Vapor vent control apparatus, system and outboard marine engine therewith
View Patent ↗An outboard marine engine has vapor vent control apparatus including a fuel inlet in fluid communication with a fuel reservoir of the engine. The fuel inlet is operably attachable to a fuel pin of a fuel connector. When attached, liquid fuel flows to the fuel reservoir and when detached, liquid fuel flow out of the fuel inlet is prevented. A vapor vent passage is configured in fluid communication with the liquid fuel reservoir and an air intake of the engine. A vent pin is disposed in the vapor vent passage. The vent pin moves between a first position upon attaching the fuel connector to the fuel inlet and a second position upon detaching the fuel connector from the fuel inlet. In the first position, the vapor vent passage is open to fuel vapor flow and, when in the second position, the vapor vent passage is closed to fuel vapor flow.
1. An outboard marine engine vapor vent control apparatus, comprising:
a body configured for detachable connection to a fuel connector upstream of said body, said body having a fuel inlet configured in fluid communication with a fuel reservoir downstream of said body, said body and having a one-way valve, said fuel inlet being configured for operable attachment to a fuel pin of the fuel connector, wherein, when attached to the fuel pin said one-way valve automatically moves to an open position to allow liquid fuel to flow through said one-way valve to the fuel reservoir and when detached from the fuel pin said one-way valve automatically moves to a closed position to prevent the flow of liquid fuel out of said fuel inlet;
a vapor vent passage extending through said body, said vapor vent passage configured to bring the liquid fuel reservoir on one side of said vapor vent passage in fluid communication with an air intake of the engine on an opposite side of said vapor vent passage;
a vent pin passage extending from said vapor vent passage outwardly from said body; and
a vent pin disposed in said vent pin passage, said vent pin being automatically movable between a first position upon attaching the fuel connector to said fuel inlet and a second position upon detaching the fuel connector from said fuel inlet, wherein, when in said first position said vapor vent passage is open to fuel vapor flow from the liquid fuel reservoir through said vapor vent passage to the air intake and when in said second position said vapor vent passage is closed to fuel vapor flow from the liquid fuel reservoir to the air intake.
2. The outboard marine engine vapor vent control apparatus of claim 1 wherein said vent pin is mechanically actuatable.
3. The outboard marine engine vapor vent control apparatus of claim 1 wherein said vent pin is magnetically actuatable.
4. The outboard marine engine vapor vent control apparatus of claim 1 further comprising a spring biasing said vent pin to one of said first or second positions.
5. The outboard marine engine vapor vent control apparatus of claim 1 further comprising a valve seat fixed in said vapor vent passage, said vent pin being configured to automatically move into sealed abutment with said valve seat when in said second position and out of sealed abutment from said valve seat when in said first position.
6. An outboard marine engine vapor vent control system, comprising:
a fuel connector having an elongate fuel pin with a fuel passage;
a body having a fuel inlet configured in fluid communication with a liquid fuel reservoir of the engine and having a one-way valve disposed therein, said fuel inlet being configured for receipt of said fuel pin, wherein, when attached to the fuel pin said one-way valve automatically moves to an open position to allow liquid fuel to flow through said one-way valve to the fuel reservoir and when detached from the fuel pin said one-way valve automatically moves to a closed position to prevent the flow of liquid fuel out of said fuel inlet;
a vapor vent passage configured in fluid communication with the liquid fuel reservoir and an air intake of the engine;
a vent pin disposed in said vapor vent passage, said vent pin being automatically movable between a first position upon attaching the fuel connector to said fuel inlet and a second position upon detaching the fuel connector from said fuel inlet, wherein, when in said first position said vapor vent passage being opened to fuel vapor flow and when in said second position said vapor vent passage being closed to fuel vapor flow; and
wherein said vent pin is magnetically actuated by said fuel connector.
7. The outboard marine engine vapor vent control system of claim 6 wherein said vent pin is ferrous and said fuel connector has a magnet configured to magnetically actuate said vent pin to said first position.
8. The outboard marine engine vapor vent control system of claim 7 further comprising a spring biasing said vent pin to said second position when said body is detached from said fuel connector.
9. The outboard marine engine vapor vent control system of claim 8 wherein said magnet imparts a magnetic force sufficient to overcome a spring force of said spring when said body is attached to said fuel connector to move said vent pin to said first position.
10. The outboard marine engine vapor vent control system of claim 6 further comprising a valve seat fixed in said vapor vent passage, said vent pin being in sealed abutment with said valve seat when in said second position and out of sealed abutment from said valve seat when in said first position.
11. An outboard marine engine in combination with an external fuel tank, with a fuel line extending from the fuel tank to a fuel connector having an elongate fuel pin configured for attachment to the outboard marine engine, comprising:
a fuel inlet configured in fluid communication with a liquid fuel reservoir of the engine, said fuel inlet being configured for receipt of said fuel pin to allow liquid fuel to flow to said fuel reservoir;
a vapor vent passage configured in fluid communication with said liquid fuel reservoir and an air intake of the engine;
a vent pin disposed in said vapor vent passage, said vent pin being automatically movable between a first position upon attaching the fuel connector to said fuel inlet and a second position upon detaching the fuel connector from said fuel inlet, wherein, when in said first position said vapor vent passage is open to fuel vapor flow and when in said second position said vapor vent passage is closed to fuel vapor flow; and
wherein said vent pin is magnetically actuatable.
12. The combination of claim 11 wherein said vent pin is actuated to move to said first position by said fuel connector.
13. The combination of claim 12 wherein said vent pin is ferrous and said fuel connector has a magnet configured to magnetically actuate said vent pin to said first position.
14. The combination of claim 13 further comprising a spring disposed in said vapor vent passage, said spring biasing said vent pin to said second position when said fuel pin is detached from said fuel inlet.
15. The combination of claim 14 wherein said magnet imparts a sufficient force to move said vent pin against the bias imparted by said spring when said fuel pin is attached in said fuel inlet.
16. The combination of claim 11 further comprising a valve seat in said vapor vent passage, said vent pin being in sealed abutment with said valve seat when in said second position and out of sealed abutment from said valve seat when in said first position.