CN107489575B - A multi-parameter measurement device and measurement method for engine fuel injection performance - Google Patents
A multi-parameter measurement device and measurement method for engine fuel injection performance Download PDFInfo
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- 239000007924 injection Substances 0.000 title claims abstract description 171
- 238000002347 injection Methods 0.000 title claims abstract description 171
- 239000000446 fuel Substances 0.000 title claims abstract description 156
- 238000005259 measurement Methods 0.000 title claims abstract description 37
- 238000000691 measurement method Methods 0.000 title claims abstract description 23
- 239000003921 oil Substances 0.000 claims abstract description 63
- 238000000034 method Methods 0.000 claims abstract description 46
- 238000009434 installation Methods 0.000 claims abstract description 25
- 230000035515 penetration Effects 0.000 claims abstract description 13
- 238000004458 analytical method Methods 0.000 claims abstract description 4
- 230000002159 abnormal effect Effects 0.000 claims description 3
- 239000010724 circulating oil Substances 0.000 claims description 3
- 238000003384 imaging method Methods 0.000 claims description 2
- 230000002459 sustained effect Effects 0.000 claims 1
- 239000000295 fuel oil Substances 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 8
- 230000002688 persistence Effects 0.000 description 3
- 229920001651 Cyanoacrylate Polymers 0.000 description 1
- 239000004830 Super Glue Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M65/00—Testing fuel-injection apparatus, e.g. testing injection timing ; Cleaning of fuel-injection apparatus
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Abstract
本发明公开了一种发动机喷油性能多参数测量装置与方法,所述装置包括测量板、曲轴安装孔、曲轴转角刻度盘、刻度盘指针、喷油器安装孔、油束测量刻度线和摄像装置,本发明的两冲程航空重油活塞发动机喷油性能多参数测量方法使用所设计的多功能测量板,能测量喷油提前角、喷油持续角、喷射贯穿度、喷油广角、喷油量、喷射速率以及进行正常喷射情况分析。解决了传统的发动机喷油性能测量方法只能测量其中一两种参数,而不能将所有参数都采集到位,而且仪器繁多,操作复杂,测量成本高的问题。具有多功能、低成本、高效率、操作方便快捷等优点。
The invention discloses a multi-parameter measuring device and method for engine fuel injection performance. The device comprises a measuring plate, a crankshaft installation hole, a crankshaft rotation angle dial, a dial pointer, a fuel injector installation hole, an oil beam measurement scale line and a camera. The device, the multi-parameter measurement method of the fuel injection performance of the two-stroke aviation heavy oil piston engine of the present invention uses the designed multi-function measuring board, which can measure the fuel injection advance angle, the fuel injection duration angle, the injection penetration, the fuel injection wide angle, and the fuel injection quantity. , injection rate, and analysis of normal injection conditions. It solves the problems that the traditional engine fuel injection performance measurement method can only measure one or two parameters, but cannot collect all parameters in place, and has many instruments, complicated operation and high measurement cost. It has the advantages of multi-function, low cost, high efficiency, convenient and quick operation and so on.
Description
技术领域technical field
本发明涉及活塞发动机喷油性能参数测量领域,具体涉及一种两冲程航空重油活塞发动机喷油性能多参数测量装置与测量方法。The invention relates to the field of measurement of fuel injection performance parameters of piston engines, in particular to a multi-parameter measurement device and measurement method for fuel injection performance of a two-stroke aviation heavy oil piston engine.
背景技术Background technique
两冲程航空重油活塞发动机在通用航空和无人机领域扮演非常重要的角色。获取发动机喷油性能的所有参数是发动机供油系统管理必不可少的一步,现有技术中所涉及的发动机喷油性能测量方法都只能测量其中一两种参数,测全发动机所有的喷油性能参数需要大量的仪器设备,不仅花销昂贵,而且过程复杂繁琐,操作不方便,测量效率低。因此开发一种能够测全两冲程航空重油活塞发动机喷油性能多参数的测量方法是十分必要的。Two-stroke aviation heavy oil piston engines play a very important role in general aviation and unmanned aerial vehicles. Obtaining all the parameters of the engine fuel injection performance is an essential step in the management of the engine fuel supply system. The engine fuel injection performance measurement methods involved in the prior art can only measure one or two of these parameters, and measure all the fuel injection of the entire engine. Performance parameters require a lot of equipment, which is not only expensive, but also complicated and cumbersome in the process, inconvenient to operate, and low in measurement efficiency. Therefore, it is necessary to develop a measurement method that can measure the multi-parameters of the fuel injection performance of the full two-stroke aviation heavy oil piston engine.
传统的发动机喷油性能参数测量方法,如中国实用新型专利CN201110261378所公开的喷油器开启时间测量设备,虽然能比较准确地确定喷油器开启时间,但是不能测量喷油提前角等其他重要喷油性能参数;又如专利CN201410248080所公开的喷油规律测量方法,能够准确测量喷油量,但整套系统部件繁多,也不能测量油束喷射贯穿度等其他喷油性能参数;再如专利CN201410429321所公开的柴油机喷油器喷油情况观察装置,有排气扇、螺旋排气管等复杂的附加装置,所测量的喷油质量和发动机真实喷油情况有较大误差。The traditional engine fuel injection performance parameter measurement method, such as the fuel injector opening time measuring device disclosed in Chinese utility model patent CN201110261378, although it can relatively accurately determine the fuel injector opening time, it cannot measure other important injectors such as fuel injection advance angle. Oil performance parameters; another example is the method for measuring the fuel injection law disclosed in patent CN201410248080, which can accurately measure the fuel injection quantity, but the whole system has many components, and cannot measure other fuel injection performance parameters such as the penetration of oil jet; The disclosed device for observing the fuel injection situation of the diesel engine injector has complex additional devices such as exhaust fans and spiral exhaust pipes, and the measured fuel injection quality has a large error with the actual fuel injection situation of the engine.
发明内容SUMMARY OF THE INVENTION
基于上述的发动机喷油性能参数测量不全、装置复杂、成本高等技术问题,本发明提供了一种两冲程航空重油活塞发动机喷油性能多参数测量装置与方法。所设计的多功能测量板能满足喷油性能多参数测量的要求,本方法相比传统测量方法具有功能多、成本低、效率高、操作方便快捷等优点。Based on the above technical problems of incomplete measurement of engine fuel injection performance parameters, complex device and high cost, the present invention provides a device and method for measuring multiple parameters of fuel injection performance of a two-stroke aviation heavy oil piston engine. The designed multifunctional measurement board can meet the requirements of multi-parameter measurement of fuel injection performance. Compared with the traditional measurement method, this method has the advantages of multi-function, low cost, high efficiency, convenient and quick operation and so on.
本发明完整的技术方案包括:The complete technical solution of the present invention includes:
一种发动机喷油性能多参数测量装置,包括测量板、曲轴安装孔、曲轴转角刻度盘、刻度盘指针、喷油器安装孔、油束测量刻度线和摄像装置。A multi-parameter measuring device for engine fuel injection performance, comprising a measuring plate, a crankshaft installation hole, a crankshaft rotation angle dial, a dial pointer, an injector installation hole, an oil beam measurement scale line and a camera device.
所述测量板设有曲轴转角刻度盘、曲轴安装孔和喷油器安装孔,曲轴安装孔位于曲轴转角刻度盘中心处,并通过曲轴安装孔安装于曲轴上,曲轴转角刻度盘与曲轴同心,所述曲轴安装孔与发动机曲轴之间为间隙配合,曲轴转角刻度盘上有角度刻度,所述刻度盘指针位于曲轴表面的安装孔内,并可随曲轴旋转,即刻度盘指针可指示曲轴转角;所述的喷油器安装孔安装于喷油器上,油束测量刻度线设于测量板上,并位于每个喷油孔正对出的位置。The measuring plate is provided with a crankshaft angle dial, a crankshaft installation hole and an injector installation hole, the crankshaft installation hole is located at the center of the crankshaft angle dial, and is installed on the crankshaft through the crankshaft installation hole, and the crankshaft angle dial is concentric with the crankshaft, There is a clearance fit between the crankshaft installation hole and the engine crankshaft. The crankshaft angle dial has an angle scale. The dial pointer is located in the installation hole on the crankshaft surface and can rotate with the crankshaft, that is, the dial pointer can indicate the crankshaft angle. The installation hole of the fuel injector is installed on the fuel injector, and the oil beam measurement scale line is arranged on the measuring plate, and is located at the position where each fuel injection hole is directly facing out.
所述的曲轴转角刻度盘上的刻度以1度为单位,共360个刻度。The scales on the crankshaft angle dial are in units of 1 degree, with a total of 360 scales.
刻度盘指针与曲轴表面安装孔之间为过盈配合。There is an interference fit between the dial pointer and the mounting hole on the crankshaft surface.
发动机的曲轴安装在测量板的左侧,喷油器安装在测量板的右侧。The crankshaft of the engine is mounted on the left side of the measuring plate, and the injectors are mounted on the right side of the measuring plate.
所述的曲轴转角刻度盘上的重要刻度以红色表示,优选的,所述的曲轴转角刻度盘为发动机活塞到达上止点时刻度盘指针所指的刻度,以及达到上止点前9度、12度、15度时对应的刻度。The important scales on the crankshaft angle dial are indicated in red. Preferably, the crankshaft angle dial is the scale pointed by the dial pointer when the engine piston reaches the top dead center, and 9 degrees before reaching the top dead center. The corresponding scale at 12 degrees and 15 degrees.
喷油器安装孔与喷油器之间为小过盈配合,喷油器与测量板形成紧配合并与其垂直,无相对运动;There is a small interference fit between the injector mounting hole and the injector, and the injector and the measuring plate form a tight fit and are perpendicular to it without relative movement;
安装后喷油器喷油孔的位置距离测量板为5mm。After installation, the position of the injection hole of the injector is 5mm away from the measuring plate.
油束测量刻度线的数量根据喷油器喷油孔的数量确定,优选的为4或5个。The number of oil beam measurement scale lines is determined according to the number of fuel injection holes of the fuel injector, preferably 4 or 5.
油束测量刻度线刻度长300mm,最小刻度为1mm,0刻度为喷油孔所在的位置。The oil beam measurement scale line scale is 300mm long, the minimum scale is 1mm, and the 0 scale is the position of the oil injection hole.
所述的测量板表面经过磨砂处理。The surface of the measuring plate is frosted.
所述的摄像装置为高速相机,优选的,所述的高速相机1秒可摄1000帧。The imaging device is a high-speed camera. Preferably, the high-speed camera can capture 1000 frames per second.
利用所述发动机喷油性能多参数测量装置对喷油性能参数进行测量的方法,其特征在于,喷油提前角测量方法为:测量在测功机反拖发动机转速至某一转速时开始,用摄像装置记录喷油器喷油的全过程,在图像处理软件中观察喷油的情况,当某一帧喷油孔出口处第一次出现油束时,刻度盘指针所在的位置与上止点位置的夹角Φ为喷油提前角。The method for measuring the fuel injection performance parameters using the multi-parameter measuring device for fuel injection performance of the engine is characterized in that, the method for measuring the fuel injection advance angle is as follows: the measurement starts when the dynamometer reverses the engine speed to a certain speed, and uses The camera device records the entire process of fuel injection by the fuel injector, and observes the fuel injection situation in the image processing software. When the fuel beam first appears at the exit of the fuel injection hole in a certain frame, the position of the dial pointer and the top dead center The included angle Φ of the position is the fuel injection advance angle.
所述的某一转速为600转/分钟。Said certain rotational speed is 600 rpm.
喷油持续角测量方法为:测量在测功机反拖发动机转速至某一转速时开始,用摄像装置记录喷油器喷油全过程,在图像处理软件中观察喷油的情况,当某一帧油束开始离开喷油孔出口处时,刻度盘指针所指的位置与喷油提前角位置的夹角△Φ为喷油持续角。The measurement method of the fuel injection duration angle is as follows: the measurement starts when the dynamometer reverses the engine speed to a certain speed, records the entire fuel injection process of the fuel injector with a camera device, and observes the fuel injection situation in the image processing software. When the frame oil beam starts to leave the outlet of the injection hole, the angle △Φ between the position pointed by the dial pointer and the position of the injection advance angle is the injection duration angle.
所述的某一转速为600转/分钟。Said certain rotational speed is 600 rpm.
喷油贯穿度测量方法为:在测功机反拖发动机转速至第一转速、第二转速、第三转速时,分别用摄像装置记录喷油器喷油全过程,在图像处理软件中观察相应转速喷油的情况,当某一帧油束开始离开喷油孔出口处时,记录油束始端到达油束测量刻度线的位置和油束末端所在的位置,两位置的刻度差L即代表喷油贯穿度的大小。The fuel injection penetration measurement method is as follows: when the dynamometer reverses the engine speed to the first speed, the second speed, and the third speed, use the camera to record the whole process of the fuel injection of the fuel injector, and observe the corresponding fuel injection in the image processing software. In the case of fuel injection at rotational speed, when the oil beam begins to leave the outlet of the injection hole in a certain frame, record the position where the beginning of the oil beam reaches the measurement scale line of the oil beam and the position where the end of the oil beam is located. The size of the oil penetration.
优选的,所述的第一转速为600转/分钟、第二转速为1800转/分钟,第三转速为2400转/分钟。Preferably, the first rotational speed is 600 rpm, the second rotational speed is 1800 rpm, and the third rotational speed is 2400 rpm.
喷油量测量方法为:在测功机反拖发动机转速至第一转速、第二转速、第三转速时,分别用摄像装置记录喷油器喷油全过程,在图像处理软件中计算相应转速油束离开喷油器时油束所占图片的像素面积,根据标定过的像素面积与油量的关系来确定喷油量。The fuel injection quantity measurement method is as follows: when the dynamometer reverses the engine speed to the first speed, the second speed and the third speed, use the camera to record the whole process of the fuel injector, and calculate the corresponding speed in the image processing software. The pixel area of the picture occupied by the oil beam when the oil beam leaves the injector, and the fuel injection amount is determined according to the relationship between the calibrated pixel area and the oil amount.
优选的,所述的第一转速为600转/分钟、第二转速为1800转/分钟,第三转速为2400转/分钟。Preferably, the first rotational speed is 600 rpm, the second rotational speed is 1800 rpm, and the third rotational speed is 2400 rpm.
喷油广角测量方法为:在测功机反拖发动机转速至第一转速、第二转速、第三转速时,分别用摄像装置记录喷油器喷油全过程;在图像处理软件中观察相应转速的油束形状,油束上边界与下边界的夹角α即为喷油广角。The fuel injection wide-angle measurement method is: when the dynamometer reverses the engine speed to the first speed, the second speed, and the third speed, use the camera to record the whole process of the fuel injector; observe the corresponding speed in the image processing software The shape of the oil beam, the angle α between the upper boundary and the lower boundary of the oil beam is the wide angle of injection.
优选的,所述的第一转速为600转/分钟、第二转速为1800转/分钟,第三转速为2400转/分钟。Preferably, the first rotational speed is 600 rpm, the second rotational speed is 1800 rpm, and the third rotational speed is 2400 rpm.
喷射速率测量方法为:在测功机反拖发动机转速至第一转速、第二转速、第三转速时,分别用摄像装置记录喷油器喷油全过程,在图像处理软件中记录相应转速某T1时刻油束始端在刻度线的上的刻度值L1以及下一帧T2时刻油束始端在刻度线上的刻度值L2,利用两刻度的差△L与时间间隔△T来计算此刻的喷油速率。The injection rate measurement method is: when the dynamometer reverses the engine speed to the first speed, the second speed, and the third speed, the camera device is used to record the whole process of the fuel injector, and the corresponding speed is recorded in the image processing software. The scale value L 1 of the beginning of the oil beam on the scale line at T1 and the scale value L 2 of the beginning of the oil beam on the scale line at the next frame T2 are calculated by using the difference ΔL of the two scales and the time interval ΔT The fuel injection rate at the moment.
优选的,所述的第一转速为600转/分钟、第二转速为1800转/分钟,第三转速为2400转/分钟。Preferably, the first rotational speed is 600 rpm, the second rotational speed is 1800 rpm, and the third rotational speed is 2400 rpm.
喷射情况分析方法为:在测功机反拖发动机转速至第一转速、第二转速、第三转速时,且柱塞转角分别调整至单缸循环油量在第一油量、第二油量位置时,用摄像装置记录喷油器在发动机多个循环的喷油全过程,在图像处理软件中观察是否出现隔次喷射和二次喷射等不正常喷射的情况,出现隔次喷射时可测量相邻循环的喷油量差是否满足要求,出现二次喷射时可测量喷油持续角、喷油贯穿度是否满足要求。The injection situation analysis method is: when the dynamometer reverses the engine speed to the first speed, the second speed, and the third speed, and the plunger angle is adjusted to the single-cylinder circulating oil volume at the first oil volume and the second oil volume respectively. When it is in position, use a camera to record the whole process of fuel injection of the fuel injector in multiple cycles of the engine, and observe whether there are abnormal injections such as alternate injection and secondary injection in the image processing software. Whether the difference in fuel injection quantity between adjacent cycles meets the requirements, and when secondary injection occurs, it can be measured whether the fuel injection duration angle and the fuel injection penetration meet the requirements.
优选的,所述的第一转速为600转/分钟、第二转速为1800转/分钟,第三转速为2400转/分钟。Preferably, the first rotational speed is 600 rpm, the second rotational speed is 1800 rpm, and the third rotational speed is 2400 rpm.
优选的,所述的第一油量为3mg,第二油量为12mg。Preferably, the first oil amount is 3 mg, and the second oil amount is 12 mg.
优选的,所述的多个循环为10个循环。Preferably, the multiple cycles are 10 cycles.
本发明相对于现有技术的优点在于:The advantages of the present invention relative to the prior art are:
(1)本发明的多功能测量板同时含有曲轴转角刻度盘、油束测量刻度线,能够耦合多种测量方法,具有多功能、高效率的优点。(1) The multifunctional measuring plate of the present invention simultaneously includes a crankshaft angle dial and an oil beam measurement scale, which can be coupled with a variety of measurement methods, and has the advantages of multifunctionality and high efficiency.
(2)本发明的测量方法所需要的仪器少,具有低成本的优点。(2) The measuring method of the present invention requires less instruments and has the advantage of low cost.
(3)本发明的测量方法操作简便,测量结果可靠,具有实用性强的优点。(3) The measurement method of the present invention has the advantages of simple operation, reliable measurement results and strong practicability.
附图说明Description of drawings
图1是本发明的多功能测量板的平面视图。FIG. 1 is a plan view of the multifunctional measuring board of the present invention.
图2是本发明喷油提前角测量方法示意图。FIG. 2 is a schematic diagram of the method for measuring the fuel injection advance angle of the present invention.
图3是本发明喷油持续角测量方法示意图。3 is a schematic diagram of the method for measuring the fuel injection persistence angle of the present invention.
图4是本发明喷射贯穿度、喷油广角、喷油量测量方法示意图。FIG. 4 is a schematic diagram of the method for measuring injection penetration, wide angle of fuel injection and fuel injection quantity according to the present invention.
图5是本发明喷射速率测量方法示意图。FIG. 5 is a schematic diagram of the method for measuring the injection rate of the present invention.
图中:101-曲轴安装孔,102-曲轴转角刻度盘,103-刻度盘指针,104-重要刻度,105-喷油器安装孔,106-油束测量刻度线,201-刻度盘指针所在的位置,202-喷油器,203-油束,204-喷油提前角。In the picture: 101- crankshaft mounting hole, 102- crankshaft angle dial, 103- dial pointer, 104- important scale, 105- fuel injector mounting hole, 106- oil beam measurement scale line, 201- where the dial pointer is located Position, 202-injector, 203-fuel beam, 204-fuel injection advance angle.
具体实施方式Detailed ways
下面结合附图和具体实施方式对本发明做进一步说明。The present invention will be further described below with reference to the accompanying drawings and specific embodiments.
本发明的一个方面,提供一种多功能测量板,实施方式为:One aspect of the present invention provides a multifunctional measuring board, the embodiment is as follows:
如附图1所示,本发明的多功能测量板包括曲轴安装孔101、曲轴转角刻度盘102、刻度盘指针103、喷油器安装孔105、油束测量刻度线106五个部分。发动机的曲轴安装在测量板的左侧,喷油器安装在测量板的右侧。As shown in FIG. 1 , the multifunctional measuring plate of the present invention includes five parts: crankshaft installation hole 101 , crankshaft angle dial 102 , dial pointer 103 , fuel injector installation hole 105 , and oil beam measurement scale line 106 . The crankshaft of the engine is mounted on the left side of the measuring plate, and the injectors are mounted on the right side of the measuring plate.
所述的曲轴安装孔101与发动机曲轴之间为间隙配合,两者之间不会造成相互摩擦,因此发动机曲轴的震动不会传递给测量板,保证了测量板的稳定性。The crankshaft mounting hole 101 and the engine crankshaft are in clearance fit, and there will be no mutual friction between the two, so the vibration of the engine crankshaft will not be transmitted to the measuring plate, which ensures the stability of the measuring plate.
所述的刻度盘安装在与曲轴同心的位置,以1度为单位,共360个刻度,其中重要的刻度104,如发动机活塞到达上止点时刻度盘指针103所指的刻度,上止点前9度、12度、15度时对应的刻度,用红线描出,方便测量时将实际喷油提前角与理论喷油提前角对比。The said dial is installed at the position concentric with the crankshaft, with 1 degree as the unit, there are 360 scales in total, among which the important scale 104, such as the scale pointed by the dial pointer 103 when the engine piston reaches the top dead center, the top dead center. The corresponding scales at the first 9 degrees, 12 degrees and 15 degrees are drawn with red lines, which is convenient for comparing the actual fuel injection advance angle with the theoretical fuel injection advance angle during measurement.
所述的刻度盘指针103座落在曲轴表面的安装孔内,两者为过盈配合,安装时在孔内加入强力胶,保证安装后的刻度盘指针103不会因为曲轴高速旋转的离心力将其甩出,指针可指示曲轴转角。The dial pointer 103 is seated in the mounting hole on the surface of the crankshaft, and the two are interference fit. During installation, super glue is added to the hole to ensure that the dial pointer 103 after installation will not be damaged due to the centrifugal force of the high-speed rotation of the crankshaft. It is thrown out, and the pointer can indicate the crankshaft angle.
所述的测量板表面经过磨砂处理,保证进行喷油性能测量拍摄时不会对镜头造成反光,性能测量需要1秒可摄1000帧的高速相机配合使用。The surface of the measuring plate is frosted to ensure that the lens will not be reflected when shooting for fuel injection performance measurement. The performance measurement needs to be used in conjunction with a high-speed camera capable of shooting 1,000 frames per second.
所述的喷油器安装孔105与喷油器之间为小过盈配合,喷油器安装后与测量板形成紧配合并与其垂直,无相对运动,保证喷油器在性能测量过程中的位置是一定的,提高测量的可靠性;安装后喷油器喷油孔的位置距离测量板为5mm。There is a small interference fit between the injector installation hole 105 and the injector. After the injector is installed, it forms a tight fit with the measuring plate and is perpendicular to it, and there is no relative movement to ensure that the injector is in the process of performance measurement. The position is fixed, which improves the reliability of the measurement; the position of the injection hole of the injector after installation is 5mm away from the measuring plate.
所述的油束测量刻度线106通过魔术贴贴在测量板上,粘贴较牢固,不会在测量过程中产生松动;刻度线的数量根据喷油器喷油孔的数量确定,通常为4或5个,贴在喷油器安装在测量板后在每个喷油孔正对出的位置,保证测量相关喷油性能参数的准确性;刻度线刻度长300mm,最小刻度为1mm,0刻度被认为是喷油孔所在的位置。The oil beam measurement scale line 106 is pasted on the measuring plate through Velcro, which is firmly pasted and will not loosen during the measurement process; 5 pieces, attached to the position facing each injection hole after the injector is installed on the measuring plate, to ensure the accuracy of measuring the relevant fuel injection performance parameters; the length of the scale line is 300mm, the minimum scale is 1mm, and the 0 scale is It is considered to be where the injection hole is located.
根据本发明的另一个方面,提供测量喷油提前角、喷油持续角、喷射贯穿度、喷油广角、喷油量、喷射速率以及分析正常喷射情况的方法,实施方式为:According to another aspect of the present invention, there is provided a method for measuring fuel injection advance angle, fuel injection duration angle, injection penetration, fuel injection wide angle, fuel injection quantity, injection rate and analyzing normal injection conditions. The embodiments are:
本发明喷油提前角测量方法示意图如附图2所示。测量在测功机反拖发动机转速至600转/分钟时开始,用高速相机记录喷油器202喷油的全过程。在专业图像处理软件中观察喷油的情况,当某一帧喷油孔出口处第一次出现油束203时,刻度盘指针103所在的位置201与上止点位置的夹角Φ204为喷油提前角。A schematic diagram of the fuel injection advance angle measurement method of the present invention is shown in FIG. 2 . The measurement starts when the speed of the dynamometer anti-drag engine reaches 600 rpm, and the whole process of fuel injection by the
本发明喷油持续角测量方法示意图如附图3所示。测量在测功机反拖发动机转速至600转/分钟时开始,用高速相机记录喷油器喷油全过程。在专业图像处理软件中观察喷油的情况,当某一帧油束303开始离开喷油孔出口处时,刻度盘指针103所指的位置301与喷油提前角位置的夹角△Φ为喷油持续角。A schematic diagram of the fuel injection persistence angle measurement method of the present invention is shown in FIG. 3 . The measurement started when the dynamometer reversed the engine speed to 600 rpm, and a high-speed camera was used to record the whole process of fuel injection by the fuel injector. Observe the situation of fuel injection in professional image processing software. When the
本发明喷射贯穿度、喷油广角、喷油量测量方法示意图如附图4所示。A schematic diagram of the method for measuring injection penetration, wide angle of fuel injection, and fuel injection quantity of the present invention is shown in FIG. 4 .
所述的喷油贯穿度测量在测功机反拖发动机转速至600、1800、2400转/分钟时开始,用高速相机记录喷油器喷油全过程。在专业图像处理软件中观察相应转速喷油的情况,当某一帧油束303开始离开喷油孔出口处时,记录油束始端到达油束测量刻度线106的位置和油束末端所在的位置,两位置的刻度差L401即可代表喷油贯穿度的大小。The fuel injection penetration measurement was started when the dynamometer anti-trag engine speed reached 600, 1800, and 2400 rpm, and a high-speed camera was used to record the entire fuel injection process of the fuel injector. Observe the fuel injection situation at the corresponding speed in professional image processing software. When a certain frame of
所述的喷油广角测量在测功机反拖发动机转速至600、1800、2400转/分钟时开始,用高速相机记录喷油器喷油全过程。在专业图像处理软件中观察相应转速的油束形状,油束上边界与下边界的夹角α402即为喷油广角。The fuel injection wide-angle measurement starts when the dynamometer anti-trag engine speed reaches 600, 1800, and 2400 rpm, and a high-speed camera is used to record the entire process of fuel injection by the fuel injector. Observe the shape of the oil beam at the corresponding speed in professional image processing software. The angle α402 between the upper boundary and the lower boundary of the oil beam is the wide angle of injection.
所述的喷油量测量在测功机反拖发动机转速至600、1800、2400转/分钟时开始,用高速相机记录喷油器喷油全过程。在专业图像处理软件中计算相应转速油束离开喷油器时油束403所占图片的像素面积,根据标定过的像素面积与油量的关系来确定喷油量。The fuel injection quantity measurement starts when the dynamometer anti-drag engine speed reaches 600, 1800, and 2400 rpm, and a high-speed camera is used to record the entire process of fuel injection by the fuel injector. In professional image processing software, calculate the pixel area of the picture occupied by the
本发明喷射速率测量方法示意图如附图5所示。测量在测功机反拖发动机转速至600、1800、2400转/分钟时开始,用高速相机记录喷油器喷油全过程。在专业图像处理软件中记录相应转速某T1时刻油束502始端在刻度线的上的刻度值L1以及下一帧T2时刻油束501始端在刻度线上的刻度值L2,利用两刻度的差△L503与时间间隔△T来计算此刻的喷油速率。The schematic diagram of the injection rate measurement method of the present invention is shown in FIG. 5 . The measurement started when the dynamometer reversed the engine speed to 600, 1800, and 2400 rpm, and a high-speed camera was used to record the whole process of fuel injection by the fuel injector. In the professional image processing software, record the scale value L 1 of the beginning of the oil beam 502 on the scale line at a certain time T1 of the corresponding rotation speed and the scale value L 2 of the beginning of the oil beam 501 on the scale line at the next frame T2. The difference between the scales ΔL503 and the time interval ΔT is used to calculate the fuel injection rate at the moment.
所述的正常喷射情况分析在测功机反拖发动机转速至600、1800、2400转/分钟、柱塞转角调整至单缸循环油量在3mg、12mg位置时开始,用高速相机记录喷油器在发动机10个循环的喷油全过程,总计测量6组,在专业图像处理软件中观察是否出现隔次喷射和二次喷射等不正常喷射的情况,出现隔次喷射时可测量相邻循环的喷油量差是否满足要求,出现二次喷射时可测量喷油持续角、喷油贯穿度是否满足要求。The analysis of the normal injection situation is started when the dynamometer anti-trag engine speed reaches 600, 1800, 2400 rpm, the plunger angle is adjusted to the position of 3 mg and 12 mg of circulating oil in a single cylinder, and the injector is recorded with a high-speed camera. In the whole process of the 10-cycle fuel injection of the engine, a total of 6 groups are measured. In the professional image processing software, observe whether there are abnormal injections such as alternate injections and secondary injections. When the alternate injection occurs, the adjacent cycles can be measured. Whether the difference in fuel injection quantity meets the requirements, and when secondary injection occurs, it can be measured whether the fuel injection duration angle and the fuel injection penetration meet the requirements.
以上所述,仅是本发明的较佳实施例,并非对本发明作任何限制,凡是根据本发明技术实质对以上实施例所作的任何简单修改、变更以及等效结构变化,均仍属于本发明技术方案的保护范围内。The above are only preferred embodiments of the present invention and do not limit the present invention. Any simple modifications, changes and equivalent structural changes made to the above embodiments according to the technical essence of the present invention still belong to the technology of the present invention. within the scope of the program.
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