Supplementary air assembly for an engine
10247148 ยท 2019-04-02
Assignee
Inventors
Cpc classification
F02M35/10072
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/1055
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B31/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10131
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10275
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1045
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02B27/006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B31/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2009/0213
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10255
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/116
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M35/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B27/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An internal combustion engine includes a crankcase including a crankshaft and at least one cylinder coupled to the crankcase. The at least one cylinder has an intake port and defines an internal combustion chamber. The engine further includes a throttle body assembly with a throttle valve coupled to the intake port of the at least one cylinder and a throttle plate. Additionally, the engine includes a supplementary air inlet fluidly coupled to the intake port and spaced apart from the throttle valve. The supplementary air inlet is configured to receive a flow of air from a location downstream of the throttle plate when the throttle plate is in a fully closed position and the flow of air is directed into the combustion chamber through the intake port for combustion therein.
Claims
1. An internal combustion engine comprising: a crankcase including a crankshaft; at least one cylinder coupled to the crankcase and defining an internal combustion chamber; an air intake system comprising an air inlet and an intake port of the at least one cylinder; a throttle body assembly having a throttle valve coupled to the air inlet and including a throttle plate; a supplementary air inlet fluidly coupled to the intake port, and configured to receive a flow of air from the air intake system from a location downstream of the throttle plate of the at least one cylinder, and the flow of air is directed into the intake port of the at least one cylinder for combustion within the combustion chamber and the flow of air is controlled and modulated by the position of the throttle plate; wherein the throttle body having a plurality of apertures extending through a wall of the throttle body, wherein at least a portion of the plurality of apertures are positioned downstream from the throttle plate when the throttle plate is in the fully closed position, and wherein a portion of the apertures are configured to receive air when the throttle plate is in a first position and each of the apertures receives air when the throttle plate is in a second position.
2. The engine of claim 1, wherein the flow of air is received through a supplementary air tube having first and second ends.
3. The engine of claim 2, wherein the first end of the supplementary air tube is positioned to direct air flow into the intake port and a second end is positioned adjacent to the throttle valve.
4. The engine of claim 3, wherein the supplementary air tube is positioned on a single cylinder.
5. The engine of claim 1, wherein at least a portion of the plurality of apertures are positioned upstream from the throttle plate when the throttle plate is in the fully closed position.
6. The engine of claim 1, wherein the at least one cylinder includes a plurality of cylinders, and a first supplementary air tube extends between a supplementary air inlet of one of the cylinders and an air inlet of another cylinder, and a second supplementary air tube extends between a supplementary air inlet of one of the cylinders and an air inlet of another cylinder.
7. The engine of claim 6, further comprising a third supplementary air tube which extends between a supplementary air inlet of one of the cylinders and an air inlet of another cylinder.
8. The engine of claim 1, further comprising a one-way valve positioned for directional flow of air.
9. The engine of claim 1, wherein operation of the throttle body assembly is electronically controlled by an engine control unit.
10. The engine of claim 1, wherein the at least one cylinder includes a plurality of cylinders, and a first end of a first supplementary air tube is fluidly coupled to a supplementary air inlet of one cylinder and a second end of the first supplementary air tube is fluidly coupled to a supplementary air inlet of another cylinder.
11. The engine of claim 10, wherein the first and second ends of the first supplementary air tube are positioned in respective intake ports of the two cylinders.
12. The engine of claim 11, wherein the engine is a V-twin configuration.
13. The engine of claim 11, wherein the at least one cylinder further includes at least a third cylinder and a fourth cylinder, and a first end of a second supplementary air tube is fluidly coupled to a supplementary air inlet of the third cylinder and a second end of the second supplementary air tube is fluidly coupled to a supplementary air inlet of the fourth cylinder.
14. The engine of claim 13, wherein the first and second ends of the second supplementary air tube are positioned in respective intake ports of the third and fourth cylinders.
15. The engine of claim 14, wherein a length of the second supplementary air tube is greater than a length of the first supplementary air tube.
16. An internal combustion engine, comprising: a crankcase including a crankshaft; at least one cylinder coupled to the crankcase and having an intake port and the at least one cylinder defining an internal combustion chamber; a throttle body assembly having a throttle valve coupled to an air inlet of the at least one cylinder and including a throttle plate; a supplementary air inlet fluidly coupled to the intake port, wherein the supplementary air inlet is configured to receive a flow of air from a location downstream of the throttle plate of the at least one cylinder, and the flow of air is directed into the intake port of the at least one cylinder for combustion within the combustion chambers wherein the throttle body includes a plurality of apertures extending through a wall of the throttle body and open into the air inlet adjacent to the throttle plate, and wherein at least a portion of the plurality of apertures are positioned downstream from the throttle plate when the throttle plate is in the fully closed position, and wherein a portion of the apertures are configured to receive air when the throttle plate is in a first position and each of the apertures receives air when the throttle plate is in a second position.
17. The engine of claim 16, wherein the flow of air is received through a supplementary air tube having first and second ends.
18. The engine of claim 17, wherein the first end of the supplementary air tube is positioned to direct air flow into the intake port and a second end is positioned adjacent to the throttle valve.
19. The engine of claim 18, wherein the first and second ends of the first supplementary air tube are positioned in respective intake ports of the two cylinders.
20. The engine of claim 19, wherein the engine is a V-twin configuration.
21. The engine of claim 17, wherein the supplementary air tube is positioned on a single cylinder.
22. The engine of claim 16, wherein the flow of air received within the supplementary air inlet is controlled by movement of the throttle plate.
23. The engine of claim 16, wherein operation of the throttle body assembly is electronically controlled by an engine control unit.
24. The engine of claim 16, wherein the at least one cylinder includes a plurality of cylinders and a first supplementary air tube extends between a supplementary air inlet of one of the cylinders and an air inlet of another cylinder, and a second supplementary air tube extends between a supplementary air inlet of one of the cylinders and an air inlet of another cylinder.
25. The engine of claim 24, further comprising a third supplementary air tube which extends between a supplementary air inlet of one of the cylinders and an air inlet of another cylinder.
26. The engine of claim 16, further comprising a one-way valve positioned for directional flow of air.
27. The engine of claim 16, wherein the at least one cylinder includes a plurality of cylinders, and a first end of a first supplementary air tube is fluidly coupled to a supplementary air inlet of one cylinder and a second end of the first supplementary air tube is fluidly coupled to a supplementary air inlet of another cylinder.
28. The engine of claim 16, wherein the at least one cylinder further includes at least a third cylinder and a fourth cylinder, and a first end of a second supplementary air tube is fluidly coupled to a supplementary air inlet of the third cylinder and a second end of the second supplementary air tube is fluidly coupled to a supplementary air inlet of the fourth cylinder.
29. The engine of claim 28, wherein a length of the second supplementary air tube is greater than a length of the first supplementary air tube.
30. The engine of claim 28, wherein the first and second ends of the second supplementary air tube are positioned in respective intake ports of the third and fourth cylinders.
31. An internal combustion engine, comprising: a crankcase including a crankshaft at least one cylinder coupled to the crankcase and having an intake port and the at least one cylinder defining an internal combustion chamber; a throttle body assembly having a throttle valve coupled to an air inlet of the at least one cylinder and including a throttle plate; a supplementary air inlet fluidly coupled to the intake port, wherein the supplementary air inlet is configured to receive a flow of air from a location downstream of the throttle plate of the at least one cylinder, and the flow of air is directed into the intake port of the at least one cylinder for combustion within the combustion chamber; wherein the throttle body includes a plurality of apertures extending through a wall of the throttle body and open into the air inlet adjacent to the throttle plate, and wherein at least a portion of the plurality of apertures are positioned upstream from the throttle plate when the throttle plate is in the fully closed position.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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(11) Corresponding reference characters indicate corresponding parts throughout the several views. Unless stated otherwise the drawings are proportional.
DETAILED DESCRIPTION
(12) The embodiments disclosed below are not intended to be exhaustive or to limit the invention to the precise forms disclosed in the following detailed description. Rather, the embodiments are chosen and described so that others skilled in the art may utilize their teachings. It should be understood that the invention may have application to various types of engine-driven equipment, such as, but not limited to generators, construction equipment, utility equipment, all-terrain vehicles, motorcycles, watercraft, utility vehicles, scooters, golf carts, automobiles, aircraft, and mopeds, or any other device or vehicle with a spark-ignited, four-stroke engine.
(13) An illustrative embodiment of an internal combustion engine 2 is shown in
(14) Referring to
(15) Additionally, as shown in
(16) In one embodiment, throttle body assembly 20 also includes an outlet 28 coupled to body portion 24, as shown in
(17) Referring still to
(18) As shown in
(19) Referring to
(20) However, when engine 2 is operating but the throttle input does not require opening throttle valve 22 to the fully open position D, for example when engine 2 is operating at low loads or at idle, ECU 30 transmits a signal to throttle body assembly 20 and throttle plate 26 may be opened to a first intermediate position B, a second intermediate position C, or any position between fully closed position A and fully open position D. As such, when throttle plate 26 is at least partially opened, at least one aperture 32 is now upstream of throttle plate 26 and may be exposed and a portion of air in throttle valve 22 flows through the exposed aperture(s) 32. The position of throttle plate 26 may affect which apertures 32 receive air and/or the quantity of air received through apertures 32 such that the position of throttle plate 26 modulates and controls air flow through supplementary air assembly 40. The portion of air received through the exposed, upstream aperture(s) 32 then flows through outlet 28, into supplementary air tube 44, through supplementary air inlet 42, into intake port 14, and then into combustion chamber 10. In this way, combustion still occurs in combustion chamber 10 even when engine 2 is at a low loads or at idle and the flow of air through apertures 32 is controlled and modulated by the position of throttle plate 26 and operation of throttle body assembly 20. Furthermore, in the embodiment of
(21) When air is in throttle valve 22, air flows toward combustion chamber 10. However, to prevent air from flowing in the opposite direction within supplementary air tube 44 (i.e., towards throttle valve 22), a one-way valve 48 (
(22) It should be understood that the embodiments of
(23) Referring to
(24) Throttle body assembly 20 is fluidly coupled to a supplementary air assembly 40 which includes supplementary air inlet 42 fluidly coupled to intake port 14 and supplementary air tubes 44.sub.1, 44.sub.2, 44.sub.3 corresponding to cylinders 6.sub.1, 6.sub.2, 6.sub.3, respectively. More particularly, supplementary air tube 44.sub.1 has a first end 44a.sub.1 coupled to supplementary air inlet 42 of cylinder 6.sub.1 and a second end 44b.sub.1 which extends into body portion 24 of cylinder 6.sub.3 and is downstream of throttle plate 26. Additionally, supplementary air tube 44.sub.2 has a first end 44a.sub.2 coupled to supplementary air inlet 42 of cylinder 6.sub.2 and a second end 44b.sub.2 which extends into body portion 24 of cylinder 6.sub.1 and is downstream of throttle plate 26. Supplementary air tube 44.sub.3 has a first end 44a.sub.3 coupled to supplementary air inlet 42 of cylinder 6.sub.3 and a second end 44b.sub.3 which extends into body portion 24 of cylinder 6.sub.2 and is downstream of throttle plate 26. As such, cylinder 6.sub.1, 6.sub.2, 6.sub.3 are fluidly coupled to each other through supplementary air assembly 40. In one embodiment, a one-way valve 48, such as a reed valve, is positioned within any of supplementary air tubes 44.sub.1, 44.sub.2, 44.sub.3 to control the direction of air flow therein.
(25) In operation, the combustion cycles of cylinders 6.sub.1, 6.sub.2, 6.sub.3 are out of phase with each other such that when one of cylinders 6.sub.1, 6.sub.2, 6.sub.3 is in one stroke of the combustion cycle (e.g., the power stroke), the other cylinders 6.sub.1, 6.sub.2, 6.sub.3 are in a different stroke (e.g., intake stroke, exhaust stroke, etc.). Because cylinders 6.sub.1, 6.sub.2, 6.sub.3 are out of phase with each other, there is a pressure difference between intake ports of cylinders 6.sub.1, 6.sub.2, 6.sub.3, which facilitates air flow between the intake ports of cylinders 6.sub.1, 6.sub.2, 6.sub.3 through supplementary air assembly 40. For example, when pressure is high in the intake port of cylinder 6.sub.1, the pressure in the intake port of cylinder 6.sub.2 is low which facilitates air flow through supplementary air tube 44.sub.2 and into supplementary air inlet 42 of the intake port of cylinder 6.sub.2. Additionally, when pressure is high in the intake port of cylinder 6.sub.2, pressure is low in the intake port of cylinder 6.sub.3 which facilitates air flow through supplementary air tube 44.sub.3 and into supplementary air inlet 42 of cylinder 6.sub.3. Similarly, when pressure is high in the intake port of cylinder 6.sub.3, pressure is low in the intake port of cylinder 6.sub.1 which facilitates air flow through supplementary air tube 44.sub.1 and into supplementary air inlet 42 of cylinder 6.sub.1. In this way, the embodiment of
(26) Referring to
(27) Referring still to
(28) In operation, the combustion cycles of cylinders 6.sub.1, 6.sub.2, 6.sub.3, 6.sub.4 are out of phase with each other such that when one of cylinders 6.sub.1, 6.sub.2, 6.sub.3, 6.sub.4 is in one stroke of the combustion cycle (e.g., the power stroke), the other cylinders 6.sub.1, 6.sub.2, 6.sub.3, 6.sub.4 are in a different stroke (e.g., intake stroke, exhaust stroke, etc.). Because cylinders 6.sub.1, 6.sub.2, 6.sub.3, 6.sub.4 are out of phase with each other, there is a pressure difference between the intake port of cylinders 6.sub.1, 6.sub.2, 6.sub.3, 6.sub.4, which facilitates air flow between the intake port of cylinders 6.sub.1, 6.sub.2, 6.sub.3, 6.sub.4 through supplementary air assembly 40. For example, when pressure is high in the intake port of cylinder 6.sub.1, the pressure in the intake port of cylinder 6.sub.4 is low which facilitates air flow through supplementary air tube 52 and into supplementary air inlet 42 of cylinder 6.sub.4. Similarly, when pressure is high in the intake port of cylinder 6.sub.4, pressure is low in the intake port of cylinder 6.sub.1 which facilitates air flow through supplementary air tube 52 in the opposite direction and into supplementary air inlet 42 of cylinder 6.sub.1. Additionally, when pressure is high in the intake port of cylinder 6.sub.3, pressure is low in the intake port of cylinder 6.sub.2 which facilitates air flow through supplementary air tube 54 and into supplementary air inlet 42 of cylinder 6.sub.2. Similarly, when pressure is high in the intake port of cylinder 6.sub.2, pressure is low in the intake port of cylinder 6.sub.3 which facilitates air flow through supplementary air tube 54 in the opposite direction and into supplementary air inlet 42 of cylinder 63. In this way, the embodiment of
(29) While this invention has been described as having an exemplary design, the present invention may be further modified within the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains.