CN203745202U - Test engine rear power take-off - Google Patents
Test engine rear power take-off Download PDFInfo
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- CN203745202U CN203745202U CN201420047941.6U CN201420047941U CN203745202U CN 203745202 U CN203745202 U CN 203745202U CN 201420047941 U CN201420047941 U CN 201420047941U CN 203745202 U CN203745202 U CN 203745202U
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Abstract
Description
技术领域technical field
本实用新型涉及一种发动机性能测试工具,尤其是涉及一种试验用发动机后取力器。The utility model relates to an engine performance testing tool, in particular to an engine rear power take-off for testing.
背景技术Background technique
后取力机构是发动机的重要附件之一。在多种工程机械机型中承担着重要的工作扭矩输出角色,在输出扭矩的同时也消耗一定的功率,所以要保证安全、可靠、顺利地完成后取力工作,就要对发动机的后取力端的输出结构进行台架试验,来模拟发动机后取力实际工作的状况;但在实际进行台架试验时,由于发动机后取力输出端内花键种类繁多,因此,设计一款通用型的后取力器,来满足不同花键结构的发动机是非常必要的。The rear power take-off mechanism is one of the important accessories of the engine. It plays an important role in the output of working torque in a variety of construction machinery models. It also consumes a certain amount of power while outputting torque. Therefore, in order to ensure safe, reliable and smooth completion of the rear power take-off work, it is necessary to control the rear take-off of the engine. The output structure of the power end is subjected to a bench test to simulate the actual working conditions of the power take-off of the engine; however, in the actual bench test, because there are many types of splines in the power take-off output end of the engine, it is necessary to design a general-purpose The rear power take-off is very necessary to meet the needs of engines with different spline structures.
目前发动机后取力台架试验中,花键形式的后取力输出端与台架测控系统的连接,有两种方式:如图1所示,第一种现有技术的方式是通过一端是外花键另一端是法兰盘的花键轴23连接的,花键轴23的花键端直接与发动机后取力输出端5的内花键相连,花键轴23的法兰盘端则与台架的万向联轴器17相连,通过这种方式连接来传递动力。对于第一种方式来说,连接由于整个传动系没有径向支撑,轴系会对花键轴23产生径向力,使花键轴23加速磨损,可靠性不高;同时该结构无封油油封,存在发动机齿轮箱机油流失的问题,极易造成因发动机机油压力过低,而损伤发动机;在台架试验过程中,需对不同发动机进行后取力输出功率测试,而每种发动机的后取力输出端5内花键结构可能都不相同,这样就要设计不同的花键轴23来满足试验要求,因花键轴23结构原因,其一端为较大的圆盘一端为花键轴,加工工艺较为复杂。如图2所示,第二种现有技术的方式是通过专用后取力器进行连接,根据发动机后取力输出端5内花键与飞轮壳16接口尺寸来设计专用后取力器、过渡连接盘1和后取力器花键轴24,过渡连接盘1完成后取力与飞轮壳16的连接固定,后取力花键轴24一端连接发动机后取力输出端5内花键,一端连台架的万向联轴器3,完成动力的传递。对于第二种方式来说,专用后取力器虽然满足了某一种制定机型后取力的试验要求,但在更换发动机后,由于发动机后取力输出端5内花键结构变化,以及飞轮壳16结构变化,造成该专用的后取力器无法继续使用,必须重新设计专用后取力器才能满足试验要求,这样无论从加工成本还是加工周期方面都是极大的浪费。At present, in the engine rear power take-off bench test, there are two ways to connect the rear power take-off output end in the form of a spline with the bench measurement and control system: as shown in Figure 1, the first prior art method is through one end is The other end of the external spline is connected by the spline shaft 23 of the flange, and the spline end of the spline shaft 23 is directly connected with the internal spline of the power take-off output end 5 of the engine, and the flange end of the spline shaft 23 is Link to each other with the universal joint 17 of stand, connect in this way and transmit power. For the first method, since the entire transmission system has no radial support, the shaft system will generate radial force on the spline shaft 23, which will accelerate the wear of the spline shaft 23, and the reliability is not high; at the same time, this structure has no seal oil Oil seal, there is a problem of oil loss in the engine gearbox, which can easily cause damage to the engine due to low engine oil pressure; The internal spline structure of the power output end 5 may be different, so it is necessary to design different spline shafts 23 to meet the test requirements. Due to the structure of the spline shaft 23, one end is a larger disc and the other end is a spline shaft , the processing technology is more complicated. As shown in Figure 2, the second prior art method is to connect through a special rear power take-off, and design the special rear power take-off, transition Connecting plate 1 and rear power take-off spline shaft 24, after the transition connecting plate 1 is completed, the connection between the power take-off and the flywheel housing 16 is fixed, and one end of the rear power take-off spline shaft 24 is connected to the internal spline of the engine rear power take-off output Connect the universal coupling 3 of the stand to complete the transmission of power. For the second method, although the special rear power take-off meets the test requirements of a certain type of rear power take-off, after the engine is replaced, due to the change of the internal spline structure of the rear power take-off output end 5 of the engine, and The change in the structure of the flywheel housing 16 has caused the special rear power take-off to be unusable, and the special rear power take-off must be redesigned to meet the test requirements, which is a huge waste in terms of processing cost and processing cycle.
实用新型内容Utility model content
本实用新型所要解决的技术问题是:提供一种试验用发动机后取力器,在更换不同规格的发动机时,只需更换通用型发动机后取力器中的过渡连接盘、第二主轴和花键隔套即可完成装配,降低工装制作成本,缩短试验准备周期,提高试验台架利用率的目的。The technical problem to be solved by the utility model is: to provide a test engine rear power take-off, when replacing engines of different specifications, only the transition connection plate, the second main shaft and the flower in the universal engine rear power take-off need to be replaced. The key spacer can be assembled, which reduces the cost of tooling production, shortens the test preparation period, and improves the utilization rate of the test bench.
为解决上述技术问题,本实用新型的技术方案是:试验用发动机后取力器,包括In order to solve the above-mentioned technical problems, the technical solution of the present invention is: the rear power take-off of the test engine, including
外套,所述外套内转动安装有第一主轴,所述第一主轴的一端通过花键连接有第二主轴,所述第二主轴的另一端设有与所述发动机的后取力输出端内花键相适配的外花键,所述第二主轴上套装有一花键轴隔套,所述花键轴隔套与所述发动机的后取力输出端内花键的端面相顶靠;Outer sleeve, the first main shaft is installed in rotation in the outer sleeve, one end of the first main shaft is connected with the second main shaft through a spline, and the other end of the second main shaft is provided with the rear power output end of the engine. An external spline that is compatible with the spline, a spline shaft spacer is set on the second main shaft, and the spline shaft spacer is against the end surface of the internal spline of the rear power output end of the engine;
过渡连接盘,所述过渡连接盘具有中空的空腔,所述第二主轴伸出所述空腔,所述外套通过紧固件安装于所述过渡连接盘上,所述过渡连接盘通过紧固件安装于所述发动机的飞轮壳上;A transition connection plate, the transition connection plate has a hollow cavity, the second main shaft protrudes from the cavity, the jacket is installed on the transition connection plate through fasteners, and the transition connection plate is tightened the firmware is mounted on the flywheel housing of the engine;
法兰轴套,所述法兰轴套套设并通过紧固件安装于所述第一主轴的另一端,所述法兰轴套通过紧固件与所述发动机后取力试验台架的万向联轴器连接。A flange bushing, the flange bushing is sheathed and installed on the other end of the first main shaft through a fastener, and the flange bushing is connected to the rear power take-off test bench of the engine through a fastener. Connect to the coupling.
优选的,所述外套包括通过紧固件安装在一起的外套体和外套体端盖,所述外套体内设有轴承安装腔,所述轴承安装腔内安装有两个轴承,所述两轴承之间设有轴承隔套,所述第一主轴安装于两所述轴承上。Preferably, the outer casing includes an outer casing and an outer casing end cap installed together by fasteners, a bearing installation cavity is arranged in the outer casing, two bearings are installed in the bearing installation cavity, and the two bearings A bearing spacer is arranged between them, and the first main shaft is installed on the two bearings.
优选的,所述轴承安装腔的两端分别设有一油封,所述外套体与轴承隔套之间形成润滑油腔,所述外套体上设有与所述润滑油腔连通的润滑油加注口,所述润滑油加注口内设有润滑油加注塞。Preferably, two ends of the bearing installation cavity are respectively provided with an oil seal, a lubricating oil chamber is formed between the outer casing and the bearing spacer, and a lubricating oil filling chamber communicating with the lubricating oil chamber is provided on the outer casing. The lubricating oil filling port is provided with a lubricating oil filling plug.
优选的,所述第一主轴靠近所述法兰轴套一端的端部设有螺纹孔,所述法兰轴套的法兰端面上设有一压块安装槽,所述压块安装槽内通过一螺栓压设有一压块,所述螺栓安装于所述螺纹孔内。Preferably, a threaded hole is provided at the end of the first main shaft close to one end of the flange bushing, and a pressing block installation groove is provided on the flange end surface of the flange bushing, and the pressing block installation groove passes through A bolt is pressed with a pressing block, and the bolt is installed in the threaded hole.
采用了上述技术方案,本实用新型的有益效果为:由于该通用型发动机后取力器的外套、过渡连接盘和法兰轴套,外套内转动安装有第一主轴,第一主轴通过花键连接有第二主轴,第二主轴的另一端设有与发动机的后取力输出端内花键相适配的外花键,第二主轴上套装有一花键轴隔套,过渡连接盘通过紧固件安装于所述发动机的飞轮壳上;法兰轴套通过紧固件与所述发动机后取力试验台架的万向联轴器连接,在发动机后取力试验台架进行更换发动机时,由于通用型后取力器只需更换过渡连接盘、第二主轴和花键轴隔套,这三种零部件结构简单,加工工艺简单,制作成本低,大大降低了试验准备成本,缩短了试验准备周期,提高了试验台架利用率,该通用型后取力器适合所有后取力发动机机型;通过安装该通用型后取力器,能将后取力输出端的扭转力可靠地传递至测工系统,从而准确的测出后取力输出功率。在更换不同规格的发动机时,只需更换通用型发动机后取力器中的过渡连接盘、第二主轴和花键隔套即可完成装配,降低工装制作成本,缩短试验准备周期,提高试验台架利用率的目的。Adopting the above-mentioned technical scheme, the beneficial effects of the utility model are as follows: due to the jacket, the transition connection plate and the flange bushing of the universal engine rear power take-off, the first main shaft is installed in rotation in the outer jacket, and the first main shaft passes through the spline It is connected with the second main shaft, and the other end of the second main shaft is provided with an external spline matching the internal spline of the rear power take-off output end of the engine. The firmware is installed on the flywheel housing of the engine; the flange bushing is connected with the universal coupling of the power take-off test bench behind the engine through fasteners, and when the engine is replaced by the power take-off test bench behind the engine , because the general-purpose rear power take-off only needs to replace the transition connection plate, the second main shaft and the spline shaft spacer, these three parts have simple structure, simple processing technology, and low manufacturing cost, which greatly reduces the test preparation cost and shortens the test time. The test preparation period improves the utilization rate of the test bench. The universal rear power take-off is suitable for all rear power take-off engine models; by installing the universal rear power take-off, the torsional force at the output end of the rear power take-off can be reliably transmitted To the measurement system, so as to accurately measure the output power of the rear force. When replacing engines of different specifications, the assembly can be completed only by replacing the transition connection plate, the second main shaft and the spline spacer in the rear power take-off of the general-purpose engine, which reduces the cost of tooling production, shortens the test preparation period, and improves the test bench. rack utilization purposes.
附图说明Description of drawings
图1是第一种现有技术的使用状态参考图;Fig. 1 is the reference diagram of the state of use of the first prior art;
图2是第二种现有技术的使用状态参考图;Fig. 2 is the reference diagram of the state of use of the second prior art;
图3是本实用新型的结构示意图;Fig. 3 is a structural representation of the utility model;
图4是本实用新型的零件分解图;Fig. 4 is an exploded view of parts of the utility model;
图5是本实用新型的使用状态参考图;Fig. 5 is the reference diagram of the use status of the utility model;
其中:1、过渡连接盘;2、法兰轴套2;3、第一主轴;4、第二主轴;5、后取力输出端;6、花键轴隔套;7、外套体;8、外套体端盖;9、轴承安装腔;10、轴承;11、轴承隔套;12、油封;13、润滑油腔;14、润滑油加注口;15、润滑油加注塞;16、飞轮壳;17、万向联轴器;18、螺纹孔;19、压块安装槽;20、螺栓;21、压块;22、止推卡簧;23、花键轴;24、后取力花键轴。Among them: 1. Transition connection plate; 2. Flange bushing 2; 3. First main shaft; 4. Second main shaft; 5. Rear power output end; 6. Spline shaft spacer; , Outer body end cover; 9, Bearing installation cavity; 10, Bearing; 11, Bearing spacer; 12, Oil seal; 13, Lubricating oil cavity; 14, Lubricating oil filling port; 15, Lubricating oil filling plug; 16, Flywheel housing; 17. Universal coupling; 18. Threaded hole; 19. Press block installation groove; 20. Bolt; 21. Press block; 22. Thrust spring; 23. Spline shaft; 24. Rear force spline shaft.
具体实施方式Detailed ways
下面结合附图和实施例对本实用新型进一步说明。Below in conjunction with accompanying drawing and embodiment the utility model is further described.
如图3和4共同所示,试验用发动机后取力器,包括外套、过渡连接盘1和法兰轴套2。As shown in Figures 3 and 4 together, the engine rear power take-off used in the test includes an outer casing, a transition connection plate 1 and a flange bushing 2 .
外套内转动安装有第一主轴3,第一主轴3的一端通过花键连接有第二主轴4,第二主轴4的另一端设有与发动机的后取力输出端5的内花键相适配的外花键,第二主轴4上套装有一花键轴隔套6,花键轴隔套6与发动机的后取力输出端5内花键的端面相顶靠,花键轴隔套6对整个传动系起到径向支撑的作用,有效的避免第二主轴4的磨损,可靠性大大提高。其中,外套包括通过紧固件安装在一起的外套体7和外套体端盖8,外套体7内设有轴承安装腔9,轴承安装腔9内安装有两个轴承10,两轴承10之间设有轴承隔套11,第一主轴3安装于两轴承10上,靠近外套体端盖8的轴承10与外套体端盖8之间设有一止推卡簧22。轴承安装腔9的两端分别设有一油封12,外套体7与轴承隔套11之间形成润滑油腔13,外套体上设有与润滑油腔13连通的润滑油加注口14,润滑油加注口14内设有润滑油加注塞15,可有效避免发动机齿轮箱机油流失的问题,保护发动机不受损伤。A first main shaft 3 is installed in rotation in the jacket, and one end of the first main shaft 3 is connected with a second main shaft 4 through a spline, and the other end of the second main shaft 4 is provided with an internal spline suitable for the rear power output end 5 of the engine. With the external spline, the second main shaft 4 is equipped with a spline shaft spacer 6, the spline shaft spacer 6 is against the end face of the internal spline at the rear power output end 5 of the engine, and the spline shaft spacer 6 It plays the role of radial support for the entire transmission system, effectively avoids the wear of the second main shaft 4, and greatly improves the reliability. Wherein, the outer casing includes an outer casing 7 and an outer casing end cap 8 installed together by fasteners, and a bearing installation cavity 9 is arranged in the outer casing 7, and two bearings 10 are installed in the bearing installation cavity 9, and a gap between the two bearings 10 A bearing spacer 11 is provided, the first main shaft 3 is mounted on two bearings 10, and a thrust retaining spring 22 is provided between the bearing 10 close to the outer cover 8 and the outer cover 8. Two ends of the bearing installation cavity 9 are respectively provided with an oil seal 12, a lubricating oil chamber 13 is formed between the outer casing 7 and the bearing spacer 11, and a lubricating oil filling port 14 communicating with the lubricating oil chamber 13 is provided on the outer casing, and the lubricating oil The filling port 14 is provided with a lubricating oil filling plug 15, which can effectively avoid the oil loss of the engine gearbox and protect the engine from damage.
过渡连接盘1具有中空的空腔,第二主轴4伸出空腔,外套通过紧固件安装于过渡连接盘1上,过渡连接盘1通过紧固件安装于发动机的飞轮壳16上。本实施例中,所涉及的紧固件均为螺栓。The transition connection plate 1 has a hollow cavity, the second main shaft 4 protrudes from the cavity, the outer casing is installed on the transition connection plate 1 through fasteners, and the transition connection plate 1 is installed on the flywheel housing 16 of the engine through fasteners. In this embodiment, the fasteners involved are all bolts.
法兰轴套2套设并通过紧固件安装于第一主轴3的另一端,法兰轴套2通过紧固件与发动机后取力试验台架的万向联轴器17连接。第一主轴3靠近法兰轴套2一端的端部设有螺纹孔18,法兰轴套2的法兰端面上设有一压块安装槽19,压块安装槽19内通过一螺栓20压设有一压块21,螺栓20安装于螺纹孔18内。The flange bushing 2 is sheathed and installed on the other end of the first main shaft 3 through fasteners, and the flange bushing 2 is connected with the universal coupling 17 of the rear power take-off test bench of the engine through fasteners. The end of the first main shaft 3 close to the end of the flange bushing 2 is provided with a threaded hole 18, and the flange end surface of the flange bushing 2 is provided with a pressing block installation groove 19, and a bolt 20 is pressed in the pressing block installation groove 19. There is a pressing block 21, and the bolt 20 is installed in the threaded hole 18.
如图5所示,在发动机后取力试验台架进行更换发动机时,由于通用型后取力器只需更换过渡连接盘1、第二主轴4和花键轴隔套6,这三种零部件结构简单,加工工艺简单,制作成本低,大大降低了试验准备成本,缩短了试验准备周期,提高了试验台架利用率,该通用型后取力器适合所有后取力发动机机型;通过安装该通用型后取力器,能将后取力输出端5的扭转力可靠地传递至测工系统,从而准确的测出后取力输出功率。在更换不同规格的发动机时,只需更换通用型发动机后取力器中的过渡连接盘1、第二主轴4和花键隔套即可完成装配,降低工装制作成本,缩短试验准备周期,提高试验台架利用率的目的。As shown in Figure 5, when the engine is replaced on the rear power take-off test bench of the engine, since the general-purpose rear power take-off only needs to replace the transition connection plate 1, the second main shaft 4 and the spline shaft spacer 6, these three parts The component structure is simple, the processing technology is simple, the production cost is low, the test preparation cost is greatly reduced, the test preparation cycle is shortened, and the utilization rate of the test bench is improved. This universal rear power take-off is suitable for all rear power take-off engine models; through Installing the universal rear power take-off can reliably transmit the torsional force of the rear power take-off output end 5 to the measuring system, thereby accurately measuring the output power of the rear power take-off. When replacing engines of different specifications, the assembly can be completed only by replacing the transition connection plate 1, the second main shaft 4 and the spline spacer in the rear power take-off of the general-purpose engine, which reduces the cost of tooling manufacturing, shortens the test preparation period, and improves Purpose of test bench utilization.
本实用新型不局限于上述具体的实施方式,本领域的普通技术人员从上述构思出发,不经过创造性的劳动,所作出的种种变换,均落在本实用新型的保护范围之内。The utility model is not limited to the above-mentioned specific implementation manners, and various transformations made by those skilled in the art starting from the above-mentioned ideas without creative work all fall within the protection scope of the utility model.
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105841953A (en) * | 2016-06-12 | 2016-08-10 | 中国重汽集团济南动力有限公司 | Test device of automobile transmission power take-off device |
| CN106195034A (en) * | 2015-05-07 | 2016-12-07 | 贵州航空发动机研究所 | A kind of switching device of aviation power accessory drive |
| CN107346000A (en) * | 2017-08-12 | 2017-11-14 | 芜湖双翼航空装备科技有限公司 | One kind is used for aviation alternator test tool and its application method |
| CN108194623A (en) * | 2018-02-26 | 2018-06-22 | 中国船舶重工集团公司第七0三研究所 | A kind of band surveys the high speed shafting for turning round function |
| CN109342065A (en) * | 2018-12-11 | 2019-02-15 | 广西玉柴机器股份有限公司 | A kind of flywheel terminal pad transmission device |
| CN109736938A (en) * | 2018-12-14 | 2019-05-10 | 玉柴联合动力股份有限公司 | A kind of novel PTO assembly and its assembly method of diesel engine |
| CN112081737A (en) * | 2020-09-17 | 2020-12-15 | 中石化石油机械股份有限公司 | Compound natural gas compressor host computer no-load operation test device |
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2014
- 2014-01-25 CN CN201420047941.6U patent/CN203745202U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106195034A (en) * | 2015-05-07 | 2016-12-07 | 贵州航空发动机研究所 | A kind of switching device of aviation power accessory drive |
| CN105841953A (en) * | 2016-06-12 | 2016-08-10 | 中国重汽集团济南动力有限公司 | Test device of automobile transmission power take-off device |
| CN107346000A (en) * | 2017-08-12 | 2017-11-14 | 芜湖双翼航空装备科技有限公司 | One kind is used for aviation alternator test tool and its application method |
| CN107346000B (en) * | 2017-08-12 | 2023-12-05 | 芜湖双翼航空装备科技有限公司 | Test tool for aviation alternating-current generator and application method thereof |
| CN108194623A (en) * | 2018-02-26 | 2018-06-22 | 中国船舶重工集团公司第七0三研究所 | A kind of band surveys the high speed shafting for turning round function |
| CN109342065A (en) * | 2018-12-11 | 2019-02-15 | 广西玉柴机器股份有限公司 | A kind of flywheel terminal pad transmission device |
| CN109342065B (en) * | 2018-12-11 | 2023-09-19 | 广西玉柴机器股份有限公司 | Flywheel connecting disc transmission device |
| CN109736938A (en) * | 2018-12-14 | 2019-05-10 | 玉柴联合动力股份有限公司 | A kind of novel PTO assembly and its assembly method of diesel engine |
| CN109736938B (en) * | 2018-12-14 | 2021-04-20 | 玉柴联合动力股份有限公司 | Novel PTO assembly of diesel engine and assembling method thereof |
| CN112081737A (en) * | 2020-09-17 | 2020-12-15 | 中石化石油机械股份有限公司 | Compound natural gas compressor host computer no-load operation test device |
| CN112081737B (en) * | 2020-09-17 | 2025-08-29 | 中石化石油机械股份有限公司 | A composite natural gas compressor host no-load operation test device |
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