CN207424201U - Unmanned plane horn testing tool - Google Patents
Unmanned plane horn testing tool Download PDFInfo
- Publication number
- CN207424201U CN207424201U CN201721535257.2U CN201721535257U CN207424201U CN 207424201 U CN207424201 U CN 207424201U CN 201721535257 U CN201721535257 U CN 201721535257U CN 207424201 U CN207424201 U CN 207424201U
- Authority
- CN
- China
- Prior art keywords
- plug
- unmanned plane
- sleeve pipe
- testing tool
- described sleeve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model is related to a kind of unmanned plane horn testing tool, the tester including casing, in described sleeve pipe, the voltage regulating module in described sleeve pipe, the power connection mounted on described sleeve pipe one end and the plug and Signal plug mounted on the described sleeve pipe other end；The tester is electrically connected respectively with the Signal plug and the voltage regulating module；The plug is electrically connected respectively with the power connection and the voltage regulating module.Above-mentioned unmanned plane horn testing tool is simple in structure, small, occupies little space；The unmanned plane horn testing tool of the utility model, instead of fuselage, economizes on resources directly by the way that test to the motor operation performance of horn can be realized with direct current and horn electric connection, and convenient test.
Description
Technical field
The utility model is related to unmanned plane technical field of measurement and test, more particularly to a kind of unmanned plane horn testing tool.
Background technology
Unmanned plane can be divided into from technical standpoint：Unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, nothing
People's dirigible and unmanned parasol.Unmanned plane can be widely used for environmental monitoring, agricultural plant protection, it is military, take photo by plane, survey, surveying and drawing, warning
With fields such as, city management, meteorology, electric power, rescue and relief works.As unmanned plane application field is more and more extensive, market is to nothing
Man-machine demand is also increasing.
Horn is an important component of unmanned plane, and to ensure that the operation of horn is in shape, machine exists in arm
, it is necessary to test the motor operation performance of horn after tentatively having produced；Traditional horn test method is to assemble horn
It is tested on fuselage, test is difficult, and needs entire fuselage as testboard, waste of resource, and body volume is larger, needs
Occupy larger space.
Utility model content
Based on this, it is necessary to horn is mounted on fuselage for the prior art and is tested, test is difficult, waste money
Source, and the problem of body volume is larger, and occupied space is big, provides a kind of convenient test, economizes on resources and small nobody
Machine horn testing tool.
A kind of unmanned plane horn testing tool, tester including casing, in described sleeve pipe, mounted on the set
Voltage regulating module in pipe, the power connection mounted on described sleeve pipe one end and the plug mounted on the described sleeve pipe other end
And Signal plug；The tester is electrically connected respectively with the Signal plug and the voltage regulating module；The plug difference
It is electrically connected with the power connection and the voltage regulating module.
Above-mentioned unmanned plane horn testing tool includes casing, the tester in casing, the tune in casing
Die block, the power connection mounted on casing one end and the plug and Signal plug mounted on the casing other end, structure letter
It is single, it is small, it occupies little space；Unmanned plane horn testing tool with direct current and horn electric connection directly by can be realized
Test to the motor operation performance of horn, instead of fuselage, economizes on resources, and convenient test.
In one of the embodiments, the secondary plug mounted on the described sleeve pipe other end is further included.
In one of the embodiments, the quantity of the secondary plug is two, and two secondary plug relative spacings are set
It puts.
In one of the embodiments, the tester is steering engine tester.
In one of the embodiments, described sleeve pipe is carbon pipe.
In one of the embodiments, described sleeve pipe is set for cylinder；The opposite end of described sleeve pipe is respectively arranged with
Baffle and partition plate, the power connection are fixedly mounted on the baffle；The plug and the fixed peace of the Signal plug
On the partition plate.
In one of the embodiments, the peripheral wall of described sleeve pipe is equipped with slot, is provided with knob on the tester, institute
It states knob and wears slot and extend to outside described sleeve pipe.
In one of the embodiments, the power connection is banana connector.
Description of the drawings
Fig. 1 is the stereogram of the unmanned plane horn testing tool of a better embodiment of utility model；
Fig. 2 is the exploded view of the unmanned plane horn testing tool of Fig. 1；
Fig. 3 is the sectional view of the unmanned plane horn testing tool of Fig. 1；
Fig. 4 is the circuit diagram of the unmanned plane horn testing tool of Fig. 1；
The meaning of each label is in attached drawing：
Casing 10, baffle 11, partition plate 12, slot 13；
Tester 20, signal wire 21, knob 22；
Voltage regulating module 30, the first conducting wire 31, the second conducting wire 32；
Power connection 40, electric wire 41, plug 50, Signal plug 60, secondary plug 70.
Specific embodiment
For the ease of understanding utility model, utility model will be described more fully below.But utility model can
To realize in many different forms, however it is not limited to embodiment described herein.On the contrary, provide the mesh of these embodiments
Be to make the more thorough and comprehensive of the understanding to the disclosure of utility model.
Unless otherwise defined, technical field of all of technologies and scientific terms used here by the article with belonging to utility model
The normally understood meaning of technical staff it is identical.It is intended merely to retouch in the term used in the description of utility model herein
State the purpose of specific embodiment, it is not intended that in limitation utility model.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly on another element
Or there may also be elements placed in the middle.When an element is considered as " connection " another element, it can be directly connected to
To another element or it may be simultaneously present centering elements.On the contrary, when element be referred to as " directly existing " another element " on " when,
There is no intermediary elements.Term as used herein " vertically ", " horizontal ", "left", "right" and similar statement are
For illustrative purposes.
It please refers to Fig.1 to Fig. 4, is the unmanned plane horn testing tool of one better embodiment of utility model, including casing
10th, the tester 20 in casing 10, the voltage regulating module 30 in casing 10, the power supply mounted on 10 one end of casing
The connector 40 and plug 50 mounted on 10 other end of casing, Signal plug 60 and secondary plug 70；Tester 20 respectively with letter
Number plug 60 and voltage regulating module 30 are electrically connected；Plug 50 is electrically connected respectively with power connection 40 and voltage regulating module 30.
Referring again to Fig. 2 and Fig. 3, casing 10 is set for cylinder, which is carbon pipe, and specifically, casing 10 is
Carbon nanotubes.The opposite end of casing 10 is respectively arranged with baffle 11 and partition plate 12, and baffle 11 and partition plate 12 are by isolation material
It is made；Partition plate 11 for power connection 40 to be fixedly mounted, for plug 50, Signal plug 60 and pair to be fixedly mounted insert by partition plate 12
First 70.The peripheral wall of casing 10 is equipped with slot 13, and knob of the slot 13 on tester 20 is worn.
Tester 20 is located in casing 10 close to one end of baffle 11.The tester 20 be steering engine tester, tester 20
Signal wire 21 is electrically connected between Signal plug 60, i.e. tester 20 is electrically connected by signal wire 21 and Signal plug 60,
Knob 22 is provided on tester 20, knob 22 wears slot 13 and extends to outside casing 10, and tester 20 is adjusted by knob 22
Control electric motor starting, closing and the rotating speed on horn.
Voltage regulating module 30 is set for cuboid, and pressure regulation template 30 is located in casing 10 close to one end of partition plate 12.Pressure regulation mould
The first conducting wire 31 is connected between one end of plate 30 and tester 20, i.e. one end of pressure regulation template 30 passes through the first conducting wire 31 and survey
Examination instrument 20 is electrically connected；The second conducting wire 32, i.e. pressure regulation template 30 are connected between the other end of pressure regulation template 30 and plug 50
It is electrically connected by the second conducting wire 32 with tester 20；So as to which direct current is from power connection 40 through plug 50 and voltage regulating module
30 are transmitted on tester 20.Voltage regulating module 30 is used to adjusting direct current into the voltage range values that can be born to tester 20, so
After be transmitted further to tester 20, it is ensured that tester 20 test when voltage stabilization, be conducive to improve measuring accuracy；Meanwhile favorably
In the service life of extended testing system instrument 20.
Power connection 40 is for connecting direct current, and the power connection 40 is fixedly mounted on baffle 11, power connection 40
Live wire 41 is connected between plug 50, i.e. power connection 40 is electrically connected by electric wire 41 and plug 50.In this implementation
In example, power connection 40 is banana connector；The quantity of power connection 40 is two, and two power connections 40 are respectively cathode power supply
Connector and negative power supply connector.Plug 50 is fixedly mounted on partition plate 12, and plug 50 is corresponding with power connection 40, electric mortiser
First 50 are used for grafting horn, are powered by plug 50 to horn and voltage regulating module 30.In the present embodiment, the number of plug 50
It measures as two, two plugs 50 are respectively anode plug and cathode plug.Signal plug 60 is also fixedly mounted on partition plate
On 12, Signal plug 60 is located at one end of partition plate 12, and Signal plug 60 is corresponding with tester 20, and Signal plug 60 is used to insert
Pick arm, and tester 20 controls the motor on horn by Signal plug 60.In the present embodiment, the quantity of Signal plug 60 is
Two, two Signal plugs 60 are respectively positive signal plug and negative signal plug.Secondary plug 70 is also fixedly mounted on partition plate
On 12, secondary plug 70 is located at the one end of partition plate away from Signal plug 60, and secondary plug 70 is used for grafting horn, with beneficial to the unmanned plane
The stability that horn testing tool is connected with horn is conducive to improve measuring accuracy.In the present embodiment, the quantity of secondary plug 70
For two, and two 70 relative spacings of secondary plug are set.
Referring again to Fig. 4, the unmanned plane horn testing tool method is as follows：
A. a unmanned plane horn testing tool is provided, tester 20 including casing 10, in casing 10 is mounted on
Voltage regulating module 30 in casing 10, the power connection 40 mounted on 10 one end of casing and the electricity mounted on 10 other end of casing
Plug 50 and Signal plug 60；
B. plug 50 and Signal plug 60 are plugged on horn, and power connection 40 is electrically connected with direct current；Power connection 40
On electric energy be transmitted on plug 50, the electric energy on plug 50 is transmitted on horn and pressure regulation template 30, pressure regulation template 20
Electric energy is transmitted on tester 20 after pressure regulation is carried out to electric energy；
C. turn knob 22, tester 20 send signal, and signal is transmitted to through Signal plug 60 on horn, the electricity on horn
Machine starts, continuation turn knob 22, and the motor speed on horn gradually increases, until knob 22 is rotated to maximum, tests
Finish.
The unmanned plane horn testing tool of the utility model includes casing, the tester in casing, mounted on set
Voltage regulating module in pipe is inserted mounted on the power connection of casing one end and the plug mounted on the casing other end and signal
Head, it is simple in structure, it is small, it occupies little space；Unmanned plane horn testing tool with direct current and horn directly by electrically connecting
The test that can be realized to the motor operation performance of horn is connect, instead of fuselage, is economized on resources, and convenient test, horn production
Cost reduction.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope that this specification is recorded all is considered to be.
Embodiment described above only expresses the several embodiments of the utility model, and description is more specific and detailed,
But therefore it can not be interpreted as the limitation to utility model patent scope.It should be pointed out that the common skill for this field
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
The scope of protection of the utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (9)
1. a kind of unmanned plane horn testing tool, which is characterized in that tester, peace including casing, in described sleeve pipe
It is voltage regulating module in described sleeve pipe, mounted on the power connection of described sleeve pipe one end and another mounted on described sleeve pipe
The plug and Signal plug at end；The tester is electrically connected respectively with the Signal plug and the voltage regulating module；It is described
Plug is electrically connected respectively with the power connection and the voltage regulating module.
2. unmanned plane horn testing tool according to claim 1, it is characterised in that：It further includes another mounted on described sleeve pipe
The secondary plug of one end.
3. unmanned plane horn testing tool according to claim 2, it is characterised in that：The quantity of the pair plug is two
It is a, and two secondary plug relative spacings are set.
4. unmanned plane horn testing tool according to claim 1, it is characterised in that：The tester is tested for steering engine
Instrument.
5. unmanned plane horn testing tool according to claim 1, it is characterised in that：Described sleeve pipe is carbon pipe.
6. unmanned plane horn testing tool according to claim 5, it is characterised in that：Described sleeve pipe is set for cylinder；
The opposite end of described sleeve pipe is respectively arranged with baffle and partition plate, and the power connection is fixedly mounted on the baffle；It is described
Plug and the Signal plug are fixedly mounted on the partition plate.
7. unmanned plane horn testing tool according to claim 1, it is characterised in that：The peripheral wall of described sleeve pipe is equipped with slot
Hole is provided with knob on the tester, and the knob wears slot and extends to outside described sleeve pipe.
8. unmanned plane horn testing tool according to claim 1, it is characterised in that：The power connection connects for banana
Head.
9. unmanned plane horn testing tool according to claim 8, it is characterised in that：The quantity of the power connection is two
A, two power connections are respectively cathode power supply connector and negative power supply connector；The quantity of the plug be two, two
A plug is respectively positive plug and negative electricity plug；The quantity of the Signal plug is two, and two signals are inserted
Head is respectively positive signal plug and negative signal plug.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721535257.2U CN207424201U (en) | 2017-11-16 | 2017-11-16 | Unmanned plane horn testing tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721535257.2U CN207424201U (en) | 2017-11-16 | 2017-11-16 | Unmanned plane horn testing tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207424201U true CN207424201U (en) | 2018-05-29 |
Family
ID=62306551
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721535257.2U Expired - Fee Related CN207424201U (en) | 2017-11-16 | 2017-11-16 | Unmanned plane horn testing tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207424201U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107942246A (en) * | 2017-11-16 | 2018-04-20 | 深圳市科比特航空科技有限公司 | Unmanned plane horn testing tool and its test method |
-
2017
- 2017-11-16 CN CN201721535257.2U patent/CN207424201U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107942246A (en) * | 2017-11-16 | 2018-04-20 | 深圳市科比特航空科技有限公司 | Unmanned plane horn testing tool and its test method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180529 Termination date: 20211116 |