US4176649A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Emission control
Assignee: Toyota Motor Corp
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Filing: 1978-09-25
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Granted: 1979-12-04
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Expires: 1998-09-25
Abstract
Abstract An internal combustion engine and a method of operating same, comprising a combustion chamber having main and auxiliary sections. The air-fuel mixture compressed in the combustion chamber causes turbulence and swirling of the mixture in the auxiliary section. On ignition, the initial combustion rate in the auxiliary section is limited by the centrifugal force on the flame. The jet of gases rushing out of the auxiliary section is not swirled and controls the rate of burning in the main section to reduce peak flame temperature and hence, to reduce CO, NO x and HC emissions.
Inventors
- 👤 Bela Karlovitz
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 21:40
CPC Classifications
F; F02; F02B; F02B19/00; F02B19/08; F02B19/12; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
331 words
A method of operating an internal combustion spark ignition engine having at least one cylinder and a reciprocating piston therein defining a combustion chamber, said combustion chamber being divided into main and auxiliary sections, there being an orifice disposed between the main and auxiliary sections and arranged on a central axis of the auxiliary section, the cross-sectional area of the orifice being smaller than the cross-sectional area of the auxiliary section, comprising the steps of: introducing a combustible mixture to the combustion chamber; compressing the combustible mixture in the combustion chamber and thereby forcing part of the mixture in the main section through the orifice into the auxiliary section; creating turbulence and swirl of the combustible mixture about the axis of and within the auxiliary section for forcing the lighter components of the combustible mixture into the area along the axis by centrifugal force; igniting the combustible mixture located along the axis of the auxiliary section within the auxiliary section of the combustion chamber from an ignition source, said swirl causing heavier uncombusted components of the combustible mixture to be forced to the peripheral areas of the auxiliary section; causing a controlled rise in the pressure in the auxiliary section to rapidly inject into the main section a burning jet of the combustible mixture located along the central axis of the auxiliary section; causing a gradual propagation of the flame of the ignited mixture toward the periphery of the swirled combustible mixture in the auxiliary section to burn the heavier uncombusted portions of the combustible mixture and to continue to inject a long-burning jet into the main section; and causing the burning jet to escape through the orifice substantially without swirling motion into the main section creating sufficient turbulence therein to cause part of the mixture to burn at substantially constant volume followed by a substantially constant pressure burning of the rest of the mixture whereby the peak temperature of the cycle is limited and the NO x emissions are reduced.
Claim 2
Independent Claim
331 words
A method of operating an internal combustion spark ignition engine having at least one cylinder and a reciprocating piston therein defining a combustion chamber, said combustion chamber being divided into main and auxiliary sections, there being an orifice disposed between the main and auxiliary sections and arranged on a central axis of the auxiliary section, the cross-sectional area of the orifice being smaller than the cross-sectional area of the auxiliary section, comprising the steps of: introducing a combustible mixture to the combustion chamber; compressing the combustible mixture in the combustion chamber and thereby forcing part of the mixture in the main section through the orifice into the auxiliary section; creating turbulence and swirl of the combustible mixture about the axis of and within the auxiliary section for forcing the lighter components of the combustible mixture into the area along the axis by centrifugal force; igniting the combustible mixture located along the axis of the auxiliary section within the auxiliary section of the combustion chamber from an ignition source, said swirl causing heavier uncombusted components of the combustible mixture to be forced to the peripheral areas of the auxiliary section; causing a controlled rise in the pressure in the auxiliary section to rapidly inject into the main section a burning jet of the combustible mixture located along the central axis of the auxiliary section; causing a gradual propagation of the flame of the ignited mixture toward the periphery of the swirled combustible mixture in the auxiliary section to burn the heavier uncombusted portions of the combustible mixture and to continue to inject a long-burning jet into the main section; and causing the burning jet to escape through the orifice substantially without swirling motion into the main section creating sufficient turbulence therein to cause part of the mixture to burn at substantially constant volume followed by a substantially constant pressure burning of the rest of the mixture whereby the peak temperature of the cycle is limited and the NO x emissions are reduced.
Claim 3
Dependent Claim
42 words
The method according to claim 1 in which the compression ratio is typically 10:1 and the ratio of the pressure at the start of the constant volume burning to the pressure at the end of the constant volume burning is typically 1:2.
Claim 4
Dependent Claim
21 words
The method according to claim 1 in which ignition is started at the end of the auxiliary section opposite the orifice.
Claim 5
Dependent Claim
29 words
The method according to claim 1 in which the part of the mixture forced through the orifice is forced past vanes positioned near the orifice to provide the swirl.
Claim 6
Dependent Claim
266 words
In an internal combustion engine having at least one cylinder and a reciprocating piston therein defining a combustion chamber, means for dividing the combustion chamber into a main section and an auxiliary cylindrical section, said dividing means defining an orifice disposed between the main section and the auxiliary section and arranged on the central axis of the auxiliary section, the cross-sectional area of the orifice being smaller than the cross-sectional area of the auxiliary section, means for introducing a combustible mixture into the combustion chamber, the ratio of the volume of the main and auxiliary sections and the size of the orifice being selected such that, during the compression cycle, part of the combustible mixture of fuel and air rushes into the auxiliary section causing turbulence, the improvement comprising: means to cause the combustible mixture in the auxiliary section to swirl about the axis in the auxiliary section and to force heavier uncombusted components of the combustible mixture to the peripheral areas of the auxiliary section; and means for igniting a long-lasting and steady jet comprising a spark plug in the combustion chamber located on the axis of the auxiliary section, wherein after ignition a burning jet of the combustible mixture located on the central axis of the auxiliary section is injected into the main section via the orifice and the flame of the burning gas gradually propagates towards the periphery through the heavier uncombusted components of the swirled combustible mixture in the auxiliary section, said means to cause swirl of the combustible mixture in the auxiliary section causing substantially no swirl in the burning jet.
Claim 7
Dependent Claim
266 words
In an internal combustion engine having at least one cylinder and a reciprocating piston therein defining a combustion chamber, means for dividing the combustion chamber into a main section and an auxiliary cylindrical section, said dividing means defining an orifice disposed between the main section and the auxiliary section and arranged on the central axis of the auxiliary section, the cross-sectional area of the orifice being smaller than the cross-sectional area of the auxiliary section, means for introducing a combustible mixture into the combustion chamber, the ratio of the volume of the main and auxiliary sections and the size of the orifice being selected such that, during the compression cycle, part of the combustible mixture of fuel and air rushes into the auxiliary section causing turbulence, the improvement comprising: means to cause the combustible mixture in the auxiliary section to swirl about the axis in the auxiliary section and to force heavier uncombusted components of the combustible mixture to the peripheral areas of the auxiliary section; and means for igniting a long-lasting and steady jet comprising a spark plug in the combustion chamber located on the axis of the auxiliary section, wherein after ignition a burning jet of the combustible mixture located on the central axis of the auxiliary section is injected into the main section via the orifice and the flame of the burning gas gradually propagates towards the periphery through the heavier uncombusted components of the swirled combustible mixture in the auxiliary section, said means to cause swirl of the combustible mixture in the auxiliary section causing substantially no swirl in the burning jet.
Claim 8
Dependent Claim
21 words
The improvement according to claim 5 wherein the spark plug is at the end of the auxiliary section opposite the orifice.
Claim 9
Dependent Claim
34 words
The improvement according to claim 5 wherein vanes are positioned near the orifice to provide the swirl to the mixture forced into the auxiliary section, said vanes lying outside said area of the orifice.
Claim 10
Dependent Claim
49 words
The improvement according to claim 7 in which the size of the orifice, the size of the auxiliary section and the amount of swirl provided by the vanes, are selected to introduce turbulence to the main section to cause substantially constant volume burning followed by substantially constant pressure burning.
Claim 11
Dependent Claim
20 words
The method according to claim 1 wherein the combustible mixture is introduced to the main section of the combustion chamber.
Claim 12
Dependent Claim
23 words
The method according to claim 1 wherein the combustible mixture is a lean air-fuel mixture having an air-fuel ratio of at least 18.
Claim 13
Dependent Claim
29 words
The method according to claim 1 wherein the compressing step further comprises causing a swirl of the part of the combustible mixture while the part flows through the orifice.
Claim 14
Dependent Claim
42 words
The method according to claim 1 wherein the step of causing a controlled rise in pressure in the auxiliary section controlled by the swirl includes the step of separating the lighter from the heavier gases by the centrifugal force of the swirl.
Claim 15
Dependent Claim
31 words
The improvement according to claim 5 wherein said auxiliary section is in communication with only the main section and wherein all of the combustible mixture is introduced to the main section.
Claim 16
Dependent Claim
42 words
The improvement according to claim 5 wherein the means to cause the gases in the auxiliary section to swirl about the axis in the auxiliary section generates swirl with sufficient centrifugal force to separate lighter from heavier gases in the auxiliary section.
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) | 1982-12-03 | 1983-06-04 | 1983-12-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-12-03 | 1987-06-04 | 1987-12-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-12-03 | 1991-06-04 | 1991-12-04 | $7700.00 | Window Closed / Lapsed |