CN109752173A - A kind of adjustable Loading for actuator device of linear torque - Google Patents
A kind of adjustable Loading for actuator device of linear torque Download PDFInfo
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- CN109752173A CN109752173A CN201910068965.7A CN201910068965A CN109752173A CN 109752173 A CN109752173 A CN 109752173A CN 201910068965 A CN201910068965 A CN 201910068965A CN 109752173 A CN109752173 A CN 109752173A
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- lead screw
- extension spring
- steering engine
- rocker arm
- bracket
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Abstract
The invention discloses a kind of linear adjustable Loading for actuator devices of torque, lead screw is fixedly connected on base upper surface, the sliding of lead screw slide is fitted on lead screw, bracket is provided on lead screw slide, horizontally disposed angular transducer is connected on bracket, mounting flange is connected in the shaft of angular transducer, the edge of mounting flange front end face is provided with connecting column, one end of extension spring is connected on connecting column, the other end of extension spring is connected to one end of rocker arm, the other end of rocker arm is connected on the output shaft of tested steering engine, tested steering engine is fixedly connected in mounting base.Offer unit by using an extension spring as loading force has the characteristics that inexpensive, simple and compact for structure;Since extension spring stretches, contraction speed is fast, and Loading for actuator response is fast;Load torque value can be adjusted when steering engine is not shut down, torque value and the linear proportionate relationship of steering engine swing angle.
Description
Technical field
The present invention relates to aviations, navigational field, more particularly to a kind of linear adjustable Loading for actuator device of torque.
Background technique
The rudder of small-sized unmanned aircraft and miniature self-service ship mostly uses electric steering engine, pneumatically or hydraulically drives.It is logical
For often, the control aerofoil of unmanned vehicle and the rudder of unmanned ship, in flight or navigation, will bear complicated air-flow or
The load impacting of water flow, and the load is mostly fast-changing state.Therefore, the driving equipment of aerofoil and rudder face, output are special
Property, need to bear load complicated and changeable, if driving equipment output characteristics is unable to satisfy loading demand, aircraft and ship will
It can not normal flight or navigation.
Common torque measuring device, although can the output torque value to steering engine axis measure, this kind measure only
It is only to be measured to the static characteristic of driving equipment.In order to test the dynamic characteristic of steering engine output shaft, design specialized is needed
Torque loading equipemtn, existing torque loading equipemtn mostly use the structure type of torque arm, and accurate measurement and control is cooperated to set
It is standby, realize torque load test, this kind of equipment precision height can satisfy every test of steering engine output shaft, but the disadvantage is that torsion
The required precision of bar is stringent, causes processing cost high, and needs to design and process multiple and different torsion according to torque range
Bar, along with complicated control system, the price of whole equipment is higher.
Summary of the invention
In order to solve the problems in the existing technology, the object of the present invention is to provide a kind of linear adjustable rudders of torque
Machine loading device, the loading device is with inexpensive, simple and compact for structure, load response is fast, load torque is adjustable, torque value line
The property good feature of degree, for testing the dynamic output characteristic of small-sized steering machine.
In order to achieve the above-mentioned object of the invention, the technical solution adopted by the present invention is that:
A kind of adjustable Loading for actuator device of linear torque, including pedestal, lead screw, lead screw slide, angular transducer, Method for Installation
Orchid, extension spring, rocker arm and mounting base, lead screw are fixedly connected on base upper surface, and the sliding of lead screw slide is fitted in lead screw
On, bracket is provided on lead screw slide, bracket is the L shape structure being integrally formed by bottom plate and side plate, and the bottom plate of bracket is fixed
It is connected on the upper surface of lead screw slide, is connected with horizontally disposed angular transducer on bracket, in the shaft of angular transducer
It is connected with mounting flange, mounting flange can be rotated with shaft, and the edge of mounting flange front end face is provided with connecting column, be drawn
The one end for stretching spring is connected on connecting column, and the other end of extension spring is connected to one end of rocker arm, the other end of rocker arm
It is connected on the output shaft of tested steering engine, tested steering engine is fixedly connected in mounting base, the central axis and quilt of angular transducer
The central axis for surveying steering engine output shaft is located in same level.
Further, the end of lead screw is fitted with handwheel.
Compared with prior art, the invention has the advantages that
By the present invention in that using an extension spring as the offer unit of loading force, have inexpensive, simple and compact for structure
Feature;Since extension spring stretches, contraction speed is fast, and Loading for actuator response is fast;Load torque value can not be shut down in steering engine
When be adjusted, torque value and the linear proportionate relationship of steering engine swing angle.
Detailed description of the invention
Fig. 1 is the main view of embodiment one;
Fig. 2 is the main view of embodiment one;
Fig. 3 is the main view of embodiment one;
Fig. 4 is the schematic diagram of original state of the present invention;
Fig. 5 is the schematic diagram of stress state of the present invention;
Fig. 6 is the tensile elongation of extension spring when being 110mm, swings the curve graph of the corresponding load torque value of drift angle α;
Fig. 7 is the tensile elongation of extension spring when being 115mm, swings the curve graph of the corresponding load torque value of drift angle α;
Fig. 8 is the tensile elongation of extension spring when being 120mm, swings the curve graph of the corresponding load torque value of drift angle α;
Fig. 9 is the tensile elongation of extension spring when being 125mm, swings the curve graph of the corresponding load torque value of drift angle α;
Figure 10 is the structural schematic diagram of embodiment two.
In figure: 1, handwheel;2, lead screw;3, lead screw slide;4, extension spring;5, rocker arm;6, it is tested steering engine;7, angle passes
Sensor;8, mounting base;9, pedestal;10, mounting flange;11, driving motor;12, linear displacement transducer.
Specific embodiment
With reference to the accompanying drawing and embodiment is described in further detail technical solution of the present invention.
Embodiment one, as shown in Figure 1, 2, 3, a kind of adjustable Loading for actuator device of linear torque, including pedestal 9, silk
Thick stick 2, lead screw slide 3, angular transducer 7, mounting flange 10, extension spring 4, rocker arm 5 and mounting base 8, lead screw 2 are fixedly connected
On 9 upper surface of pedestal, the sliding of lead screw slide 3 is fitted on lead screw 2, and the end of lead screw 2 is fitted with handwheel 1, by rotating hand
1 is taken turns to drive lead screw 2 to be driven;Bracket is provided on lead screw slide 3, bracket is the L shape knot being integrally formed by bottom plate and side plate
Structure, the bottom plate of bracket are fixedly connected on the upper surface of lead screw slide 3, and the angular transducer 7 is fixedly connected on the side of bracket
On plate, it is connected with mounting flange 10 in the shaft of angular transducer 7, the edge of 10 front end face of mounting flange is provided with connection
One end of column, extension spring 4 is connected on connecting column, and the other end of extension spring 4 is connected to one end of rocker arm 5, rocker arm 5
The other end be connected on the output shaft of tested steering engine 6, tested steering engine 6 is fixedly connected in mounting base 8, and mounting base 8 is fixed to be connected
It connects on 9 upper surface of pedestal, the central axis of the central axis of angular transducer 7 and tested 6 output shaft of steering engine is located at same water
In plane.
In the present invention, the both ends of rocker arm 5 are provided with connecting hole, the company of being fitted in the connecting hole of 5 one end of rocker arm
The other end of outbound, the extension spring 4 is connected on connecting pin, rocker arm 5 by the connecting hole of its other end be fitted in by
It surveys on the output shaft of steering engine 6, also, is interference fit between the connecting hole of 5 other end of rocker arm and the output shaft of tested steering engine 6
Relationship.
As a preferred solution of the present invention, being tested mounting height of the steering engine 6 in mounting base 8 can adjust, in this way can be with
The central axis of the central axis and tested steering engine output shaft that ensure angular transducer is located in same level.
In actual test, in original state, as shown in figure 4, the output shaft of tested steering engine 6 is in zero-bit, adjusting screw
The position of slide 3, so that extension spring 4 is in horizontal extension state, the tensile elongation of extension spring 4 is H at this time;In load shape
When state, as shown in figure 5, the output shaft of tested steering engine 6 drives rocker arm 5 to swing, swing drift angle is α, and 5 one end of rocker arm was swung
Extension spring 4 is constantly elongated in journey, 4 pulling force of extension spring increases, and 4 pulling force of extension spring acts on tested rudder by rocker arm 5
On the output shaft of machine 6, load torque is formed.
Selecting the coefficient of elasticity K of extension spring 4 is 10, and in original state, the tensile elongation of extension spring 4 is adjusted respectively
When to 110mm, 115mm, 120mm and 125mm, the curve of the corresponding load torque value of drift angle α is swung as shown in Fig. 6,7,8,9,
As can be seen that the increase of the tensile elongation H with extension spring, swings the corresponding load torque value of drift angle α and increases, also,
It loads torque value and swings the linear proportionate relationship of drift angle α.
It, can be by rotating the position of handwheel adjusting screw slide unit when Loading for actuator is tested, and then adjust and stretch bullet
The tensile elongation H of spring reaches variable torque load test with this, and tensile elongation H can be by being indicated in screw slide 3 in advance
Scale read.
Embodiment two, the embodiment and embodiment the difference is that: as shown in Figure 10, the handwheel 1 can with drive
Dynamic motor 11 substitutes, and the output shaft of driving motor 11 is sequentially connected by shaft coupling and lead screw 2, and is arranged sliding for detecting lead screw
The linear displacement transducer 12 of 3 practical shift positions of seat, driving motor 11 and linear displacement transducer 12 are cooperated accordingly
More complicated dynamic torque load test can be realized in control system.
In addition, it is necessary to explanation, lead screw 2 preferentially selects T-type lead screw.
The above is only preferable practical embodiment of the invention, not does limit in any form to the present invention
Fixed, any person skilled in the art is changed or is modified to equivalent variations possibly also with the technical solution of the disclosure above
Equivalence enforcement example, but without departing from the technical solutions of the present invention, according to the technical essence of the invention to above-mentioned reality
Any simple modification, equivalent change and modification that example is done are applied, in the range of still belonging to technical solution of the present invention.
Claims (2)
1. a kind of linear adjustable Loading for actuator device of torque, including pedestal, lead screw, lead screw slide, angular transducer, installation
Flange, extension spring, rocker arm and mounting base, it is characterised in that: lead screw is fixedly connected on base upper surface, and lead screw slide is sliding
It is dynamic to be fitted on lead screw, bracket is provided on lead screw slide, bracket is the L shape structure being integrally formed by bottom plate and side plate, branch
The bottom plate of frame is fixedly connected on the upper surface of lead screw slide, and the angular transducer is fixedly connected on the side plate of bracket, angle
It spends in the shaft of sensor and is connected with mounting flange, mounting flange can be rotated with shaft, at the edge of mounting flange front end face
Place is provided with connecting column, and one end of extension spring is connected on connecting column, and the other end of extension spring is connected to the one of rocker arm
End, the other end of rocker arm are connected on the output shaft of tested steering engine, and tested steering engine is fixedly connected in mounting base, angle sensor
The central axis of the central axis of device and tested steering engine output shaft is located in same level.
2. the adjustable Loading for actuator device of linear torque according to claim 1, it is characterised in that: match the end of lead screw
Equipped with handwheel.
Priority Applications (1)
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CN201910068965.7A CN109752173A (en) | 2019-01-24 | 2019-01-24 | A kind of adjustable Loading for actuator device of linear torque |
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CN201910068965.7A CN109752173A (en) | 2019-01-24 | 2019-01-24 | A kind of adjustable Loading for actuator device of linear torque |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110657979A (en) * | 2019-10-28 | 2020-01-07 | 北京交通大学 | Follow-up device for axial movement of steering engine |
CN111975452A (en) * | 2020-08-26 | 2020-11-24 | 山东理工大学 | Vertical Two-Way Torque Adjustment Device for Machining |
CN112362370A (en) * | 2020-10-19 | 2021-02-12 | 中国运载火箭技术研究院 | Simple steering engine load testing 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 |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU844482A1 (en) * | 1979-08-17 | 1981-07-07 | Предприятие П/Я А-1097 | Loading device for testing steering engines |
CN101539476A (en) * | 2009-03-12 | 2009-09-23 | 北京理工大学 | Aerocraft steering engine non-rubber deviation load torque following mechanism |
US20110283844A1 (en) * | 2010-05-21 | 2011-11-24 | Hon Hai Precision Industry Co., Ltd. | Torque-adjusting machine for hinge |
CN104634562A (en) * | 2015-02-05 | 2015-05-20 | 南京理工大学 | Bearing direction manual loading mechanism and loading method for rolling linear guide rail pair |
CN105632276A (en) * | 2016-02-26 | 2016-06-01 | 南京航空航天大学 | Rudder load simulator not generating surplus torque |
CN105738021A (en) * | 2016-02-04 | 2016-07-06 | 中国航天空气动力技术研究院 | Linear steering engine loading device |
CN106945779A (en) * | 2017-05-04 | 2017-07-14 | 南京奥特博机电科技有限公司 | A kind of integrated form bicycle power-assisted device and moped |
CN107121301A (en) * | 2017-06-02 | 2017-09-01 | 哈尔滨工业大学 | A kind of Loading for actuator demo system |
CN107121261A (en) * | 2017-06-28 | 2017-09-01 | 中国科学院沈阳自动化研究所 | A kind of force application apparatus based on lever augmented principle |
-
2019
- 2019-01-24 CN CN201910068965.7A patent/CN109752173A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU844482A1 (en) * | 1979-08-17 | 1981-07-07 | Предприятие П/Я А-1097 | Loading device for testing steering engines |
CN101539476A (en) * | 2009-03-12 | 2009-09-23 | 北京理工大学 | Aerocraft steering engine non-rubber deviation load torque following mechanism |
US20110283844A1 (en) * | 2010-05-21 | 2011-11-24 | Hon Hai Precision Industry Co., Ltd. | Torque-adjusting machine for hinge |
CN104634562A (en) * | 2015-02-05 | 2015-05-20 | 南京理工大学 | Bearing direction manual loading mechanism and loading method for rolling linear guide rail pair |
CN105738021A (en) * | 2016-02-04 | 2016-07-06 | 中国航天空气动力技术研究院 | Linear steering engine loading device |
CN105632276A (en) * | 2016-02-26 | 2016-06-01 | 南京航空航天大学 | Rudder load simulator not generating surplus torque |
CN106945779A (en) * | 2017-05-04 | 2017-07-14 | 南京奥特博机电科技有限公司 | A kind of integrated form bicycle power-assisted device and moped |
CN107121301A (en) * | 2017-06-02 | 2017-09-01 | 哈尔滨工业大学 | A kind of Loading for actuator demo system |
CN107121261A (en) * | 2017-06-28 | 2017-09-01 | 中国科学院沈阳自动化研究所 | A kind of force application apparatus based on lever augmented principle |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110657979A (en) * | 2019-10-28 | 2020-01-07 | 北京交通大学 | Follow-up device for axial movement of steering engine |
CN111975452A (en) * | 2020-08-26 | 2020-11-24 | 山东理工大学 | Vertical Two-Way Torque Adjustment Device for Machining |
CN112362370A (en) * | 2020-10-19 | 2021-02-12 | 中国运载火箭技术研究院 | Simple steering engine load testing 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 |
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