The present disclosure relates generally to fuel delivery systems and, more particularly, to inlet control valves for use with fuel delivery systems.
A fuel system of a marine craft typically includes a fuel filler tube coupled to a fuel tank. The filler tube may include a deckfill that is adapted for mounting to a deck of the marine craft such as, for example, a deck of a boat. The deckfill includes an opening for receiving a nozzle such as, for example, a nozzle of a fuel pump, etc. During a fuel filling operation, as the fuel tank is being filled via the deck fill, the fuel vapors in the fuel tank are displaced and vented from the fuel tank via a vent line and/or via the filler tube to the atmosphere. However, such displacement of the fuel vapors from the fuel tank may cause the fuel vapors to carry liquid fuel through the filler tube line and out to the atmosphere or the environment through the deckfill apparatus. As a result, the air and/or fuel vapors carry liquid fuel from the fuel tank to, for example, the deck of the marine craft via the filler tube, thereby causing liquid fuel spillage.
Additionally or alternatively, some deckfill apparatus include means for venting the fuel vapors inside the fuel tank to the atmosphere. However, government agencies (e.g., the Environmental Protection Agency) have enacted regulations to limit the amount of evaporative emissions that can be legally emitted by boats and other marine vehicles during operation and/or non-operation of the marine vehicles. More specifically, government regulations (e.g., title 40 of the Code of Federal Regulations) have been enacted to control diurnal evaporative emissions of marine vehicles. In particular, these regulations limit the amount of evaporative diurnal emissions that a marine vehicle may permissibly emit during a diurnal cycle (e.g., periods of non-operation). Thus, a deckfill apparatus having venting means may allow diurnal emissions via a fuel line of the fuel delivery system. When the pressure in the fuel tank increases during a diurnal cycle, the fuel vapors may fill the fuel line and pass to the atmosphere via the venting means of the deckfill apparatus.
In general, the example fuel delivery systems described herein may be used with marine crafts or vehicles. The example fuel delivery systems described herein include enhanced or improved inlet control valve apparatus having a multi-piece valve body that is snap-fit together after a flow control apparatus is coupled (e.g., pivotally coupled) within a fluid flow passageway of the valve body. The multi-piece valve body is snap-fit (e.g., via an arbor press) to eliminate welding (e.g., sonic welding) that is otherwise required with conventional inlet control valves. A seal (e.g., an O-ring) is disposed between the multi-piece valve body to substantially reduce or prevent leakage between the multi-piece valve body. Further, the example inlet control valve apparatus described herein substantially reduce or prevent fuel spillage via a deckfill opening during an overfilling condition or event.
Additionally or alternatively, the example inlet control valves provide modularity by receiving different types of flow control apparatus based on the type of fuel delivery system being used. For example, a first flow control apparatus may be provided to allow venting of fuel vapors and/or air across the flow control member, while preventing liquid fuel from flowing across flow control apparatus during an overfill condition. Another example flow control apparatus described herein provides a relatively tight seal to substantially reduce or prevent diurnal emissions across the flow control apparatus and redirect the fuel vapors to a venting system of the fuel delivery system.
As used herein, a “fluid” includes, but is not limited to, a liquid such as fuel (e.g., gasoline), a vapor such as fuel vapor (e.g., gasoline vapor), a gas (e.g., air) and/or any combination or mixture thereof.
In this example, the venting system 108 includes a vent valve 126 and a grade valve 128 that are coupled to the fuel tank 104. Tubing 130 fluidly couples the vent valve 126 and the grade valve 128. The vent valve 126 is fluidly coupled to a vent 132 that vents to, for example, the atmosphere. To help reduce venting emissions and/or pollutants to the environment, the venting system 108 may include a vapor collection apparatus 134, which is disposed between the vent 132 and the vent valve 126. An inlet 136 of the vapor collection apparatus 134 is fluidly coupled to the vent valve 126 via tubing 138 and an outlet 140 of the vapor collection apparatus 134 is fluidly coupled to the vent 132 via tubing 142. The vapor collection apparatus 134 comprises a canister 144 having an emission(s)-capturing or filter material (e.g., an adsorbent material) such as, for example, activated carbon, charcoal, etc., that collects and stores evaporative emissions such as, for example, hydrocarbons to reduce pollution to the environment. The emissions captured and stored by the canister 144 are returned or carried to the fuel tank 104 as air is drawn from the atmosphere and flows through the canister 144 between the outlet 140 and the inlet 136 and to the fuel tank 104 via the venting system 108.
The venting system 108 equalizes the pressure in the fuel tank 104 to accommodate volumetric changes (e.g., expansion) in the fuel tank 104. For example, when the pressure of fuel and/or vapors in the fuel tank 104 increases, fuel vapors are released from the fuel tank 104 through the venting system 108. In other words, an increase in pressure in the fuel tank 104 causes fuel vapors containing hydrocarbons in the fuel tank 104 to vent or release to the atmosphere via the vent 132. The vapor collection apparatus 134 then captures the hydrocarbons to prevent or significantly reduce such emissions to the atmosphere.
To fill the fuel tank 104, the fuel cap 124 is removed from the deckfill 122. During a filling operation, as the fuel tank 104 is being filled via the deckfill 122, the level of fuel 105 stored in the fuel tank 104 rises. The fuel vapors in the fuel tank 104 are displaced and vented from the fuel tank 104 via the venting system 108 and/or the filler tube 106 during a filling event. Additionally, such displacement of the fuel vapors from the fuel tank 104 may cause the fuel vapors to carry liquid fuel up through the filler tube 106.
Thus, fuel leakage or overflow may occur via the filler tube 106 during a filling operation. Such overflow can occur during a filling event when using a manually operated nozzle and/or an automatic nozzle when an automated shut-off is not activated. Such overflow typically occurs as the liquid level in the fuel tank 104 approaches an upper, interior surface 146 of the fuel tank 104 (e.g., when the fuel tank 104 is substantially full). As the liquid is filling in the fuel tank 104, the liquid fuel is displacing the air and/or fuel vapors in the fuel tank 104 to the atmosphere and/or environment via the filler tube 106. Further, as the liquid in the fuel tank 104 is filled beyond a recommended ullage, the liquid fuel restricts or prevents venting of the fuel vapors via the venting system 108 (e.g., via the grade valve 128 and/or the vent valve 126). As a result, the air and/or fuel vapors carry liquid fuel from the fuel tank 104 to, for example, the deck of a marine vehicle via the filler tube 106 and thereby causing liquid fuel spillage.
As described in greater detail below, the example inlet control valve 102 significantly reduces or prevents liquid fuel from flowing between the outlet 112 and the inlet 118 during an overflow event when liquid fuel is flowing within the filler tube 106 in a direction toward the opening of the deckfill 122 (e.g., a closed position of the inlet control valve 102). Thus, the inlet control valve 102 prevents liquid fuel from flowing from the fuel tank 104 and spilling onto a surface of a marine vehicle's deck via the deckfill 122. However, when the inlet control valve 102 is in the closed position, the inlet control valve 102 enables fuel vapors and/or air to flow between the outlet 112 and the inlet 118 of the inlet control valve 102 to equalize the pressure in the fuel tank 104 and/or the pressure within the filler tube 106 during an overfilling event if the liquid fuel inside the fuel tank 104 prevents venting via the venting system 108 as described above.
The second body portion 206 includes a flange 306 adjacent the second body portion 206. The flange 306 includes a plurality of apertures or slots 308 corresponding to the plurality of fasteners 304 of the first body portion 204. The second body portion 206 also includes a valve seat 310 having a seating surface 312 adjacent the flange 306 of the second body portion 206. In this example, the valve seat 310 is coaxially aligned with a longitudinal axis 314 of the valve body 202. The second body portion 206 also includes a mounting member 316 to receive or mount a flow control member assembly 318 to the second body portion 206. The flange 306, the valve seat 310 and the mounting member 316 are integrally formed with the second body member 206 as a unitary piece or structure and may be composed of, for example, a plastic material (e.g., a High Density Polyethelyne), a metallic material (e.g., stainless steel) or any other suitable materials. The second body portion 206 may be manufactured via injection molding or any other suitable manufacturing process.
The mounting member 316 protrudes from an inner peripheral edge 320 of the second body portion 206 adjacent the valve seat 310. As shown, the mounting member 316 has an elongated C-shaped cross-sectional profile. The mounting member 316 includes legs 322a and 322b that extend or depend from an upper or outwardly facing curved surface 324. The leg 322a includes a foot or tab 326a that defines a first channel 328a and the leg 322b includes a foot or tab 326b that defines a second channel 328b. Each of the tabs 326a and 326b projects inwardly (e.g., substantially perpendicular) from a respective one of the legs 322a and 322b toward the longitudinal axis 314. An inner surface of each of the legs 322a and 322b includes a groove or slot 329 (
The support structure 402, which in this example is a control arm or pivot arm, includes a main body 432 having arms 434a and 434b extending from the main body 432 such that the support structure 402 has a Y-shaped cross-sectional profile. The main body 432 includes an opening 436 to receive the coupling pin 412 of the disc 406. The main body 432 also includes protruding members or alignment pins 438a-c to engage the respective bosses 426a-c protruding from the second side 410 of the disc 406. In particular, the alignment pins 438a-c are received by the respective apertures 428a-c of the bosses 426a-c to align the disc 406 and the support structure 402. Further, the alignment pin 438a engages the bearing surface 430 to provide structural support when the disc 406 is coupled to the support structure 402.
The arms 434a and 434b include respective tabs 440a and 440b that project outwardly from respective ends 442a and 442b of the arms 434a and 434b such that an axis 444 of the tabs 440a and 440b is substantially perpendicular to the longitudinal axis 314 of the valve body 202 of the inlet control valve 102. Further, the arm 434a includes a biasing element support member 446 (e.g., a cylindrical member) that extends at least partially between the arms 434a and 434b of the support structure 402. The biasing element support member 446 is to receive a biasing element 448. In this example, the biasing element 448 is a torsion spring.
Referring also to
The tabs 440a and 440b of the arms 434a and 434b of the support structure 402 are then disposed within the respective channels 328a and 328b of the legs 322a and 322b of the mounting member 316 and are slidably engaged with the slots or grooves 329 (
During assembly, the flow control member assembly 318 is coupled to the second body portion 206 and then the first body portion 204 is coupled to the second body portion 206 via a snap-fit connection as described below in connection with
Although not shown, in other examples, a portion (e.g., a portion of the flange 302) of the first body portion 204 is integrally coupled to a portion (e.g., a portion of the flange 306) of the second body portion 206 via, for example, a thin, flexible hinge member (e.g., a thin member composed of plastic) so that the first body portion 204 pivots relative to the second body portion 206 prior to being assembled (i.e., the first and second body portions 204 and 206 are in a decoupled state or condition). A second side (e.g., opposite the flexible hinge) includes a fastener (e.g., the slots 308 and the clips 306) to couple the first and second body portions 204 and 206 together (e.g., via a clip and slot configuration) after the flow control assembly 318 is assembled with the second body portion 206.
Referring to
As more clearly shown in
During normal operation (i.e., a non-filling event), the biasing element 448 biases the disc 406 toward the valve seat 310 so that the inlet control valve 102 is in a closed position. As shown, the biasing element 448 biases the disc 406 toward the valve seat 310 so that the valve seat engaging portion 504 of the disc 406 engages the seating surface 312 of the valve seat 310. In other words, the second side 410 of the disc 406 is substantially perpendicular to the longitudinal axis 314 of the valve body 202 when the inlet control valve is in the closed position. As most clearly shown in
During a filling event, when the fuel tank 104 is being filled with liquid fuel 105, the liquid fuel traveling through the passageway 806 moves or pivots the disc 406 to an open position so that the valve seat engaging surface 504 of the disc 406 is away from the valve seating surface 312 of the valve seat 310 to allow the liquid fuel to flow through passageway 806 between the inlet 118 and the outlet 112 and to the fuel tank 104. In other words, the liquid fuel moves or pivots the disc 406 against the force of the biasing element 448 to move the disc 406 away from the valve seat 310 such that the second side 410 of the disc 406 is adjacent (i.e., substantially parallel with) the mounting member 316 or the longitudinal axis 314 when in the open position.
As the volume or the level of liquid fuel 105 within the fuel tank 104 rises or increases, the vapors and/or air within the fuel tank 104 are vented or displaced via the venting system 108 and/or via the filler tube 106 through the passageway 806 of the inlet control valve 102. Thus, the fuel vapors may vent to the atmosphere via the filler tube 106 and through the inlet control valve 102 to enable the pressure within the fuel tank 104 to equalize.
However, in some cases, such displacement of the fuel vapors from the fuel tank 104 may cause the fuel vapors to carry liquid fuel through the filler tube 106 and out to the environment through the filler tube 106. Such overflow typically occurs as the liquid level in the fuel tank 104 approaches the upper, interior surface 146 of the fuel tank 104 (e.g., when the fuel tank 104 is substantially full). Thus, the increasing pressure may cause the liquid fuel to travel toward the deckfill 122 via the filler tube 106. As the liquid fuel from the fuel tank 104 enters the outlet 112 of the inlet control valve 102, the liquid fuel fills the enlarged body portion 212 and engages the second side 410 of the disc 406. This liquid fuel from the outlet 112 causes the disc 406 to move toward the valve seat 310 such that the valve seat engaging portion 504 of the disc 406 engages the seating surface 312 of the valve seat 310. Because the pressure of the liquid fuel within the fuel tank 104 (i.e., the outlet 112 side of the inlet control valve 102) is greater than the pressure of the liquid fuel of the inlet 118 side of the inlet control valve 102 (e.g., atmospheric pressure), the pressure differential across the disc 406 along with the biasing element 484 cause the disc 406 to pivot and engage the valve seat 310.
Although the disc 406 engages the valve seat 310 to prevent liquid fuel from flowing through the passageway 806 from the outlet 112 to the inlet 118, the disc 406 does not provide a tight seal and allows fuel vapors and/or air to flow through the passageway 806 between the inlet 118 and the outlet 112 to vent the fuel tank 104 during an overfill condition. For example, the seating surface 312 of the valve seat 310 and the sealing surface 504 of the disc 406 may include a relatively smooth non-textured surface. However, even with the use of a relatively smooth non-textured surface, the surface finish or roughness of the disc 406 and/or the valve seat 310 enables fuel vapors and air to flow past the sealing surface 504 and the seating surface 312 when the disc 406 engages the valve seat 310 due to surface finish imperfections or variations. In other examples, the surface finish of the sealing surface 504 and/or the seating surface 312 may include a relatively rough surface finish to allow greater fuel vapor and/or air flow through the inlet control valve 102. In yet another example, a groove or notch (e.g., an annular groove) may be formed within the sealing surface 504 of the disc 406 and/or the seating surface 312 of the valve seat 310 to provide a gap between the disc 406 and the valve seat 310 and provide a relatively greater flow of fuel vapors and/or air through the inlet control valve 102 when the disc 406 is in engagement the valve seat 310. Thus, the example inlet control valve 102 substantially restricts or prevents liquid fuel from flowing between the fuel tank 104 and the atmosphere during an overflow filling event, while allowing fuel vapors and/or air to flow between the atmosphere and the fuel tank 104 to equalize the pressure within the fuel tank 104 and/or the filler tube 106.
In this example, the fuel delivery system 900 includes a filler tube 904 having a deckfill 906 and a venting system 908 that vents to the atmosphere via a fuel cap 910 of the deckfill 906. The inlet control valve 902 is in fluid communication with the fuel tank 104 and the fuel cap 910. In particular, tubing 912a fluidly couples the fuel tank 104 to the outlet 112 of the inlet control valve 902 and tubing 912b fluidly couples the inlet 118 of the inlet control valve 902 to the fuel cap 910. The venting system 908 includes a grade valve 914 and a vent valve 916 coupled to the fuel tank 104. The grade valve 914 is fluidly coupled to the vent valve 916 via tubing 918a and the vent valve 916 is in fluid communication with the fuel cap 910 of the deckfill 906. In this example, the venting system 908 includes a vapor collection apparatus 920 disposed between the vent valve 916 and the fuel cap 910 of the deckfill 906. Tubing 918b fluidly couples the vent valve 916 to an inlet 922 of the vapor collection apparatus 920 and tubing 918c fluidly couples an outlet 924 of the vapor collection apparatus 920 to the fuel cap 910. In this example, the fuel cap 910 enables venting to the atmosphere. Therefore, fuel vapors and/or air can vent to the atmosphere via the fuel cap 910. Such an example fuel cap 910 is described in U.S. patent application Ser. No. 12/061,183, which is incorporated herein by reference in its entirety.
During a filling event, and similar to the inlet control valve 102 of
Additionally, during non-operation of the marine vehicle, the fuel delivery system 900 may be subjected to daily ambient temperature changes that may cause or affect the pressure of the fuel and/or fuel vapors within the fuel delivery system 900 (e.g., during diurnal temperature cycles). For example, an increase in fuel tank pressure may cause the release of hydrocarbons or gasoline to the environment. Diurnal emissions are evaporative emissions that are released due to daily temperature changes or cycles that may cause liquid fuel to become fuel vapor during the daylight hours and condensing fuel vapors to liquid during the night hours. As a result, the pressure cycling that occurs in response to these temperature changes causes the release of hydrocarbons from the fuel tank 104 to the environment via the venting system 908 and the fuel cap 910. The vapor collection apparatus 920 captures the hydrocarbons to prevent emissions to the atmosphere.
As described in greater detail below, the inlet control valve 902 prevents fuel vapors, air and/or diurnal emissions from flowing between the fuel tank 104 and the fuel cap 910. In other words, the inlet control valve 902 provides a seal so that the fuel vapors, air and/or diurnal emissions travel through the vapor collection apparatus 920 of the venting system 908. As noted above, the vapor collection apparatus 920 includes an emission(s)-capturing or filter material (e.g., an adsorbent material) such as, for example, activated carbon, charcoal, etc., that collects and stores evaporative emissions such as, for example, hydrocarbons to reduce pollution to the environment. In other examples, the fuel delivery system 900 may be implemented with the pressure relief system, a pressure relief valve, and/or any other pressure relief apparatus instead of the vapor collection apparatus 920. The pressure relief system allows diurnal emissions to vent to the environment via the fuel cap 910 when the pressure inside the fuel tank 104 is greater than a predetermined or preset pressure value (e.g., 5 psi) and prevent diurnal emissions from venting to the atmosphere when the pressure inside the fuel tank 104 is below the predetermined pressure. Such an example fuel cap and pressure relief system is described in U.S. patent application Ser. No. 12/793,003, which is incorporated herein by reference in its entirety.
In other examples, the disc 1006 may be composed of a plastic material having an annular groove or channel adjacent the peripheral edge that is to receive a seal such as, for example, an O-ring. In yet other examples, the disc 1006 may be composed of a rubber material, a composite material, or any other material that provides a relatively tight seal to prevent liquid fuel, fuel vapors, air and/or diurnal emissions from flowing past the orifice 808 of the valve seat 310 when the disc 1006 sealingly engages the valve seat 310.
During normal operation (i.e., a non-filling event), the biasing element 448 biases the disc 1006 toward the valve seat 310 so that the valve 902 is in a closed position to prevent fluid flow through the passageway 806. During a filling event, liquid fuel flowing from the inlet 118 to the outlet 112 (and to the fuel tank 104) causes the disc 1006 to move away from the valve seat 310 to an open position to allow liquid fuel flow through the passageway 806 and to the fuel tank 104. However, during a filling event, the inlet control valve 902 prevents liquid fuel from flowing between the fuel tank 104 and the filler tube 904 as the liquid fuel level in the fuel tank 104 rises and the fuel vapors displace liquid fuel up within the filler tube 904 from the fuel tank 104 toward the inlet 118. The liquid fuel in the second body portion 204 and the biasing element 484 cause the disc 1006 to sealingly engage the seating surface 312 of the valve seat 310. The sealing surface 1004 of the disc 1006 sealingly engages the seating surface 312 to prevent fluid flow through the passageway 806. Thus, when the inlet control valve 902 is in a closed position, the sealing surface 1004 provides a tight seal through the passageway 806, thereby causing fuel vapors, air and/or diurnal emissions to flow through the venting system 908.
Although certain apparatus, methods, and articles of manufacture have been described herein, the scope of coverage of this patent is not limited thereto. To the contrary, this patent covers all apparatus, methods, and articles of manufacture fairly falling within the scope of the appended claims either literally or under the doctrine of equivalents.
This patent claims the benefit of U.S. Provisional Patent Application Ser. No. 61/386,250, filed on Sep. 24, 2010, entitled INLET CONTROL VALVES FOR USE WITH FUEL DELIVERY SYSTEMS, which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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61386250 | Sep 2010 | US |