CN207510743U - Unmanned plane test platform - Google Patents
Unmanned plane test platform Download PDFInfo
- Publication number
- CN207510743U CN207510743U CN201721517825.6U CN201721517825U CN207510743U CN 207510743 U CN207510743 U CN 207510743U CN 201721517825 U CN201721517825 U CN 201721517825U CN 207510743 U CN207510743 U CN 207510743U
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- China
- Prior art keywords
- unmanned plane
- test platform
- support
- adjusting mechanism
- angle adjusting
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Abstract
The utility model provides a kind of unmanned plane test platform, including can support in the support base in plane, and the support panel on support base and for placing unmanned plane is installed on, unmanned plane test platform, which further includes, to be connected between support base and support panel and for adjusting the angle adjusting mechanism for supporting panel rotation angle on horizontal plane and vertical plane.Unmanned plane test platform provided by the utility model, pass through the setting of angle adjusting mechanism, so that when unmanned plane carries out various flight attitudes, the angle of support panel can change with the variation of the flight attitude of unmanned plane, so that the unmanned plane test platform can simulate more true flight environment of vehicle so that each parameter testing result of unmanned plane is more accurate.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is to be related to a kind of unmanned plane test platform more specifically.
Background technology
With the development of unmanned air vehicle technique, more and more industries start to carry out related operation, therefore nothing using unmanned plane
The test of man-machine parameters also becomes very important, such as the vibration frequency of unmanned plane, acceleration and flight frequency ginseng
Number.At present, multi-rotor unmanned aerial vehicle does not have the test and debugging platform of digitization in flight course is assembled, all intuitive with operator
Judgement, although the testing jig suggested can be sometimes used, but still mainly by the experience of operator.
In the prior art, have some unmanned plane test platform cases, but its support panel for being used to place unmanned plane
It is not adjustable, degree of freedom is low, and more true flight environment of vehicle cannot be simulated, and then lead so as to cause unmanned plane test platform
The parameters test result for causing unmanned plane is inaccurate.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane test platform, with solve it is in the prior art nobody
Support panel schedulable low the technical issues of causing unmanned plane parameters test result inaccurate in machine test platform.
To achieve the above object, the technical solution adopted in the utility model is：A kind of unmanned plane test platform is provided, is wrapped
Include the support panel that can support in the support base in plane and be installed on the support base and be used to place unmanned plane, institute
It states unmanned plane test platform and further includes and be connected between the support base and the support panel and for adjusting the supporting surface
The angle adjusting mechanism of plate rotation angle on horizontal plane and vertical plane.
Preferably, the angle adjusting mechanism is universal footed glass.
Preferably, the rotation angle of the angle adjusting mechanism in the horizontal plane is 360 degree, and the angle adjusting mechanism exists
Rotation angle on vertical plane is positive and negative 45 degree.
Further, it is equipped with pinboard between the support panel and the angle adjusting mechanism.
Further, the pinboard is suspended at the lower section of the support panel by multiple studs.
Further, the pinboard is equipped with to measure the vibration data of the unmanned plane and shaking for acceleration information
Dynamic measurement module.
Further, it is equipped with to measure the unmanned plane pressure between the angle adjusting mechanism and the support base
Tension-compression sensor component.
Further, the angle adjusting mechanism is equipped with for by the angle adjusting mechanism and the tension-compression sensor
The fixing nut that component is fixedly connected.
Further, the support base includes more support bars, and the support bar is connected by connecting corner yard.
Preferably, the support bar is aluminium section bar part.
The advantageous effect of unmanned plane test platform provided by the utility model is：Compared with prior art, this practicality is new
The setting that the unmanned plane test platform of type passes through angle adjusting mechanism so that support panel rotation angle on horizontal plane and vertical plane
Degree can be adjusted, in this way so that when unmanned plane carries out various flight attitudes, support the angle of panel can be with unmanned plane
The variation of flight attitude and change so that the unmanned plane test platform can simulate more true flight environment of vehicle, make
Each parameter testing result for obtaining unmanned plane is more accurate.
Description of the drawings
It, below will be to embodiment or the prior art in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing is briefly described needed in description, it should be apparent that, the accompanying drawings in the following description is only that this practicality is new
Some embodiments of type, for those of ordinary skill in the art, without having to pay creative labor, can be with
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the structure diagram of unmanned plane test platform that the utility model embodiment provides；
Fig. 2 is the partial enlarged view of the unmanned plane test platform in Fig. 1.
Wherein, each reference numeral in figure：
1- supports panel；2- vibration measurement modules；3- pinboards；4- angle adjusting mechanisms；5- fixing nuts；6- tension and compression pass
Sensor component；7- support bases；8- studs；9- bolts；10- end brackets；11- cables；41- chassis；42- screw rods；71- first
Support bar；The second support bars of 72-；73- third support bars；The 4th support bars of 74-；75- connecting corner yards.
Specific embodiment
In order to which technical problem to be solved in the utility model, technical solution and advantageous effect is more clearly understood, with
Lower combination accompanying drawings and embodiments, the present invention is further described in detail.It should be appreciated that specific reality described herein
It applies example to be only used to explain the utility model, is not used to limit the utility model.
It should be noted that when element is referred to as " being fixed on " or " being set to " another element, it can be directly another
On one element or it is connected on another element.When an element is known as " being connected to " another element, it can
To be directly to another element or be indirectly connected on another element.
It is to be appreciated that term " length ", " width ", " on ", " under ", " vertical ", " level ", " top ", " bottom " " interior ",
The orientation or position relationship of instructions such as " outer " are based on orientation shown in the drawings or position relationship, are for only for ease of and describe this reality
There must be specific orientation, with device that is simplifying description rather than instruction or hint meaning or element with specific with novel
Azimuth configuration and operation, therefore it is not intended that limitation to the utility model.
In addition, term " first ", " second " are only used for description purpose, and it is not intended that instruction or hint relative importance
Or the implicit quantity for indicating indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include one or more this feature." multiple " are meant that two or two in the description of the present invention,
More than, unless otherwise specifically defined.
Also referring to Fig. 1 and Fig. 2, now unmanned plane test platform provided by the utility model is illustrated.This nobody
Machine test platform includes support base 7, support panel 1 and angle adjusting mechanism 4, support base 7 can upright support in plane (as
The larger plane of face homalographic) on, support panel 1 is installed on support base 7, and support panel 1 is used to place unmanned plane, angle tune
Section mechanism 4 is connected between support panel 1 and support base 7, angle adjusting mechanism 4 for adjust support panel 1 in horizontal plane and
Rotation angle on vertical plane.The unmanned plane test platform of the utility model when in use, is first put the unmanned plane for needing to test
It is placed on support panel 1, ensures positioning of the unmanned plane on support panel 1, then start unmanned plane so that unmanned plane is in not
Same state of flight, and angle adjusting mechanism 4 is so that support panel 1 can adapt to the various flight attitudes of unmanned plane, so as to real
Now the parameters such as the vibration of unmanned plane, acceleration and pulling force are tested.
Unmanned plane test platform provided by the utility model, compared with prior art, the unmanned plane test of the utility model
The setting that platform passes through angle adjusting mechanism 4 so that the support rotation angle on horizontal plane and vertical plane of panel 1 can be adjusted,
In this way so that when unmanned plane carries out various flight attitudes, the angle of support panel 1 can be with the flight attitude of unmanned plane
Change and change, so that the unmanned plane test platform can simulate more true flight environment of vehicle so that unmanned plane
Each parameter testing result is more accurate.
Preferably, it please refers to Fig.1 and Fig. 2, a kind of specific reality as unmanned plane test platform provided by the utility model
Apply mode, above-mentioned angle adjusting mechanism 4 is preferably universal footed glass, by using can be with the universal footed glass of multi-angle regulation so that
Support panel 1 is adapted to the various flight attitudes of unmanned plane when unmanned plane is tested, and then can simulate more true
Flight environment of vehicle, and its is simple in structure, it is easy for installation, it is at low cost.Specifically, universal footed glass includes screw rod 42 and chassis 41, screw rod
It is adjustable connection between 42 and chassis 41, the bottom end on chassis 41 is fixedly connected with support panel 1, the outer end of screw rod 42 and support base
7 connections.Chassis 41 is generally using metal, plastics and rubber these types material manufacture, and metal is preferably carbon steel or stainless steel, plastics
Preferably PA engineering nylons or other plastics, rubber are preferably NR or CR.Certainly, in the other embodiment of the utility model,
According to actual conditions and specific requirement, above-mentioned angle adjusting mechanism 4 can also be preferably that spherical pair etc. is capable of providing support panel 1
The structure of degree of freedom does not do unique restriction herein.
Preferably as a kind of specific embodiment of unmanned plane test platform provided by the utility model, above-mentioned angle
The rotation angle of regulating mechanism 4 in the horizontal plane is 360 degree, and horizontal plane here is plane parallel to the ground, and at this
In embodiment, support panel 1 is also parallel with horizontal plane in a non-operative state.Above-mentioned angle adjusting mechanism 4 is on vertical plane
Rotation angle is positive and negative 45 degree, i.e., angle adjusting mechanism 4 can meet support panel 1 and be revolved clockwise or counterclockwise on vertical plane
Turn 45 degree, in this way, the various flight attitudes that unmanned plane can occur in normal flight can be met, and then ensure unmanned plane
Test platform can simulate more true flight environment of vehicle.
Further, referring to Fig. 2, a kind of specific embodiment party as unmanned plane test platform provided by the utility model
Formula, is equipped with pinboard 3 between above-mentioned support panel 1 and angle adjusting mechanism 4, pinboard 3 is in lamellar, the length and width of pinboard 3
The length and width on chassis 41 in angle adjusting mechanism 4 are all higher than, pinboard 3 is fixed on the underface of support panel 1, and chassis 41 passes through spiral shell
Bolt 9 is fixed on the downside of pinboard 3, in this way, the setting by pinboard 3 so that angle adjusting mechanism 4 with support panel 1 it
Between connection area bigger, improve angle adjusting mechanism 4 and support the bonding strength between panel 1, and improve angle tune
Save support strength of the mechanism 4 to support panel 1.
Further, referring to Fig. 2, a kind of specific embodiment party as unmanned plane test platform provided by the utility model
Formula, above-mentioned pinboard 3 are suspended at the lower section of support panel 1 by multiple studs 8, specifically, multiple studs 8 are along circle
Circumferential direction is uniformly distributed, and one end of studs 8 is fixedly connected with support panel 1, the other end and the pinboard 3 of studs 8
It is fixedly connected, passes through the connection of studs 8 so that being connected firmly between support panel 1 and pinboard 3, and cause support
Accommodation space is formed between panel 1 and pinboard 3, so as to provide installation space for vibration measurement module 2 hereinafter.
Further, it please refers to Fig.1 and Fig. 2, one kind as unmanned plane test platform provided by the utility model is specific
Embodiment, above-mentioned pinboard 3 are equipped with vibration measurement module 2, and vibration measurement module 2 is used to measure the vibration data of unmanned plane
And acceleration information.Specifically, vibration measurement module 2 be installed on pinboard 3 and positioned at support panel 1 and unmanned plane just under
Side, vibration measurement module 2 are electrically connected by cable 11 and the control panel in unmanned plane test system, the vibration measurement module
Vibration data and acceleration information of the 2 measurable unmanned planes on tri- axis of X, Y, Z, i.e. vibration frequency and speed, acceleration
The parameters such as displacement.
Further, it please refers to Fig.1 and Fig. 2, one kind as unmanned plane test platform provided by the utility model is specific
Embodiment, is equipped with tension-compression sensor component 6 between above-mentioned angle adjusting mechanism 4 and support base 7, tension-compression sensor component 6 is used
In measurement unmanned plane pressure.Specifically, the shape of tension-compression sensor component 6 is cylindrical, and intermediate equipped with mounting hole, angle
42 one end of screw rod of regulating mechanism 4 is stretched into mounting hole, to realize between angle adjusting mechanism 4 and tension-compression sensor component 6
Connection.Tension-compression sensor component 6 is electrically connected again by cable 11 and the control panel in unmanned plane test system, so as to real
Now measure various drawings, the pressure value of unmanned plane.
Further, it please refers to Fig.1 and Fig. 2, one kind as unmanned plane test platform provided by the utility model is specific
Embodiment, above-mentioned angle adjusting mechanism 4 are equipped with fixing nut 5, and fixing nut 5 is used for angle adjusting mechanism 4 and tension and compression
Sensor module 6 is fixedly connected.Specifically, one end because of screw rod 42 is equipped with screw thread, fixed by the way that one end of screw rod 42 is passed through
Nut 5, is inserted into mounting hole, last tightening nut, so that the fastening of screw rod 42 is installed on tension-compression sensor component 6
On.
Preferably, it please refers to Fig.1 and Fig. 2, a kind of specific reality as unmanned plane test platform provided by the utility model
Mode is applied, end bracket 10 is additionally provided between above-mentioned tension-compression sensor component 6 and support base 7, end bracket 10 is in lamellar, end bracket
10 upper and lower ends are fixedly connected respectively with tension-compression sensor component 6 and support base 7, and tension-compression sensor is realized by end bracket 10
Component 6 arrives the transition connection between support base 7, so that entire tension-compression sensor component 6 is connected firmly with support base 7.
Further, referring to Fig. 1, a kind of specific embodiment party as unmanned plane test platform provided by the utility model
Formula, above-mentioned support base 7 include four support bars, respectively the first support bar 71, the second support bar 72, third support bar 73 and the
Four support bars 74, wherein, the first support bar 71, the second support bar 72 and third support bar 73 are horizontally disposed, the first support bar
71 are arranged in parallel with the second support bar 72, and third support bar 73 is connect respectively with the first support bar 71 and the second support bar 72, and
Tie point is respectively positioned on the point midway of the first support bar 71 and the second support bar 72, and the 4th support bar 74 is erected in third support bar
73 point midway, tension-compression sensor component 6, angle adjusting mechanism 4 and support panel 1 are installed on the 4th support bar 74 successively
Top.In addition, being attached between each support bar by connecting corner yard 75, each connecting corner yard 75 is direct corner brace, and respectively connect
Corner brace 75 is connect to be made of aluminium section bar.Certainly, in the other embodiment of the utility model, according to actual conditions and specific requirement,
The planform of above-mentioned support base 7 can also be other kinds of, can also include five, six roots of sensation support bar, not do herein
It is unique to limit.
Preferably as a kind of specific embodiment of unmanned plane test platform provided by the utility model, above-mentioned support
Item is preferably aluminium section bar part, specially 6060 aluminium section bars, and aluminium shape material manufacture craft is simple, with specific tensile strength, is bent
It takes intensity, ductility and corresponding work hardening rate and dominates permission deflection
Variation, support strength is high and practicability is good.Certainly, in the other embodiment of the utility model, according to reality
Border situation and specific requirement, above-mentioned support bar are alternatively other types metal material and nonmetallic materials, do not do unique limit herein
It is fixed.
5 the above is only the preferred embodiment of the utility model only, is not intended to limit the utility model,
All any modification, equivalent and improvement made within the spirit and principles of the present invention etc. should all wrap
Containing being within the protection scope of the utility model.
Claims (10)
1. unmanned plane test platform, including can support in the support base in plane and be installed on the support base and be used for
Place the support panel of unmanned plane, which is characterized in that the unmanned plane test platform, which further includes, is connected to the support base and institute
State support panel between and for adjust it is described support panel rotation angle on horizontal plane and vertical plane angle adjusting mechanism.
2. unmanned plane test platform as described in claim 1, which is characterized in that the angle adjusting mechanism is universal footed glass.
3. unmanned plane test platform as described in claim 1, which is characterized in that the angle adjusting mechanism is in the horizontal plane
Rotation angle is 360 degree, and rotation angle of the angle adjusting mechanism on vertical plane is positive and negative 45 degree.
4. unmanned plane test platform as described in claim 1, which is characterized in that the support panel and the angular adjustment machine
Pinboard is equipped between structure.
5. unmanned plane test platform as claimed in claim 4, which is characterized in that the pinboard is hanged by multiple studs
Set on the lower section of the support panel.
6. unmanned plane test platform as claimed in claim 4, which is characterized in that the pinboard is equipped with described for measuring
The vibration data of unmanned plane and the vibration measurement module of acceleration information.
7. unmanned plane test platform as described in claim 1, which is characterized in that the angle adjusting mechanism and the support base
Between be equipped with for the tension-compression sensor component that measures the unmanned plane pressure.
8. unmanned plane test platform as claimed in claim 7, which is characterized in that the angle adjusting mechanism, which is equipped with, to be used to incite somebody to action
The fixing nut that the angle adjusting mechanism is fixedly connected with the tension-compression sensor component.
9. unmanned plane test platform as described in claim 1, which is characterized in that the support base includes more support bars, institute
Support bar is stated to connect by connecting corner yard.
10. unmanned plane test platform as claimed in claim 9, which is characterized in that the support bar is aluminium section bar part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721517825.6U CN207510743U (en) | 2017-11-14 | 2017-11-14 | Unmanned plane test platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721517825.6U CN207510743U (en) | 2017-11-14 | 2017-11-14 | Unmanned plane test platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207510743U true CN207510743U (en) | 2018-06-19 |
Family
ID=62538938
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721517825.6U Expired - Fee Related CN207510743U (en) | 2017-11-14 | 2017-11-14 | Unmanned plane test platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207510743U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109341993A (en) * | 2018-11-20 | 2019-02-15 | 中国电力科学研究院有限公司 | The environmental suitability test method of unmanned plane cruising inspection system used for transmission line |
| CN109823566A (en) * | 2018-12-29 | 2019-05-31 | 清华大学 | A kind of vertically taking off and landing flyer flight control system test platform |
| CN109927932A (en) * | 2018-09-18 | 2019-06-25 | 山东大学 | A kind of adjustable flapping wing aircraft force plate/platform and its installation and application |
| CN111516903A (en) * | 2020-05-15 | 2020-08-11 | 蜂巢航宇科技（北京）有限公司 | Test bench for tilt rotor unmanned aerial vehicle |
| CN113365919A (en) * | 2020-06-23 | 2021-09-07 | 深圳市大疆创新科技有限公司 | Test equipment, test method and flight test system |
| CN113636103A (en) * | 2021-10-14 | 2021-11-12 | 南京鹿达电器有限公司 | Unmanned aerial vehicle vibration testing arrangement |
-
2017
- 2017-11-14 CN CN201721517825.6U patent/CN207510743U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927932A (en) * | 2018-09-18 | 2019-06-25 | 山东大学 | A kind of adjustable flapping wing aircraft force plate/platform and its installation and application |
| CN109927932B (en) * | 2018-09-18 | 2021-06-29 | 山东大学 | Adjustable flapping wing aircraft force measuring platform and installation and use method thereof |
| CN109341993A (en) * | 2018-11-20 | 2019-02-15 | 中国电力科学研究院有限公司 | The environmental suitability test method of unmanned plane cruising inspection system used for transmission line |
| CN109823566A (en) * | 2018-12-29 | 2019-05-31 | 清华大学 | A kind of vertically taking off and landing flyer flight control system test platform |
| CN111516903A (en) * | 2020-05-15 | 2020-08-11 | 蜂巢航宇科技（北京）有限公司 | Test bench for tilt rotor unmanned aerial vehicle |
| CN113365919A (en) * | 2020-06-23 | 2021-09-07 | 深圳市大疆创新科技有限公司 | Test equipment, test method and flight test system |
| WO2021258310A1 (en) * | 2020-06-23 | 2021-12-30 | 深圳市大疆创新科技有限公司 | Test device, test method and flight test system |
| CN113636103A (en) * | 2021-10-14 | 2021-11-12 | 南京鹿达电器有限公司 | Unmanned aerial vehicle vibration testing arrangement |
| CN113636103B (en) * | 2021-10-14 | 2022-06-24 | 南京鹿达电器有限公司 | Unmanned aerial vehicle vibration testing device |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180619 Termination date: 20211114 |
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| CF01 | Termination of patent right due to non-payment of annual fee |