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US3613649A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel injection systems for internal-combustion engines fed with a fuel-and-air mixture

Assignee: Eaton Corp
•
Filing: 1970-06-01
•
Granted: 1971-10-19
•
Expires: 1990-06-01
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Abstract

Abstract In a fuel injection system for a mixture-aspiring internalcombustion engine, fuel is injected through a nozzle unit equipped with an ultrasonic transducer so that when the transducer is deenergized the nozzle produces a solid jet passing across the induction pipe of the engine into a collector tube through which the fuel returns to the fuel tank, while when the transducer is energized, the jet disintegrates, the fuel being atomized and therefore substantially all admixed to the induced air. The quantity of fuel thus introduced during each stroke or revolution with the airflow in the induction pipe is determined by the length of the energization period of the transducer.

Inventors

  • 👤 Norman Moss
  • 👤 Michael John Broad

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 10:24
CPC Classifications
F; F02; F02M; F02M69/00; F02M69/04; F02M69/041; Y; Y10; Y10S; Y10S261/00; Y10S261/48; Y10S261/69

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 166 words
A fuel injection system for an internal-combustion engine fed with a fuel-and-air mixture with a nozzle for injecting fuel into a flow duct through which air flows to the engine, and with an ultrasonic vibrator associated with the nozzle for producing atomization of the fuel injected by the nozzle, characterized by the combination of a fuel-feed device which maintains a continuous flow of fuel to the nozzle, the nozzle being so constructed as to emit in the absence of ultrasonic vibrations, a solid jet of fuel, a timing control device which limits the energization of the ultrasonic atomizer to uniformly spaced periods each constituting an adjustable part of a cycle related to the revolution of the engine, and the provision, in the flow duct of a collector aperture connected to a fuel-return line and so arranged in the flow duct as to intercept substantially all the fuel coming from the nozzle when said fuel omitted from the nozzle is in the form of a solid jet.
Claim 2
Dependent Claim 166 words
A fuel injection system for an internal-combustion engine fed with a fuel-and-air mixture with a nozzle for injecting fuel into a flow duct through which air flows to the engine, and with an ultrasonic vibrator associated with the nozzle for producing atomization of the fuel injected by the nozzle, characterized by the combination of a fuel-feed device which maintains a continuous flow of fuel to the nozzle, the nozzle being so constructed as to emit in the absence of ultrasonic vibrations, a solid jet of fuel, a timing control device which limits the energization of the ultrasonic atomizer to uniformly spaced periods each constituting an adjustable part of a cycle related to the revolution of the engine, and the provision, in the flow duct of a collector aperture connected to a fuel-return line and so arranged in the flow duct as to intercept substantially all the fuel coming from the nozzle when said fuel omitted from the nozzle is in the form of a solid jet.
Claim 3
Dependent Claim 48 words
A fuel injection system as claimed in claim 1 for a reciprocating piston engine, characterized by a timing device so connected to the engine as to limit energization of the ultrasonic atomizer to an adjustable part of each suction stroke of each cylinder fed by the flow duct.
Claim 4
Dependent Claim 21 words
A fuel system as claimed in claim 1 characterized by an automatic adjusting device for the length of said adjustable part.
Claim 5
Dependent Claim 21 words
A fuel system as claimed in claim 2 characterized by an automatic adjusting device for the length of said adjustable part.

References Cited (Backward Citations)

US2732835A Cited
US2414494A Cited
US2532554A Cited
US2908443A Cited
US2706976A Cited
US2791994A Cited
US2791990A Cited
US2949900A Cited
US3451379A Cited
GB1138536A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-10-18 1975-04-19 1975-10-19 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-10-18 1979-04-19 1979-10-19 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-10-18 1983-04-19 1983-10-19 $7700.00 Window Closed / Lapsed

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