WO2011031464A2 - Fuel vapor separator with evaporative emissions chamber and marine fuel system and engine therewith - Google Patents

Fuel vapor separator with evaporative emissions chamber and marine fuel system and engine therewith Download PDF

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Publication number
WO2011031464A2
WO2011031464A2 PCT/US2010/046577 US2010046577W WO2011031464A2 WO 2011031464 A2 WO2011031464 A2 WO 2011031464A2 US 2010046577 W US2010046577 W US 2010046577W WO 2011031464 A2 WO2011031464 A2 WO 2011031464A2
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WIPO (PCT)
Prior art keywords
fuel
fuel vapor
evaporative emissions
separator
vapor separator
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.)
Ceased
Application number
PCT/US2010/046577
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French (fr)
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WO2011031464A3 (en
Inventor
Kyle Achor
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Federal Mogul LLC
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Federal Mogul LLC
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Publication date
Application filed by Federal Mogul LLC filed Critical Federal Mogul LLC
Publication of WO2011031464A2 publication Critical patent/WO2011031464A2/en
Publication of WO2011031464A3 publication Critical patent/WO2011031464A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F02M25/0854—Details of the absorption canister
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
    • F02M25/0872—Details of the fuel vapour pipes or conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/20—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines characterised by means for preventing vapour lock

Definitions

  • This invention relates generally to fuel systems, and more particularly to marine fuel systems and vapor and evaporative devices therefor.
  • an engine In inboard/outboard marine engine applications, an engine is mounted to boat and a separate fuel tank is carried on the boat.
  • a fuel line is configured in fluid communication with the fuel tank and the engine to supply fuel the engine.
  • the fuel line is connected to an intervening vapor separator, with the fuel line then continuing to directed fuel under high pressure via a fuel pump from the fuel vapor separator to the fuel injection system.
  • a vapor vent line generally extends from the fuel vapor separator to an air intake of the engine.
  • a separate vapor vent line typically extends from the fuel tank to vent fuel vapor directly to the atmosphere.
  • Some applications are known to incorporate a separate evaporative emission control tank in fluid communication with the vapor vent line downstream from the fuel tank to capture fuel vapor prior to its being expelled to the atmosphere.
  • some evaporative emission control tanks in addition to venting to the atmosphere, have a fuel vapor line configured in direct fluid communication with the engine to burn the fuel vapor.
  • a unitized fuel vapor separator and evaporative emission device includes a fuel vapor separator configured for fluid communication with an upstream fuel tank and with a fuel pump and having a fuel vapor outlet to channel fuel vapor outwardly from the fuel vapor separator.
  • the devices further includes an evaporative emissions chamber configured for fluid communication with the fuel tank to receive fuel vapor therefrom and having an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor and having an air outlet to channel the air outwardly from the evaporative emissions chamber.
  • the fuel vapor separator and said evaporative emissions chamber have a common wall separating the fuel vapor separator from the evaporative emissions chamber.
  • a marine fuel system in accordance with another aspect of the invention, includes a fuel tank; a fuel pump; with a fuel vapor separator configured in fluid communication with the fuel tank to receive liquid fuel therefrom and with the fuel pump to pump liquid fuel from the fuel vapor separator downstream to a combustion chamber and having a fuel vapor outlet to channel fuel vapor outwardly from the fuel vapor separator.
  • the system further includes an evaporative emissions chamber configured for vapor communication with the fuel tank via a fuel vapor line to receive fuel vapor from the fuel tank.
  • the evaporative emissions chamber has an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor through an air outlet to channel the air outwardly from the evaporative emissions chamber, wherein the fuel vapor separator and the evaporative emissions chamber have a common wall separating the fuel vapor separator from the evaporative emissions chamber.
  • a marine engine has an air intake, a combustion chamber, and a fuel pump in fluid communication with the combustion chamber. Further, the engine has a fuel vapor separator configured in fluid communication with an upstream fuel tank via a fuel line to receive liquid fuel from the fuel tank and in communication with the fuel pump to pump liquid fuel from the fuel vapor separator downstream to the combustion chamber. In addition, the fuel vapor separator has a fuel vapor outlet to channel fuel vapor outwardly from the fuel vapor separator. The engine further includes an evaporative emissions chamber configured for fluid communication with the fuel tank via a fuel vapor line to receive fuel vapor from the fuel tank.
  • the evaporative emissions chamber has an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor through an air outlet to channel the air outwardly from the evaporative emissions chamber, wherein the fuel vapor separator and the evaporative emissions chamber have a common wall separating the fuel vapor separator from the evaporative emissions chamber.
  • Figure 1 is a schematic view of a marine fuel system in accordance with one aspect of the invention.
  • Figure 2 is a an enlarged schematic view of a vapor separator/evaporative emissions device of Figure 1 ;
  • Figure 3 is a an enlarged schematic view of a vapor separator/evaporative emissions device constructed in accordance with another presently preferred aspect of the invention.
  • Figure 1 illustrates a marine fuel system, referred to hereafter generally as system 10, configured in accordance with one presently preferred embodiment of the invention.
  • system 10 includes a source of liquid fuel, represented as a separate fuel tank 12 configured removed from and in fluid communication with an engine 14.
  • the liquid fuel is driven by a low pressure lift pump 16 and a high pressure fuel pump 18.
  • the lift pump 16 is responsible for pumping the liquid fuel from the fuel tank 12 to a single component, unitized fuel vapor separator/evaporative emissions device, referred to hereafter as device 20, constructed in accordance with one aspect of the invention.
  • liquid fuel is pumped under high pressure via the fuel pump 18 through a fuel line 22 to one or more combustion chambers 23 and fuel vapor is preferably directed to an air intake 25 of the engine via a fuel vapor line 24.
  • the device 20 is able to perform dual functions including separating fuel vapor from liquid fuel to prevent fuel vapor from being pumped through the high pressure fuel pump 18 and capturing evaporative emissions from the fuel tank 12 via a vapor emissions line 26 for circulation to the air intake of the engine.
  • the device 20 although constructed as a single component, such as in a molding process, for example, has separate chambers with one chamber being configured as a vapor separator 26 and the other being configured as an evaporative emissions chamber 28.
  • the vapor separator 26 and the evaporative emissions chamber 28, although being constructed as a single component, are bounded as separate containers out of direct fluid communication with one another, such as by an intervening wall 35 that is common to both chambers 26, 28.
  • the vapor separator 26 is in direct fluid communication with the fuel tank 12 via a liquid fuel line 30 and the evaporative emissions chamber 28 is in direct vapor communication with the fuel tank via a vapor line 32.
  • the liquid fuel line 30 and the vapor line 32 are separate and out of communication with one another between the device 20 and the fuel tank 12.
  • the vapor separator 26 receives liquid fuel from the fuel tank via the fuel line 30. Within the fuel separator 26, fuel vapor rises from the liquid fuel and is channeled to the fuel vapor line 24 via an upstream passage or fuel vapor line 34, while the liquid fuel is pumped to the engine via the fuel pump 18 through the fuel line 22.
  • the evaporative emissions chamber 28 contains a fuel vapor adsorption material, such as granular charcoal 36.
  • a fuel vapor adsorption material such as granular charcoal 36.
  • the evaporative emission from the fuel tank 12 is channeled to the chamber 28 via the vapor line 32, wherein the vapor is adsorbed by the charcoal 36, and air separated from the vapor is then allowed to be channeled to the air intake 23 for combustion in the engine 14 through the fuel vapor line 24 via an upstream evaporative emission vapor line 38.
  • a single process can be used, such as molding, to substantially form the fuel separator 26 and emissions chamber 28.
  • the device 20 can be molded having a common peripheral outer wall 40 extending about the fuel separator 26 and the emissions chamber 28, with the inventing wall 35 being molded to separate the adjacent chambers.
  • the outer wall 40 is preferably formed of a single piece of "as molded" material. It should be recognized that the intervening wall 35 can be formed separately and attached between the outer wall 40, if desired.
  • a lid or cover 42 can then be formed and attached in sealed abutment with an upper surface of the outer and intervening walls 40, 35 to isolate the separate chambers 26, 28 from direct fluid communication with one another.
  • the openings accommodating the fuel line 30, vapor line 32, vapor line 34 and emission line 38 can be formed in the respective walls, as desired.
  • a liquid fuel flow passage 44 is provided to bring the fuel vapor separator 26 into fluid communication with the fuel pump 18 so that the fuel pump 18 can receive and pump the liquid fuel to the engine under high pressure.
  • the fuel pump 18 is illustrated as being external to the fuel vapor separator 26, wherein at least a portion of a wall 46 of the fuel pump 18 can be attached and/or formed as one piece of material with the outer wall 40 of the device 20, such as in the aforementioned molding process. Although illustrated being external, the fuel pump 18 can be internal to the fuel vapor separator 26 as well.
  • FIG. 3 a device 120 constructed in accordance with another presently preferred aspect of the invention is shown, wherein the same reference numerals, offset by a factor of 100, are used to identify like features.
  • the device 120 is constructed similarly to the device 20, having a vapor separator 126 and an evaporative emissions chamber 128 separated from one another via an intermediate, intervening wall 135 with respective fuel and vapor lines 130, 132 extending from a fuel tank to channel liquid fuel and fuel vapor from the fuel tank to the vapor separator 126 and evaporative emission chamber 128, respectively.
  • a fuel pump 1 18 is configured in fluid communication with the vapor separator 126 via a liquid fuel flow passage 144 so that the fuel pump 1 18 can receive liquid fuel from the vapor separator 126 and pump the liquid fuel to the engine directly from the separator 126.
  • a passage or fuel vapor line 134 extends from the fuel vapor separator 126 to channel fuel vapor in unidirectional fashion therefrom, however, rather than the fuel vapor line 134 being configured in direct fluid communication with an air intake of the engine, it is configured in direct fluid communication with the evaporative emissions chamber 128.
  • the fuel vapor flows outwardly from the fuel vapor separator 126, preferably from an upper most outlet in a cover 142 thereof, directly to the evaporative emissions chamber 128 having an adsorptive material 136 therein.
  • the evaporative emissions chamber 128 has an emissions line 138 extending therefrom to route filtered air outwardly from the chamber 128.
  • the filtered air comprises air from both the filtered vapor from the vapor separator 126 and air from the filtered evaporative emissions from the fuel tank routed through the evaporative emissions chamber 128. Accordingly, rather than having two filtered air lines as in the device 20 of Figure 2, the single filter air line 138 communicates the filtered vapor of the vapor separator 126 and the evaporative emission chamber 128 to the desired location, whether directly to the atmosphere or to an air intake of the engine.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supplying Secondary Fuel Or The Like To Fuel, Air Or Fuel-Air Mixtures (AREA)
  • Separation Of Gases By Adsorption (AREA)

Abstract

A unitized fuel vapor separator and evaporative emission device; marine fuel system, and marine engine therewith are provided. The device includes a fuel vapor separator and evaporative emissions chamber having a common wall separating the fuel vapor separator from the evaporative emissions chamber. The fuel vapor separator is configured for fluid communication with an upstream fuel tank and with a fuel pump and has a fuel vapor outlet to channel fuel vapor outwardly therefrom. The evaporative emissions chamber is configured for fluid communication with the fuel tank to receive fuel vapor therefrom and has an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor through an air outlet to channel the air outwardly therefrom.

Description

FUEL VAPOR SEPARATOR WITH EVAPORATIVE EMISSIONS CHAMBER AND MARINE FUEL SYSTEM AND ENGINE THEREWITH
BACKGROUND OF THE INVENTION
1. Technical Field
[0001 ] This invention relates generally to fuel systems, and more particularly to marine fuel systems and vapor and evaporative devices therefor.
2. Related Art
[0002] In inboard/outboard marine engine applications, an engine is mounted to boat and a separate fuel tank is carried on the boat. A fuel line is configured in fluid communication with the fuel tank and the engine to supply fuel the engine. Typically, the fuel line is connected to an intervening vapor separator, with the fuel line then continuing to directed fuel under high pressure via a fuel pump from the fuel vapor separator to the fuel injection system. In addition, a vapor vent line generally extends from the fuel vapor separator to an air intake of the engine. To relieve vapor pressure from within the fuel tank, a separate vapor vent line typically extends from the fuel tank to vent fuel vapor directly to the atmosphere. Some applications are known to incorporate a separate evaporative emission control tank in fluid communication with the vapor vent line downstream from the fuel tank to capture fuel vapor prior to its being expelled to the atmosphere. In addition, some evaporative emission control tanks, in addition to venting to the atmosphere, have a fuel vapor line configured in direct fluid communication with the engine to burn the fuel vapor.
[0003] Although the fuel systems discussed above can be effective in routing fuel and fuel vapor, certain improvements can be made to enhance the overall effectiveness and efficiency of removing fuel vapor from the fuel tank, while at the same time maximizing the running efficiency of the engine.
SUMMARY OF THE INVENTION
[0004] A unitized fuel vapor separator and evaporative emission device includes a fuel vapor separator configured for fluid communication with an upstream fuel tank and with a fuel pump and having a fuel vapor outlet to channel fuel vapor outwardly from the fuel vapor separator. The devices further includes an evaporative emissions chamber configured for fluid communication with the fuel tank to receive fuel vapor therefrom and having an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor and having an air outlet to channel the air outwardly from the evaporative emissions chamber. The fuel vapor separator and said evaporative emissions chamber have a common wall separating the fuel vapor separator from the evaporative emissions chamber.
[0005] In accordance with another aspect of the invention, a marine fuel system is provided. The system includes a fuel tank; a fuel pump; with a fuel vapor separator configured in fluid communication with the fuel tank to receive liquid fuel therefrom and with the fuel pump to pump liquid fuel from the fuel vapor separator downstream to a combustion chamber and having a fuel vapor outlet to channel fuel vapor outwardly from the fuel vapor separator. The system further includes an evaporative emissions chamber configured for vapor communication with the fuel tank via a fuel vapor line to receive fuel vapor from the fuel tank. The evaporative emissions chamber has an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor through an air outlet to channel the air outwardly from the evaporative emissions chamber, wherein the fuel vapor separator and the evaporative emissions chamber have a common wall separating the fuel vapor separator from the evaporative emissions chamber.
[0006] In accordance with another aspect of the invention, a marine engine is provided. The marine engine has an air intake, a combustion chamber, and a fuel pump in fluid communication with the combustion chamber. Further, the engine has a fuel vapor separator configured in fluid communication with an upstream fuel tank via a fuel line to receive liquid fuel from the fuel tank and in communication with the fuel pump to pump liquid fuel from the fuel vapor separator downstream to the combustion chamber. In addition, the fuel vapor separator has a fuel vapor outlet to channel fuel vapor outwardly from the fuel vapor separator. The engine further includes an evaporative emissions chamber configured for fluid communication with the fuel tank via a fuel vapor line to receive fuel vapor from the fuel tank. The evaporative emissions chamber has an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor through an air outlet to channel the air outwardly from the evaporative emissions chamber, wherein the fuel vapor separator and the evaporative emissions chamber have a common wall separating the fuel vapor separator from the evaporative emissions chamber. BRIEF DESCRIPTION OF THE DRAWINGS
[0007] These and other aspects, features and advantages of the invention will become more readily appreciated when considered in connection with the following detailed description of presently preferred embodiments and best mode, appended claims and accompanying drawings, in which:
[0008] Figure 1 is a schematic view of a marine fuel system in accordance with one aspect of the invention;
[0009] Figure 2 is a an enlarged schematic view of a vapor separator/evaporative emissions device of Figure 1 ; and
[00010] Figure 3 is a an enlarged schematic view of a vapor separator/evaporative emissions device constructed in accordance with another presently preferred aspect of the invention.
DETAILED DESCRIPTION OF PRESENTLY PREFERRED EMBODIMENTS
[0001 1 ] Referring in more detail to the drawings, Figure 1 illustrates a marine fuel system, referred to hereafter generally as system 10, configured in accordance with one presently preferred embodiment of the invention. The system 10, although shown in an outboard marine engine configuration, can be incorporated into an inboard marine engine configuration as well. The system 10 includes a source of liquid fuel, represented as a separate fuel tank 12 configured removed from and in fluid communication with an engine 14. The liquid fuel is driven by a low pressure lift pump 16 and a high pressure fuel pump 18. The lift pump 16 is responsible for pumping the liquid fuel from the fuel tank 12 to a single component, unitized fuel vapor separator/evaporative emissions device, referred to hereafter as device 20, constructed in accordance with one aspect of the invention. From the unitized device 20, liquid fuel is pumped under high pressure via the fuel pump 18 through a fuel line 22 to one or more combustion chambers 23 and fuel vapor is preferably directed to an air intake 25 of the engine via a fuel vapor line 24. Accordingly, the device 20 is able to perform dual functions including separating fuel vapor from liquid fuel to prevent fuel vapor from being pumped through the high pressure fuel pump 18 and capturing evaporative emissions from the fuel tank 12 via a vapor emissions line 26 for circulation to the air intake of the engine.
[00012] The device 20, although constructed as a single component, such as in a molding process, for example, has separate chambers with one chamber being configured as a vapor separator 26 and the other being configured as an evaporative emissions chamber 28. The vapor separator 26 and the evaporative emissions chamber 28, although being constructed as a single component, are bounded as separate containers out of direct fluid communication with one another, such as by an intervening wall 35 that is common to both chambers 26, 28. The vapor separator 26 is in direct fluid communication with the fuel tank 12 via a liquid fuel line 30 and the evaporative emissions chamber 28 is in direct vapor communication with the fuel tank via a vapor line 32. The liquid fuel line 30 and the vapor line 32 are separate and out of communication with one another between the device 20 and the fuel tank 12.
[00013] The vapor separator 26 receives liquid fuel from the fuel tank via the fuel line 30. Within the fuel separator 26, fuel vapor rises from the liquid fuel and is channeled to the fuel vapor line 24 via an upstream passage or fuel vapor line 34, while the liquid fuel is pumped to the engine via the fuel pump 18 through the fuel line 22.
[00014] The evaporative emissions chamber 28 contains a fuel vapor adsorption material, such as granular charcoal 36. The evaporative emission from the fuel tank 12 is channeled to the chamber 28 via the vapor line 32, wherein the vapor is adsorbed by the charcoal 36, and air separated from the vapor is then allowed to be channeled to the air intake 23 for combustion in the engine 14 through the fuel vapor line 24 via an upstream evaporative emission vapor line 38.
[00015] In constructing the device 20, a single process can be used, such as molding, to substantially form the fuel separator 26 and emissions chamber 28. For example, the device 20 can be molded having a common peripheral outer wall 40 extending about the fuel separator 26 and the emissions chamber 28, with the inventing wall 35 being molded to separate the adjacent chambers. The outer wall 40 is preferably formed of a single piece of "as molded" material. It should be recognized that the intervening wall 35 can be formed separately and attached between the outer wall 40, if desired. A lid or cover 42 can then be formed and attached in sealed abutment with an upper surface of the outer and intervening walls 40, 35 to isolate the separate chambers 26, 28 from direct fluid communication with one another. Of course, the openings accommodating the fuel line 30, vapor line 32, vapor line 34 and emission line 38 can be formed in the respective walls, as desired. In addition, a liquid fuel flow passage 44 is provided to bring the fuel vapor separator 26 into fluid communication with the fuel pump 18 so that the fuel pump 18 can receive and pump the liquid fuel to the engine under high pressure. The fuel pump 18 is illustrated as being external to the fuel vapor separator 26, wherein at least a portion of a wall 46 of the fuel pump 18 can be attached and/or formed as one piece of material with the outer wall 40 of the device 20, such as in the aforementioned molding process. Although illustrated being external, the fuel pump 18 can be internal to the fuel vapor separator 26 as well.
[00016] In Figure 3, a device 120 constructed in accordance with another presently preferred aspect of the invention is shown, wherein the same reference numerals, offset by a factor of 100, are used to identify like features. The device 120 is constructed similarly to the device 20, having a vapor separator 126 and an evaporative emissions chamber 128 separated from one another via an intermediate, intervening wall 135 with respective fuel and vapor lines 130, 132 extending from a fuel tank to channel liquid fuel and fuel vapor from the fuel tank to the vapor separator 126 and evaporative emission chamber 128, respectively. A fuel pump 1 18 is configured in fluid communication with the vapor separator 126 via a liquid fuel flow passage 144 so that the fuel pump 1 18 can receive liquid fuel from the vapor separator 126 and pump the liquid fuel to the engine directly from the separator 126. In addition, a passage or fuel vapor line 134 extends from the fuel vapor separator 126 to channel fuel vapor in unidirectional fashion therefrom, however, rather than the fuel vapor line 134 being configured in direct fluid communication with an air intake of the engine, it is configured in direct fluid communication with the evaporative emissions chamber 128. As such, the fuel vapor flows outwardly from the fuel vapor separator 126, preferably from an upper most outlet in a cover 142 thereof, directly to the evaporative emissions chamber 128 having an adsorptive material 136 therein.
[00017] The evaporative emissions chamber 128 has an emissions line 138 extending therefrom to route filtered air outwardly from the chamber 128. The filtered air comprises air from both the filtered vapor from the vapor separator 126 and air from the filtered evaporative emissions from the fuel tank routed through the evaporative emissions chamber 128. Accordingly, rather than having two filtered air lines as in the device 20 of Figure 2, the single filter air line 138 communicates the filtered vapor of the vapor separator 126 and the evaporative emission chamber 128 to the desired location, whether directly to the atmosphere or to an air intake of the engine. Given the fuel vapors have been filtered by the adsorptive material 136 in the emissions chamber 128, the resulting air flowing outwardly from the emissions chambers 128 is able to be channeled directly to the atmosphere, if desired. [00018] Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.

Claims

What is claimed is:
1 . A unitized fuel vapor separator and evaporative emission device, comprising: a fuel vapor separator configured for fluid communication with an upstream fuel tank and with a fuel pump and having a fuel vapor outlet to channel fuel vapor outwardly from said fuel vapor separator;
an evaporative emissions chamber configured for fluid communication with the fuel tank to receive fuel vapor therefrom and having an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor and having an air outlet to channel the air outwardly from said evaporative emissions chamber; and
wherein said fuel vapor separator and said evaporative emissions chamber have a common wall separating said fuel vapor separator from said evaporative emissions chamber.
2. The device of claim 1 further comprising a fuel vapor passage extending from the fuel vapor separator in direct fluid communication with the evaporative emissions chamber to channel fuel vapor from said fuel vapor separator to said evaporative emissions chamber.
3. The device of claim 2 wherein said adsorption material adsorbs fuel vapor from the fuel vapor separator along with fuel vapor from the fuel tank.
4. The device of claim 3 wherein said air outlet expels air from the filtered fuel vapor from the fuel vapor separator and the fuel tank.
5. The device of claim 1 wherein said fuel vapor separator and said evaporative emissions chamber have a common peripheral outer wall.
6. The device of claim 5 wherein said outer wall is a single piece of material "as molded".
7. A marine fuel system, comprising:
a fuel tank; a fuel pump;
a fuel vapor separator configured in fluid communication with said fuel tank to received liquid fuel therefrom and with said fuel pump to pump liquid fuel from said fuel vapor separator downstream to a combustion chamber and having a fuel vapor outlet to channel fuel vapor outwardly from said fuel vapor separator;
an evaporative emissions chamber configured in fluid communication with said fuel tank via a fuel vapor line to receive fuel vapor from said fuel tank and having an adsorption material for adsorbing fuel vapor and dissipating air from the fuel vapor and having an air outlet to channel the air outwardly from said evaporative emissions chamber; and
wherein said fuel vapor separator and said evaporative emissions chamber have a common wall separating said fuel vapor separator from said evaporative emissions chamber.
8. The marine fuel system of claim 7 further comprising a fuel vapor passage extending from the fuel vapor separator in direct fluid communication with the evaporative emissions chamber to channel fuel vapor from said fuel vapor separator to said evaporative emissions chamber.
9. The marine fuel system of claim 8 wherein said adsorption material adsorbs fuel vapor from the fuel vapor separator along with fuel vapor from the fuel tank and wherein said air outlet expels air from the filtered fuel vapor from the fuel vapor separator and the fuel tank.
10. The marine fuel system of claim 7 wherein said fuel vapor separator and said evaporative emissions chamber have a common peripheral outer wall.
1 1 . A marine engine, comprising:
an air intake;
a combustion chamber;
a fuel pump in fluid communication with said combustion chamber;
a fuel vapor separator configured in fluid communication with an upstream fuel tank via a fuel line to receive liquid fuel from the fuel tank and with said fuel pump to pump liquid fuel from said fuel vapor separator downstream to said combustion chamber and having a fuel vapor outlet to channel fuel vapor outwardly from said fuel vapor separator;
an evaporative emissions chamber configured for fluid communication with the fuel tank via a fuel vapor line to receive fuel vapor from the fuel tank and having an adsorption material for adsorbing fuel vapor and to dissipate air from the fuel vapor and having an air outlet to channel the air outwardly from said evaporative emissions chamber; and
wherein said fuel vapor separator and said evaporative emissions chamber have a common wall separating said fuel vapor separator from said evaporative emissions chamber.
12. The marine engine of claim 1 1 further comprising a fuel vapor passage extending from the fuel vapor separator in direct fluid communication with the evaporative emissions chamber to channel fuel vapor from said fuel vapor separator to said evaporative emissions chamber.
13. The device of claim 12 wherein said adsorption material adsorbs fuel vapor from the fuel vapor separator along with fuel vapor from the fuel tank.
14. The device of claim 13 wherein said air outlet expels air from the filtered fuel vapor from the fuel vapor separator and the fuel tank to said air intake.
15. The device of claim 1 1 wherein said fuel vapor separator and said evaporative emissions chamber have a common peripheral outer wall.
PCT/US2010/046577 2009-08-27 2010-08-25 Fuel vapor separator with evaporative emissions chamber and marine fuel system and engine therewith Ceased WO2011031464A2 (en)

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US12/548,813 US8166955B2 (en) 2009-08-27 2009-08-27 Fuel vapor separator with evaporative emissions chamber and marine fuel system and engine therewith
US12/548,813 2009-08-27

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WO2011031464A2 true WO2011031464A2 (en) 2011-03-17
WO2011031464A3 WO2011031464A3 (en) 2011-06-30

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Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102782298A (en) * 2010-01-08 2012-11-14 费德罗-莫格尔公司 Vapor Separator with Integral Low Pressure Lift Pump
US20130291734A1 (en) * 2012-05-01 2013-11-07 Ford Global Technologies, Llc Carbon canister with integrated filter
US11780323B1 (en) * 2022-06-07 2023-10-10 GM Global Technology Operations LLC Fuel tank venting system with liquid collection and active purging
US12292022B2 (en) * 2023-03-08 2025-05-06 Caterpillar Inc. Containerized alternative fuel control unit

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3610221A (en) 1969-10-06 1971-10-05 Gen Motors Corp Fuel tank purge system and method
US3683597A (en) * 1970-09-17 1972-08-15 Gen Motors Corp Evaporation loss control
US4876993A (en) 1988-07-12 1989-10-31 Brunswick Corporation Fuel system with vapor bypass of oil-fuel mixer halting oil pumping
US5404858A (en) * 1991-10-18 1995-04-11 Sanshin Kogyo Kabushiki Kaisha High pressure fuel feeding device for fuel injection engine
US5389245A (en) 1993-08-10 1995-02-14 Brunswick Corporation Vapor separating unit for a fuel system
US5355861A (en) 1993-12-07 1994-10-18 Kyosan Denki Co., Ltd. Evaporative emission control system
JP3337975B2 (en) * 1998-04-30 2002-10-28 愛三工業株式会社 Evaporative fuel treatment system canister
US6257208B1 (en) * 1999-08-17 2001-07-10 Federal-Mogul World Wide, Inc. Marine-vapor separator
JP3706785B2 (en) 2000-02-02 2005-10-19 本田技研工業株式会社 Evaporative fuel processing equipment
EP1124053A3 (en) 2000-02-09 2003-01-08 Nissan Motor Co., Ltd. Fuel vapor treatment system
JP4259744B2 (en) * 2000-11-27 2009-04-30 ヤマハ発動機株式会社 Fuel supply system for 4-cycle engine for outboard motor
JP3924672B2 (en) * 2001-01-30 2007-06-06 株式会社ケーヒン Vapor separator in outboard motor
US6553974B1 (en) * 2001-10-24 2003-04-29 Brunswick Corporation Engine fuel system with a fuel vapor separator and a fuel vapor vent canister
DE10209491A1 (en) * 2002-03-05 2003-09-18 Ti Automotive Technology Ct Gm Fuel tank with venting system has inlet opening in form of open line end and liquid separator arranged between inlet opening and active carbon filter
US6959696B2 (en) 2002-04-12 2005-11-01 Briggs & Stratton Corporation Internal combustion engine evaporative emission control system
US6694955B1 (en) * 2002-07-09 2004-02-24 Brunswick Corporation Marine engine with primary and secondary fuel reservoirs
US6718953B1 (en) * 2002-07-19 2004-04-13 Brunswick Corporation Fuel vapor separator with a flow directing component within a fuel recirculating flow path
US6892710B2 (en) * 2003-02-21 2005-05-17 Charles Bradley Ekstam Fuel/air separation system
DE60320782D1 (en) 2003-07-30 2008-06-19 Delphi Tech Inc Apparatus for treating vaporized fuel
US20050045160A1 (en) * 2003-09-03 2005-03-03 Alicia Peterson Evaporative emissions canister with incorporated liquid fuel trap
US7267112B2 (en) * 2004-02-02 2007-09-11 Tecumseh Products Company Evaporative emissions control system including a charcoal canister for small internal combustion engines
US7438059B2 (en) 2005-03-04 2008-10-21 Eaton Corporation Evaporative emission control system and method for small engines
JP4530982B2 (en) * 2005-12-27 2010-08-25 本田技研工業株式会社 Evaporative fuel emission suppression device for fuel tank
US7631635B2 (en) * 2007-06-01 2009-12-15 Ti Automotive Technology Center Gmbh Liquid separator and vented fuel tank arrangement
US20080308073A1 (en) 2007-06-13 2008-12-18 Allen Christopher D Evaporative emissions canister having an integral membrane
US7431021B1 (en) 2007-09-19 2008-10-07 Federal - Mogul World Wide, Inc. Fuel vapor separator
US7677225B2 (en) * 2008-02-04 2010-03-16 Kohler Co. Fuel delivery system for engine
JP5014269B2 (en) * 2008-06-20 2012-08-29 本田技研工業株式会社 Evaporative fuel processing device for work equipment
US7895991B2 (en) * 2009-05-11 2011-03-01 Ford Global Technologies, Llc Integrated canister strainer

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US20110048386A1 (en) 2011-03-03
US8166955B2 (en) 2012-05-01

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