US4699109A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Closed end fuel injection system
Assignee: Brunswick Corp
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Filing: 1986-08-19
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Granted: 1987-10-13
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Expires: 2006-08-19
Abstract
Abstract A marine fuel supply system for a fuel injected engine (10) deadheads a high pressure fuel line (27) with a closed-end connection to the fuel injectors (24) without a recirculating return fuel line to the fuel injection pump (25) and without a return fuel line to the remote fuel tank (29). A differential pressure transducer (33) senses differential pressure across the fuel injector (24) between the high pressure fuel line (27) and the low pressure induction manifold (17) and turns off the fuel pump (25) above a first value of relative differential pressure and turns on fuel pump (25) at a second value below the first value, to maintain the fuel pressure in the high pressure line (27) within a given range relative to induction manifold pressure.
Inventors
- 👤 Robert J. Hensel
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 04:11
CPC Classifications
F; F02; F02D; F02D41/00; F02D41/30; F02D41/3082; F02M; F02M69/00; F02M69/10; F02M69/46; F02B; F02B75/00; F02B75/02; F02B2075/022; F02B2075/025; F02D2250/00; F02D2250/31; F02D2400/00; F02D2400/04
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
233 words
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 fuel pump means connected to draw fuel from said fuel tank and supply fuel under pressure to said fuel injection means, and pressure sensor means connected to sense the fuel pressure at said fuel injection means and connected to turn off said fuel pump means when said fuel pressure at said fuel injection means is above a first value and to turn on said fuel pump means when said fuel pressure at said fuel injection means is below a second value less than said first value, wherein said fuel is delivered by a high pressure fuel line from said fuel pump means to said fuel injection means, and wherein said high pressure fuel line is connected to said fuel injection means without a return fuel line to said fuel pump means and without a return fuel line to said remote fuel tank, the pressure in said high pressure fuel line being maintained between said first and second values, wherein said pressure sensor means comprises differential pressure transducer means connected to sense differential pressure between said high pressure fuel line and said induction system, to sense differential pressure across said fuel injection means.
Claim 2
Dependent Claim
233 words
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 fuel pump means connected to draw fuel from said fuel tank and supply fuel under pressure to said fuel injection means, and pressure sensor means connected to sense the fuel pressure at said fuel injection means and connected to turn off said fuel pump means when said fuel pressure at said fuel injection means is above a first value and to turn on said fuel pump means when said fuel pressure at said fuel injection means is below a second value less than said first value, wherein said fuel is delivered by a high pressure fuel line from said fuel pump means to said fuel injection means, and wherein said high pressure fuel line is connected to said fuel injection means without a return fuel line to said fuel pump means and without a return fuel line to said remote fuel tank, the pressure in said high pressure fuel line being maintained between said first and second values, wherein said pressure sensor means comprises differential pressure transducer means connected to sense differential pressure between said high pressure fuel line and said induction system, to sense differential pressure across said fuel injection means.
Claim 3
Dependent Claim
57 words
The invention according to claim 1 wherein said engine comprises a crankcase and an induction manifold, and wherein said fuel injection means injects fuel into said induction manifold, and wherein said differential pressure transducer means has a high pressure input connected to said high pressure fuel line and a low pressure input connected to said induction manifold.
Claim 4
Dependent Claim
202 words
A marine fuel system for an internal combustion engine with a remote fuel tank, comprising: an induction system for supplying combustion air to said engine; fuel injection means for mixing fuel with said combustion air; fuel pump means connected to draw fuel from said remote fuel tank and supply fuel under pressure to said fuel injection means; pressure sensor means connected to sense the fuel pressure at said fuel injection means and connected to turn off said fuel pump means when said fuel pressure at said fuel injection means is above a first value, and to turn on said fuel pump means when said fuel pressure at said fuel injection means is below a second value less than said first value; a high pressure fuel line connected from said fuel pump means to said fuel injection means, and wherein: said pressure sensor means comprises differential pressure transducer means connected between said high pressure fuel line and said induction system to sense differential pressure across said fuel injection means; and said high pressure fuel line is connected to said fuel injection means without a return fuel line to said fuel pump means and without a return fuel line to said remote fuel tank.
Claim 5
Dependent Claim
202 words
A marine fuel system for an internal combustion engine with a remote fuel tank, comprising: an induction system for supplying combustion air to said engine; fuel injection means for mixing fuel with said combustion air; fuel pump means connected to draw fuel from said remote fuel tank and supply fuel under pressure to said fuel injection means; pressure sensor means connected to sense the fuel pressure at said fuel injection means and connected to turn off said fuel pump means when said fuel pressure at said fuel injection means is above a first value, and to turn on said fuel pump means when said fuel pressure at said fuel injection means is below a second value less than said first value; a high pressure fuel line connected from said fuel pump means to said fuel injection means, and wherein: said pressure sensor means comprises differential pressure transducer means connected between said high pressure fuel line and said induction system to sense differential pressure across said fuel injection means; and said high pressure fuel line is connected to said fuel injection means without a return fuel line to said fuel pump means and without a return fuel line to said remote fuel tank.
Claim 6
Dependent Claim
60 words
The invention according to claim 3 wherein: said induction system includes an induction manifold varying in pressure from atmospheric to below atmospheric; said fuel injection means injects fuel into said induction manifold; and said differential pressure transducer means has a high pressure input connected to said high pressure fuel line and a low pressure input connected to said induction manifold.
Claim 7
Dependent Claim
96 words
The invention according to claim 3 wherein said fuel pump means comprises first and second fuel pumps, said first fuel pump connected to draw fuel from said tank and supply said fuel at low pressure through a low pressure fuel line, said second fuel pump connected to receive said low pressure fuel through said low pressure fuel line from said first fuel pump and providing high pressure fuel through said high pressure fuel line to said fuel injection means, and wherein said second fuel pump is turned on and off by said differential pressure transducer means.
Claim 8
Dependent Claim
22 words
The invention according to claim 5 comprising reservoir means in said low pressure fuel line between said first and second fuel pumps.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-10-12 | 1991-04-13 | 1991-10-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-10-12 | 1995-04-13 | 1995-10-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-10-12 | 1999-04-13 | 1999-10-13 | $7700.00 | Window Closed / Lapsed |