CN206594259U - UAV flight's supersonic reflectoscope detects service cable paradoxical discharge Arc System - Google Patents
UAV flight's supersonic reflectoscope detects service cable paradoxical discharge Arc System Download PDFInfo
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- CN206594259U CN206594259U CN201720258860.4U CN201720258860U CN206594259U CN 206594259 U CN206594259 U CN 206594259U CN 201720258860 U CN201720258860 U CN 201720258860U CN 206594259 U CN206594259 U CN 206594259U
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- China
- Prior art keywords
- unmanned plane
- supersonic reflectoscope
- shell
- plane shell
- rotor motor
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Abstract
Service cable paradoxical discharge Arc System is detected the utility model discloses UAV flight's supersonic reflectoscope, including unmanned plane shell and rotor motor, the top middle position of the unmanned plane shell is provided with wireless receiving antenna, the preceding surface of the unmanned plane shell is provided with heat emission hole, the one end of preceding surface away from heat emission hole of the unmanned plane shell is provided with power interface, and the left and right sides of unmanned plane shell is provided with rotor motor fixed support, the rotor motor fixed support is with being provided with support enhancing plate below the junction of unmanned plane shell, one end away from unmanned plane shell on the rotor motor fixed support is provided with electric motor protecting shell, the rotor motor is arranged on the inside of electric motor protecting shell；Using the principle of the producible ultrasonic signal of cable paradoxical discharge electric arc, supersonic reflectoscope can effectively detect whether the power cable paradoxical discharge occurs, and detection more facilitates.
Description
Technical field
The utility model belongs to service cable paradoxical discharge detection technique field, and in particular to UAV flight's ultrasonic wave is examined
Survey instrument detection service cable paradoxical discharge Arc System.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned aircraft that presetting apparatus is manipulated.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
When there is damaged paradoxical discharge in existing power cable, electric power maintenance personnel detection inconvenience, it is impossible to find line in time
The position of cable paradoxical discharge, the easily loss during increase power Transmission, and then add the increase of power Transmission cost, detection
When the problem of easily cause security incident, be this it is proposed that UAV flight's supersonic reflectoscope detection service cable is put extremely
Electric Arc System.
The content of the invention
The purpose of this utility model is to provide UAV flight's supersonic reflectoscope detection service cable paradoxical discharge electricity
Arc system, during solving to propose that damaged paradoxical discharge occurs in existing power cable in above-mentioned background technology, electric power maintenance personnel
Detection inconvenience, it is impossible to find the position of cable paradoxical discharge in time, the easily loss during increase power Transmission, and then increase
The increase of power Transmission cost, the problem of easily causing security incident during detection.
To achieve the above object, the utility model provides following technical scheme：UAV flight's supersonic reflectoscope is detected
In service cable paradoxical discharge Arc System, including unmanned plane shell and rotor motor, the top of the unmanned plane shell
Between be provided with wireless receiving antenna at position, the preceding surface of the unmanned plane shell is provided with heat emission hole, the unmanned plane shell
The one end of preceding surface away from heat emission hole be provided with power interface, and the left and right sides of unmanned plane shell is provided with rotor motor
Fixed support, the rotor motor fixed support is with being provided with support enhancing plate, the rotation below the junction of unmanned plane shell
One end away from unmanned plane shell on wing motor fixed rack is provided with electric motor protecting shell, and the rotor motor is arranged on electricity
It is provided with below unmanned plane rotor, the electric motor protecting shell and sets above the inside of machine containment vessel, the rotor motor
It is equipped with one end away from electric motor protecting shell on undercarriage, the undercarriage and is provided with undercarriage bottom plate, the undercarriage bottom plate
Lower section is provided with abrasion-proof rubber cushion, and the lower section middle position of the unmanned plane shell is provided with supersonic reflectoscope, described super
The junction of sonic wave detector and unmanned plane shell, which is provided with supersonic reflectoscope base, the supersonic reflectoscope base, to be set
Supersonic reflectoscope fixing bolt is equipped with, the power interface is electrically connected with built-in power, the wireless receiving antenna, rotor
Motor and supersonic reflectoscope are electrically connected with built-in power.
It is preferred that, the support enhancing plate is provided with four altogether, and four support enhancing plates are separately mounted to four rotors
The junction lower section of motor fixed rack and unmanned plane shell.
It is preferred that, the supersonic reflectoscope is examined with unmanned plane shell by supersonic reflectoscope fixing bolt and ultrasonic wave
Instrument base is surveyed to be fixedly connected.
It is preferred that, the undercarriage is provided with four altogether, and four undercarriages are separately mounted to four electric motor protecting shells
Lower section.
It is preferred that, the abrasion-proof rubber cushion is provided with 16 altogether, and 16 abrasion-proof rubber cushions are separately mounted to four
The lower section of undercarriage bottom plate.
Compared with prior art, the beneficial effects of the utility model are：It is producible super using cable paradoxical discharge electric arc
The principle of acoustic signals, supersonic reflectoscope can effectively detect whether the power cable paradoxical discharge occurs, and detection is more
Plus conveniently, it is to avoid it is artificial the problem of checked, detection time is saved, detection efficiency is improved, coordinates unmanned plane can be right
Cable between higher electric tower detected, detection more safe ready, it is to avoid when cable is in higher position, artificial inspection
Survey the problem of inconvenience easily triggers security incident；Undercarriage is separately mounted to the lower section of four rotor motor shells, is easy to reduction
Support is excessively concentrated and supersonic reflectoscope is impacted, while multiple abrasion-proof rubber cushions are provided with below undercarriage is easy to buffering
Impulsive force during landing, also allows for keeping unmanned plane balance.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is overlooking the structure diagram of the present utility model；
In figure：1- unmanned planes rotor, 2- rotor motors fixed support, 3- unmanned planes shell, 4- wireless receivings antenna, 5- dissipate
Hot hole, 6- power interfaces, 7- rotors motor, 8- undercarriages bottom plate, 9- abrasion-proof rubber cushions, 10- supersonic reflectoscopes are fixed
Bolt, 11- supersonic reflectoscopes, 12- supersonic reflectoscopes base, 13- supports enhancing plate, 14- undercarriages, 15- electric motor protectings
Shell.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
Fig. 1 and Fig. 2 are referred to, the utility model provides a kind of technical scheme：UAV flight's supersonic reflectoscope is detected
In the middle of service cable paradoxical discharge Arc System, including unmanned plane shell 3 and rotor motor 7, the top of unmanned plane shell 3
Wireless receiving antenna 4 is provided with position, the preceding surface of unmanned plane shell 3 is provided with heat emission hole 5, the preceding table of unmanned plane shell 3
The one end of face away from heat emission hole 5 is provided with power interface 6, and the left and right sides of unmanned plane shell 3 is provided with rotor motor and consolidated
Fixed rack 2, rotor motor fixed support 2 is with being provided with support enhancing plate 13, rotor motor below the junction of unmanned plane shell 3
One end away from unmanned plane shell 3 on fixed support 2 is provided with electric motor protecting shell 15, and rotor motor 7 is protected installed in motor
The inside of protective case 15, the top of rotor motor 7 is provided with unmanned plane rotor 1, and the lower section of electric motor protecting shell 15 has been provided with
Fall one end away from electric motor protecting shell 15 on frame 14, undercarriage 14 and be provided with undercarriage bottom plate 8, the lower section of undercarriage bottom plate 8 is set
Abrasion-proof rubber cushion 9 is equipped with, the lower section middle position of unmanned plane shell 3 is provided with supersonic reflectoscope 11, supersonic reflectoscope
11 be provided with the junction of unmanned plane shell 3 on supersonic reflectoscope base 12, supersonic reflectoscope base 12 be provided with it is super
Sonic wave detector fixing bolt 10, power interface 6 is electrically connected with built-in power, wireless receiving antenna 4, rotor motor 7
It is electrically connected with supersonic reflectoscope 11 with built-in power.
For the ease of increasing in the intensity of rotor motor fixed support 2, the present embodiment, it is preferred that support enhancing plate 13 is total to
Four are provided with, and four support enhancing plates 13 are separately mounted to the company of four rotor motor fixed supports 2 and unmanned plane shell 3
Connect place lower section.
Be fixedly mounted for the ease of supersonic reflectoscope 11, in the present embodiment, it is preferred that supersonic reflectoscope 11 and nobody
Machine shell 3 is fixedly connected by supersonic reflectoscope fixing bolt 10 with supersonic reflectoscope base 12.
For the ease of unmanned plane stable landing, in the present embodiment, it is preferred that undercarriage 14 is provided with four, and four altogether
Undercarriage 14 is separately mounted to the lower section of four electric motor protecting shells 15.
For the ease of protection unmanned plane, reduce in cushion effect when landing, the present embodiment, it is preferred that abrasion-proof rubber cushion 9 is set altogether
16 are equipped with, and 16 abrasion-proof rubber cushions 9 are separately mounted to the lower section of four undercarriage bottom plates 8.
Supersonic reflectoscope 11 in the utility model utilizes the ultrasonic wave generally meeting in elastic fluid in the way of compressional wave
Propagate, be a kind of mode of propagation of energy, be characterized in that supersonic frequency is high, wavelength is short, has in certain distance along straightline propagation
The feature for having good beam and directionality judges the position of paradoxical discharge electric arc, is easy to improve detection efficiency.
Operation principle of the present utility model and use flow：UAV flight's supersonic reflectoscope detection service cable is different
Normal electrical discharge arc system, is charged to built-in power by power interface 6, after charging complete, is sent out using unmanned controller
Go out enabling signal, after wireless receiving antenna 4 receives enabling signal, rotor motor 7 starts, driving unmanned plane rotor 1
Then rotation, user's operation unmanned plane during flying to the position for needing to detect starts supersonic reflectoscope 11 and carries out ultrasonic wave inspection
Survey, judge whether cable paradoxical discharge occurs, and paradoxical discharge position is determined, then will by wireless receiving antenna 4
Signal is transmitted to control end, after the completion of detection, and the abrasion-proof rubber cushion 9 of the lower section of undercarriage bottom plate 8 first lands, and slows down impulsive force, protects
Hold unmanned plane balance.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out in the case where not departing from principle of the present utility model and spirit a variety of changes, repaiies
Change, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. UAV flight's supersonic reflectoscope detects service cable paradoxical discharge Arc System, including unmanned plane shell（3）With
Rotor motor（7）, it is characterised in that：The unmanned plane shell（3）Top middle position be provided with wireless receiving day
Line（4）, the unmanned plane shell（3）Preceding surface be provided with heat emission hole（5）, the unmanned plane shell（3）Preceding surface it is remote
Heat emission hole（5）One end be provided with power interface（6）, and unmanned plane shell（3）The left and right sides be provided with rotor motor consolidate
Fixed rack（2）, the rotor motor fixed support（2）With unmanned plane shell（3）Junction below be provided with support enhancing plate
（13）, the rotor motor fixed support（2）Upper remote unmanned plane shell（3）One end be provided with electric motor protecting shell（15）, institute
State rotor motor（7）Installed in electric motor protecting shell（15）Inside, the rotor motor（7）Top be provided with nothing
Man-machine rotor（1）, the electric motor protecting shell（15）Lower section be provided with undercarriage（14）, the undercarriage（14）Upper remote motor
Containment vessel（15）One end be provided with undercarriage bottom plate（8）, the undercarriage bottom plate（8）Lower section be provided with abrasion-proof rubber cushion
（9）, the unmanned plane shell（3）Lower section middle position be provided with supersonic reflectoscope（11）, the supersonic reflectoscope
（11）With unmanned plane shell（3）Junction be provided with supersonic reflectoscope base（12）, the supersonic reflectoscope base
（12）On be provided with supersonic reflectoscope fixing bolt（10）, the power interface（6）It is electrically connected with built-in power, the nothing
Line reception antenna（4）, rotor motor（7）And supersonic reflectoscope（11）It is electrically connected with built-in power.
2. UAV flight's supersonic reflectoscope according to claim 1 detects service cable paradoxical discharge Arc System,
It is characterized in that：The support strengthens plate（13）Four, and four support enhancing plates are provided with altogether（13）It is separately mounted to four
Rotor motor fixed support（2）With unmanned plane shell（3）Junction below.
3. UAV flight's supersonic reflectoscope according to claim 1 detects service cable paradoxical discharge Arc System,
It is characterized in that：The supersonic reflectoscope（11）With unmanned plane shell（3）Pass through supersonic reflectoscope fixing bolt（10）With
Supersonic reflectoscope base（12）It is fixedly connected.
4. UAV flight's supersonic reflectoscope according to claim 1 detects service cable paradoxical discharge Arc System,
It is characterized in that：The undercarriage（14）Four, and four undercarriages are provided with altogether（14）It is separately mounted to four electric motor protectings
Shell（15）Lower section.
5. UAV flight's supersonic reflectoscope according to claim 1 detects service cable paradoxical discharge Arc System,
It is characterized in that：The abrasion-proof rubber cushion（9）16, and 16 abrasion-proof rubber cushions are provided with altogether（9）It is separately mounted to four
Individual undercarriage bottom plate（8）Lower section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720258860.4U CN206594259U (en) | 2017-03-17 | 2017-03-17 | UAV flight's supersonic reflectoscope detects service cable paradoxical discharge Arc System |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720258860.4U CN206594259U (en) | 2017-03-17 | 2017-03-17 | UAV flight's supersonic reflectoscope detects service cable paradoxical discharge Arc System |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206594259U true CN206594259U (en) | 2017-10-27 |
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ID=60124373
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720258860.4U Expired - Fee Related CN206594259U (en) | 2017-03-17 | 2017-03-17 | UAV flight's supersonic reflectoscope detects service cable paradoxical discharge Arc System |
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|---|---|
| CN (1) | CN206594259U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114013671A (en) * | 2021-12-10 | 2022-02-08 | 南京中智腾飞航空科技研究院有限公司 | Carry pipeline nondestructive test device in unmanned aerial vehicle |
-
2017
- 2017-03-17 CN CN201720258860.4U patent/CN206594259U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114013671A (en) * | 2021-12-10 | 2022-02-08 | 南京中智腾飞航空科技研究院有限公司 | Carry pipeline nondestructive test device in unmanned aerial vehicle |
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| 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: 20171027 Termination date: 20200317 |