US4471616A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Device for regulating the air supply of an internal combustion engine
Assignee: Alpine Racing SAS
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Filing: 1982-08-04
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Granted: 1984-09-18
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Expires: 2002-08-04
Abstract
Abstract In a device for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven in rotation by the engine's exhaust, the intake of the rotating compressor is controlled by an intake regulation (or gating) system capable of reducing the compressive effect of the rotor of the compressor. Control elements of said regulation (or gating) system are connected with the accelerator linkage so as to close the regulation (or gating) system and reduce the compressive effect to the maximum degree when the accelerator moves toward the idling position of the engine.
Inventors
- 👤 Jean-Pierre Boudy
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 20:03
CPC Classifications
F; F02; F02B; F02B37/00; F02B37/12; F02B37/22; F02B37/225; F02B37/24; F02B37/18; F02D; F02D9/00; F02D9/02; F02D2009/0201; F02D2009/0283; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
159 words
A device for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven by engine exhaust and including a compressor, a compressor air intake and a turbine, said engine including air flow control means in an air flow path between said turbo-compressor and the cylinders of said engine, said engine further including accelerator linkage connected to said air flow control means, said device for regulating comprising means in said compressor intake and connected to said accelerator linkage for adjusting the compressive effect of said compressor wherein said means for adjusting are constructed and adapted to reduce said compressive effect as said accelerator linkage moves towards an idle position, wherein said means for adjusting includes means for sensing the fluid pressure in said air flow path downstream from said air flow control means and means responsive to said means for sensing, said means responsive to said means for sensing operating upon said compressor air intake.
Claim 2
Independent Claim
159 words
A device for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven by engine exhaust and including a compressor, a compressor air intake and a turbine, said engine including air flow control means in an air flow path between said turbo-compressor and the cylinders of said engine, said engine further including accelerator linkage connected to said air flow control means, said device for regulating comprising means in said compressor intake and connected to said accelerator linkage for adjusting the compressive effect of said compressor wherein said means for adjusting are constructed and adapted to reduce said compressive effect as said accelerator linkage moves towards an idle position, wherein said means for adjusting includes means for sensing the fluid pressure in said air flow path downstream from said air flow control means and means responsive to said means for sensing, said means responsive to said means for sensing operating upon said compressor air intake.
Claim 3
Dependent Claim
14 words
The device of claim 1 wherein said air flow control means comprise butterfly valves.
Claim 4
Independent Claim
280 words
A device for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven by engine exhaust and including a compressor, a compressor air intake and a turbine, said engine including air flow control means in an air flow path between said turbo-compressor and the cylinders of said engine, said engine further including accelerator linkage connected to said air flow control means, said device for regulating comprising means in said compressor intake and connected to said accelerator linkage for adjusting the compressive effect of said compressor wherein said means for adjusting are constructed and adapted to reduce said compressive effect as said accelerator linkage moves towards an idle position, wherein said compressor air intake includes an annular portion and said means for adjusting comprise: a circumferentially spaced plurality of blades in said annular portion, each of said blades being pivoted on an axis parallel to the axis of said annular portion whereby each of said blades may be pivoted between a radial position and a circumferential position; blade pivoting means connected to said accelerator linkage for pivoting said blades about said axes, wherein said blade pivoting means comprise: a cylinder fixed to said linkage; a piston in said cylinder and fixed to a blade pivoting control element connected between said axes and said piston for pivoting said blades in response to the movement of said piston; means communicating a first portion of the interior of said cylinder on one side of said piston with the fluid pressure in said air flow path downstream from said air flow control means; and spring means in a second portion of said interior on the other side of said piston.
Claim 5
Independent Claim
280 words
A device for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven by engine exhaust and including a compressor, a compressor air intake and a turbine, said engine including air flow control means in an air flow path between said turbo-compressor and the cylinders of said engine, said engine further including accelerator linkage connected to said air flow control means, said device for regulating comprising means in said compressor intake and connected to said accelerator linkage for adjusting the compressive effect of said compressor wherein said means for adjusting are constructed and adapted to reduce said compressive effect as said accelerator linkage moves towards an idle position, wherein said compressor air intake includes an annular portion and said means for adjusting comprise: a circumferentially spaced plurality of blades in said annular portion, each of said blades being pivoted on an axis parallel to the axis of said annular portion whereby each of said blades may be pivoted between a radial position and a circumferential position; blade pivoting means connected to said accelerator linkage for pivoting said blades about said axes, wherein said blade pivoting means comprise: a cylinder fixed to said linkage; a piston in said cylinder and fixed to a blade pivoting control element connected between said axes and said piston for pivoting said blades in response to the movement of said piston; means communicating a first portion of the interior of said cylinder on one side of said piston with the fluid pressure in said air flow path downstream from said air flow control means; and spring means in a second portion of said interior on the other side of said piston.
Claim 6
Dependent Claim
15 words
The device of claim 1 including means for supplying atmospheric pressure to said second portion.
Claim 7
Dependent Claim
21 words
The device of claim 1 including means for supplying the fluid pressure in said compressor air intake to said second portion.
Claim 8
Dependent Claim
14 words
The device of claim 1 wherein said air flow control means comprise butterfly valves.
Claim 9
Independent Claim
172 words
A method for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven by engine exhaust and including a compressor, a compressor air intake having an annular portion, and a turbine, said engine including air flow control means in an air flow path between said turbo-compressor and the cylinders of said engine, said engine further including accelerator linkage connected to said air flow control means, said method comprising: providing on said annular portion a plurality of blades pivotable about an axis parallel with the axis of said annular portion; providing blade pivot control means responsive to said accelerator linkage and the fluid pressure in said air flow path downstream from said air flow control means; and arranging said blade pivot control means such that when said engine is idling, said blades are pivoted towards an oblique alignment relative to said annular portion axis such that inflowing air is rotated in the direction of rotation of said compressor and helps drive said compressor while increasing intake pressure loss.
Claim 10
Independent Claim
172 words
A method for regulating the air supply of an internal combustion engine supercharged by a turbo-compressor unit driven by engine exhaust and including a compressor, a compressor air intake having an annular portion, and a turbine, said engine including air flow control means in an air flow path between said turbo-compressor and the cylinders of said engine, said engine further including accelerator linkage connected to said air flow control means, said method comprising: providing on said annular portion a plurality of blades pivotable about an axis parallel with the axis of said annular portion; providing blade pivot control means responsive to said accelerator linkage and the fluid pressure in said air flow path downstream from said air flow control means; and arranging said blade pivot control means such that when said engine is idling, said blades are pivoted towards an oblique alignment relative to said annular portion axis such that inflowing air is rotated in the direction of rotation of said compressor and helps drive said compressor while increasing intake pressure loss.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-09-18 | 1988-03-19 | 1988-09-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-09-18 | 1992-03-19 | 1992-09-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-09-18 | 1996-03-19 | 1996-09-18 | $7700.00 | Window Closed / Lapsed |