INTERNAL COMBUSTION ENGINE AND METHOD FOR STARTING AN INTERNAL COMBUSTION ENGINE
20180135571 ยท 2018-05-17
Inventors
Cpc classification
Y02T10/30
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
F02D41/0027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/062
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M21/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B33/446
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/162
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10163
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B29/0412
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M35/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Internal combustion engine with at least one turbocharger having a compressor, a bypass valve by means of which the compressor can be bypassed by at least a partial flow of a fuel mixture provided for the combustion, and a control or regulating unit connected to the bypass valve for regulating or controlling a degree of opening of the bypass valve, whereby the control or regulating unit is designed to open and/or at least partially keep open the bypass valve when starting the internal combustion engine.
Claims
1. An internal combustion engine with at least one turbocharger, which has a compressor, a bypass valve, by means of which the compressor can be bypassed at least by a partial flow of a fuel mixture provided for the combustion, and a control or regulating unit connected to a bypass valve for the regulation or control of the degree of opening of the bypass valve, wherein the control or regulating unit is designed to at least partly open, or keep open, the bypass valve when the internal combustion engine is started.
2. The internal combustion engine according to claim 1, wherein exactly one turbocharger is provided.
3. The internal combustion engine according to claim 1, wherein at least two turbochargers are provided, wherein the compressors of the at least two turbochargers are preferably connected in series.
4. The internal combustion engine according to claim 3, wherein the compressors of all the turbochargers of the internal combustion engine can be bypassed at least by a partial flow of the fuel mixture provided for the combustion by means of the bypass valve.
5. The internal combustion engine according to claim 1, wherein a bypass line for bypassing the compressor of the at least one turbocharger is provided, wherein the bypass valve is arranged in the bypass line.
6. The internal combustion engine according claim 1, wherein a bypass line for bypassing the at least one mixture cooler, wherein the bypass valve is arranged in the bypass line.
7. The internal combustion engine according to claim 6, wherein the bypass line for bypassing the at least one mixture cooler is combined with the bypass line for bypassing the compressor of the at least one turbocharger.
8. The internal combustion engine according to claim 1, wherein a mixing device is provided, by means of which the fuel mixture can be produced.
9. The internal combustion engine according to claim 8, wherein the bypass line is connected to an outlet of the mixing device for the fuel mixture.
10. The internal combustion engine according to claim 1, wherein the internal combustion engine is a preferably stationary gas engine.
11. A method for starting an internal combustion engine, wherein, during the startup of the internal combustion engine, at least a partial flow of a fuel mixture provided for the combustion is circulated around a compressor of at least one turbocharger.
12. The method according to claim 11, wherein a bypass valve is at least partly opened and/or at least partially kept open to bypass the compressor.
13. The method according to claim 12, wherein the bypass valve is completely opened and/or completely kept open in the startup of the internal combustion engine.
14. The method according to claim 11, wherein a generatorpreferably suitable for feeding electrical energy into a power supply networkis driven by the internal combustion engine after the startup.
15. The method according to claim 11, wherein a gas compressor is driven by means of the internal combustion engine after the startup.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025] Further advantages and details of the invention can be found in the figures and the related description of the figures. They are as follows:
[0026]
[0027]
[0028]
[0029]
DETAILED DESCRIPTION
[0030]
[0031] Two turbochargers 3 are provided, wherein a compressor 4 of the turbochargers 3 is arranged in the supply line 11. The turbines 5 of the turbochargers 3 are arranged in the exhaust gas line 12. The compressors 4 are connected in series in the supply line 11. Analogously, the turbines 5 are also connected in series. The compressors 4 are each followed by two mixture coolers 13. The turbines 5 drive the compressors 4, which generate an increased pressurethe charge-air pressureof the fuel-air mixture. As a result of this increased pressure, more fuel-air mixture reaches the cylinders than in a naturally aspirated engine design, which increases the performance.
[0032] A bypass line 8 is also provided, in which the bypass valve 6 is arranged. During the operation of the internal combustion engine 1, a partial flow of the fuel-air mixture cannot be supplied to the engine block 2 by opening the bypass valve 6. Due to the charge-air pressure, a partial flow is instead fed back into the supply line 11 (via the bypass line 8 in the flow direction B). This reduces the power of the internal combustion engine 1. As a result of this measure, the power of the internal combustion engine 1 can be regulated or controlled. This regulation or control takes place in a control or regulation device 7, which is connected to the bypass valve 6.
[0033] A common or individual wastegate (not shown) for the turbocharger 3 can also be present.
[0034] Before starting the internal combustion engine 1, both the supply line 11 and the bypass line 8 are not filled with fuel-air mixture. This is not done for safety reasons. For example, the fuel-air mixture could ignite due to the effect of heat in the supply line 11.
[0035] If the internal combustion engine 1 is now towed by an external drive (not shown), the fuel-air mixture is aspirated. In the prior art, the fuel-air mixture had to be suctioned through the supply line 11, the compressors 4 and the mixture coolers 13. By opening the bypass valve 6, the fuel-air mixture must travel down a substantially shorter and more resistance-free path via the bypass line 8 (in the flow direction A), which reduces the startup time.
[0036] A generator 10 is driven by means of the internal combustion engine 1in this case, a stationary gas engine. The generator 10 can, for example, be connected to a power supply network and can supply it with energy. The internal combustion engine 1 can, of course, also serve other consumers, for example mechanical drives or compressors.
[0037]
[0038]
[0039] Thus, when the bypass valve 6 is opened, the fuel mixture for the starting process is provided with a shorter path reduced flow resistance, but the fuel mixture must pass through a compressor 4 during the starting process.
[0040] It can nevertheless be advantageous to arrange the bypass valve 6 as shown in
[0041]
[0042] The engine block 2, turbocharger 3, mixing device 9 and bypass valve 6 can be seen.
[0043] In starting according to the prior art, the fuel mixture was required to take the long path indicated by the reference signs 14. The path indicated by reference sign 15 is the path that the fuel-air mixture according to embodiments of the invention must take. According to an embodiment of the invention, the fuel/air mixture must fill up only a fraction of the dead volume, or only a fraction of the path length must be travelled, whereby flow resistances must also be overcome.
[0044] This written description uses examples to disclose the invention, including the preferred embodiments, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.