing a larger sealing area), the gasoline pressure produces a net upward force on valve 88 acting against spring 90. Spring 90 is sized to prevent upward movement of the pilot valve until the pressure within passage 60 exceeds 12 psig (844 grams per sq. cm.).At this threshold level, the pilot valve moves slightly upwardly, lifting o-ring 92 from seat 62 to break that seal, causing the pilot valve to pop upwardly to an open position due to the upward force provided by the gasoline pressure acting against the remaining net sealing area provided by u-cup 94 (the sealing area provided by u-cup 94 minus the sealing area provided by u-cup 98). Once the pilot valve pops open, it will remain open until the pressure within passage 60 falls below approximately 5 psig (352 grams per sq. cm.), at which point the pressure acting against the net sealing area provided by u-cup 94 will be overcome by the downward force of spring 90 and the pilot valve will close. This operation of the pilot valve makes my jet pump system compatible with fuel dispensing systems which have detection equipment which monitor the system for leaks during an initial pressure buildup.
When pilot valve 88 opens, the gasoline within passage 60 flows through jet orifice 66, drawing vapor from conduit 38, through surge chamber 64, out mixing tube 36, and through pipe 37 into reservoir 10.
The vacuum produced by the liquid jet gas pump is regulated to a predetermined maximum. Upper chamber 76 is maintained at atmospheric pressure by vent 81. Lower chamber 78 communicates with surge chamber 64 through bore 80. As the vacuum level in surge chamber 64 and, therefore, lower chamber 78, increases, vapor pressure regulator diaphragm 74 will produce a downward force acting against spring 86. Spring 86 is sized to support a vacuum level of 16 to 20 inches of water. Any increase of the vacuum above this threshold level will draw the diaphragm 7 downwardly against disc 84, moving needle rod 82 toward jet orifice 66, increasingly blocking the flow of gasoline through the jet orifice and hence decreasing the rate of withdrawal of vapor from and, therefore, the vacuum within surge chamber 64 and vapor conduit 38 until the predetermined maximum vacuum level is obtained.
For normal refueling rates (5 to 10 U.S.
gallons - 18.9 to 37.8 liters - per mintue), the vapor velocity in vapor hose 42 is sufficient (e.g., greater than 1500 feet per minute) to entrain any liquid therein and carry it out of the conduit. At lower refueling rates, the vapor will still percolate through any liquid in the vapor hose.
When the vapor flow from vapor control nozzle 18 and then fuel supply from fuel pump 22 are suddenly shut off, liquid remaining in mixing tube 36 will be drawn up into surge chamber 64 by the residual vacuum therein.
The volume of surge chamber 64 is large enough to hold the liquid remaining in the mixing tube - allowing it to drain out once the pressure has stabilized. This prevents liquid from surging into vapor conduit 38 during shutdown.
The dual function valving arrangement provided in the cap assembly 164 can best be described by considering the operation of the regulator diaphragm 182 absent the shutoff diaphragm 184, and then considering the constraints imposed by the presence of the shut-off diaphragm 184. The vapor pressure regulator diaphragm is biased away from the valve seat 180 (i.e., in a "valve open" configuration) by the spring 194. In this "normal" orientation of the diaphragm 182, vapor is free to pass through the chamber 166, passageway 168, and vapor hose 42 to the jet pump 34. Excessive vacuum levels beneath the diaphragm 182, however can overcome the biasing force of spring 194 and cause the regulator valve to close (i.e., the diaphragm 182 to engage the valve seat 180).
It is very desirable, however, that the vapor conduit be sealed at all times when fuel is not being dispensed by the nozzle. This is accomplished by the vapor shut-off diaphragm 184. As is illustrated in Figure 3, absent the flow of fuel through the nozzle, the spring 192 overcomes the force of spring 194 and its force is transmitted through diaphragm 184 and spacer disc 186 to force the diaphragm 182 against the valve seat 180. Thus, even if a suction is applied by jet pump 34 to vapor hose 42, air is prevented from being sucked into the vapor return system. When fuel is being dispensed, however, a slight vacuum is created in the chamber 190 above the shut-off diaphragm 184 by the venturi effect as fuel flows past the mouth of conduit 138. The suction is transmitted through conduits 138, 196, and 198 to the chamber 190.Spring 192 is chosen to have the force such that the vacuum level produced in chamber 190 (e.g., about 2 to 3 inches [5.1 to 7.6 cm] of water), when acting upon the exposed surface of diaphragm 184, is sufficient to overcome the force of spring 192, thereby causing a compression of spring 192 and a movement of the diaphragm 184 away from the diaphragm 182. When this occurs, of course, the regulator diaphragm 182 is free to act independently of the shut-off diaphragm 184 and to perform its regulatory function. An interruption in the flow of fuel causes the return of diaphragm 184 and spring 192 to the configuration shown in Figure 3, so that the operation of diaphragm 182 is overridden by the shut-off diaphragm 184.
As will be evident to those skilled in the art, the vapor shut-off valving arrangement shown in Figure 3 can be provided in a system where no vapor pressure regulator valve is required. In the so-called "vapor balance" systems for example, there is no suction applied to the vapor hose 42 and no possibility of damage to the vehicle's fuel tank by excessive vacuum levels. The regulator valve is thus superfluous. It would still be desirable, however, to positively seal the vapor return conduit system when the nozzle is not in use in order to prevent air from entering that system. The vapor shut-off valve arrangement shown in Figure 3 would provide a simple and effective way of achieving this, with the diaphragm 184 engaging the valve seat 180 directly.
The cap assembly 164 which provides the vapor conduit valving arrangements can be provided as a replacement assembly for the conventional caps which enclose the full tank shut-off mechanism in existing fuel dispensing nozzles. Naturally, there may be modification of the cap assembly parts as illustrated in Figure 3 in order to accommodate slightly different structural features of existing nozzles and/or different vapor handling systems (e.g., with a "vapor balance" system the diaphragm 182, spring 194, spacer 174, and spacer disc 186 could be eliminated). Similarly, the shroud 114 can be provided as an "add-on" feature for existing nozzles.
WHAT I CLAIM IS: 1. As liquid dispensing nozzle apparatus comprising a body having a liquid conduit leading to a spout insertable into a volatile liquid container in use of the nozzle; a manually operable dispensing valve in the liquid conduit; a vapor conduit for transporting vapor displaced from said container to a remote vapor handling system in use of the nozzle; a vapor shut-off valve in the vapor conduit, said vapor shut-off valve comprising a first diaphragm having a first surface facing the vapor conduit and a second surface facing a chamber within
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (23)

**WARNING** start of CLMS field may overlap end of DESC **. acting against spring 86. Spring 86 is sized to support a vacuum level of 16 to 20 inches of water. Any increase of the vacuum above this threshold level will draw the diaphragm 7 downwardly against disc 84, moving needle rod 82 toward jet orifice 66, increasingly blocking the flow of gasoline through the jet orifice and hence decreasing the rate of withdrawal of vapor from and, therefore, the vacuum within surge chamber 64 and vapor conduit 38 until the predetermined maximum vacuum level is obtained. For normal refueling rates (5 to 10 U.S. gallons - 18.9 to 37.8 liters - per mintue), the vapor velocity in vapor hose 42 is sufficient (e.g., greater than 1500 feet per minute) to entrain any liquid therein and carry it out of the conduit. At lower refueling rates, the vapor will still percolate through any liquid in the vapor hose. When the vapor flow from vapor control nozzle 18 and then fuel supply from fuel pump 22 are suddenly shut off, liquid remaining in mixing tube 36 will be drawn up into surge chamber 64 by the residual vacuum therein. The volume of surge chamber 64 is large enough to hold the liquid remaining in the mixing tube - allowing it to drain out once the pressure has stabilized. This prevents liquid from surging into vapor conduit 38 during shutdown. The dual function valving arrangement provided in the cap assembly 164 can best be described by considering the operation of the regulator diaphragm 182 absent the shutoff diaphragm 184, and then considering the constraints imposed by the presence of the shut-off diaphragm 184. The vapor pressure regulator diaphragm is biased away from the valve seat 180 (i.e., in a "valve open" configuration) by the spring 194. In this "normal" orientation of the diaphragm 182, vapor is free to pass through the chamber 166, passageway 168, and vapor hose 42 to the jet pump 34. Excessive vacuum levels beneath the diaphragm 182, however can overcome the biasing force of spring 194 and cause the regulator valve to close (i.e., the diaphragm 182 to engage the valve seat 180). It is very desirable, however, that the vapor conduit be sealed at all times when fuel is not being dispensed by the nozzle. This is accomplished by the vapor shut-off diaphragm 184. As is illustrated in Figure 3, absent the flow of fuel through the nozzle, the spring 192 overcomes the force of spring 194 and its force is transmitted through diaphragm 184 and spacer disc 186 to force the diaphragm 182 against the valve seat 180. Thus, even if a suction is applied by jet pump 34 to vapor hose 42, air is prevented from being sucked into the vapor return system. When fuel is being dispensed, however, a slight vacuum is created in the chamber 190 above the shut-off diaphragm 184 by the venturi effect as fuel flows past the mouth of conduit 138. The suction is transmitted through conduits 138, 196, and 198 to the chamber 190.Spring 192 is chosen to have the force such that the vacuum level produced in chamber 190 (e.g., about 2 to 3 inches [5.1 to 7.6 cm] of water), when acting upon the exposed surface of diaphragm 184, is sufficient to overcome the force of spring 192, thereby causing a compression of spring 192 and a movement of the diaphragm 184 away from the diaphragm 182. When this occurs, of course, the regulator diaphragm 182 is free to act independently of the shut-off diaphragm 184 and to perform its regulatory function. An interruption in the flow of fuel causes the return of diaphragm 184 and spring 192 to the configuration shown in Figure 3, so that the operation of diaphragm 182 is overridden by the shut-off diaphragm 184. As will be evident to those skilled in the art, the vapor shut-off valving arrangement shown in Figure 3 can be provided in a system where no vapor pressure regulator valve is required. In the so-called "vapor balance" systems for example, there is no suction applied to the vapor hose 42 and no possibility of damage to the vehicle's fuel tank by excessive vacuum levels. The regulator valve is thus superfluous. It would still be desirable, however, to positively seal the vapor return conduit system when the nozzle is not in use in order to prevent air from entering that system. The vapor shut-off valve arrangement shown in Figure 3 would provide a simple and effective way of achieving this, with the diaphragm 184 engaging the valve seat 180 directly. The cap assembly 164 which provides the vapor conduit valving arrangements can be provided as a replacement assembly for the conventional caps which enclose the full tank shut-off mechanism in existing fuel dispensing nozzles. Naturally, there may be modification of the cap assembly parts as illustrated in Figure 3 in order to accommodate slightly different structural features of existing nozzles and/or different vapor handling systems (e.g., with a "vapor balance" system the diaphragm 182, spring 194, spacer 174, and spacer disc 186 could be eliminated). Similarly, the shroud 114 can be provided as an "add-on" feature for existing nozzles. WHAT I CLAIM IS:
1. As liquid dispensing nozzle apparatus comprising a body having a liquid conduit leading to a spout insertable into a volatile liquid container in use of the nozzle; a manually operable dispensing valve in the liquid conduit; a vapor conduit for transporting vapor displaced from said container to a remote vapor handling system in use of the nozzle; a vapor shut-off valve in the vapor conduit, said vapor shut-off valve comprising a first diaphragm having a first surface facing the vapor conduit and a second surface facing a chamber within
the nozzle, said first diaphragm causing the vapor conduit to be blocked when the diaphragm is in a first position and not to be blocked when the diaphragm is in a second position, and biasing means urging said first diaphragm to said first position; valve opening means for urging the first diaphragm toward the second position only when liquid is flowing past the dispensing valve; and a vapor regulator valve in said vapor conduit operable in response to a predetermined vapor pressure condition in the container, said vapor pressure regulator valve comprising a second diaphragm mounted in the nozzle with a first surface facing the first said diaphragm and a second surface facing the vapor conduit, said second diaphragm blocking said vapor conduit in a first position and not blocking said vapor conduit in a second position, and biasing means urging said second diaphragm to said second position.
2. Apparatus according to Claim 1, wherein said nozzle further includes a vent linking the region between said diaphragms with the ambient exterior of said nozzle.
3. A valve apparatus for use in a liquid dispensing nozzle comprising a body including a liquid conduit and a dispensing valve and a vapor conduit, the valve apparatus comprising a rigid body member for abutting engagement with the nozzle body and having internal vapor passage means defining a portion of the vapor conduit, the body member also defining a peripheral surface around a portion of the passage means; a hollow cap member overlying said body member, a first flexible diaphragm clamped around its periphery between said cap and body members, said hollow cap member defining a chamber adjacent a first surface of said first diaphragm and said vapor passage means of said body member being adjacent the second surface of said first diaphragm, said first diaphragm being movable between a first position in which it causes blockage of the vapor passage means at said peripheral surface and a second position; biasing means urging said diaphragm toward the first position: valve opening means for urging the first diaphragm toward the second position only when liquid is flowing past the dispensing valve; and a vapor regulator valve in said vapor passage means operable in response to a predetermined vapor pressure condition in the container, said vapor pressure regulator valve comprising a second diaphragm mounted between the first diaphragm and the peripheral surface, said second diaphragm engaging said peripheral surface in a first position and being spaced apart therefrom in a second position, biasing means urging the second diaphragm to said second position.
4. Apparatus according to Claim 3, wherein said valve body member further includes a vent linking the region between said diaphragms with the ambient exterior of the nozzle.
5. Apparatus according to Claim 2 or 4, wherein the biasing means for the second diaphragm comprise a spring having a lower biasing force than the biasing force of said biasing means that biases said first diaphragm, thereby enabling said first diaphragm to cause blockage of said passage means in the absence of liquid flow in said liquid conduit but enabling independent operation of said second diaphragm in response to pressure conditions in said container when liquid is flowing in said liquid conduit.
6. Apparatus according to Claim 2,4 or 5, wherein the biasing means for each said diaphragm each comprise a spring.
7. Apparatus according to Claim 2,4,5, or 6, wherein said first and second diaphragms are mounted to be substantially parallel when the first diaphragm is in said first position.
8. Apparatus according to Claim 7, wherein said first and second diaphragms are spaced apart, a spacer dise being provided intermediate said first and second diaphragms.
9. Apparatus according to Claim 8, wherein said spacer dise is formed from a closed-cell foam rubber.
10. Apparatus according to any preceding claim, wherein said biasing means that biases the first diaphragm has a biasing force which can be overcome by a vacuum level in the range of from two to three inches of water in the chamber.
11. Apparatus according to any preceding claim, wherein the valve opening means comprise a conduit extending between said chamber and a portion of said liquid conduit, whereby liquid flow in said liquid conduit produces a reduced pressure in said chamber.
12. Apparatus according to Claim 11 when appendant to Claim 1, wherein the conduit comprising said valve opening means communicates with said liquid conduit substantially at the location of said dispensing valve.
13. Apparatus according to any preceding claim, wherein caid biasing means for the first diaphragm comprise a spring disposed in said chamber.
14. Nozzle apparatus according to Claim 1 or any preceding claim when appendant thereto, wherein a flexible enclosure is provided spaced apart from and encircling said spout at the end thereof adjacent the nozzle body.
15. Apparatus according to Claim 14, wherein the flexible enclosure terminates in an end plate disposed to engage the container mouth when said spout is inserted into the container, said flexible enclosure comprising an attachment portion for securing it to said nozzle, said end plate comprising a magnetic material, thereby enabling positive contact of said end plate with said tank mouth to prevent the escape to the ambient of vapors from said tank, the flexible enclosure further comprising a member secured to said attachment portion and to said end plate and having a length along said spout such that said member is taut when said end plate engages said fuel tank mouth.
16. Apparatus according to Claim 14 or 15, wherein a pressure relief valve is provided in the flexible enclosure for altering the pressure in the vapor conduit when it deviates by more than a predetermined amount from the ambient pressure exterior of the flexible enclosure, said pressure relief valve comprising an opening in a wall of the flexible enclosure, a pair of flexible flaps in face-to-face contact with each other when the pressure within said vapor conduit deviates from said ambient pressure by no more than said predetermined amount, and flap biasing panels urging said flaps together and being sealed around the edges of said opening.
17. Apparatus according to Claim 16, wherein said wall of said flexible enclosure, said flexible flaps, and said flaps biasing panels are formed integrally from a flexible material.
18. Apparatus according to Claim 16 or 17, wherein said flaps are provided interiorly of said vapor conduit, whereby said pressure relief valve is a negative pressure relief valve enabling the relief of excessive vacuum conditions within said vapor conduit.
19. Apparatus according to Claim 16, 17 or 18, wherein said flaps are provided exteriorly of said vapor conduit, whereby said pressure relief valve is a positive pressure relief valve enabling relief of excessive over-pressure conditions within said vapor conduit.
20. Apparatus according to any one of Claims 16 to 19, wherein said flap biasing panels abut along lines of contact with their respective flexible flaps, the panels together forming an acute angle.
21. Apparatus according to Claim 20, wherein said acute angle is approximately 30".
22. A liquid dispensing nozzle constructed and arranged to operate substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings.
23. A valve apparatus for use in a liquid dispensing nozzle constructed and arranged to operate substantially ashereinbefore described with reference to and as illustrated in the accompanying drawings
GB3120578A 1977-10-05 1977-10-05 Vapour recovery in a liquid dispensing unit Expired GB1582585A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3120578A GB1582585A (en) 1977-10-05 1977-10-05 Vapour recovery in a liquid dispensing unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3120578A GB1582585A (en) 1977-10-05 1977-10-05 Vapour recovery in a liquid dispensing unit

Publications (1)

Publication Number Publication Date
GB1582585A true GB1582585A (en) 1981-01-14

Family

ID=10319593

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3120578A Expired GB1582585A (en) 1977-10-05 1977-10-05 Vapour recovery in a liquid dispensing unit

Country Status (1)

Country Link
GB (1) GB1582585A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2671789A1 (en) * 1991-01-21 1992-07-24 Schlumberger Ind Sa DEVICE FOR DISPENSING HYDROCARBONS WITH RECOVERY OF VAPORS.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2671789A1 (en) * 1991-01-21 1992-07-24 Schlumberger Ind Sa DEVICE FOR DISPENSING HYDROCARBONS WITH RECOVERY OF VAPORS.
EP0497015A1 (en) * 1991-01-21 1992-08-05 Schlumberger Industries Device for dispensing hydrocarbons with vapor recovery
US5222532A (en) * 1991-01-21 1993-06-29 Schlumberger Industries Device for dispensing hydrocarbons with vapor recovery

Similar Documents

Publication Publication Date Title
US4095626A (en) Vapor recovery in a liquid dispensing unit
US4056131A (en) Vapor control in a fuel dispensing nozzle
EP0888236B1 (en) Vapor recovery system accommodating orvr vehicles
US5676181A (en) Vapor recovery system accommodating ORVR vehicles
WO1997034805A9 (en) Vapor recovery system accommodating orvr vehicles
US5850857A (en) Automatic pressure correcting vapor collection system
US4260000A (en) Fuel dispensing system with controlled vapor withdrawal
CA1052744A (en) Liquid dispensing and vapor recovery system utilizing an injector and an improved vapor flow control unit
US4157104A (en) Gasoline dispensing and vapor recovery apparatus
US4082122A (en) Closed fuel system with vacuum assist
AU8101994A (en) Automatic shut-off valve
CA1089816A (en) Hydrocarbon fuel dispensing, vapor controlling system
US4100758A (en) Vacuum assist fuel system
US3941168A (en) Liquid dispensing and vapor recovery system utilizing an injector and a vapor flow control valve
EP0659167B1 (en) Apparatus for controlling fuel vapor flow
US20240102567A1 (en) Pressure vacuum valve
US5386859A (en) Fuel dispensing nozzle having transparent boot
US4256151A (en) System for dispensing a volatile fuel
US6805173B2 (en) Vapor space pressure control system for underground gasoline storage tank
US11905159B1 (en) Vapor recovery system for mobile fuelers
US6138707A (en) Fuel storage tanks
US4167957A (en) Hydrocarbon fuel dispensing, vapor controlling system
CA2102569A1 (en) Automatic shut-off valve arrangement
GB1582585A (en) Vapour recovery in a liquid dispensing unit
US5613535A (en) Fuel dispenser shutoff switch

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19931005