ENGINE SYSTEM
20170159580 ยท 2017-06-08
Inventors
- Dong Hee Han (Seoul, KR)
- Joowon LEE (Gwangju-si, KR)
- Hyungbok LEE (Seongnam-si, KR)
- Dong Ho CHU (Ansan-si, KR)
- Jong Il Park (Seoul, KR)
Cpc classification
F02D2250/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D23/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/162
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B75/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0087
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B2075/1816
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D17/02
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
F01N13/107
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D17/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B75/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An engine system includes an engine including a plurality of cylinders generating driving torque by combustion of fuel, a cylinder deactivation apparatus (CDA) disposed at one or more of the plurality of cylinders for selectively deactivating the one or more of the plurality of cylinders, a first exhaust manifold connected to cylinders at which the CDA apparatus is disposed, a second exhaust manifold connected to cylinders at which the CDA apparatus is not disposed, a turbocharger including a turbine rotated by exhaust gas exhausted from the first exhaust manifold, and further including a compressor rotated together with the turbine for compressing air supplied to the cylinders, and an electric supercharger including a motor and an electric compressor operated by the motor for supplying compressed air to the cylinders.
Claims
1. An engine system comprising: an engine including a plurality of cylinders generating driving torque by combustion of fuel; a cylinder deactivation apparatus (CDA) disposed at one or more of the plurality of cylinders for selectively deactivating the one or more of the plurality of cylinders; a first exhaust manifold connected to cylinders at which the CDA apparatus is disposed; a second exhaust manifold connected to cylinders at which the CDA apparatus is not disposed; a turbocharger including a turbine rotated by exhaust gas exhausted from the first exhaust manifold, and further including a compressor rotated together with the turbine for compressing air supplied to the cylinders; and an electric supercharger including a motor and an electric compressor operated by the motor for supplying compressed air to the cylinders.
2. The engine system of claim 1, wherein the cylinders are in a four-cylinder engine in which a first cylinder, a second cylinder, a third cylinder, and a fourth cylinder are sequentially disposed, and the CDA apparatus is disposed at the second cylinder and the third cylinder.
3. The engine system of claim 1, wherein the first exhaust manifold is connected to the turbine.
4. The engine system of claim 1, wherein the compressor of the turbocharger and the electric supercharger are disposed at an intake line into which fresh air flows, and an intercooler for cooling the fresh air is disposed at the intake line.
5. The engine system of claim 4, wherein a bypass line for bypassing a part of the air supplied to the electric supercharger is disposed at the intake line, and a bypass valve is disposed at the bypass line.
6. The engine system of claim 1, wherein a first exhaust line connected to the first exhaust manifold and a second exhaust line connected to the second exhaust manifold are joined at a main exhaust line, and an exhaust gas purification apparatus is disposed at the main exhaust line.
7. The engine system of claim 1, wherein the CDA apparatus deactivates some of the cylinders by being operated at a low speed region.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025] The drawings are provided for reference in describing exemplary embodiments of the present disclosure, and the spirit of the present disclosure should not be construed only by the accompanying drawings.
[0026]
[0027]
DETAILED DESCRIPTION
[0028] The present disclosure will be described more fully hereinafter with reference to the accompanying drawings, in which exemplary embodiments of the disclosure are shown. As those skilled in the art would realize, the described embodiments may be modified in various different ways, all without departing from the spirit or scope of the present disclosure.
[0029] In describing the present disclosure, parts that are not related to the description will be omitted. Like reference numerals generally designate like elements throughout the specification.
[0030] In addition, the size and thickness of each configuration shown in the drawings may be arbitrarily shown for better understanding and ease of description, but the present disclosure is not limited thereto. In the drawings, the thickness of layers, films, panels, regions, etc., may be exaggerated for clarity.
[0031] Hereinafter, an engine system according to an exemplary embodiment of the present disclosure will be described in detail with reference to accompanying drawings.
[0032]
[0033] As shown in
[0034] The engine 10 may be a four-cylinder engine having four cylinders. The plurality of cylinders, that is, a first cylinder 11, a second cylinder 12, a third cylinder 13, and a fourth cylinder 14, may be sequentially, and/or linearly disposed. It is also to be understood that more or fewer cylinders, and any arrangement of cylinders, may be used in the engine 10.
[0035] The CDA (cylinder deactivation apparatus) 20 may be disposed at some, or all, of the cylinders, and may selectively deactivate some of the cylinders. When the CDA apparatus 20 is operated, fuel may not be supplied to a deactivated cylinder, and an operation of an intake valve and an exhaust valve may be stopped. The CDA apparatus 20 is widely known in the art, so a more detailed description thereof will not be presented in the present specification.
[0036] The CDA apparatus 20 may be disposed at the second cylinder 12 and the third cylinder 13 among the four cylinders.
[0037] The exhaust manifold may include a first exhaust manifold 31 connected to cylinders at which the CDA apparatus 20 is mounted, and a second exhaust manifold 35 connected to cylinders at which the CDA apparatus 20 is not mounted.
[0038] The first exhaust manifold 31 may be connected to a first exhaust line 33, and the second exhaust manifold 35 may be connected to a second exhaust line 37. The first exhaust line 33 and the second exhaust line 37 may be joined at a main exhaust line 30. An exhaust gas purification apparatus 80 for purifying exhaust gas may be disposed at the main exhaust line 30 where the first exhaust line 33 and the second exhaust line 37 are joined.
[0039] The turbocharger 40 may supply compressed air to the cylinders, and include a turbine 41 rotated by exhaust gas discharged from the cylinder and a compressor 43 rotated by a rotation force of the turbine and compressing intake air. The turbine 41 may be disposed at the first exhaust line 33 and may be operated by exhaust gas exhausted through the first exhaust manifold 31.
[0040] The electric supercharger 50 for supplying compressed air to the cylinder may include the motor 51 and an electric compressor 53. The electric compressor 53 may be operated by the motor 51 and compress intake air, and the compressed intake air may be supplied to the cylinders.
[0041] The compressor 43 of the turbocharger 40 and the electric supercharger 50 may be disposed at an intake line 60 into which external air flows. An air cleaner 68 for filtering external air may be disposed at an inlet of the intake line 60. An intercooler 67 for cooling external air may be disposed at the intake line 60.
[0042] The compressor 43 of the turbocharger 40 may be disposed at an upstream side of the intake line 60, and the electric supercharger 50 may be disposed at a downstream side of the intake line 60. The external air flowing through the intake line 60 may be supplied to the cylinder through an intake manifold 70. A throttle valve 64 may be mounted at the intake manifold 70, and an air amount supplied to the cylinder may be adjusted by an opening of the throttle valve 64.
[0043] A bypass line 62 may be disposed at the intake line 60, and the bypass line 62 may bypass a part of external air supplied to the electric supercharger 50. A bypass valve 66 may be disposed at the bypass line 62. An amount of air supplied by the electric supercharger 50 may be adjusted by opening of the bypass valve 66.
[0044] Hereinafter, an operation of an engine system according to an exemplary embodiment of the present disclosure will be described in detail with reference to accompanying drawings.
[0045]
[0046] In
[0047] Referring to
[0048] Therefore, the engine 10 may be operated as a two-cylinder engine, and compressed air may be supplied to the first cylinder 11 and the fourth cylinder 14 by the electric supercharger 50.
[0049] Further, since exhaust gas discharged from the first cylinder 11 and the fourth cylinder 14 may not pass through the turbocharger 40 and may be discharged to the main exhaust line 30 through the second exhaust manifold 35 and the second exhaust line 37, the back pressure of the engine may be reduced. Therefore, the compression ratio of the first cylinder 11 and the fourth cylinder 14 may be increased, and fuel consumption may be improved.
[0050] Since compressed air may be supplied to the first cylinder 11 and the fourth cylinder 14 by the electric supercharger 50, a driving region (refer to II of
[0051] That is, the A region of
[0052] However, since the CDA apparatus 20 may not be operated at a low speed and high load, the engine may be operated as a four-cylinder engine. At this time, compressed air may be supplied to the cylinder by the electric supercharger 50, and thus the driving region may be expanded at the low speed region. Despite the engine being operated as a four-cylinder engine, an exhaust gas amount discharged from the first cylinder 11 and the fourth cylinder 14 may be low, and thus boosting by the turbocharger 40 may be limited.
[0053] The CDA apparatus may not be operated during a middle speed region in which the engine speed is relatively fast compared to the low speed region, so the engine 10 may be operated as a four-cylinder engine.
[0054] The turbocharger 40 may be operated by exhaust gas discharged from the first cylinder 11 and the fourth cylinder 14, so compressed air may be supplied to the cylinders by the turbocharger 40. Further, compressed air may be also supplied to the cylinders by the electric supercharger 50.
[0055] That is, engine boosting may be performed by the turbocharger 40 and the electric supercharger 50 at the middle speed region.
[0056] The CDA apparatus may not be operated in a high speed region in which the engine speed is relatively fast compared to the middle speed region, so the engine 10 may be operated as a four-cylinder engine.
[0057] The turbocharger 40 may be operated by exhaust gas discharged from the first cylinder 11 and the fourth cylinder 14, so compressed air may be supplied to the cylinders by the turbocharger 40.
[0058] That is, engine boosting may be performed by the turbocharger 40 in the high speed region.
[0059] According to a conventional turbocharger, since a supply amount of exhaust gas may be increased in the high speed region and rotation speed of a turbine wheel of the turbine 41 may deviate from a predetermined tolerance limit, there is a problem that the turbine wheel may become overloaded. To solve the above problem, exhaust gas discharged from the cylinder may be bypassed using a waste gate valve. At this time, about half of the exhaust gas discharged from the four cylinders may be detoured from the turbine 41.
[0060] However, according to an exemplary embodiment of the present disclosure, since the two cylinders (second cylinder 12 and third cylinder 13) are connected to the turbine 41 of the turbocharger 40, there is no need to bypass exhaust gas suppled to the turbine 41 of the turbocharger 40 in the high speed region. Therefore, it is possible to eliminate the waste gate valve disposed in the conventional turbocharger, and the manufacturing costs of the vehicle can be reduced.
[0061] As described above, the engine system according to an exemplary embodiment of the present disclosure may be selectively operated as a two-cylinder engine or a four-cylinder engine by the CDA apparatus 20. Therefore, since the engine system is operated as a two-cylinder engine in the low speed region, unnecessary pumping losses are reduced and fuel consumption of the vehicle may be improved.
[0062] Further, since some of the cylinders (second cylinder 12 and third cylinder 13) may be deactivated in the low speed region and exhaust gas discharged from the active cylinders (first cylinder 11 and fourth cylinder 14) may not pass through the turbocharger 40, back pressure of the engine may be reduced and a high compression ratio may be realized.
[0063] While this disclosure has been described in connection with what is presently considered to be practical exemplary embodiments, it is to be understood that the disclosure is not limited to the disclosed embodiments, but, on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.