INJECTOR FOR INTRODUCING A FLUID WITH IMPROVED FLOW ROBUSTNESS
20230107782 · 2023-04-06
Inventors
Cpc classification
F02M61/1826
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/1846
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/1886
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
An injector for introducing a fluid. The injector has a valve seat in which a multiplicity of injection holes are formed, and a closing element that releases and closes a fluid path to the injection holes, a size of an inlet area of at least two injection holes being different, and a spacing of the injection holes in the circumferential direction to the adjacent injection hole in each case being selected as a function of the size of the inlet areas of the injection holes.
Claims
1-9. (canceled)
10. An injector for introducing a fluid, comprising: a valve seat in which a multiplicity of injection holes are formed; and a closing element that releases and closes a fluid path to the injection holes, a size of an inlet area of at least two of the injection holes being different from one another; wherein a spacing in a circumferential direction of the injection holes to each adjacent injection hole is selected as a function of a size of inlet areas of the injection holes.
11. The injector as recited in claim 10, wherein a circular segment going out from a center axis of the injector is assigned to each injection hole of the injector holes, each injection hole center axis is situated in a range of ±5° around a center line of the circular segment, sizes of the circular segments being selected corresponding to the sizes of the inlet areas of the injection holes.
12. The injector as recited in claim 11, wherein each of the injection holes is situated on the center line of a circular segment of the circular segments.
13. The injector as recited in claim 10, wherein the injection area of each of a largest injection hole of the injection holes and a smallest injection hole of the injection holes differs by a maximum of 45% from an average value of all inlet areas of the injection holes.
14. The injector as recited in claim 10, wherein each injection hole has an injection hole center axis that has a radial distance to a center axis of the injector, each of the radial distances of the injection hole center axes differing by a maximum of 30% from an average value of all radial distances of the injection hole center axes to the center axis of the injector.
15. The injector as recited in claim 14, wherein all injection hole center axes are situated at the same radius around the center axis.
16. The injector as recited in claim 10, wherein the injector has from five to seven injection holes.
17. The injector as recited in claim 10, wherein the injector is an inwardly opening injector.
18. The injector as recited in claim 10, wherein the injector is a fuel injector or a urea injector or a water injector.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0014] In the following, a preferred exemplary embodiment of the present invention is described in detail with reference to the figures.
[0015]
[0016]
[0017]
DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS
[0018] In the following, an injector 10 according to a preferred exemplary embodiment of the present invention is described in detail with reference to
[0019] Injector 10 is a fuel injector for the direct injection of fuel into a combustion chamber of an internal combustion engine. Injector 10 includes a closing element 20 in the form of a valve needle on whose free end there is situated a ball 21. The closing element is pressed into a closed position, shown in
[0020] In this exemplary embodiment, injector 10 is an inwardly opening injector, closing element 20 being moved against the reset force of reset element 9 in order to open injector 10.
[0021] Injector 10 includes a multiplicity of injection holes 30, situated in a valve seat 8 of the injector.
[0022] In this exemplary embodiment, as shown schematically in
[0023] Closing element 20 is actuated by actuator 40, which in this exemplary embodiment is a magnetic actuator. However, it is to be noted that a piezo actuator may also be provided for the actuation of closing element 20.
[0024] Closing element 20 thus releases or closes a fluid path to a sealing seat 7 for the fuel to be injected.
[0025] As can be seen in
[0026] In addition, a spacing of the respectively adjacent injection holes 30 in the circumferential direction is selected as a function of the size of the inlet areas of injection holes 30. In this way, it is ensured that the largest quantities of fuel can flow to the injection holes having numbers 2 and 5 when the injector is open, without there being local oversupplying or competition with regard to the mass distribution of the fuel to the respective injection holes.
[0027] Here, each injection hole has assigned to it a pie piece-shaped circular segment (see
[0028] In addition, injection hole center axes S are all situated at a common radius R about a center axis X-X of injector 10.
[0029] As can be seen in
[0030] In addition, the largest and the smallest injection hole 30 have an inlet area that is a maximum of 45% of an average value of all inlet areas. The average value of the inlet areas is obtained by addition of the individual inlet areas and division by the number of injection holes.
[0031] The sizes of the circular segments are then selected corresponding to the sizes of the inlet areas of injection holes 30. It is to be noted that midpoints S of the injection holes do not necessarily have to lie on the center lines of the circular segments, but can have a deviation of ±5°.
[0032] In
[0033] Correspondingly, the center lines of the circular segments are also defined by the arcs α1/2 and α2/2.
[0034] Thus, injector 10 according to the present invention can provide an increase in a flow robustness compared to the related art. In particular, it is possible to achieve reduced scattering of injected quantities, both at different injectors and also at one injector in successive injections. In addition, a particularly homogenous flow distribution of the fuel mass flow, without mutual interference of adjacent injection holes, is achieved. In