US4651693A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Swirl control arrangement for internal combustion engine
Assignee: Nissan Motor Co Ltd
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Filing: 1986-04-07
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Granted: 1987-03-24
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Expires: 2006-04-07
Abstract
Abstract In order to accurately control the operation of the engine while still achieving near optimal swirl rate control, the swirl is controlled by a valve which is separate from the engine throttle valve and which is basically controlled in response to the pressure prevailing across the same. Various operating parameters such as the instant air-fuel ratio of the charge being combusted in the combustion chambers are utilized to modify prerecorded values to those which will induce the best setting for the valve.
Inventors
- 👤 Yasuo Nakajima
- 👤 Tooru Yoshimura
- 👤 Katsunori Terakasa
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 03:01
CPC Classifications
F; F02; F02B; F02B31/00; F02B31/08; F02B31/085; F02D; F02D41/00; F02D41/0002; F02D2041/0015; F02D9/00; F02D9/08; F02D9/12; F02D9/14; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
197 words
In an internal combustion engine having a combustion chamber; an induction system comprising: an induction passage leading to the combustion chamber; means for forming and air fuel mixture in one of said combustion chamber and said induction passage; an inlet valve which controls communication between said combustion chamber and said induction passage; a throttle valve disposed in said induction passage for controlling the amount of air which is inducted into said combustion chamber when said inlet valve is open; a swirl control valve disposed in said induction passage downstream of said throttle valve; a first sensor for sensing the pressure differential between the section of said induction passage upstream of said swirl control valve and the section of said induction passage downstream of said swirl control valve; a second sensor for sensing the air-fuel ratio of the air-fuel mixture being combusted in the combustion chamber; a servo for controlling the position of said swirl control valve; and a control circuit responsive to said first and second sensors for controlling said servo in a manner to optimize the swirl generation within the combustion chamber for the air-fuel ratio of the air-fuel mixture being combusted in said combustion chamber.
Claim 2
Dependent Claim
197 words
In an internal combustion engine having a combustion chamber; an induction system comprising: an induction passage leading to the combustion chamber; means for forming and air fuel mixture in one of said combustion chamber and said induction passage; an inlet valve which controls communication between said combustion chamber and said induction passage; a throttle valve disposed in said induction passage for controlling the amount of air which is inducted into said combustion chamber when said inlet valve is open; a swirl control valve disposed in said induction passage downstream of said throttle valve; a first sensor for sensing the pressure differential between the section of said induction passage upstream of said swirl control valve and the section of said induction passage downstream of said swirl control valve; a second sensor for sensing the air-fuel ratio of the air-fuel mixture being combusted in the combustion chamber; a servo for controlling the position of said swirl control valve; and a control circuit responsive to said first and second sensors for controlling said servo in a manner to optimize the swirl generation within the combustion chamber for the air-fuel ratio of the air-fuel mixture being combusted in said combustion chamber.
Claim 3
Dependent Claim
93 words
An induction system as claimed in claim 1, wherein said swirl control valve takes the form of a sliding valve comprised of a flat valve element reciprocatively disposed in a rack, said valve element being formed with an aperture through which air flows; said valve element being operatively connected with said servo to be moved in said rack in a manner that said aperture is selectively moved to a position with respect to said induction passage wherein a throttling effect is produced which accelerates the flow of air passing through said induction passage.
Claim 4
Dependent Claim
40 words
An induction system as claimed in claim 1, wherein said air-fuel mixture forming means takes the form of a fuel injector which is arranged to inject fuel into said induction passage at a location downstream of said swirl control valve.
Claim 5
Dependent Claim
163 words
An induction system as claimed in claim 1, further including: a third sensor for sensing the rotational speed of the engine; a fourth sensor for sensing the load on said engine; and a fifth sensor for sensing a temperature which varies with the temperature of the engine; said control circuit containing means responsive to said first, second, third, fourth and fifth sensors for: determining the pressure differential which, if induced between said upstream and downstream sections of said induction passage, will produce the optimal swirl for the instant set of operating conditions; determining a correction factor which will bring the instant air-fuel mixture to a value deemed optimal for the instant set of operating conditions; modifying the value of determined pressure differential using said correction factor to determine a target pressure diffential and outputting a control signal to said servo which will cause said swirl control valve to assume a position wherein the instant pressure differential will be changed toward the target value.
Claim 6
Independent Claim
151 words
A method of operating an internal combustion engine comprising the steps of: forming an air fuel mixture in one of an induction conduit leading to a combustion chamber of the engine or in the combustion chamber; controlling the amount of air which passes through said induction passage using a throttle valve; inducing a swirl in said combustion chamber by introducing the flow of fluid which flows through said induction passage into said combustion chamber in a predetermined manner; controlling the intensity of the swirl using a swirl control valve which is disposed in said induction passage between said combustion chamber and said throttle valve; controlling the position of said swirl control valve using a control circuit which is responsive to the pressure differential which prevail between the section of said induction passage upstream of said swirl control valve and the section of said induction passage downstream of said swirl control valve.
Claim 7
Independent Claim
151 words
A method of operating an internal combustion engine comprising the steps of: forming an air fuel mixture in one of an induction conduit leading to a combustion chamber of the engine or in the combustion chamber; controlling the amount of air which passes through said induction passage using a throttle valve; inducing a swirl in said combustion chamber by introducing the flow of fluid which flows through said induction passage into said combustion chamber in a predetermined manner; controlling the intensity of the swirl using a swirl control valve which is disposed in said induction passage between said combustion chamber and said throttle valve; controlling the position of said swirl control valve using a control circuit which is responsive to the pressure differential which prevail between the section of said induction passage upstream of said swirl control valve and the section of said induction passage downstream of said swirl control valve.
Claim 8
Dependent Claim
144 words
A method as claimed in claim 5, further comprising the steps of: sensing the air-fuel ratio of the air-fuel mixture being combusted in said combustion chamber; sensing the rotational speed of the engine; sensing the load on said engine; sensing a temperature which varies with the temperature of said engine; deriving a pressure differential value which, if induced between said upstream and downstream sections of said induction passage, will induce the optimal swirl rate in said combustion chamber; deriving a correction factor which will bring the instant air-fuel ratio to a value predetermined to be suitable for the instant set of operating conditions; modifying the derived pressure differential using said correction factor; using the modified pressure differential as a target value; and controlling the position of said swirl control valve in a manner which varies the pressure differential prevaling thereacross toward said target value.
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) | 1990-03-23 | 1990-09-22 | 1991-03-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-23 | 1994-09-22 | 1995-03-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-23 | 1998-09-22 | 1999-03-24 | $7700.00 | Window Closed / Lapsed |