The present disclosure relates generally to fuel tanks on passenger vehicles and more particularly to a fuel tank that allows point venting during extreme tip angles.
Proper venting and handling of fuel and fuel vapor is required for fuel tanks. More particularly, fuel tanks must be properly vented for passenger motor vehicles. Furthermore, fuel tanks must properly account for containment of liquid fuel.
The background description provided herein is for the purpose of generally presenting the context of the disclosure. Work of the presently named inventors, to the extent it is described in this background section, as well as aspects of the description that may not otherwise qualify as prior art at the time of filing, are neither expressly nor impliedly admitted as prior art against the present disclosure.
A fuel tank system constructed in accordance to one example of the present disclosure includes a fuel tank, a liquid trap and a tank venting assembly. The fuel tank can be configured as a reservoir for holding fuel to be supplied to an internal combustion engine. The fuel tank can define a first vapor space and a second vapor space at an area distinct from the first vapor space. The tank venting assembly can include a vent valve, a first vent line, a second vent line and a third vent line. The vent valve can have a movable member that is configured to move between a first open position wherein a front vent point is open and a second closed position wherein the front vent point is closed. The first vent line can be fluidly connected between the liquid trap and the vent valve. The second vent line can be fluidly connected between the vent valve and an auxiliary vent point at the first vapor space. The third vent line can be fluidly connected between the liquid trap and an upper vent point at the second vapor space. The vent valve is configured to move to the closed position upon a fuel level reaching a predetermined level. In the closed position, the auxiliary vent point and the upper vent point remain open and vented to the liquid trap.
According to additional features, the fuel tank further defines a third vapor space at the vent valve. The third vapor space can occupy an area distinct from the first and second vapor space. The liquid trap can further comprise a drain mechanism. The movable member can sealingly engage a valve seat in the second closed position. The movable member can comprise a cup that is configured to float relative to liquid fuel. The vent valve can permit vapor to pass between the first vent line and the second vent line in the first open position. The auxiliary vent point and the upper vent point can both concurrently open during a refueling event. The auxiliary vent point and the upper vent point are both concurrently open at a fuel level full condition. The fuel tank system can further comprise a purge canister adapted to collect fuel vapor emitted by the fuel tank and subsequently release the fuel vapor to the internal combustion engine.
A fuel tank system constructed in accordance to another example of the present disclosure includes a fuel tank, a liquid trap and a tank venting assembly. The fuel tank can be configured as a reservoir for holding fuel to be supplied to an internal combustion engine. The fuel tank can have a first vapor space, a second vapor space and a third vapor space. The first, second and third vapor spaces can be located at distinct areas within the fuel tank. The liquid trap can be disposed in the fuel tank. The tank venting assembly can comprise a vent valve, a first vent line, a second vent line and a third vent line. The vent valve can have a movable member that is configured to move between a first open position wherein a front vent point located at the third vapor space is open and a second closed position wherein the front vent point is closed. The first vent line can be fluidly connected between the liquid trap and the vent valve. The second vent line can be fluidly connected between the vent valve and an auxiliary vent point at the first vapor space. The third vent line can be fluidly connected between the liquid trap and an upper vent point at the second vapor space. The vent valve can be configured to move to the closed position upon a fuel level reaching a predetermined level. In the closed position, the auxiliary vent point and the upper vent point remain open and vented.
According to other features, the third vapor space occupies an area near a front portion of the fuel tank at an elevation between the liquid trap and the auxiliary vent point. The liquid trap can further comprise a drain mechanism. The movable member can sealingly engage a valve seat in the second closed position. The movable member can comprise a cup that is configured to float relative to liquid fuel. The vent valve can permit vapor to pass between the first vent line and the second vent line in the first open position. The auxiliary vent point and the upper vent point can both concurrently open during a refueling event. The auxiliary vent point and the upper vent point are both concurrently open at a fuel level full condition.
According to additional features, the fuel tank system can include a purge canister adapted to collect fuel vapor emitted by the fuel tank and subsequently release the fuel vapor to the internal combustion engine. The fuel tank system can further include a purge canister configured to collect fuel vapor emitted by the fuel tank and subsequently release the fuel vapor to the internal combustion engine during a purge event. The fuel tank system can additionally include a first vapor line fluidly connected between the liquid trap and the purge canister.
The present disclosure will become more fully understood from the detailed description and the accompanying drawings, wherein:
With reference now to
In the example shown in
The following disclosure can further be applicable to electronic venting systems as well such as disclosed in commonly owned PCT/US2015/051950, filed Sep. 24, 2015, the disclosure of which is expressly incorporated herein by reference.
With reference to
A first vapor line 140 can be fluidly connected between the liquid trap 130 and the purge canister 132. The first vapor line 140 can collectively be formed by vapor line 140a connected between the liquid trap 130 and safety valve 126 and vapor line 140b connected between the manifold assembly 124 and the purge canister 132. A second vapor line 142 can be connected between the purge canister 132 and the engine 114. In the example implementation, the manifold assembly 124 can be configured to control a flow of fuel vapor between the fuel tank 112 and the purge canister 132. The purge canister 132 can be adapted to collect fuel vapor emitted by the fuel tank 112 and can subsequently release the fuel vapor to the engine 114 through the second vapor line 142. A canister vent line 144 can be connected from the purge canister 132 to atmosphere. During a purge event, fresh air is drawn through the purge canister 123. In one example the safety valve 126 can inhibit liquid fuel from entering the vapor line 140b.
The fuel tank system 110 according to the present disclosure can further include a tank venting assembly 150. As will become appreciated the tank venting assembly 150 can provide sufficient venting during refueling when the vehicle is at various grades. The tank venting assembly 150 includes a first vent line 160, a second vent line 162 and a third vent line 164. A vent valve 170 can fluidly couple the first vent line 160 and the second vent line 162. The first vent line 160 can be fluidly connected between the liquid trap 130 and the vent valve 170. The second vent line 162 can have a first end that is fluidly connected to the vent valve 170 and a second end 174 that extends to an auxiliary vent point 176 at a first vapor space 180. The third vent line 164 can have a first end that is fluidly connected to the liquid trap 130 and a second end 184 that extends to an upper vent point 178 at a second vapor space 190. The vent valve 170 can generally be located at a third vapor space 192. In the example shown, the first and second vapor spaces 180 and 190 can be located generally near an upper area of the fuel tank 112. The third vapor space 192 can be located generally near a front area of the fuel tank 112. The third vapor space 192 occupies an area near a front portion of the fuel tank 112 at an elevation between the liquid trap 130 and the auxiliary vent port 176 when the vehicle is on level ground. In the example shown the front area of the fuel tank can generally be shallower as compared to the remainder of the fuel tank 112. It will be appreciated by those skilled in the art that the geometry of the fuel tank 112 is exemplary and the present teachings can be applicable to fuel tanks having other configurations.
The vent valve 170 can include a movable member or cup 210 that is configured to move between a first open position (
When the fuel level is below the cup 210, the cup 210 will occupy the position in
When the fuel level rises above the cup 210, the cup 210 will sealingly engage the valve seat 212. In this position, the front vent point 220 is closed. However, the second vent line 162 remains open at the auxiliary vent point 176. In this regard, when fuel level is above the vent valve 170 such as at a fuel level full (100% full) line 230, the vent valve 170 closes permitting venting at the auxiliary vent point 176 (and at the upper vent point 178). Explained further, when the vent valve 170 is closed, the upper vent point 178 and the auxiliary vent point 176 remain vented making available two distinct vent points during a refueling event.
The foregoing description of the examples has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular example are generally not limited to that particular example, but, where applicable, are interchangeable and can be used in a selected example, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
This application is a continuation of International Application No. PCT/US2016/024668 filed Mar. 29, 2016, which claims priority to U.S. Provisional Application No. 62/139,776 filed on Mar. 29, 2015, which is incorporated by reference in its entirety as if set forth herein.
Number | Date | Country | |
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62139776 | Mar 2015 | US |
Number | Date | Country | |
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Parent | PCT/US2016/024668 | Mar 2016 | US |
Child | 15718543 | US |