FUEL SUPPLY SYSTEM OF AN ENGINE DESIGNED AS GAS ENGINE OR DUAL-FUEL ENGINE AND ENGINE
20230036725 · 2023-02-02
Inventors
Cpc classification
F02M43/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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
F02M51/061
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M61/166
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A fuel supply system of an engine designed as a gas engine or dual-fuel engine, has at least one solenoid valve. The solenoid valve is designed for introducing gas fuel into charge air or into a charge air line leading to at least one cylinder of the engine. The respective solenoid valve includes a valve body and an actuator with at least one magnetic plate and with at least one coil for actuating the valve body. The at least one solenoid valve of the solenoid valve is formed out of a corrosion-resistant material or is coated with a corrosion-resistant material.
Claims
1. A fuel supply system of an engine configured as a gas engine or as a dual-fuel engine, comprising: at least one solenoid valve, wherein the at least one solenoid valve is configured to introduce gas fuel into charge air or into a charge air line leading to at least one cylinder of the engine, wherein the respective solenoid valve comprises: a valve body; an actuator with at least one magnetic plate; and at least one coil configured to actuate the valve body, wherein the at least one magnetic plate of the respective solenoid valve is formed from a corrosion-resistant material or is coated with a corrosion-resistant material.
2. The fuel supply system according to claim 1, wherein the at least one magnetic plate and/or the at least one coil of the at least one solenoid valve is separated or sealed from a corrosive atmosphere by at least one separating element.
3. The fuel supply system according to claim 2, wherein the at least one separating element is formed out of a corrosion-resistant material or is coated with a corrosion-resistant material.
4. A fuel supply system of an engine configured as gas engine or dual-fuel engine, comprising: at least one solenoid valve configured to introduce gas fuel into charge air or into a charge air line leading to at least one cylinder of the engine, wherein the at least one solenoid valve comprises: a valve body; an actuator with at least one magnetic plate; at least one coil configured to actuate the valve body; and at least one separating element, which is formed out of a corrosion-resistant material or is coated with a corrosion-resistant material and is configured to separate or seal the at least one magnetic plate of the at least one solenoid valve from a corrosive atmosphere which is one of the charge air or a charge air-containing atmosphere.
5. The fuel supply system according to claim 4, wherein the at least one coil of the at least one solenoid valve is also separated or sealed from the corrosive atmosphere, which is one of the charge air or the charge air-containing atmosphere, via the at least one separating element.
6. The fuel supply system according to claim 4, wherein the at least one separating element is a separating plate that separates or seals the at least one magnetic plate of the at least one solenoid valve from a chamber of the at least one solenoid valve containing the corrosive atmosphere.
7. The fuel supply system according to claim 4, wherein the at least one separating element is a seal that separates and seals a gap between an armature of the valve body of the at least one solenoid valve and a guide for the armature.
8. The fuel supply system according to claim 4, wherein the at least one magnetic plate of the at least one solenoid valve is formed out of a corrosion-resistant material or coated with a corrosion-resistant material.
9. An engine, namely gas engine or dual-fuel engine, comprising: at least one cylinder; and a fuel supply system, comprising: at least one solenoid valve, wherein the at least one solenoid valve is configured to introduce gas fuel into charge air or into a charge air line leading to the at least one cylinder of the engine, wherein the respective solenoid valve comprises: a valve body; an actuator with at least one magnetic plate; and at least one coil configured to actuate the valve body, wherein the at least one magnetic plate of the respective solenoid valve is formed from a corrosion-resistant material or is coated with a corrosion-resistant material.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Preferred further developments of the invention are obtained from the subclaims and the following description. Exemplary embodiments of the invention are explained in more detail by way of the drawing without being restricted to this. There it shows:
[0014]
[0015]
[0016]
[0017]
DETAILED DESRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS
[0018] One aspect of the invention relates to a fuel supply system of an engine designed as gas engine or as dual-fuel engine and to such an engine having such a fuel supply system.
[0019] A fuel supply system of an engine designed as gas engine or dual-fuel engine includes at least one solenoid valve, wherein the respective solenoid valve is designed for introducing gas fuel into a charge air line leading to at least one cylinder of the engine and thus into the charge air.
[0020] This solenoid valve can be the valve 14 shown in
[0021] Such a solenoid valve 14 is shown in greater detail in
[0022] The valve body 15 is equipped with an armature 15a, an armature plate 15b, and a valve plate 15c. The armature plate 15b is formed at a first end of the armature 15a and the valve plate 15c at a second end of the armature 15a located opposite.
[0023] The valve plate 15c of the valve body 15 is followed by a fixed sealing plate 17. The first armature plate 15b is positioned in a first chamber 16b and the second armature plate 15c in a second chamber 16c of the housing 16 of the solenoid valve 14, wherein these chambers 16b and 16c are connected via the guide 16a. Here, the guide 16a is formed by a guide bore in the housing 16.
[0024] Spring elements 18 act on the valve plate 15c, which press the valve plate 15c and thus the valve body 15 against the sealing plate 17. In particular when the valve plate 15c is pressed against the sealing plate 17 the solenoid valve 14 is closed.
[0025] For actuating the valve body 15 the solenoid valve 14, furthermore, comprises an actuator 19, which is equipped with magnetic plates 20 and at least one solenoid 21. The or each solenoid 21 is typically embedded, at least partially, in an encapsulating material 22.
[0026] By electrically energising the actuator 19, the same magnetically attracts the valve body 15 lifting the same against the spring force of the spring elements 18 off the sealing plate 17 to open the solenoid valve 14. Then, gas fuel can flow out of the chamber 16c via the at least one recess 17a in the sealing plate 17.
[0027] In
[0028] In the process, the charge air can be enriched with water. Charge air enriched with water is a corrosive atmosphere.
[0029] In order to protect the respective magnetic plate 20 of the solenoid valve 14 from corrosion it is provided in
[0030] In
[0031]
[0032] In order to prevent a corrosion of the separating element 24, 25 the same is formed out of the corrosion-resistant material or coated with the corrosion-resistant material.
[0033] The measures of
[0034]
[0035] The aspect of
[0036] Thus, while there have shown and described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.