Vacuum bleed and flow restrictor fitting for fuel injected engines with vapor separator

Claim 2

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with the combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, means connected in said vapor supply line limiting fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuel-air mixture in said induction system otherwise causing rough idling or stalling, wherein said last mentioned means comprises in combination vacuum bleed orifice means in said vapor supply line partially venting vacuum from said induction system to atmosphere to limit the peak vacuum applied to said vapor separator from said induction system, and flow restrictor means in said vapor supply line limiting the volume of flow of fuel vapor from said vapor separator to said induction system, wherein said vacuum bleed orifice means and said flow restrictor means are at all times in continuous communication with each other and with said vapor separator and with said induction system.

Claim 3

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with the combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first fuel pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second fuel pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, a fitting in said vapor supply line having first and second reduced diameter passages, said first passage in said fitting being a vacuum bleed passage partially venting vacuum from said induction system to atmosphere, to limit peak vacuum applied to said vapor separator from said induction system, said second passage in said fitting being a flow restrictor passage limiting the volume of flow of fuel vapor from said vapor separator to said induction system, to limit fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuelair mixture in said induction system otherwise causing rough idling or stalling, wherein said first and second passages are at all times in continuous communication with each other and with said vapor separator and with said induction system.

Claim 4

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with the combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first fuel pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second fuel pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, a fitting in said vapor supply line having first and second reduced diameter passages, said first passage in said fitting being a vacuum bleed passage partially venting vacuum from said induction system to atmosphere, to limit peak vacuum applied to said vapor separator from said induction system, said second passage in said fitting being a flow restrictor passage limiting the volume of flow of fuel vapor from said vapor separator to said induction system, to limit fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuelair mixture in said induction system otherwise causing rough idling or stalling, wherein said first and second passages are at all times in continuous communication with each other and with said vapor separator and with said induction system.

Claim 5

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with te combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first fuel pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second fuel pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, a fitting in said vapor supply line having first and second reduced diameter passages, said first passage in said fitting being a vacuum bleed passage partially venting vacuum from said induction system to atmosphere, to limit peak vacuum applied to said vapor separator from said induction system, said second passage in said fitting being a flow restrictor passage limiting the volume of flow of fuel vapor from said vapor separator to said induction system, to limit fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuel-air mixture in said induction system otherwise causing rough idling or stalling, wherein said first passage is coaxial with and axially offset and spaced from said second passage.

Claim 6

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with te combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first fuel pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second fuel pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, a fitting in said vapor supply line having first and second reduced diameter passages, said first passage in said fitting being a vacuum bleed passage partially venting vacuum from said induction system to atmosphere, to limit peak vacuum applied to said vapor separator from said induction system, said second passage in said fitting being a flow restrictor passage limiting the volume of flow of fuel vapor from said vapor separator to said induction system, to limit fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuel-air mixture in said induction system otherwise causing rough idling or stalling, wherein said first passage is coaxial with and axially offset and spaced from said second passage.

Claim 7

The invention according to claim 3 wherein said diameter of said first passage is greater than said diameter of said second passage.

Claim 8

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with te combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first fuel pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second fuel pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, a fitting in said vapor supply line having first and second reduced diameter passages, said first passage in said fitting being a vacuum bleed passage partially venting vacuum from said induction system to atmosphere, to limit peak vacuum applied to said vapor separator from said induction system, said second passage in said fitting being a flow restrictor passage limiting the volume of flow of fuel vapor from said vapor separator to said induction system, to limit fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuel-air mixture in said induction system otherwise causing rough idling or stalling, wherein said reduced diameter of said first passage is sized to limit vacuum to an upper limit of about 30 inches of water, and wherein said reduced diameter of said second passage is sized to provide sufficient fuel vapor flow at high engine speed.

Claim 9

A marine fuel system for an internal combustion engine having an induction system for supplying combustion air to the engine and fuel injection means for mixing fuel with te combustion air, and having a remote fuel tank, said fuel system comprising a first fuel pump connected to draw fuel from said tank and a second fuel pump connected to receive fuel from said first fuel pump and provide fuel under pressure to said fuel injection means, a vapor separator connected between said first and second fuel pumps to remove fuel vapors supplied to said second fuel pump, and a vapor supply line connected between said vapor separator and said induction system to supply the vapor removed from said fuel to said induction system, a fitting in said vapor supply line having first and second reduced diameter passages, said first passage in said fitting being a vacuum bleed passage partially venting vacuum from said induction system to atmosphere, to limit peak vacuum applied to said vapor separator from said induction system, said second passage in said fitting being a flow restrictor passage limiting the volume of flow of fuel vapor from said vapor separator to said induction system, to limit fuel vapor supplied from said vapor separator to said induction system at peak vacuum from said induction system during rapid engine deceleration to prevent an overly rich fuel-air mixture in said induction system otherwise causing rough idling or stalling, wherein said reduced diameter of said first passage is sized to limit vacuum to an upper limit of about 30 inches of water, and wherein said reduced diameter of said second passage is sized to provide sufficient fuel vapor flow at high engine speed.