US4306526A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Internal combustion engine
Assignee: Cameron International Corp
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Filing: 1978-05-30
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Granted: 1981-12-22
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Expires: 1998-05-30
Abstract
Abstract A method of combusting natural gas fuel in a two cycle, turbocharged internal combustion engine substantially reduces the production of nitrogen-oxygen emissions. An improved turbocharger design provides increased air charging pressure, produces a controlled lean air/fuel mixture and lowers peak combustion temperatures. A jet cell ignition device ensures uniform, reliable ignition of the lean air/fuel mixture under all operating conditions and the lean air/fuel mixture in turn encourages complete fuel combustion and provides excellent combustion characteristics with methane, ethane and heavier paraffinic hydrocarbon fuels. These structural modifications and adjustment of other operating parameters combine to reduce nitric oxide (NO) and nitrogen dioxide (NO2) emissions by as much as 75% while effecting only a negligible increase in fuel consumption.
Inventors
- 👤 Fred S. Schaub
- 👤 Melvin J. Helmich
- 👤 Robert L. Hubbard
- 👤 Melvin C. Hoagland
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 14:41
CPC Classifications
F; F02; F02B; F02B43/00; F02B19/00; F02B19/10; F02B19/1019; F02B19/108; F02F; F02F1/00; F02F1/24; F02F1/242; F02B75/00; F02B75/02; F02B2075/022; F02B2075/025; F02F7/00; F02F7/006; F02F2007/0063; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12; Y02T10/30
Claims Analysis
Total Claims: 19
Claim 1
Independent Claim
214 words
The method of operating an internal combustion engine comprising the steps of: compressing intake air to a pressure between 15 and 30 inches of mercury, moving said intake air through a heat extraction device to remove at least a portion of the heat of compression, moving said intake air into a main combustion chamber of such internal combustion engine, moving a portion of said intake air into a jet cell ignition chamber having an internal volume less than 3% of the clearance volume of such main combustion chamber, injecting a paraffinic hydrocarbon fuel into such jet cell ignition chamber to form a mixture richer than a stoichiometric mixture, further compressing said intake air and said mixture, injecting a paraffinic hydrocarbon fuel into such main combustion chamber while further compressing said intake air and said mixture to form a mixture within such main combustion chamber leaner than a stoichiometric ratio, igniting said mixture in such jet cell ignition chamber before full compression of said mixtures is achieved to form a stream of hot gases, and projecting said stream of hot gases into said mixture within such main combustion chamber to ignite said just recited mixture, whereby the products of combustion include total nitric oxide and nitrogen dioxide constituents of less than 350 parts per million.
Claim 2
Independent Claim
214 words
The method of operating an internal combustion engine comprising the steps of: compressing intake air to a pressure between 15 and 30 inches of mercury, moving said intake air through a heat extraction device to remove at least a portion of the heat of compression, moving said intake air into a main combustion chamber of such internal combustion engine, moving a portion of said intake air into a jet cell ignition chamber having an internal volume less than 3% of the clearance volume of such main combustion chamber, injecting a paraffinic hydrocarbon fuel into such jet cell ignition chamber to form a mixture richer than a stoichiometric mixture, further compressing said intake air and said mixture, injecting a paraffinic hydrocarbon fuel into such main combustion chamber while further compressing said intake air and said mixture to form a mixture within such main combustion chamber leaner than a stoichiometric ratio, igniting said mixture in such jet cell ignition chamber before full compression of said mixtures is achieved to form a stream of hot gases, and projecting said stream of hot gases into said mixture within such main combustion chamber to ignite said just recited mixture, whereby the products of combustion include total nitric oxide and nitrogen dioxide constituents of less than 350 parts per million.
Claim 3
Dependent Claim
32 words
The method of claim 1, wherein the stoichiometric weight ratio of said mixture in such jet cell combustion chamber just prior to ignition is between 12.5 to 1 and 14 to 1.
Claim 4
Dependent Claim
31 words
The method of claim 1, wherein the stoichiometric weight ratio of said mixture in such main combustion chamber just prior to ignition is between 18 to 1 and 22.5 to 1.
Claim 5
Dependent Claim
23 words
The method of claim 1, wherein energy of said removed products of combustion is utilized to perform said step of compressing intake air.
Claim 6
Dependent Claim
22 words
The method of claim 1, wherein each of said steps occurs once during each reciprocating cycle of the piston of such engine.
Claim 7
Dependent Claim
15 words
The method of claim 1, wherein said paraffinic hydrocarbon fuel comprises substantially ethane and methane.
Claim 8
Independent Claim
253 words
The method of operating a two cycle internal combustion engine comprising the steps of: compressing intake air to a pressure between 15 and 30 inches of mercury, reducing the temperature of such compressed intake air, moving said compressed intake air into a main combustion chamber of such internal combustion engine, moving less than about 3% of said compressed air into a jet cell ignition chamber, supplying natural gas fuel to such engine in quantities less than about 7300 BTU/horsepower hour, injecting a portion of said natural gas fuel into such jet cell ignition chamber to form a mixture having a stoichiometric weight ratio between 12.5 to 1 and 14 to 1, further compressing said intake air and said mixture to a pressure above 500 p.s.i., injecting the remaining portion of said natural gas fuel into such main combustion chamber while further compressing said intake air and said mixture to form a mixture within such main combustion chamber having a stoichiometric weight ratio between 18 to 1 and 22.5 to 1, igniting said mixture in such jet cell ignition chamber before full compression of said mixture is achieved to form a stream of hot gases, projecting said stream of hot gases into said mixture within such main combustion chamber to ignite said just recited mixture and, removing substantially all the products of combustion from such main combustion chamber and such jet cell ignition chamber, whereby said products of combustion typically include less than 350 parts per million total nitric oxide and nitrogen dioxide constituents.
Claim 9
Independent Claim
253 words
The method of operating a two cycle internal combustion engine comprising the steps of: compressing intake air to a pressure between 15 and 30 inches of mercury, reducing the temperature of such compressed intake air, moving said compressed intake air into a main combustion chamber of such internal combustion engine, moving less than about 3% of said compressed air into a jet cell ignition chamber, supplying natural gas fuel to such engine in quantities less than about 7300 BTU/horsepower hour, injecting a portion of said natural gas fuel into such jet cell ignition chamber to form a mixture having a stoichiometric weight ratio between 12.5 to 1 and 14 to 1, further compressing said intake air and said mixture to a pressure above 500 p.s.i., injecting the remaining portion of said natural gas fuel into such main combustion chamber while further compressing said intake air and said mixture to form a mixture within such main combustion chamber having a stoichiometric weight ratio between 18 to 1 and 22.5 to 1, igniting said mixture in such jet cell ignition chamber before full compression of said mixture is achieved to form a stream of hot gases, projecting said stream of hot gases into said mixture within such main combustion chamber to ignite said just recited mixture and, removing substantially all the products of combustion from such main combustion chamber and such jet cell ignition chamber, whereby said products of combustion typically include less than 350 parts per million total nitric oxide and nitrogen dioxide constituents.
Claim 10
Independent Claim
214 words
The method of operating an internal combustion engine comprising the steps of: turbocharging intake air to a pressure between 15 and 30 inches of mercury, reducing the temperature of such intake air by passing it through a heat extraction device, moving said turbocharged intake air into a main combustion chamber and an ignition cell of such internal combustion engine, said air in such ignition cell having a volume of less than 3% of the air in the clearance volume of such main combustion chamber, injecting a paraffinic hydrocarbon fuel into such ignition cell to form a mixture having a stoichiometric weight ratio between 12.5 to 1 and 14 to 1, further compressing said intake air and said mixture to a pressure above 500 p.s.i., supplying a paraffinic hydrocarbon fuel to such main combustion chamber to form a mixture within such main combustion chamber having a stoichiometric weight ratio between 18 to 1 and 22.5 to 1, igniting said mixture in such jet cell combustion chamber before full compression of said mixture is achieved, projecting said ignited mixture into said mixture within such main combustion chamber to ignite said just recited mixture and, whereby such operation produces products of combustion having total nitric oxide and nitrogen dioxide constituents of less than 350 parts per million.
Claim 11
Independent Claim
214 words
The method of operating an internal combustion engine comprising the steps of: turbocharging intake air to a pressure between 15 and 30 inches of mercury, reducing the temperature of such intake air by passing it through a heat extraction device, moving said turbocharged intake air into a main combustion chamber and an ignition cell of such internal combustion engine, said air in such ignition cell having a volume of less than 3% of the air in the clearance volume of such main combustion chamber, injecting a paraffinic hydrocarbon fuel into such ignition cell to form a mixture having a stoichiometric weight ratio between 12.5 to 1 and 14 to 1, further compressing said intake air and said mixture to a pressure above 500 p.s.i., supplying a paraffinic hydrocarbon fuel to such main combustion chamber to form a mixture within such main combustion chamber having a stoichiometric weight ratio between 18 to 1 and 22.5 to 1, igniting said mixture in such jet cell combustion chamber before full compression of said mixture is achieved, projecting said ignited mixture into said mixture within such main combustion chamber to ignite said just recited mixture and, whereby such operation produces products of combustion having total nitric oxide and nitrogen dioxide constituents of less than 350 parts per million.
Claim 12
Dependent Claim
22 words
The method of claim 8, wherein each of said steps occurs once during each reciprocating cycle of a piston of such engine.
Claim 13
Dependent Claim
16 words
The method of claim 8, wherein the compression ratio of such engine is greater than 6:1.
Claim 14
Dependent Claim
25 words
The method of claim 1 or claim 8 wherein such paraffinic hydrocarbon fuel is supplied to such engine at less than about 7300 BTU/horsepower hour.
Claim 15
Independent Claim
146 words
The method of operating a two cycle internal combustion engine comprising the steps of: compressing air to a pressure between about 15 to 30 inches of mercury, reducing the temperature of such compressed air, providing such compressed air to a main and an auxiliary combustion chamber of such engine, such auxiliary combustion chamber having a volume of less than 3% of the clearance volume of such main combustion chamber, providing a paraffinic hydrocarbon fuel to such auxiliary combustion chamber to form a mixture richer than a stoichiometric mixture, providing a paraffinic hydrocarbon fuel to such main combustion chamber to form a mixture leaner than a stoichiometric mixture, igniting said mixture in such auxiliary combustion chamber, directing said ignited mixture into said mixture in such main combustion chamber to ignite said just recited mixture, and removing substantially all of the combustion products from such main combustion chamber.
Claim 16
Independent Claim
146 words
The method of operating a two cycle internal combustion engine comprising the steps of: compressing air to a pressure between about 15 to 30 inches of mercury, reducing the temperature of such compressed air, providing such compressed air to a main and an auxiliary combustion chamber of such engine, such auxiliary combustion chamber having a volume of less than 3% of the clearance volume of such main combustion chamber, providing a paraffinic hydrocarbon fuel to such auxiliary combustion chamber to form a mixture richer than a stoichiometric mixture, providing a paraffinic hydrocarbon fuel to such main combustion chamber to form a mixture leaner than a stoichiometric mixture, igniting said mixture in such auxiliary combustion chamber, directing said ignited mixture into said mixture in such main combustion chamber to ignite said just recited mixture, and removing substantially all of the combustion products from such main combustion chamber.
Claim 17
Dependent Claim
18 words
The method of claim 12, wherein products of combustion are utilized to provide energy to compress such air.
Claim 18
Dependent Claim
15 words
The method of claim 12, wherein such paraffinic hydrocarbon fuel comprises substantially ethane and methane.
Claim 19
Dependent Claim
22 words
The method of claim 12 wherein such paraffinic hydrocarbon fuel is supplied to such engine at less than about 7300 BTU/horsepower hour.
References Cited (Backward Citations)
US2773490A
Cited
US2723653A
Cited
US2763248A
Cited
US2849992A
Cited
US2799255A
Cited
US2936575A
Cited
US3029594A
Cited
US3650255A
Cited
US3680305A
Cited
US3890942A
Cited
US3937188A
Cited
US3983847A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-12-21 | 1985-06-22 | 1985-12-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-12-21 | 1989-06-22 | 1989-12-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-12-21 | 1993-06-22 | 1993-12-22 | $7700.00 | Window Closed / Lapsed |