CN1164270A - fuel nozzle - Google Patents
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- CN1164270A CN1164270A CN 95196309 CN95196309A CN1164270A CN 1164270 A CN1164270 A CN 1164270A CN 95196309 CN95196309 CN 95196309 CN 95196309 A CN95196309 A CN 95196309A CN 1164270 A CN1164270 A CN 1164270A
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Abstract
Description
发明的领域field of invention
本发明涉及一种给诸如柴油发动机的内燃式发动机供给燃料的喷嘴。更特指地,它涉及能通过改变针阀的提升量和起喷射作用的喷嘴孔的总开口面积而获得各种喷射模式的燃料喷嘴。The present invention relates to a nozzle for supplying fuel to an internal combustion engine, such as a diesel engine. More specifically, it relates to fuel nozzles capable of obtaining various injection patterns by changing the lift amount of the needle valve and the total opening area of the nozzle holes functioning as injection.
相关技术的说明Description of related technologies
内燃式发动机中所用的燃料喷嘴包括例如日本未审查专利公开文件NO.S59-200063中所公开的一种喷嘴,它通过一个形成于喷嘴本体的前端部的喷嘴孔喷出燃料,在一个以可滑动方式封装于喷嘴本体内的针阀处设有一楔形的压力承接表面,并且是通过将燃料压力施加到压力承接表面而使针阀打开的。Fuel nozzles used in internal combustion engines include, for example, a nozzle disclosed in Japanese Unexamined Patent Publication No. S59-200063, which ejects fuel through a nozzle hole formed at the front end of the nozzle body, in a A wedge-shaped pressure-receiving surface is provided at the needle valve which is slidably packaged in the nozzle body, and the needle valve is opened by applying fuel pressure to the pressure-receiving surface.
另外,更近期的例子包括日本未审查专利公开文件NO.H4-76266中所公开的燃料喷嘴,其特点是一项能实现促进燃烧、提高动力和燃料效率、降低燃烧噪音和减少NOx排放的技术,它是通过形成一个将加压燃料导至喷嘴本体1的前端部分的通道,形成多个与此通道连通的喷嘴孔2,穿过一个对燃料至该通道的间歇流入量进行控制的针阀插入一回转阀(转动轴)17,并改变回转阀(转动轴)17的转动位置,以增大/减小起燃料喷射作用的喷嘴孔的张开面积,从而可以改变喷射压力、喷射时间和喷射量。Also, more recent examples include the fuel nozzle disclosed in Japanese Unexamined Patent Publication No. H4-76266, which features a technology that achieves enhanced combustion, improved power and fuel efficiency, reduced combustion noise, and reduced NOx emissions , which is formed by forming a passage leading pressurized fuel to the front end portion of the
但是,在第一个燃料喷嘴中,它采用了这样的结构,喷射压力、喷射量、喷射时间和类似参数由一向燃料喷嘴输送燃料的喷射泵决定,喷嘴孔的数目是固定的,随之而来的是要增大/减小起喷射作用的喷嘴孔的总面积从结构上讲是不可能的。这出现一个问题,即难于保持良好的燃烧状态,因为在发动机低速旋转时喷射压力将降低,且在发动机的低负载状态下喷射时间将缩短。However, in the first fuel nozzle, it adopts such a structure that the injection pressure, injection quantity, injection time and similar parameters are determined by the injection pump delivering fuel to the fuel nozzle, the number of nozzle holes is fixed, and accordingly It follows that it is structurally impossible to increase/decrease the total area of the spray nozzle openings. This presents a problem that it is difficult to maintain a good combustion state because the injection pressure will be lowered when the engine rotates at a low speed, and the injection time will be shortened under a low load state of the engine.
另外,在第二个燃料喷嘴中,它采用了这样的系统,喷嘴本体内的喷嘴孔由转动轴从内部堵住(如图26所示),由于喷嘴孔仅从内部进行制约,因此在喷嘴本体的表面喷嘴孔的张开面积实际没有改变。这样就有一个问题,所喷射的燃料没有实实在在地微细雾化。再者,如图1所示,在日本未审查专利公开文件NO.S4-76266中,对于喷嘴本体中的喷嘴孔是从内部堵住的系统,需要多个导槽18,不能减少吸入量,且随之而来则存在喷射后发生残余燃料流溢的可能,增加HC的排放量。再进一步,在这样一种结构中,需要提高针阀3和转动轴17的轴向对准精度。In addition, in the second fuel nozzle, it adopts such a system that the nozzle hole in the nozzle body is blocked from the inside by the rotating shaft (as shown in Fig. 26), since the nozzle hole is only restricted from the inside, so in the nozzle The open area of the nozzle holes on the surface of the body is practically unchanged. Thus, there is a problem that the injected fuel is not really finely atomized. Furthermore, as shown in Figure 1, in Japanese Unexamined Patent Publication No.S4-76266, for the nozzle hole in the nozzle body is blocked from the inside,
另外,在现有技术的结构中还存在另一个问题,即由于该结构不允许有目的地改变针阀的提升量,所以通过调节该提升量改变压力损失和使喷射量增加或减少,用改变喷射压力和喷射速度或类似参数来有目的地改变喷射状态是不可能的。In addition, there is another problem in the structure of the prior art, that is, since the structure does not allow the lift amount of the needle valve to be purposefully changed, by adjusting the lift amount to change the pressure loss and to increase or decrease the injection amount, it is necessary to change the lift amount. It is not possible to purposefully change the injection state by changing the injection pressure and injection speed or similar parameters.
针对上述问题,本发明的一个目的是提供一种燃料喷嘴,它能通过有目的地改变针阀的提升量或通过改变起喷射作用的喷嘴孔的总面积来获得所需的喷射模式,因此喷射压力、喷射时间、喷射量和其它类似的与发动机负载和转速相适应的参数最终均可获得,从而实现减少NOx、提高燃料效率等目的。In view of the above problems, an object of the present invention is to provide a fuel nozzle that can obtain the desired injection pattern by purposefully changing the lift of the needle valve or by changing the total area of the nozzle hole that is used for injection, so that the injection Pressure, injection time, injection quantity and other similar parameters adapted to the engine load and speed can be finally obtained, so as to achieve the purpose of reducing NOx and improving fuel efficiency.
本发明的另一个目的是提供一种考虑了以下需要的燃料喷嘴,它包括使所喷燃料微细雾化、防止吸入量增加、允许改变喷嘴孔的有效面积的转动件和针阀的轴向对准精度不十分严格。Another object of the present invention is to provide a fuel nozzle that takes into consideration the needs of a fine atomization of the injected fuel, prevention of an increase in the amount of suction, a rotary member that allows the effective area of the nozzle hole to be changed, and an axial alignment of the needle valve. Accuracy is not very strict.
本发明概要Summary of the invention
相应地,根据本发明的燃料喷嘴包括,一个带有在其前端部形成的用于喷出加压燃料的喷嘴孔的喷嘴本体,一个以可滑动方式插入喷嘴本体用以打开/关闭喷嘴孔的针阀,一个向针阀施加一个沿喷嘴孔关闭的方向的力的弹簧,一个设置在针阀的轴线的延长线上的可随针阀一起移动的转子,一个设置在针阀的轴线的延长线上的面对转子的定子,当电流通过时它抵消弹簧力以电磁作用吸引转子,一个由一外部信号驱动和控制的第一微电机和一提升量改变机构,它利用第一微电机实现定子在针阀的轴线的延长线上的位移,最终使改变针阀的最大提升量成为可能。Accordingly, a fuel nozzle according to the present invention includes a nozzle body having a nozzle hole for spraying pressurized fuel formed at its front end, a nozzle body slidably inserted into the nozzle body for opening/closing the nozzle hole. Needle valve, a spring that applies a force to the needle valve in the direction of closing the nozzle hole, a rotor set on the extension of the axis of the needle valve that can move with the needle valve, and a rotor set on the extension of the axis of the needle valve The stator facing the rotor on the line, when the current passes, it counteracts the spring force to attract the rotor electromagnetically, a first micro-motor driven and controlled by an external signal and a lifting amount changing mechanism, which utilizes the first micro-motor to realize The displacement of the stator on the extension line of the axis of the needle valve finally makes it possible to change the maximum lift of the needle valve.
该提升量改变机构可如此构成:以使其可螺旋状前进或后退的方式将定子在针阀的轴线方向上紧固住,使定子在针阀的轴线方向上随着一个与定子的外圆周表面上形成的齿相啮合的且其转动源于第一微电机的齿轮位移;通过提供一可在针阀的轴线方向上滑动的定子,且使定子随着一个与在定子的外圆周表面的一部分上形成的一个齿条部分相啮合的且其转动源于第一微电机的筒形蜗轮在针阀的轴线方向上位移;或者通过在定子的一侧提供一个在定子轴线方向延伸、其上形成有阴螺纹的悬臂部分,并通过一阳螺纹部分使定子在针阀的轴线方向上位移,该阳螺纹部分由于第一微电机而转动,从而在悬臂部分的阴螺纹上螺旋前进或后退。The lifting amount changing mechanism can be constructed as follows: the stator is fastened in the axial direction of the needle valve in such a manner that it can advance or retreat in a spiral shape, so that the stator moves along with the outer circumference of the stator in the axial direction of the needle valve. The teeth formed on the surface are meshed and its rotation is derived from the gear displacement of the first micro-motor; by providing a stator that can slide in the axial direction of the needle valve, and making the stator follow a contact with the outer circumferential surface of the stator A rack part formed on a part meshes and its rotation originates from the displacement of the cylindrical worm gear of the first micro-motor in the axial direction of the needle valve; A cantilever portion with a female thread is formed, and the stator is displaced in the axial direction of the needle valve through a male thread portion, which is rotated by the first micro-motor, thereby spirally advancing or retreating on the female thread of the cantilever portion.
结果,由于针阀的最大提升量可由提升量改变机构来控制,所以在例如发动机起动时的低负载下、低转速操作情况下,可通过增大提升量以提高喷射压力和延长喷射时间来促进喷射的微细雾化。另外,在高负载、高速转动操作中,通过减少提升量以降低喷射压力和缩短喷射时间来实现稳定燃烧。再者,通过横截面的流量可通过改变提升量来改变流动阻力而变化,所以在例如蓄积式燃料喷射泵的情况下,通过改变提升量来变化喷射量成为可能,而在脉动式燃料喷射泵情况下,通过改变提升量来改变喷射压力和喷射速度成为可能。As a result, since the maximum lift amount of the needle valve can be controlled by the lift amount changing mechanism, it can be facilitated by increasing the lift amount to increase the injection pressure and prolong the injection time under low-load, low-speed operation such as when the engine is started. Jet fine atomization. In addition, in high-load, high-speed rotation operation, stable combustion is achieved by reducing the boost amount to lower the injection pressure and shorten the injection time. Furthermore, the flow rate through the cross-section can be changed by changing the flow resistance by changing the lift amount, so in the case of an accumulator fuel injection pump, for example, it is possible to change the injection amount by changing the lift amount, while in the pulse type fuel injection pump Under certain circumstances, it is possible to change the injection pressure and injection speed by changing the lift amount.
另外,根据本发明的燃料喷嘴包括一个带有在其前端部形成的用于喷射加压燃料的喷嘴孔的喷嘴本体,一个以可滑动方式插于喷嘴本体内以打开/关闭喷嘴孔的针阀,一个带有阻塞部分的能以滑动方式绕喷嘴本体转动的外罩部件,该阻塞部分与外罩部件构成整体,根据外罩部件的转动角度成比例地改变喷嘴孔的阻塞程度,以及包括一个由外部信号驱动和控制的第二微电机。在此燃料喷嘴中,第二微电机使外罩部件能够转动,从而可以改变起喷射作用的喷嘴孔的张开面积。In addition, the fuel nozzle according to the present invention includes a nozzle body having a nozzle hole for injecting pressurized fuel formed at its front end, a needle valve slidably inserted in the nozzle body to open/close the nozzle hole , a housing member with a blocking portion that can rotate around the nozzle body in a sliding manner, the blocking portion is integral with the housing member, changes the degree of clogging of the nozzle hole in proportion to the rotation angle of the housing member, and includes an external signal Drive and control the second micromotor. In this fuel nozzle, the second micro-motor enables the rotation of the cover part, so that the opening area of the nozzle hole for injection can be changed.
这种结构可这样实现,例如在喷嘴本体的圆周方向按特定的间隔形成多个喷嘴孔,并且通过转动外罩部件改变由阻塞部件所阻断的喷嘴孔的数目,从而最终改变起喷射作用的喷嘴孔的张开面积,或者是在喷嘴本体的前端部的圆周上的一特定角度范围内形成狭缝状喷嘴孔,而不是形成多个喷嘴孔,并且利用阻塞部分阻塞这些狭缝状喷嘴孔的一部分,以改变张开面积。在前一实例的喷嘴孔的情况下,可采用这种结构,即喷嘴孔的直径按照喷嘴孔为阻塞部件所阻断的顺序是逐渐缩小的,而在后一实例的喷嘴孔的情况下,可采用一楔形结构,其中在喷射面积为阻塞部分所减少的方向上狭缝宽度是逐渐减小的。This structure can be realized in such a way that, for example, a plurality of nozzle holes are formed at specific intervals in the circumferential direction of the nozzle body, and the number of nozzle holes blocked by the blocking member is changed by rotating the cover member, thereby finally changing the nozzle that performs the spraying function. The opening area of the hole, or forming a slit-shaped nozzle hole within a certain angle range on the circumference of the front end of the nozzle body, instead of forming a plurality of nozzle holes, and blocking these slit-shaped nozzle holes with a blocking portion part to change the open area. In the case of the nozzle hole of the former example, such a structure can be adopted that the diameter of the nozzle hole is gradually reduced in the order in which the nozzle hole is blocked by the blocking member, while in the case of the nozzle hole of the latter example, A wedge-shaped structure may be employed in which the slit width is gradually reduced in the direction in which the ejection area is reduced by the blocking portion.
另外,在外罩部件的阻塞部件上沿圆周方向按特定的间隔,可形成多个能与在喷嘴本体的前端所形成的喷嘴孔相连通的喷嘴孔,因此随着外罩部件的转动,可以改变阻塞部件上与喷嘴本体上的喷嘴孔相连通的喷嘴孔的数目,从而改变起喷射作用的喷嘴孔的张开面积。同样,在此例中,在阻塞部分的圆周方向上所形成的多个喷嘴孔的直径按其与喷嘴本体上的喷嘴孔的连通被阻断的顺序是逐渐减小的。In addition, a plurality of nozzle holes that can communicate with the nozzle holes formed at the front end of the nozzle body can be formed at specific intervals in the circumferential direction on the blocking part of the cover part, so that the blocking part can be changed as the cover part rotates. The number of nozzle holes on the component that communicates with the nozzle holes on the nozzle body, thereby changing the opening area of the nozzle holes that play a role in spraying. Also in this example, the diameters of the plurality of nozzle holes formed in the circumferential direction of the blocking portion are gradually reduced in the order in which their communication with the nozzle holes on the nozzle body is blocked.
结果,根据本发明,因为外罩部件的转动位置由第二微电机调节,使改变起喷射作用的喷嘴孔的张开面积成为可能,所以在例如发动机起动时的低负载、低速转动运转过程中,通过转动外罩部件缩小起喷射作用的喷嘴孔的总面积可以增大喷射压力和延长喷射时间。这样,可望促进喷雾的微细雾化和提高喷雾内的过量空气因数,以减少NOx。As a result, according to the present invention, because the rotational position of the cover member is regulated by the second micro-motor, it is possible to change the opening area of the nozzle hole that plays a role in spraying. The spraying pressure and spraying time can be increased and the spraying time can be increased by reducing the total area of the spraying nozzle hole by rotating the cover part. In this way, it is expected to promote the fine atomization of the spray and increase the excess air factor in the spray to reduce NOx.
另外,由于起喷射作用的喷嘴孔的总面积可以从外面改变,所以减少在喷嘴本体内形成的吸入量是可以实现的,同时,改变喷嘴孔的有效面积的外罩部件和喷嘴本体内的针阀的轴向对准不需要了。再者,由于改变喷嘴孔的张开面积可通过外罩部件在喷嘴本体的表面上进行,所以同喷嘴孔的张开面积是从喷嘴本体内进行改变的喷嘴相比,所喷燃料的微细雾化更能实实在在地实现。In addition, since the total area of the nozzle hole that plays a role in spraying can be changed from the outside, it is possible to reduce the amount of suction formed in the nozzle body. At the same time, the outer cover member that changes the effective area of the nozzle hole and the needle valve in the nozzle body The axial alignment is not required anymore. Furthermore, since changing the opening area of the nozzle hole can be carried out on the surface of the nozzle body through the outer cover member, the fine atomization of the injected fuel can be improved compared with the nozzle whose opening area of the nozzle hole is changed from inside the nozzle body. more realistically.
再进一步,如果在高负载、高速转动运转情况下通过转动外罩部件增大了起喷射作用的喷嘴孔的总面积,那么则喷射压力降低且喷射时间缩短。这将保证喷射是在高负载操作所需的流速下进行的,且更均匀弥散,实现稳定的燃烧和高功率输出。Still further, if the total area of nozzle holes for injection is increased by rotating the cover member under high-load, high-speed rotational operation, the injection pressure is lowered and the injection time is shortened. This will ensure that the injection is at the flow rates required for high load operation and is more evenly dispersed for stable combustion and high power output.
附图的简要说明Brief description of the drawings
图1是表示根据本发明的燃料喷嘴的一示意性结构的横截面图;1 is a cross-sectional view showing a schematic structure of a fuel nozzle according to the present invention;
图2是表示图1所示的燃料喷嘴中的驱动机构和喷嘴本体的前端部之一例的放大横截面图;2 is an enlarged cross-sectional view showing an example of a drive mechanism and a front end portion of a nozzle body in the fuel nozzle shown in FIG. 1;
图3是表示图1所示的燃料喷嘴的驱动机构和喷嘴本体的前端部之另一例的放大横截面图;3 is an enlarged cross-sectional view showing another example of the driving mechanism of the fuel nozzle shown in FIG. 1 and the front end portion of the nozzle body;
图4-7示出喷嘴的前端部的一第一种结构的实例,表示在喷嘴本体上所形成的多个喷嘴孔和外罩部件之间的位置关系;Fig. 4-7 shows the example of a first structure of the front end portion of the nozzle, representing the positional relationship between a plurality of nozzle holes formed on the nozzle body and the outer cover member;
图8是由控制装置来完成的喷嘴的控制操作之一例的流程图;Fig. 8 is the flow chart of an example of the control operation of the nozzle that is accomplished by the control device;
图9是图1所示燃料喷嘴中的驱动机构的另一例的放大横截面图;9 is an enlarged cross-sectional view of another example of the drive mechanism in the fuel nozzle shown in FIG. 1;
图10是提升量改变机构的另一例部分放大的横截面图;Fig. 10 is a partially enlarged cross-sectional view of another example of the lifting amount changing mechanism;
图11是提升量改变机构又再一例部分放大的横截面图;Fig. 11 is a partially enlarged cross-sectional view of yet another example of the lifting amount changing mechanism;
图12是自图11中XII-XII线所截取的横截面图;Fig. 12 is a cross-sectional view taken from line XII-XII in Fig. 11;
图13-16示出燃料喷嘴的前端部的一第二种结构的实例,表示喷嘴本体上所形成的喷嘴孔和外罩部件上所形成的多个喷嘴孔之间的联通关系;13-16 show an example of a second structure of the front end of the fuel nozzle, showing the communication relationship between the nozzle hole formed on the nozzle body and the plurality of nozzle holes formed on the cover member;
图17-20示出燃料喷嘴的前端部的一第三种结构的实例,表示在喷嘴本体上所形成的狭缝状喷嘴孔和外罩部件之间的位置关系;17-20 show an example of a third structure of the front end of the fuel nozzle, showing the positional relationship between the slit-shaped nozzle hole formed on the nozzle body and the cover member;
图21-24示出燃料喷嘴的前端部的一第四种结构的实例,表示在喷嘴本体上所形成的狭缝状喷嘴孔和外罩部件之间的位置关系;21-24 show an example of a fourth structure of the front end of the fuel nozzle, showing the positional relationship between the slit-shaped nozzle hole formed on the nozzle body and the cover member;
图25是表示本发明喷嘴孔附近的横截面图;以及Figure 25 is a cross-sectional view showing the vicinity of the nozzle hole of the present invention; and
图26是表示现有技术喷嘴孔附近的横截面图。Fig. 26 is a cross-sectional view showing the vicinity of a conventional nozzle hole.
本发明实施例的详细说明Detailed description of the embodiment of the invention
下面是参照附图对本发明的详细说明。The following is a detailed description of the present invention with reference to the accompanying drawings.
图1所示是一喷嘴1的一第一种结构的实例。在图1中,喷嘴1是这样构成的,即在一喷嘴壳体2的前端提供一喷嘴本体3,且用一止动螺母4将喷嘴壳体2和喷嘴本体3紧固在一起呈一整体,止动螺母4是旋拧在喷嘴壳体2上的。FIG. 1 shows an example of a first configuration of a
在喷嘴壳体2的上方侧表面上形成一燃料入口5,此燃料入口5通过在喷嘴壳体2中形成的通道6和在喷嘴本体3内形成的通道7与在喷嘴本体3的中部形成的一喷嘴腔8连通。一个以可滑动方式插入到喷嘴本体3的一装配孔9内的针阀(针阀)10的压力承接部分11面对喷嘴腔8,且通过燃料入口5流入的高压燃料被引导向针阀10的压力承接部分11。On the upper side surface of the
被导向燃料入口5的高压燃料供自一燃料喷射泵12,它通过管线连接,处在10MPa-150MPa范围。尽管我们在此不准备对它做详细说明,但是燃料喷射泵12可以是例如一台脉动式燃料喷射泵,它迫使燃料以与发动机的运行环境和类似因素相符合的所需的量和所要求的时刻自燃料罐13供入喷嘴1。The high-pressure fuel directed to the
沿喷嘴壳体2的轴线形成一个与喷嘴本体3的装配孔9在一条直线上的通孔14,且在此通孔14内提供有一个与针阀10相接触的移动式弹簧插孔15、一个装配在通孔14内从而堵塞其上部且固定在喷嘴壳体2上的堵塞件16和一个置于移动式弹簧插孔15和堵塞件16之间的螺簧17。移动式弹簧插孔15、弹簧17的中空部分和一个移动针阀的杆18在针阀10处啮合在一起,其中杆18是穿过堵塞件16而与后面一个将详述的转子19相粘结的。A through
在喷嘴壳体2的上部提供有一驱动机构20。如图2所示,更具体地讲,一定子21以可旋转的方式固定在堵塞件16的上端的一螺纹部分上,而且随着定子21的旋转,可使定子21相对于堵塞件16螺旋前进或后退,从而使得存放于定子21和堵塞件16之间所形成的一空间22内的转子19和定子21面对转子19的表面之间的距离L1可以被改变。A
在定子21上缠绕有一螺线管47,且给螺线管47的供电由一控制装置25(示于图1)来控制。请注意,参考标记72指的是一根螺旋状导线,它将与控制装置25相连的电缆连接到螺线管47上,而且它可吸收定子21的转动。A
另外,为了控制定子21的转动的程度,在定子21的一侧上提供有一齿轮23,它与在定子21的外圆周表面上形成的齿24相互啮合,而且齿轮23按照需要由一第一微电机26转动,后者是由控制装置25(示于图1)发出的控制信号来驱动的。应注意,此第一微电机26安装在一第一减速齿轮65处,且插入到一固定于喷嘴壳体2的上部的一个头部27的一安装孔28内。第一微电机26利用一第一盖板29固定在第一电机安装位置30处,盖板29将安装孔28封闭住,齿轮23固定到第一减速齿轮65的转动轴上。In addition, in order to control the degree of rotation of the
再者,在头部27还形成有一用于安装一第二微电机31的安装孔48,且第二微电机31插入安装孔48中,其状态是安装于一第二减速齿轮66处,并通过封闭住安装孔48的一第二盖板49固定在第二微电机安装位置32处。齿轮33固定到第二减速齿轮66的转动轴上,与一个固定在一挠性杆34的一端的齿轮35相互啮合。Furthermore, a mounting
在这种结构中,第一和第二微电机26和31采用例如市售的两极驱动、双相步进电机,外径为Ф10mm,电压5V,输出扭矩1mN·m;而第一和第二减速齿轮65和66采用例如市售的减速比1∶15的减速齿轮,外径为Ф12mm、额定允许扭矩约10mN·m,因此微电机的扭矩通过减速齿轮得到提高。In this structure, the first and second micromotors 26 and 31 adopt, for example, commercially available two-pole drive, two-phase stepping motors with an outer diameter of Ф10mm, a voltage of 5V, and an output torque of 1mN·m; while the first and second The reduction gears 65 and 66 are, for example, commercially available reduction gears with a reduction ratio of 1:15, with an outer diameter of Ф12 mm and a rated allowable torque of about 10 mN·m, so the torque of the micromotor is improved through the reduction gears.
根据第一和第二微电机26和31的另一种模式,可以采用日本未审查专利申请NoH6-189569中所公开的超声电机。而且,如果采用了大扭矩电机,那么齿轮23和33可以直接安装在第一和第二微电机26和31的转动轴上,如图3所示,不安装减速齿轮箱。在这样一种结构中,节省了用于安装减速齿轮箱所需的空间,有助于喷嘴的小型化。According to another mode of the first and second micromotors 26 and 31, an ultrasonic motor disclosed in Japanese Unexamined Patent Application NoH6-189569 may be used. And, if adopted high-torque motor, so
柔性杆34的另一端分别通过在头部27、喷嘴壳体2和喷嘴本体3上形成的杆插孔36、37和38,伸入喷嘴本体3和止动螺母4之间所形成的空间39内,在挠性杆34的这个另一端上固定有齿轮40,它的直径较小,置放于空间39内。The other end of the
在喷嘴本体3自止动螺母4伸出的部分,提供有一外罩部件41,方式是其转动只能是在喷嘴本体的圆周表面上的滑动。外罩部件41的一端通过喷嘴本体3和止动螺母4之间的区域伸出进入空间39内,且在在此伸出部分的外圆周缘上形成与齿轮40相互啮合的齿轮42。结果,当第二微电机31被旋转时,挠性杆34转动,且最后使该外罩部件41也转动。At the portion where the
在喷嘴本体3的前端部形成喷嘴孔43,它随着外罩部件41的转动打开和关闭,因此,如图1所示,可将燃料喷入发动机的燃烧室44内。如图4至7所示,喷嘴孔43包括大直径的喷嘴孔43a、中直径的喷嘴孔43b和小直径的喷嘴孔43c,它们以特定的偏移角顺序形成,且各直径均形成有相互相位差为180°的两个喷嘴孔。根据所要求的发动机技术参数,喷嘴孔的大小将有所变化。在此例中,对于大直径、中直径和小直径的孔,孔的尺寸分别为Ф0.24mm、Ф0.19mm和Ф0.14mm。另外,起始于大直径的喷嘴孔43a直至小直径的喷嘴孔43c的相位角设定为小于90°。In the front end portion of the
沿着外罩部件41的前端部的圆周缘,交替形成缺口部分45和可覆盖喷嘴孔43的阻塞部分46各两个,各自相位彼此偏移180°。阻塞部分46和缺口部分45均大于自大直径的喷嘴孔43a至小直径的喷嘴孔43c的相位角。Along the circumferential edge of the front end portion of the
再参见图1,参考标记A表示一个流速传感器,其位于燃料入口附近,以探测供自喷射泵的燃料流速,参考标记B表示一个压力传感器,其位于燃料入口附近,以探测供自喷射泵的燃料压力,参考标记C表示一个加速器张开传感器,利用发动机负载,以探测加速器相对于发动机负载的张开角度,参考标记D表示一个燃烧室温度传感器,其探测发动机内的燃烧室的温度,参考标记E表示燃烧室压力传感器,其探测发动机内的燃烧室的压力,参考标记F表示一个针阀提升传感器,其探测针阀的提升量,参考标记G表示一转速传感器,其探测发动机的转速。来自这些传感器的信号被输入到控制装置25。Referring again to Fig. 1, reference sign A indicates a flow rate sensor, which is located near the fuel inlet to detect the flow rate of fuel supplied from the injection pump, and reference sign B indicates a pressure sensor, which is located near the fuel inlet to detect the flow rate of fuel supplied from the injection pump. Fuel pressure, reference sign C denotes an accelerator opening sensor using engine load to detect the opening angle of the accelerator relative to the engine load, reference sign D denotes a combustion chamber temperature sensor which detects the temperature of the combustion chamber in the engine, reference Reference numeral E denotes a combustion chamber pressure sensor which detects the pressure of the combustion chamber in the engine, reference numeral F denotes a needle lift sensor which detects the lift amount of the needle valve, and reference numeral G denotes a rotational speed sensor which detects the rotational speed of the engine. Signals from these sensors are input to the
控制装置25是一种已知技术中的控制装置,它包括一个控制微电机26和31及螺线管47的输出电路,一个控制该输出电路的微电脑,一个自各传感器向该微电脑和类似装置输入信号的输入电路。该微电脑配备有一个中央处理单元(CPU)、一个内存和类似元件,且根据来自传感器的信号,按照特定的程序完成运算处理,以控制由第一微电机26调节的起喷射作用的喷嘴孔的张开面积;由第二微电机31调节的针阀10的最大提升量;通过给螺线管47供电所控制的进行燃料喷射的时刻,喷射的时间和类似变量。
换言之,控制喷嘴1的变量有许多个,这包括外罩部件41的转动角度,针阀10的提升量,给螺线管47供电的时刻,供电的持续时间和类似变量,通过改变这些变量,来调节起喷射作用的喷嘴孔的总面积、喷射压力、喷射时刻、喷射时间和类似参数,以改变喷射模式。图8以流程图的形式给出了一个控制操作的特定实例,下面参照此流程图做某些说明。应注意到,发动机负载(加速器张开角度)、发动机的转速、燃烧室压力、燃烧室温度、针阀的提升量、燃料压力和燃料流速以及上述控制变量最佳组合的控制图存贮于控制装置25的内存内,而此控制图是利用以前通过基础试验和类似手段所获得的数据创造出来的。In other words, there are many variables for controlling the
当接通点火开关时,控制装置25开始步骤50的信号输入过程。在步骤50,是输入在预定的某一特定曲轴角度(膨胀冲程或排气冲程所适当的曲轴角度)所测出的来自燃烧室压力传感器和类似测量元件的测量数据,和在发动机的前一次旋转过程中已由转速传感器所测得的发动机转速。When the ignition switch is turned on, the
然后,在随后的步骤52,根据输入信号决定一燃料喷射模式。换言之,即根据存贮于控制装置25的内存内的控制图确定外罩部件41的转动角和针阀10的提升量的最佳值,接着,根据前一次运转过程中针阀的提升量和喷嘴孔的张开面积,计算出第一微电机26的转动角和第二微电机31的转动角,前者将使针阀的提升改变到预定值,而后者将起喷射作用的喷嘴孔43的总面积调节到预定值。另外,在此,还要计算给螺线管47供电的持续时间。Then, in subsequent step 52, a fuel injection mode is determined based on the input signal. In other words, the optimal value of the rotation angle of the
这以后,在步骤54,一个驱动脉动供给到第一微电机26,从而可以完成步骤52中已确定的针阀10的提升位移量。通过这样处理,使第一微电机26转动,它接着使定子21转动,从而调整转子19和面对转子19的定子21之间的距离L1。另外,在步骤56,提供一个驱动脉动操纵第二微电机31,从而调节喷嘴孔43的张开状态。After that, in step 54, a driving pulse is supplied to the first micro-motor 26, so that the lifting displacement amount of the
在此状态下,确定与控制图一致的阀门打开时间和阀门打开时刻,并且提供将其与在特定曲轴角度下所得到的数据相比较,当达到特定的时刻(曲轴角)时,产生一个脉动宽度与阀门打开时间相一致的矩形波。然后,供电给螺线管47,使得在该矩形波的上升段针阀10提升(步骤58)。此时刻与活塞提起以在一脉动式喷射泵开始燃料供给的时间是吻合的,随之,随着针阀10提升,得到燃料流动通道,且燃料喷射开始。In this state, determine the valve opening time and valve opening moment consistent with the control chart, and compare it with the data obtained at a specific crankshaft angle. When a specific moment (crankshaft angle) is reached, a pulse is generated A rectangular wave whose width coincides with the opening time of the valve. Then, power is supplied to the
当开始给螺线管47供电经过一特定的时间长度时,即当针阀10的提升完成而针阀10与定子21相接触时,驱动电流由起动电流转换为保持电流(步骤60)。此保持电流只需处于平衡弹簧17的弹簧力而使转子19与定子21保持接触的水平,而且当需要迅速加速时,此电流可以小于起动所需的电流。然后,将由针阀提升传感器F所测得的针阀10的位移达到一恒定状态的时间点时的针阀10的位置存贮于控制装置25的内存中。When starting to energize the
然后,在矩形波的下降段,给螺线管47的供电停止(步骤62)。伴随之,针阀10朝着由于弹簧17所施加的弹簧力使其关闭的方向运动,关闭喷嘴孔43。Then, in the falling section of the rectangular wave, the power supply to the
这一系列过程的特色之处尤其表现在针阀10的最大提升量在步骤54中由第一微电机26调节。换言之,在步骤54中通过使第一微电机26朝使定子21与转子19之间距离增大的方向转动,针阀10的最大提升量增加,从而增大供给喷嘴孔43的燃料量。反之,通过使第一微电机26朝使定子21与转子19相互靠近的方向转动,针阀10的提升量减小,从而最终减少供给喷嘴孔43的燃料量。The feature of this series of processes is that the maximum lift of the
例如,在发动机起动的低负载、低转速操作过程中,通过增大提升量(通过增大定子21和转子19之间的距离L1),提高喷射压力,且最终延长给螺线管的供电时间,可以促进所喷燃料的微细雾化,而在大负载、高转速操作过程中,通过减少提升量,以降低喷射压力,且最终缩短给螺线管的供电时间,可以实现稳定燃烧。这样,可以获得多种喷射模式。For example, during low-load, low-rpm operation at engine start, by increasing the amount of lift (by increasing the distance L1 between the
另外,改变针阀的提升量的操作也是通过改变流动通道面积来改变流动通道阻力的操作,而且在如本实施例在采用脉动式燃料喷射泵的情况下,由于燃料自泵流出的量是恒定的,所以燃料流动通道中压力损失的变化也构成喷射压力和喷射速度的变化。换言之,当提升量小,由于流动通道面积小,所以压力损失增加,以增大喷射压力的峰值,也增加喷射速度的变化。反之,当提升量大,由于流动通道面积增大,所以压力损失相对减小,以降低喷射压力的峰值,也减少喷射速度的变化。从另一方面讲,如果采用一个蓄积式喷射泵,由于燃料自泵流出的压力是恒定的,所以当由于提升量的改变使燃料流动通道内的压力损失变化时,输出流速也会变化。换言之,采用蓄积式燃料喷射泵,可以通过改变提升量来改变喷射量。结果,通过驱动和控制第一微电机来改变提升量,可以有目的地改变喷射量或喷射压力和喷射速度,以获得所需的喷射模式。In addition, the operation of changing the lifting amount of the needle valve is also an operation of changing the resistance of the flow passage by changing the area of the flow passage, and in the case of using a pulse type fuel injection pump as in this embodiment, since the amount of fuel flowing out of the pump is constant Yes, so changes in pressure loss in the fuel flow passage also constitute changes in injection pressure and injection velocity. In other words, when the lift amount is small, since the flow passage area is small, the pressure loss increases to increase the peak value of the injection pressure and also increase the variation of the injection velocity. On the contrary, when the lifting amount is large, the pressure loss is relatively reduced due to the increase of the flow channel area, so as to reduce the peak value of the injection pressure and also reduce the change of the injection velocity. On the other hand, if an accumulator jet pump is used, since the pressure of the fuel flowing out of the pump is constant, when the pressure loss in the fuel flow path changes due to a change in lift, the output flow rate also changes. In other words, with an accumulator fuel injection pump, the injection quantity can be changed by changing the lift quantity. As a result, by driving and controlling the first micro-motor to change the lifting amount, the injection amount or injection pressure and injection speed can be purposefully changed to obtain the desired injection pattern.
本发明的特点还包括,在步骤54中完成的处理与在步骤56中由第二微电机31完成的喷嘴孔的张开面积的控制是结合起来进行的。也就是说,在步骤56处理过程中,通过使外罩部件41的阻塞部分46定位在未形成喷嘴孔43的区域上,如图4所示,大直径的喷嘴孔43a、中直径的喷嘴孔43b和小直径的喷嘴孔43c全部通过缺口部分45向燃烧室44打开。The characteristics of the present invention also include that the processing completed in step 54 is combined with the control of the opening area of the nozzle hole completed by the second micro-motor 31 in step 56 . That is, in the process of step 56, by positioning the blocking
如果如图5所示,第二微电机31的转动使阻塞部分46只阻塞住大直径的喷嘴孔43a,那么中直径的喷嘴孔43b和小直径的喷嘴孔43c仍然向燃烧室44打开;然而,如果如图6所示,第二微电机31的转动使大直径的喷嘴孔43a和中直径的喷嘴孔43b均被阻塞部分46阻塞住,那么只有小直径的喷嘴孔43c向燃烧室44打开。在此状态下提升针阀,燃料将只通过张开的喷嘴孔喷出。如图7所示,通过继续转动外罩部件41,所有喷嘴孔43可全部堵塞,因此即使提升起针阀10,喷射也不能进行。If as shown in Figure 5, the rotation of the second micro-motor 31 makes the blocking
例如,如果在发动机起动时的低负载、低转速运转过程中达到如图6所示的状态,由于张开的喷嘴孔的数目和张开的喷嘴孔的总面积减小,喷射压力将增大,以延长喷射时间。For example, if the state shown in Figure 6 is reached during low-load, low-rpm operation at engine start, the injection pressure will increase due to the decrease in the number of opened nozzle holes and the total area of the opened nozzle holes , to prolong the injection time.
喷雾颗粒的大小主要由喷嘴孔43(43a、43b和43c)的张开面积和喷射压力决定,且由于燃料雾随着喷嘴孔的张开面积的减小和喷射压力的增大而变得更微细,所以如图6所示的状态可以促进微细雾化,从而有望增大喷雾中的过量空气系数,以减少NOx。反之,在大负载、高转速运转过程中,如果达到图4或图5所示状态,那么由于张开的喷嘴孔的数目和张开的喷嘴孔的总面积增加,喷射压力降低,以缩短喷射时间。在此状态下,喷雾在供给至燃烧室44的同时始终是弥散的,以获得稳定燃烧和高功率输出。The size of the spray particles is mainly determined by the opening area of the nozzle holes 43 (43a, 43b and 43c) and the injection pressure, and since the fuel mist becomes more dense with the decrease of the opening area of the nozzle holes and the increase of the injection pressure Fine, so the state shown in Figure 6 can promote fine atomization, which is expected to increase the excess air coefficient in the spray to reduce NOx. Conversely, in the process of high load and high speed operation, if the state shown in Figure 4 or Figure 5 is reached, the injection pressure will decrease due to the increase in the number of opened nozzle holes and the total area of the opened nozzle holes, so as to shorten the injection time. time. In this state, the spray is always dispersed while being supplied to the
结果,改变起喷射作用的喷嘴孔的张开状态构成改变喷射压力、喷射时间和雾化程度的操作,并且通过将其与前述步骤54中完成的操作相结合,改变喷射模式的自由度可以更大。另外,如图25所示,在如本发明的结构中,由于起喷射作用的喷嘴孔43的面积是由覆罩在喷嘴本体3的外侧的外罩部件41调节的,所以改变的是实际喷嘴孔43前端的张开面积,同图26中所示的喷嘴孔从内部阻塞的结构相比,其获得的优点是便于所喷燃料的微细雾化。As a result, changing the opening state of the nozzle hole that plays a role in spraying constitutes an operation of changing the spraying pressure, spraying time, and degree of atomization, and by combining it with the operation completed in the aforementioned step 54, the degree of freedom in changing the spraying pattern can be more big. In addition, as shown in Figure 25, in the structure of the present invention, because the area of the
应注意,对于改变转子19和定子21之间距离L1的机构,除了上述模式外,定子21可借助螺纹部分进行安装,该螺纹部分相对于头部27的内圆周表面67可以转动,如图9所示,同前述模式相同,在定子的外圆周表面上形成有齿,利用第一微电机使与这些齿啮合的齿轮23转动,从而使定子21在针阀的轴线方向上移动。It should be noted that for the mechanism for changing the distance L1 between the
再者,如图10所示,定子21可以是这样一种形式,它面对转子19,其设置成罩盖在堵塞件16的端部,它可以在针阀10的轴线方向上运动,而在定子21的侧面,有一个在定子的运动方向上延伸、带一阴螺纹部分68的悬臂部分69,从而可使一由第一微电机26转动的阳螺纹部分71(此螺纹可以刻入微电机的转动轴)在悬臂部分69的阴螺纹部分68上螺旋前进或后退,使定子21在针阀的轴线方向上移动。Furthermore, as shown in FIG. 10, the
在再另一种模式中,如图11和12所示,定子21以类似的方式设置成罩盖在堵塞件16的端部,且在定子21的内表面上形成有一个沿堵塞件16的轴线方向延伸的键槽73,从而固定在堵塞件16上的一固定键锁74与键槽73相接合,以防止定子21转动,因此只允许定子21在针阀的轴线方向上运动。另外,通过在定子21的外侧表面的一部分上刻出一弧形的槽来形成一齿条部分75,在此齿条部分75上沿定子21的由线方向形成有齿。一个与该齿条部分75的齿相啮合的筒形蜗轮76固定地安装在第一微电机26的转动轴上,因此通过转动第一微电机26,定子21可在针阀的轴线方向上移动。In yet another mode, as shown in FIGS. 11 and 12 , the
在图13至16中给出了实现喷嘴孔43的张开状态的调节所采用的一第二种结构的例子。在此实施例中,与前面的实施例不同,一外罩部件41的阻塞部分46覆盖整个圆周,在阻塞部分46上有大直径的喷嘴孔70a、中直径的喷嘴孔70b和小直径的喷嘴孔70c以特定的偏移角依次形成。每个直径均由两个喷嘴孔,它们相互间相位偏移为180°。在此实施例中,从大直径的喷嘴孔70a至小直径的喷嘴孔70c之间的相位角同样设定为小于90°。An example of a second structure employed to realize the adjustment of the opening state of the
另一方面,在喷嘴本体3的前端形成有两个大角度的喷嘴孔43,它们相互间相位偏移180°,且喷嘴孔43的圆周角和没有喷嘴孔区域的圆周的角度均大于在外罩部件41上形成的大直径的喷嘴孔43a至小直径的喷嘴孔43c的目位角。On the other hand, two large-angle nozzle holes 43 are formed at the front end of the
应注意,此实施例的其它结构特点与第一实施例的一致,所以省略了对其的说明,图13至16中元件所标的参考数字与图4至7中所标的参考数字是一样的。It should be noted that other structural features of this embodiment are the same as those of the first embodiment, so the description thereof is omitted, and the reference numerals attached to the elements in FIGS. 13 to 16 are the same as those in FIGS. 4 to 7.
在此结构中,也可以通过利用第二微电机31调节喷嘴本体3上的喷嘴孔43与外罩部件41上的喷嘴孔70a、70b和70c之间的连通状态,来改变喷射模式。换言之,如图13所示,通过使喷嘴本体3上的喷嘴孔43与在外罩部件41的堵塞部件46上形成的喷嘴孔70a、70b和70c连通,燃料通过所有喷嘴孔,即大直径的喷嘴孔70a、中直径的喷嘴孔70b和小直径的喷嘴孔70c,喷入燃烧室44;然而,如图14所示,通过转动外罩部件41切断大直径的喷嘴孔43a和喷嘴本体3上的喷嘴孔43的连通,燃料则通过中直径的喷嘴孔43b和小直径的喷嘴孔43c喷入燃烧室。如图15所示,通过转动外罩部件41,使大直径的喷嘴孔43a和中直径的喷嘴孔43b与喷嘴本体3的喷嘴孔43断开,燃料只通过小直径的喷嘴孔43c喷入燃烧室44。当外罩部件41再进一步转动时,外罩部件41的喷嘴孔可全部与喷嘴本体3上的喷嘴孔43断开,因此即使针阀10提起,燃料也不喷射。结果,通过控制第二微电机31,也可如第一实施例那样地改变喷射压力、喷射时间和雾化程度,获得各种喷射模式。In this structure, the spraying mode can also be changed by adjusting the communication state between the
在图17至20中给出了为了实现喷嘴孔的张开状态的调节所采用的一第三种结构的例子,在此实施例中,在相互间相位偏移为180°的两个位置上提供有一呈狭缝形状且具有一特定圆周角的喷嘴孔43。此喷嘴孔43的圆周角设定为小于90°。应注意,狭缝状喷嘴孔43的狭缝宽度设定为大约等于前述大直径的喷嘴孔的直径(最大0.24mm),如果在喷嘴本体3的前端四个位置上形成喷嘴孔43,那么其圆周角只需设定为小于45°。An example of a third structure adopted in order to realize the adjustment of the opening state of the nozzle hole is given in FIGS. There is provided a
另一方面,在外罩部件41的前端部,缺口部分45和能够覆盖喷嘴孔43的阻塞部分46在前端的圆周上其相位偏移为180°的两个位置上交替形成,如同在第一实施例(图4~7)的情况一样。阻塞部分46和缺口部分45形成均大于形成狭缝状的喷嘴孔43的圆周角。On the other hand, at the front end portion of the
其中喷嘴孔43以上述形式提供的结构相当于在一特定的范围上连续形成等直径的喷嘴孔的结构,结果,通过改变喷嘴本体3上的喷嘴孔43与外罩部件41的阻塞部分46之间的相对位置,可以改变喷射模式。换言之,通过使喷嘴本体3的喷嘴孔43面对燃烧室44而完全不为外罩部件41的阻塞部件46所阻断,如图17所示,大量燃料可在一较宽角度上喷入燃烧室44;然而,通过转动外罩部件41以阻塞部件46阻断喷嘴本体3上的喷嘴孔43的一部分,如图18或19所示,则喷射的范围变窄。再者,通过进一步转动外罩部件41,喷嘴本体3上的喷嘴孔43变为全部被阻塞部件阻断,如图20所示,则即使针阀10提升,也没有燃料喷射。结果,通过控制第二微电机31,可以改变所喷喷雾的弥散程度和喷嘴孔的张开面积,从而如前述第一实施例,可以改变喷射压力、喷射时间和雾化程度,获得多种喷射模式。The structure in which the
如图21至24所示,为了实现对喷嘴孔43的张开状态的调节,还有另一种结构的例子,即一第四种结构的例子。在此实施例中,与第三种结构的例子类似,在其相互间相位偏移为180°的两个位置上形成有狭缝状喷嘴孔,但喷嘴孔43是楔形的,在喷嘴孔的张开面积为外罩部件41所缩小的方向上它们是逐渐减小的。由于此实施例的其它方面与第三实施例的一致,所以与图17至20中所示一致的部件也标出同样的参考数字,且对它们的说明也省略了。在此结构中,也获得了与第三实施例中所获得的相类似的优点。As shown in FIGS. 21 to 24, in order to realize the adjustment of the opening state of the
正如已经说明的,根据本发明的实施例,由于打开和关闭喷嘴孔的针阀的最大提升量由提升量改变机构进行调节,所以就有可能促进喷雾的微细雾化和保持稳定燃烧。另外,通过有目的地改变喷射模式,即在一蓄积式喷嘴的情况下通过改变喷射量,而在一脉动式喷嘴的情况下通过改变喷射压力和喷射速度,它能够适合于多种环境。As has been explained, according to the embodiment of the present invention, since the maximum lift of the needle valve opening and closing the nozzle hole is adjusted by the lift changing mechanism, it is possible to promote fine atomization of spray and maintain stable combustion. In addition, it can be adapted to various environments by purposefully changing the spray pattern, that is, by changing the spray quantity in the case of an accumulation type nozzle, and by changing the spray pressure and spray speed in the case of a pulse type nozzle.
另外,由于起喷射作用的喷嘴孔的总面积可以通过转动外罩部件来调节,所以使获得一个与一给定负载和发动机转速相符合的喷射压力、喷射时间和喷射量,进而实现减少NOx和提高燃料效率成为可能。再者,由于起喷射作用的喷嘴孔的总面积可以通过采用外罩部件来从外面进行调节,所以在喷嘴本体内部就不需要有用于改变喷嘴孔面积的部件,进而成功地减少了就在喷嘴孔前形成的吸入量。在这样一种结构中,改变喷嘴孔的有效面积的外罩部件的轴线和喷嘴本体内的阀门不需要在一条直线上。再有,由于改变了喷嘴孔的前端的张开面积,所以便于所喷燃料的微细雾化。In addition, since the total area of the nozzle holes that are used for injection can be adjusted by rotating the outer cover part, an injection pressure, injection time and injection amount that are consistent with a given load and engine speed are obtained, thereby reducing NOx and improving Fuel efficiency is possible. Furthermore, since the total area of the nozzle hole for spraying can be adjusted from the outside by using the cover member, there is no need for a part for changing the area of the nozzle hole inside the nozzle body, thereby successfully reducing the area of the nozzle hole in the nozzle hole. The amount of inhalation formed before. In such a structure, the axis of the housing member which changes the effective area of the nozzle hole and the valve in the nozzle body need not be in a straight line. Furthermore, since the opening area of the front end of the nozzle hole is changed, fine atomization of the injected fuel is facilitated.
再者,通过结合起喷射作用的喷嘴孔的总面积的调节进行针阀提升量的调节,可以以更大的自由度改变喷射模式,以适于多种环境条件。Furthermore, by adjusting the lift amount of the needle valve in combination with the adjustment of the total area of the nozzle holes that perform the injection function, the injection mode can be changed with greater freedom to adapt to various environmental conditions.
Claims (14)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 95196309 CN1164270A (en) | 1994-09-22 | 1995-08-31 | fuel nozzle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP254539/94 | 1994-09-22 | ||
| CN 95196309 CN1164270A (en) | 1994-09-22 | 1995-08-31 | fuel nozzle |
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| CN1164270A true CN1164270A (en) | 1997-11-05 |
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| CN 95196309 Pending CN1164270A (en) | 1994-09-22 | 1995-08-31 | fuel nozzle |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100373044C (en) * | 2004-03-31 | 2008-03-05 | 三菱扶桑卡客车公司 | Fuel jetting device |
| CN100374711C (en) * | 2004-03-31 | 2008-03-12 | 三菱扶桑卡客车公司 | fuel injection device |
| CN101598096B (en) * | 2009-05-12 | 2012-04-25 | 靳北彪 | Global fuel injection device for engine |
| CN107559883A (en) * | 2017-09-25 | 2018-01-09 | 上海泛智能源装备有限公司 | A kind of fuel nozzle and gas turbine |
| CN109690069A (en) * | 2016-09-16 | 2019-04-26 | 珀金斯发动机有限公司 | Fuel injector and piston cup |
-
1995
- 1995-08-31 CN CN 95196309 patent/CN1164270A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100373044C (en) * | 2004-03-31 | 2008-03-05 | 三菱扶桑卡客车公司 | Fuel jetting device |
| CN100374711C (en) * | 2004-03-31 | 2008-03-12 | 三菱扶桑卡客车公司 | fuel injection device |
| CN101598096B (en) * | 2009-05-12 | 2012-04-25 | 靳北彪 | Global fuel injection device for engine |
| CN109690069A (en) * | 2016-09-16 | 2019-04-26 | 珀金斯发动机有限公司 | Fuel injector and piston cup |
| CN107559883A (en) * | 2017-09-25 | 2018-01-09 | 上海泛智能源装备有限公司 | A kind of fuel nozzle and gas turbine |
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