HIGH-PRESSURE ACCUMULATOR AND METHOD FOR PRODUCING A HIGH-PRESSURE ACCUMULATOR
20200325866 ยท 2020-10-15
Inventors
Cpc classification
F02M55/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M2200/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M2200/80
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
F02M2200/315
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M55/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The invention relates to a high-pressure accumulator (1) for internal combustion engines for storing highly pressurized fuel. The high-pressure accumulator (1) comprises an accumulator pipe (2) with an accumulator chamber (3) formed in the accumulator pipe (2). The high-pressure accumulator (1) comprises a supply connection (7) for supplying highly pressurized fuel and at least one discharge connection (4) for discharging highly pressurized fuel. A honeycomb structure (10) is arranged in the accumulator chamber (3).
Claims
1. A high pressure accumulator (1) for internal combustion engines for storing highly pressurized fuel, the high pressure accumulator (1) comprising a common rail (2) with an accumulator space (3) which is configured in the common rail (2), the high pressure accumulator (1) having a feed connector (7) for feeding in highly pressurized fuel and at least one discharge connector (4) for discharging highly pressurized fuel, characterized in that a honeycomb structure (10) is arranged in the accumulator space (3).
2. The high pressure accumulator (1) as claimed in claim 1, characterized in that the common rail (2) and the honeycomb structure (10) are configured in one piece.
3. The high pressure accumulator (1) as claimed in claim 1, characterized in that the honeycomb structure (10) comprises at least one disk (11), a plurality of honeycomb-shaped recesses (12) being configured in the disk (11).
4. (canceled)
5. The high pressure accumulator (1) as claimed in claim 3, characterized in that the recesses (12) have the basic shape of a regular hexagon.
6. The high pressure accumulator (1) as claimed in claim 5, characterized in that an edge length (s) of the regular hexagon is 0.75 mm.
7. The high pressure accumulator (1) as claimed in claim 1, characterized in that the honeycomb structure (10) comprises at least one honeycomb cup (15), a plurality of honeycomb-shaped recesses (12) being configured in the honeycomb cup (15).
8. The high pressure accumulator (1) as claimed in claim 7, characterized in that each honeycomb cup (15) has a head region (17), a diameter of which corresponds to a diameter of the accumulator space (3), and wherein each honeycomb cup (15) has a tapered base region (16).
9. (canceled)
10. The high pressure accumulator (1) as claimed in claim 7, characterized in that the honeycomb cups (15) have a length (L) of 5 mm.
11. The high pressure accumulator (1) as claimed in claim 7, characterized in that the recesses (12) have a basic shape of a regular hexagon.
12. The high pressure accumulator (1) as claimed in claim 11, characterized in that an edge length of each regular hexagon is 0.75 mm.
13. A method for producing a high pressure accumulator (1) as claimed in claim 1, the common rail (2) and the honeycomb structure (10) being configured in one piece, characterized in that the high pressure accumulator (1) is manufactured using the 3D printing process.
14. The high pressure accumulator (1) as claimed in claim 1, characterized in that the honeycomb structure (10) comprises from 10 to 15 disks (11), a plurality of honeycomb-shaped recesses (12) being configured in each disk (11).
15. The high pressure accumulator (1) as claimed in claim 14, characterized in that the disks (11) are lined up one after another in each case at the same axial spacing (a).
16. The high pressure accumulator (1) as claimed in claim 14, characterized in that the recesses (12) have the basic shape of a regular hexagon.
17. The high pressure accumulator (1) as claimed in claim 16, characterized in that an edge length (s) of the regular hexagon is 0.75 mm.
18. The high pressure accumulator (1) as claimed in claim 1, characterized in that the honeycomb structure (10) comprises from 10 to 15 honeycomb cups (15), a plurality of honeycomb-shaped recesses (12) being configured in each honeycomb cup (15).
19. The high pressure accumulator (1) as claimed in claim 18, characterized in that each honeycomb cup (15) has a head region (17), a diameter of which corresponds to a diameter of the accumulator space (3), and wherein each honeycomb cup (15) has a tapered base region (16).
20. The high pressure accumulator (1) as claimed in claim 19, characterized in that the honeycomb cups (15) are arranged in such a way that in each case a head region (17) interacts with a head region (17) and a base region (16) interacts with a base region (16).
21. The high pressure accumulator (1) as claimed in claim 18, characterized in that the honeycomb cups (15) have a length (L) of 5 mm.
22. The high pressure accumulator (1) as claimed in claim 18, characterized in that the recesses (12) have a basic shape of a regular hexagon.
23. The high pressure accumulator (1) as claimed in claim 22, characterized in that an edge length of each regular hexagon is 0.75 mm.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0020] In the following text, exemplary embodiments of the invention will be described in greater detail with reference to the appended drawings, in which:
[0021]
[0022]
[0023]
DETAILED DESCRIPTION
[0024] In the longitudinal section of
[0025] A plurality of discharge connectors 4 for fuel pressure lines to injectors (not shown) are configured on the common rail 2 of the high pressure accumulator 1. Furthermore, a feed connector 7 to a high pressure pump (not shown) is configured on the common rail 2. In addition, receptacles 5 and 6 for attachment components 8 and 9 are configured on the common rail 2. The attachment component 8 is usually a rail pressure sensor for determining the pressure in the accumulator space 3. In addition, the attachment component 9 is a pressure valve, preferably a pressure control valve for controlling the pressure in the accumulator space 3. The pressure valve 9 or pressure control valve 9 is configured, for example, as an electromagnetic valve and has an electric connector (not shown) for connecting to a control unit or a power supply (not shown).
[0026] The receiving opening 6 for the pressure valve 9 is connected via an outlet duct 32 to a low pressure connector 34, with the result that a fuel quantity which is output in a controlled manner via the pressure valve 9 can be guided to a low pressure return line. Here, the outlet duct 32 opens into the receiving opening 6 in such a way that a seal is ensured between the high pressure part and the low pressure part (outlet duct 32) in the case of a pressure valve 9 which is attached to the high pressure accumulator 1.
[0027] In the exemplary case, the pressure valve 9 and the rail pressure sensor 8 are arranged at ends of the high pressure accumulator 1 which face away from one another. Here, the distribution of said attachment components 8, 9 on the high pressure accumulator 1 is in principle freely selectable.
[0028]
[0029] The high pressure accumulator 1 has the common rail 2, in which the accumulator space 3 for storing the highly pressurized fuel is configured. Flow conditions of the fuel in the accumulator space 3 which are dependent on the operating point are produced with pressure oscillations on account of the feeding of the fuel from the high pressure pump and the discharge of the fuel to the injectors.
[0030] A honeycomb structure 10 is arranged in the accumulator space 3 in order to damp said pressure oscillations. In the embodiment of
[0031] The accumulator space 3 is divided by way of the disks 11 into individual chambers 3a, 3b, etc., which are connected to one another via the cross-sectional reduction by way of the honeycomb-shaped recesses 12. Accordingly, the honeycomb-shaped recesses 12 represent throttles in the axial flow direction which effectively damp any pressure overshoots during the throughflow. As a result, the maximum pressure peaks within the high pressure accumulator 1 and also within the downstream injectors are damped. Accordingly, the service life of said components is increased.
[0032] The common rail 2 and the honeycomb structure 10 are advantageously configured in one piece, with the result that a complicated connecting technique is not required. The corresponding production process to this end is preferably the 3D printing process; a conventional casting process is not suitable for geometries of this type in high quantities.
[0033]
[0034] On account of the positively locking lining up of the individual honeycomb cups 15, the honeycomb structure 10 in said embodiment has a high rigidity and thus also increases the strength of the common rail 2 or the entire high pressure accumulator 1, both in the radial and in the axial direction. The individual honeycomb cups 15 preferably have a length L of 5 mm, from 10 to 15 honeycomb cups 15 advantageously being lined up in the accumulator space 3. Furthermore, the honeycomb-shaped recesses 12 in each case have the shape of a uniform hexagon with an edge length s of 0.75 mm, in a manner which is advantageous for an accumulator space 3 with a diameter D of approximately 10 mm. Here, the web width u of the honeycomb structure 10 between the individual recesses 12 is preferably 0.55 mm.
[0035] In general, a very complex geometry of the honeycomb structure 10 can be realized using the 3D printing process, specifically if the honeycomb structure 10 is configured in one piece with the common rail 2. Here, the above-described embodiments prove particularly effective for damping the pressure oscillations in the accumulator space 3, caused by way of the periodic conveying of highly pressurized fuel from the high pressure pump via the feed connector 7 and the sudden discharge of fuel via one or more discharge connectors 4 to the injectors.