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US3685503A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel supply systems

Assignee: Petrol Injection Ltd
•
Filing: 1970-08-31
•
Granted: 1972-08-22
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Expires: 1990-08-31
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Abstract

Abstract A petrol injection system for an internal combustion engine in which separate main injectors in main air inlet tubes feeding such port are supplemented by a constricted and possibly heated common air inlet tube having a further injector. The supplementary inlet tube is effective during idling and low power running and the main injectors and main air inlet tubes are used for higher powers, the supplementary inlet being phased out.

Inventors

  • 👤 Harold Ernest Jackson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 21:54
CPC Classifications
F; F02; F02M; F02M69/00; F02M69/30; F02M69/32; F02M69/325; F02D; F02D9/00; F02M1/00; F02M31/00; F02M31/02; F02M31/16; F02M31/18; F02D2700/00; F02D2700/02; F02D2700/0217; F02D2700/0225; F02D2700/0228; F02D2700/0243; F02M2700/00; F02M2700/43; F02M2700/4302; F02M2700/4392; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 307 words
A fuel supply system for an internal combustion engine having a plurality of cylinders, air supply conduit means and a plurality of main intake tubes connecting the cylinders to the air supply conduit means, said system comprising a respective main injection nozzle positioned to introduce fuel into each intake tube and main air control means operable to regulate air flow from the supply conduit means to the main intake tubes, a secondary, heated, intake tube of relatively small crosssectional area connected to the air supply conduit means, a sole secondary injection nozzle positioned to introduce fuel directly into the heated portion of the secondary intake tube, and secondary air control means operable to regulate air flow from the supply conduit means to the secondary intake tube, the secondary intake tube also being connected to the cylinders to supply heated fuel air mixture thereto, fuel flow control means for controlling the supply of fuel to said main injection nozzles and to said secondary injection nozzle separately, a control mechanism for operating both said air control means and said fuel control means, said control mechanism being connected to operate said fuel flow control means to admit fuel to said secondary injection nozzle only, and to operate said secondary air control means to admit air to the secondary intake tube at a rate which increases with increasing fuel supply to said secondary injection nozzle, at least up to a predetermined point, as said control mechanism is moved through a first operating range, and to then operate said fuel flow control means to initiate fuel supply to said main injection nozzles and operate the main air control means to admit air to the main intake tubes at a rate which increases with increasing fuel supply to said main injection nozzles, as said control mechanism is moved beyond said first operating range.
Claim 2
Dependent Claim 307 words
A fuel supply system for an internal combustion engine having a plurality of cylinders, air supply conduit means and a plurality of main intake tubes connecting the cylinders to the air supply conduit means, said system comprising a respective main injection nozzle positioned to introduce fuel into each intake tube and main air control means operable to regulate air flow from the supply conduit means to the main intake tubes, a secondary, heated, intake tube of relatively small crosssectional area connected to the air supply conduit means, a sole secondary injection nozzle positioned to introduce fuel directly into the heated portion of the secondary intake tube, and secondary air control means operable to regulate air flow from the supply conduit means to the secondary intake tube, the secondary intake tube also being connected to the cylinders to supply heated fuel air mixture thereto, fuel flow control means for controlling the supply of fuel to said main injection nozzles and to said secondary injection nozzle separately, a control mechanism for operating both said air control means and said fuel control means, said control mechanism being connected to operate said fuel flow control means to admit fuel to said secondary injection nozzle only, and to operate said secondary air control means to admit air to the secondary intake tube at a rate which increases with increasing fuel supply to said secondary injection nozzle, at least up to a predetermined point, as said control mechanism is moved through a first operating range, and to then operate said fuel flow control means to initiate fuel supply to said main injection nozzles and operate the main air control means to admit air to the main intake tubes at a rate which increases with increasing fuel supply to said main injection nozzles, as said control mechanism is moved beyond said first operating range.
Claim 3
Dependent Claim 47 words
A system as claimed in claim 1 in which said control mechanism is connected to reduce the supply of fuel to said secondary injection nozzle and the admission of air to said secondary intake tube as the supply of fuel to said main injection nozzles is increased.
Claim 4
Dependent Claim 20 words
A system according to claim 1 in which the secondary intake tube is heated by exhaust gas from the engine.
Claim 5
Dependent Claim 43 words
A system according to claim 1 in which the air supply conduit means includes an air inlet tube in which the air control means are located, the main air control means being positioned to receive air passed by the secondary air control means.
Claim 6
Dependent Claim 68 words
A system according to claim 1 in which the fuel flow control means is responsive to the setting of the air control means to regulate fuel flow to the main injection nozzles in dependence on the setting of the main air control means and to regulate fuel flow to the secondary injection nozzle in dependence on the setting of both the main and the secondary air control means.

References Cited (Backward Citations)

US1894510A Cited
US2264133A Cited
US2793633A Cited
US2884913A Cited
US3456634A Cited
US3444848A Cited
US3461850A Cited
US3443552A Cited
US3543736A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-08-22 1976-02-21 1976-08-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-08-22 1980-02-21 1980-08-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-08-22 1984-02-21 1984-08-22 $7700.00 Window Closed / Lapsed

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