CN205066985U - Steering wheel loading device - Google Patents
Steering wheel loading device Download PDFInfo
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- CN205066985U CN205066985U CN201520809048.7U CN201520809048U CN205066985U CN 205066985 U CN205066985 U CN 205066985U CN 201520809048 U CN201520809048 U CN 201520809048U CN 205066985 U CN205066985 U CN 205066985U
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- steering wheel
- output shaft
- bearing
- base plate
- torsion spring
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Abstract
The utility model discloses a steering wheel loading device, it includes steering wheel shaft coupling, torque sensor, torsional spring and bottom plate, the steering wheel beam warp by the motor cabinet with the one end of steering wheel shaft coupling links to each other, the other end of steering wheel shaft coupling links to each other and has the output shaft, the output shaft via the bearing with the help of torque sensor with the torsional spring links to each other, the motor cabinet is installed on the bottom plate, the bearing with the torsional spring all through respective mount pad install in on the bottom plate. This device is carrying on loaded while of moment of torsion load the steering wheel, can show the actual moment of torsion load that the steering wheel output shaft bore in real time. The inertia of a whole set of mechanism is less, and the steering wheel output shaft can not damage the inside gear assembly of steering wheel because of the inertia of a whole set of mechanism when high -speed the rotation. And a whole set of mechanism structure is simple, realizes that the cost is lower.
Description
Technical field
The utility model relates to a kind of Loading for actuator device, particularly relates to a kind of charger for testing flying vehicle steering engine output torque.
Background technology
When testing flying vehicle steering engine output torque, the output torque of normally used hydraulic loaded platform is large, travelling speed fast, but its mechanism is complicated, easily occurs leaking oil condition.Further, due to characteristics such as hydraulic mechanism output torque are large, it is made to be bad to load little moment of torsion steering wheel.Servomotor loading bench uses a set of larger relative to tested motor torque, that rotating speed is higher servo electrical machinery system to load steering wheel, this system needs to utilize sensor detect in real time the moment between two motors and angle and carry out direct torque, makes to be obtained corresponding rotational load by measured motor.This plant machinery and control circuit complexity, cost is higher.Magnetic powder brake loading bench is applicable to the continuous unidirectional loading of motor, and steering wheel is two-way, low-angle, frequently moves.Magnetic powder brake internal mechanical structure moment of inertia is comparatively large, in motion process repeatedly, can impact, cause structure permanent damage to physical constructions such as steering wheel internal gear, keys.
Summary of the invention
Complexity, higher, the easy deficiency tested electric machine structure being produced to damage of cost is controlled in order to overcome existing Loading for actuator device, the utility model provides a kind of Loading for actuator device, this device can not only load steering wheel, and can show the torque value of loaded load in real time.
Loading for actuator device of the present utility model comprises steering wheel shaft coupling, torque sensor, torsion spring and base plate, steering wheel beam warp is connected by motor cabinet one end with described steering wheel shaft coupling, the other end of described steering wheel shaft coupling is connected with output shaft, described output shaft is connected with described torsion spring by described torque sensor via bearing, described motor cabinet is arranged on described base plate, and described bearing and described torsion spring are all installed on described base plate by respective mount pad.
Preferred described steering wheel shaft coupling is enclosed within described output shaft, described bearing is arranged in bearing mounting base, and be fixed on described bearing seat with bearing baffle, described bearing mounting base is arranged on described base plate, described output shaft through described bearing, and utilizes spring collar to be stuck in by described output shaft on described bearing ground inner ring.
Preferred described output shaft is connected with torque sensor bolt.
Described torsion spring is clamped by four bolts by the mount pad of preferred described torsion spring, and the mount pad of described torsion spring is installed on described base plate by bolt.
Preferably also comprise mount holder, it is installed on described base plate by bolt, for supporting described base plate.
Preferably also comprise Displaying Meter, it is connected with described torque sensor by data line, and described Displaying Meter is by 220 volts of Alternating Current Power Supplies.
The beneficial effects of the utility model are, while carrying out torque load loading to steering wheel, can show the actual torque load that steering wheel output shaft bears in real time.The moment of inertia of sleeve mechanism is less, and steering wheel output shaft, when high-speed rotation, can not damage steering wheel internal gear assembly because of the moment of inertia of sleeve mechanism.And sleeve mechanism structure is simple, realizes cost lower.
Accompanying drawing explanation
Fig. 1 is the structural drawing of Loading for actuator device.
Fig. 2 is motor cabinet part drawing.
Fig. 3 is steering wheel coupler component part figure.
Fig. 4 is output shaft part drawing.
Fig. 5 is bearing baffle part drawing.
Fig. 6 is Process for Bearing Seat figure.
Fig. 7 is torque sensor figure.
Fig. 8 is torsion spring connector part figure.
Fig. 9 is torsion spring part drawing.
Figure 10 is torsion spring holder part drawing.
Figure 11 is slide block part drawing.
Figure 12 is base plate part drawing.
Figure 13 is mount holder part drawing.
Figure 14 is Displaying Meter.
Figure 15 is bearing seat and output shaft mounting structure figure.
Figure 16 is the stereographic map of Loading for actuator device.
1. motor cabinets in figure, 2. steering wheel shaft coupling, 3. output shaft, 4. bearing baffle, 5. bearing seat, 6. torque sensor, 7. torsion spring connector, 8. torsion spring, 9. torsion spring holder, 10. slide block, 11. base plates, 12. mount holders, 13. Displaying Meters, 14. bearings, 15. spring collars
Embodiment
In FIG, motor cabinet 1 is arranged on base plate 11, and steering wheel shaft coupling 2 is enclosed within output shaft 3.Bearing 14 is arranged in bearing seat 5, and is fixed on bearing seat 5 with bearing baffle 4, and bearing seat 5 is arranged on base plate 11.Output shaft 3 through bearing 14, and blocks with spring collar 15.Output shaft 3 is connected with bolt with torque sensor 6, and torque sensor 6, torsion spring connector 7, torsion spring 8 are linked in sequence.Torsion spring 8 is clamped by four bolts by torsion spring holder 9, and torsion spring holder 9, base plate 11, slide block 10 are bolted.Mount holder 12 is installed on base plate 11, for base for supporting by bolt.
In fig. 14, Displaying Meter 13 is connected with torque sensor 6 by data line, and Displaying Meter 13 is by 220 volts of Alternating Current Power Supplies.
In fig .15, steering wheel shaft coupling 2, output shaft 3, torque sensor 6, torsion spring connector 7 are linked in sequence.Bearing 14 is arranged in bearing seat 5, and fixes with bearing baffle 4.Output shaft 3 through bearing 14, and blocks with spring collar 15.
When carrying out work, steering wheel beam warp is connected with steering wheel shaft coupling 2 by motor cabinet 1.Then above-mentioned Loading for actuator device is utilized, the torsional moment of steering wheel axle is overcome and the loading realized steering wheel axle by torsion spring 8, and measured the size of this moment of torsion in real time by torque sensor, thus the actual torque load that steering wheel output shaft bears can be shown in real time.
The moment of inertia of sleeve mechanism of the present utility model is less, and steering wheel output shaft, when high-speed rotation, can not damage steering wheel internal gear assembly because of the moment of inertia of sleeve mechanism.And sleeve mechanism structure is simple, realizes cost lower.
Above preferred implementation of the present utility model is illustrated, but the utility model is not limited to above-described embodiment.To one skilled in the art, in the category described in claims, various modification or fixed case can be expected apparently, certainly also belong to technology category of the present utility model.
The non-detailed description of the utility model is known to the skilled person technology.
Claims (6)
1. a Loading for actuator device, it is characterized in that: comprise steering wheel shaft coupling, torque sensor, torsion spring and base plate, steering wheel beam warp is connected by motor cabinet one end with described steering wheel shaft coupling, the other end of described steering wheel shaft coupling is connected with output shaft, described output shaft is connected with described torsion spring by described torque sensor via bearing, described motor cabinet is arranged on described base plate, and described bearing and described torsion spring are all installed on described base plate by respective mount pad.
2. Loading for actuator device according to claim 1, it is characterized in that: described steering wheel shaft coupling is enclosed within described output shaft, described bearing is arranged in bearing mounting base, and be fixed on described bearing seat with bearing baffle, described bearing mounting base is arranged on described base plate, described output shaft through described bearing, and utilizes spring collar to be stuck in by described output shaft on described bearing ground inner ring.
3. Loading for actuator device according to claim 1, is characterized in that: described output shaft is connected with torque sensor bolt.
4. Loading for actuator device according to claim 1, is characterized in that: described torsion spring is clamped by four bolts by the mount pad of described torsion spring, and the mount pad of described torsion spring is installed on described base plate by bolt.
5. Loading for actuator device according to claim 1, is characterized in that: also comprise mount holder, and it is installed on described base plate by bolt, for supporting described base plate.
6. Loading for actuator device according to claim 1, is characterized in that: also comprise Displaying Meter, and it is connected with described torque sensor by data line, and described Displaying Meter is by 220 volts of Alternating Current Power Supplies.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520809048.7U CN205066985U (en) | 2015-10-19 | 2015-10-19 | Steering wheel loading device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520809048.7U CN205066985U (en) | 2015-10-19 | 2015-10-19 | Steering wheel loading device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205066985U true CN205066985U (en) | 2016-03-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520809048.7U Active CN205066985U (en) | 2015-10-19 | 2015-10-19 | Steering wheel loading device |
Country Status (1)
| Country | Link |
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| CN (1) | CN205066985U (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106482939A (en) * | 2016-11-01 | 2017-03-08 | 北京航空航天大学 | A kind of general-purpose vertical Loading for actuator testing stand |
| CN106769013A (en) * | 2016-12-27 | 2017-05-31 | 湖北三江航天红峰控制有限公司 | A kind of loading inertia test apparatus of motor-driven cylinder |
| CN107264778A (en) * | 2016-04-08 | 2017-10-20 | 陕西飞机工业（集团）有限公司 | A kind of empennage axis of rudder bearing attachment structure |
| CN107588972A (en) * | 2017-09-29 | 2018-01-16 | 兰州飞行控制有限责任公司 | A kind of Loading for actuator exerciser for simulating missile wing rudder face loading condition |
| CN108106934A (en) * | 2016-11-24 | 2018-06-01 | 兰州飞行控制有限责任公司 | A kind of steering engine is two-way to use loading device |
| CN108638075A (en) * | 2018-06-12 | 2018-10-12 | 郑宝生 | A kind of steering engine |
| CN110261152A (en) * | 2019-06-18 | 2019-09-20 | 长春理工大学 | A kind of superposition adjustment type multichannel Rudder Loading System |
| CN110608909A (en) * | 2019-09-20 | 2019-12-24 | 西安联飞智能装备研究院有限责任公司 | Two-way loading equipment of rotatory steering wheel |
| CN110723312A (en) * | 2019-10-25 | 2020-01-24 | 北京机电工程研究所 | Steering engine loading device |
| CN111103090A (en) * | 2018-10-25 | 2020-05-05 | 北京振兴计量测试研究所 | Torque calibration device of steering engine test system |
| CN112362372A (en) * | 2020-11-24 | 2021-02-12 | 中国航天空气动力技术研究院 | High-power linear steering engine loading device |
| CN113640604A (en) * | 2021-08-12 | 2021-11-12 | 四川航天烽火伺服控制技术有限公司 | Comprehensive test device for electric steering engine |
| CN117007301A (en) * | 2023-10-08 | 2023-11-07 | 航天江南集团有限公司 | High-power steering engine loading device |
-
2015
- 2015-10-19 CN CN201520809048.7U patent/CN205066985U/en active Active
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107264778B (en) * | 2016-04-08 | 2019-06-25 | 陕西飞机工业（集团）有限公司 | A kind of empennage rudder bearing block connection structure |
| CN107264778A (en) * | 2016-04-08 | 2017-10-20 | 陕西飞机工业（集团）有限公司 | A kind of empennage axis of rudder bearing attachment structure |
| CN106482939A (en) * | 2016-11-01 | 2017-03-08 | 北京航空航天大学 | A kind of general-purpose vertical Loading for actuator testing stand |
| CN106482939B (en) * | 2016-11-01 | 2019-04-30 | 北京航空航天大学 | A kind of general-purpose vertical Loading for actuator testing stand |
| CN108106934A (en) * | 2016-11-24 | 2018-06-01 | 兰州飞行控制有限责任公司 | A kind of steering engine is two-way to use loading device |
| CN106769013B (en) * | 2016-12-27 | 2019-05-10 | 湖北三江航天红峰控制有限公司 | A kind of load inertia test apparatus of motor-driven cylinder |
| CN106769013A (en) * | 2016-12-27 | 2017-05-31 | 湖北三江航天红峰控制有限公司 | A kind of loading inertia test apparatus of motor-driven cylinder |
| CN107588972A (en) * | 2017-09-29 | 2018-01-16 | 兰州飞行控制有限责任公司 | A kind of Loading for actuator exerciser for simulating missile wing rudder face loading condition |
| CN108638075A (en) * | 2018-06-12 | 2018-10-12 | 郑宝生 | A kind of steering engine |
| CN111103090A (en) * | 2018-10-25 | 2020-05-05 | 北京振兴计量测试研究所 | Torque calibration device of steering engine test system |
| CN110261152B (en) * | 2019-06-18 | 2021-08-27 | 长春理工大学 | Superposition adjustment type multichannel steering engine loading system |
| CN110261152A (en) * | 2019-06-18 | 2019-09-20 | 长春理工大学 | A kind of superposition adjustment type multichannel Rudder Loading System |
| CN110608909A (en) * | 2019-09-20 | 2019-12-24 | 西安联飞智能装备研究院有限责任公司 | Two-way loading equipment of rotatory steering wheel |
| CN110723312A (en) * | 2019-10-25 | 2020-01-24 | 北京机电工程研究所 | Steering engine loading device |
| CN112362372A (en) * | 2020-11-24 | 2021-02-12 | 中国航天空气动力技术研究院 | High-power linear steering engine loading device |
| CN113640604A (en) * | 2021-08-12 | 2021-11-12 | 四川航天烽火伺服控制技术有限公司 | Comprehensive test device for electric steering engine |
| CN117007301A (en) * | 2023-10-08 | 2023-11-07 | 航天江南集团有限公司 | High-power steering engine loading device |
| CN117007301B (en) * | 2023-10-08 | 2023-12-12 | 航天江南集团有限公司 | High-power steering engine loading device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170420 Address after: 313216 Zhejiang city of Huzhou province Deqing County Qianyuan town Nanyang Road No. 58 Patentee after: Aerospace Nanyang (Zhejiang) Technology Co., Ltd. Address before: 100074 Beijing, Fengtai District Yungang West Road, No. 17 Patentee before: China Aerospace Aerodynamic Technology Institute |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170814 Address after: 100074 Beijing, Fengtai District Yungang West Road, No. 17 Patentee after: China Aerospace Aerodynamic Technology Institute Address before: 313216 Zhejiang city of Huzhou province Deqing County Qianyuan town Nanyang Road No. 58 Patentee before: Aerospace Nanyang (Zhejiang) Technology Co., Ltd. |
|
| TR01 | Transfer of patent right |