Internal combustion engine comprising a turbocharger with variability at the compressor inlet
11300043 · 2022-04-12
Assignee
Inventors
Cpc classification
F02M26/51
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/21
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B2037/125
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/225
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/4213
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/0215
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
International classification
F02B37/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An internal combustion engine having a turbocharger with variability at the compressor inlet, and a turbocharger. An internal combustion engine having a turbocharger, and a turbocharger, are described. A device which both performs a change in the cross section of the compressor inlet and brings about an adjustment of the exhaust gas recirculation rate is arranged in the region of the compressor inlet. As a result, the turbocharger is of space-saving and low-cost construction in the compressor inlet region.
Claims
1. An internal combustion engine having a turbocharger with a turbine and a compressor and having an exhaust gas recirculation line, by way of which exhaust gas is recirculated downstream of the turbine of the turbocharger into an intake region upstream of the compressor, wherein a device for changing a cross section of a compressor inlet is provided in the region of the compressor inlet, wherein the device which both performs the change in the cross section of the compressor inlet and brings about an adjustment of an exhaust gas recirculation rate is arranged in the region of the compressor inlet, wherein the device has a first throttle arranged in the region of the compressor inlet and a second throttle arranged downstream at a distance therefrom, between which the recirculated exhaust gas is introduced.
2. The internal combustion engine as claimed in claim 1, wherein the device has a single adjusting member which ensures performance of both functions of the device.
3. The internal combustion engine as claimed in claim 1, wherein the introduction of the recirculated exhaust gas is implemented in by way of an introduction duct or ring.
4. The internal combustion engine as claimed in claim 1, wherein the throttles are actuated by means of a common adjusting ring arranged between them.
5. The internal combustion engine as claimed in claim 4, wherein introduction of the recirculated exhaust gas is accomplished by apertures in the common adjusting ring.
6. The internal combustion engine as claimed in claim 5 wherein webs arranged between the apertures of the adjusting ring have a streamlined configuration.
7. The internal combustion engine as claimed in claim 4, wherein different transmission ratios are provided between the first throttle and the adjusting ring and between the second throttle and the adjusting ring.
8. The internal combustion engine as claimed in claim 4, wherein the common adjusting ring is rotated by means of an actuator in order to adjust the throttles.
9. The internal combustion engine as claimed in claim 1, wherein the throttles include variable iris diaphragms.
10. The internal combustion engine as claimed in claim 9, wherein each iris diaphragm comprises a plurality of rotatably mounted lamellae which can be pivoted inward/outward by rotation of the adjusting ring.
11. The internal combustion engine as claimed in claim 10, wherein bearing points for the rotatable mounting of the lamellae are integrated into the compressor housing/inlet housing.
12. The internal combustion engine as claimed in claim 10, wherein each lamella of an iris diaphragm has a first pin for the rotatable mounting thereof and a second pin, which is guided in a groove of the adjusting ring.
13. The internal combustion engine as claimed claim 9, wherein the variable iris diaphragms are mounted in a cartridge inserted into the compressor housing.
14. The internal combustion engine as claimed in claim 1, wherein a compressor hub extends as far as the first throttle or beyond the latter.
15. The internal combustion engine as claimed in claim 1, wherein the first throttle is designed as a variable cone, and the second throttle is designed as a variable iris diaphragm.
16. The internal combustion engine as claimed in claim 1, wherein introduction of the exhaust gas recirculation is designed as a Venturi nozzle.
17. The internal combustion engine as claimed in claim 1, wherein the device has two throttles, which are adjustable by means of two adjusting rings that can be rotated independently of one another.
18. The internal combustion engine as claimed in claim 17, wherein the two independently rotatable adjusting rings are separated from one another by a partition housing.
19. A turbocharger for an internal combustion engine, the turbocharger including: a turbine; a compressor; an exhaust gas recirculation line by way of which exhaust gas is recirculated downstream of the turbine of the turbocharger into an intake region upstream of the compressor; and a device for changing a cross section of a compressor inlet is positioned in the region of the compressor inlet, the device performs the change in the cross section of the compressor inlet and brings about an adjustment of an exhaust gas recirculation rate, wherein the device has a first throttle arranged in the region of the compressor inlet and a second throttle arranged downstream at a distance therefrom, between which the recirculated exhaust gas is introduced.
Description
DESCRIPTION OF DRAWINGS
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(16) Like reference symbols in the various drawings indicate like elements.
DETAILED DESCRIPTION
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(18) Provided in the inlet region of the compressor is a double throttle, by way of which it is possible both to supply fresh air via the compressor inlet 6 and to regulate the rate of exhaust gas recirculation. This double throttle has a first iris throttle 8 and a second iris throttle 9, arranged downstream thereof, which are designed in the manner of an iris diaphragm and have lamellae, by way of the pivoting of which the opening cross section of the compressor inlet can be reduced or increased.
(19) Here,
(20) Here, the bearing points for the lamellae of the iris throttles 8, 9 are integrated into the adjacent housings, namely the inlet housing and the compressor housing 5.
(21) The example shown in
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(23) As can be seen from
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(26) The sectional view of
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(28) The implementations and examples described and illustrated above make it possible to position the double throttle located close to the compressor directly upstream of the compressor wheel 2. In all cases, the compressor hub 22 extends only to a point upstream of the second iris throttle 9 located close to the compressor, as shown in
(29) To control and optimize the inlet throttles and distribute the EGR mass flow, and to increase compressor efficiency levels when the throttles are closed, it may be advantageous to extend the hub region of the compressor wheel 2 beyond the second iris throttle 9 located close to the compressor, as far as a location upstream of the first throttle 8, as illustrated in
(30) Apart from the normal implementation as a double throttle with a first iris throttle 8 and a second iris throttle 9, which are arranged in series in the inlet region of the compressor, it is possible to combine a variable inlet cone, which then acts as the first throttle, and a variable diaphragm, which then acts as the second throttle.
(31) Yet another example is shown in
(32) Yet another example of a double throttle is illustrated in
(33) A number of implementations have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the disclosure. Accordingly, other implementations are within the scope of the following claims.